20080111001352008011100135SO  2008       1          11         0001             220070925G8530AEC631397       CYLINDER                                CESSNA414   414A        2075907CE  CONT  O520  TSIO520NB   17040SO                              RT ENGINE       CRACKED         B  FCPRO   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      NM09919FA1120                   414A0628    276632R                     PILOT WAS INFORMED BY LINE PERSONNEL DURING TAXI TO TIE DOWN, THAT ENGINE WAS MAKING A LOUD (AIR PULSING) SOUND. PILOT COULD ONLY HEAR THE SOUND AFTER REMOVING NOISE CANCELLING HEAD SET. PILOT THEN SHUTDOWN ENGINE. INSPECTION REVEALED THE NR 4 CYLINDER TO BE CRACKED AT THE PARTING SURFACE. EXHAUST WAS ESCAPING FROM THE CRACK CAUSING THE (AIR PULSING) SOUND.                                                                                                                                                                                                                                                                                                                                                                         1L72 3O3  O  A7CE    E8CE                 
20070504001632007050400163GL  2007       5          4          050207           120070502G5210649             ROD END         CIRRUS                  CIRRUSSR    SR22        2130001GL  CONT  O550  IO550*           SO                              CABIN DOOR      BROKEN          G      B   EMER. DESCENT                                                                                   D  INFLIGHT SEPARATION                                                           CRCRUISE         1                      SO13299JW300                    1034                                    CABIN DOOR DEPARTED AIRCRAFT IN FLIGHT DUE TO THE ROD END HINGE FAILURE. IT APEARS THE ROD END FAILED DUE TO FATIGUE. THE ROD END SHOULD BE MADE OF A STRONGER MATERIAL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L71 3O3  ONTA00009CHE3SO                 
20070625000132007062500013CE  2007       6          25         061371           120070613G3397NTE5916         DIODE                                   RAYTHNDH125 HAWKER800XP 7150012CE                                                               LIGHTS          OVERHEATED      B      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CE01800RC745  745               258660                                  PILOT'S NOTED THAT LANDING AND TAXI PULSE LIGHT SYSTEM WAS INOPERATIVE ... LIGHTS WOULD NOT PULSE IN FLIGHT.  SYSTEM HAD BEEN UPDATED PER RAYTHEON MANDATORY SERVICE BULLETIN 33-3682.  UPON INSPECTION AND TROUBLE SHOOTING SYSTEM, THE CONNECTORS ATTACHED TO THE DIODES (CR1 THRU CR4) THAT WERE ADDED TO THE SYSTEM AS A RESULT OF THE BULLETIN, WERE LOOSE AND APPEAR TO HAVE OVERHEATED. IN DISCUSSIONS WITH RAYTHEON, IT WAS DETERMINED THAT POSITION OF THE DIODE INSULATORS ON PAGE 25 OR 39 OF THE SERVICE BULLETINS IS INCORRECT AND SHOWN OPPOSITE OF WHAT THEY SHOULD BE.  AS A RESULT, THE THINNER INSULATOR CRACKS AND ALLOWS THE TERMINAL TO SHORT TO GROUND AND OVERHEAT.   VISUALLY INSPECT DIODE PANEL AND VERIFY THAT THE   2L72 4F    RTA3EU                         
20070917000142007091700014WP  2007       9          17         090107           220070904G7200TFE7312B        ENGINE                                  LEAR  35    36A         5170603CE  GARRTTTFE731TFE73122B   01518WP                                              UNKNOWN         E  ESPAA   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CLCLIMB          1                      SO11545PA1101714                028         74118                       DURING CLIMB OUT SHORTLY AFTER TAKEOFF LT ENGINE QUIT.  CREW DECLARED AN EMERGENCY WITH DEPARTURE CONTROL, THEY VECTOR AIRPLANE TO PROPER MSA ALTITUDE AND RETURN FOR LANDING. CREW ELECTED, IN FLIGHT ENGINE START CHECK LIST, THE LT ENGINE STARTED, AND WAS OPERATING NORMAL. AT THIS POINT CREW NOTIFIED ATC THAT LT ENGINE WAS BACK UNDER NORMAL OPERATING CONDITIONS. AIRPLANE LANDED UNEVENTFULLY.                                                                                                                                                                                                                                                                                                                                       2L72 4F4  F  A10CE   E6WE                 
20080108003582008010800358CE  2008       1          8          102N07110026     120071015G3597                CABLE                                   BEECH 56    56TC        1152736CE  LYC   O541  TIO541*     41536EA                              OXYGEN SYSTEM   CHAFED          F      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      UKUNKNOWN        1                      NM09420S 463  463               TG74                                    ISSUE WITH THE FIXED OXYGEN SYSTEM DISPLAY FOR STC SA01078SE WHERE THE DISPLAY (NOT IN CONTACT WITH OXYGEN) RIBBON CABLE CHAFED AND CREATED A SHORT TO GROUND WHERE THE RIBBON CABLE SMOKED BUT DID NOT FAIL, THE INDICATOR LIGHT OF THE SYSTEM, NOR FAILED TO OPERATE.  ISSUE WAS NOTED DURING ANNUAL INSPECTION AND NOT REPORTED AT THE TIME OF INCIDENT.  MFG HAS BEEN IN CONTACT WITH THE ACO AND IS ISSUING A SERVICE BULLETIN.                                                                                                                                                                                                                                                                                                            1L72 3O3  O  3A16    E10EA                
20071205000602007120500060SO  2007       12         5          110107           120071120G6320                WARNING LIGHT   ROTOL                   GULSTMG159  G159        3952202SO  RROYCEDART  DART529     54507EU                              GEARBOX         ILLUMINATED     C      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      SO11810CB           148599      023                                     DURING CRUISE FLIGHT MISSION, THE RT GEARBOX LIGHT CAME ON STEADY. THE ENGINE WAS SHUTDOWN IAW AFM PROCEDURES. THE AIRCRAFT LANDED UNEVENTFULLY, AND TAXIED TO THE RAMP. NO EMERGENCY WAS DECLARED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4T4  T  1A17    E297                 
20070615001962007061500196GL  2007       6          15         110DJ0507        120070515G5522                SKIN                                    AMTR  500   ECLIPSE500  05614K5GL                                                               RT ELEVATOR     CRACKED         C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA27110DJ117        203452      000007                                  DURING REMOVAL OF THE ELEVATORS, A SMALL CRACK WAS DISCOVERED ON RT ELEVATOR SKIN BY OB MOST HINGE BRACKET ATTACH POINT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3F    RTEXPA1L72                     
20080109003922008010900392EU  2008       1          9          120107           220071217G7200                ENGINE                                  GULSTMG1159 G1159       3953505SO  RROYCESPEY  SPEY511*    54523EU                              LEFT            VIBRATION       E  ESPAA   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      SO11183PA                       108         8571                        AFTER LANDING, TEMP.AROUND -12C, FREEZING FOG, CREW ELECTED TO TURN OFF ANTI-ICE AFTER LND.  AIRCRAFT SAT FOR 1 HR,ENG'S STARTED. LT ENG HAD VIBRATION HUMMING, RT ENG WAS STABLE.TAXIED OUT W/ANTI-ICE ON THRUOUT.  A/C TOOKOFF, IT SEEMED TO BE SMOOTH ON THE ROLL AND INITIAL CLIMB, HOWEVER, OUT OF 10,000 FT LT ENG VIB WAS AROUND 1.5 MILS,ABNORMAL FOR THIS AIRPLANE. CREW ELECTED TO DIVERT (MAINT.BASE). LANDING WAS UNEVENTFUL. BOTH ENG'S HAD VISUAL CKS, NOTHING NOTED. CONCLUSION IT MUST HAVE BEEN AN ICING/MELTING PROBLEM.                                                                                                                                                                                                      2L72 4F4  FRTA12EA   E2EU                 
20071214003452007121400345EA  2007       12         14         120507           120071205G6310A1902           V-BELT                                  BLANCA1413  14132       1201004EA                                                               ENGINE TO TRANS DISINTEGRATED   C      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      SO19413R 503                    1531                                    DURING IFR TRAINING FLIGHT WHILE IN CROSS COUNTRY CRUISE, LOUD NOISES FROM ENGINE AREA PROMPTED CREW TO MAKE UNSCHEDULED LANDING TO SAFE AREA OF FLORIDA STATE ROAD 80 MEDIAN TURN AROUND PAVEMENT. UPON LANDING FOUND AFT BELT OF MAIN DRIVE BELT HAD SHED ITS OUTER LAYER AND DISINTEGRATED, CAUSING DAMAGE ONLY TO THE FAN SHROUD BEHIND THE ENGINE OIL COOOLER, AND MINOR SKIN DENT BEHIND THE FUEL TANK IN OUTER SKIN. ONE MULTIFUNCTION ANTENNA RG58 TNC CONNECTOR DAMAGED. AIRCRAFT TRAILERED TO HANGAR AND AFFECTED AREAS DISSASSEMBLED. REPLACEMANT SERVICABLE FAN SHROUD ASSEMBLY TO BE INSTALLED WITH NEW PARTS ORDERED FROM ROBINSON. NO ENGINE OR ROTOR OVERSPEED OCCURED. AUTOROTATION WAS NOT REQUIRED. PART 91 FLIGHT TRAINING O1L71 3O      A773                         
20071214003472007121400347GL  2007       12         14         15DR             120070411G2421BC4101          ALTERNATOR                              CIRRUSSR    SR22        2130001GL  CONT  O550  IO550*           SO                              NR 2            DESTROYED       B  ODARO   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      EA2115DR                        0394                                    OWNER REPORTED NR2 ALTERNATOR LIGHT ILLUMINATED.  REMOVED TOP COWLING TO INSPECT NR2 ALTERNATOR.  FOUND NR2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS.  ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE.  REMOVED P/N BC410-1, S/N 0921403.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  ONTA00009CHE3SO                 
20070402001672007040200167    2007       4          2          200345493        120070316G79204012T16P01      OIL FILTER                                                                                                                              OIL SYSTEM      DEFECTIVE       D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL25                                                                    INTERNAL BORE TO EACH END OF THE OIL FILTER ASSEMBLIES ARE SHARP AND UNSMOOTH.  THIS CONDITION WAS NOTED ON 3 ADDITIONAL FILTERS IN OUR STOCK, LOT 583085.  THIS CONDITION CAUSES THE PACKINGS ON THE OIL FILTER BODY TO SHEAR UPON INSTALLATION OF THE FILTER ELEMENT AND COULD CAUSE OIL BYPASS TO OCCUR.  THIS FILTER ELEMENT IS USED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                            
20070201000312007020100031SO  2007       2          1          200600073        120070131G5730                SKIN                                    LKHEED282   C130A       5262502SO                                                               WING            CRACKED         B  KGBRK   NONE                                                                                            Z  SIGNIFICANT FAILURE REPORT                                                    ININSP/MAINT     1                      NM04131HP20233                  56534                                   2EA CRACKS WERE DETECTED WHILE PERFORMING AD 2002-19-14, 1 CRACK EMANATING FROM A FASTENER HOLE LOCATED AT FS 543 RT CW STA 70 LOWER WING AND 1 CRACK EMANATING FROM A FASTENER HOLE AT  FS 569, LT CW STA 57, LOWER WING.  BOTH CRACKS ARE .1250 INCH LONG.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2H74 4T      A31NM                        
20070201000152007020100015WP  2007       2          1          200600083        120070131G5711                SPAR CAP                                CVAC  PB4Y2 PB4Y2       2421102WP  WRIGHTR2600 R260035     67050EA  HAMSTD23E   23E50       NE  WING            CRACKED         B  KGBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM042872G7162                   66300                                   WHILE PERFORMING THE REQUIREMENTS IN AD 2003-18-01, CRACKS WERE NOTED THRU-OUT THE WING.  THE MAJOR CRACK IS A 4-5 INCH CRACK IN THE FWD LT LOWER SPAR CAP AFT ANGLE AT THE WING ATTACH POINT TO THE BELT FRAME.  THE CRACK IS IN THE ANGLE (SPAR CAP AFT LEG), DOUBLER AND SPAR WEB.  THERE ARE ALSO CRACKS .1250-.2500 INCH EMANATING FROM 3 OF THE 4 BELT FRAME CUTOUTS ON THE LOWER WING.                                                                                                                                                                                                                                                                                                                                                   2H74 4R4  RRT        PAGE42  6  CP603     
20071101001882007110100188NM  2007       11         1          200700026        120071017G2797WMBMS136OT7C4G20WIRE                                    BOEING737   737205      1384456NM  PWA   JT8   JT8D17      52049NE                              TE FLAPS        CHAFED          C  SROMO   OTHER                                                                                           S  AFFECT SYSTEMS                                                                APAPPROACH       1                      AL03733PA38672                  23466                                   TRAILING EDGE FLAPS ASYMMETRY LOCKOUT BETWEEN ZERO AND ONE DEGREE.  THERE IS A SPLIT IN T/E FLAP INDICATION, LT T/E FLAPS INDICATE ONE DEGREE AND RT T/E FLAPS INDICATE ZERO.  FLIGHT CREW EXPERIENCED AN UNEVENTFUL LANDING AND NO UNCOMMANDED ROLL.  MAINTENANCE DISCOVERED RT T/E FLAP POSITION TRANSMITTER WIRE HARNESS HAD CHAFED WIRES.  REPLACED WIRE HARNESS FROM RT TRANSMITTER TO DISCONNECT STATION 720R CONNECTOR D4876P.                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA16WE   E2EA                 
20070807001672007080700167SW  2007       8          7          2007001          120070717G5714                SPAR CAP                                CVAC  P4Y   P4Y2TRANSAIR2421102SW  WRIGHTR2600 R260035     67050EA  HAMSTD23E   23E50       NE  CENTER WING     CRACKED         B  KGBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM042872G7162                   66300                                   WHILE PERFORMING AD 2003-18-01, CRACKS WERE FOUND UNDER THE LT LOWER, FWD, SPAR CAP DOUBLER IN THE CAP, SPAR WEB AND THE DOUBLER ITSELF.  CRACKS WERE ALSO FOUND IN THE WING SKIN CUTOUTS AT ALL 4 LOWER CENTER WING BELT FRAME CUT-OUTS. RT FWD LOWER SPAR CAP CRACKED IN (2) PLACES UNDER THE DOUBLER.                                                                                                                                                                                                                                                                                                                                                                                                                                        2H74 4R4  R  AR29    PAGE42  6  CP603     
20070201000142007020100014WP  2007       2          1          200700105        120070131G5711                SPAR CAP                                CVAC  PB4Y2 PB4Y2       2421102WP  WRIGHTR2600 R260035     67050EA  HAMSTD23E   23E50       NE  WING            CRACKED         B  KGBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM042871G7192                   66302                                   WHILE PERFORMING THE REQUIREMENTS IN AD 2003-18-01, CRACKS WERE NOTED THRU-OUT THE WING.  THE MAJOR CRACK IS A 1.5 INCH CRACK IN THE FWD LT LOWER SPAR CAP AFT ANGLE AT THE WING ATTACH POINT TO THE BELT FRAME.  THE CRACK IS IN THE ANGLE (SPAR CAP AFT LEG), DOUBLER AND SPAR WEB.  THERE ARE ALSO CRACKS .1250-.2500 INCH EMANATING FROM THE 4 BELT FRAME CUTOUTS ON THE LOWER WING.                                                                                                                                                                                                                                                                                                                                                        2H74 4R4  RRT        PAGE42  6  CP603     
20070131001682007013100168EU  2007       1          31         200700114        120070130G57202121151091      STIFFENER                               CASA  C212  C212        2410200EU  GARRTTTPE331TPE33110R   0517 WP  ROTOL R334  R334482F13  GL  LT WING         CRACKED         B  KGBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM04515RL5409                   405                                     WHILE PERFORMING CASA COM LETTER 212-224 AND CASA SB 212-57-57-30, A CRACK WAS NOTED FROM THE 4TH RIVET TO THE 5TH RIVET FROM THE BOTTOM, ON THE VERTICAL STIFFINER LOCATED ON THE LT WING AT STA 4700, AFT SPAR WEB.  THREE STIFFINERS NEXT TO THE ORIGINAL ARE CRACKED EXACTLY THE SAME, CRACKS ARE LOCATED INT HE SAME POSITIONS, BETWEEN THE 4TH AND 5TH RIVIT FROM THE BOTTOM.  THIS TOTALS 4EA CRACKED STIFFINERS.                                                                                                                                                                                                                                                                                                                        2H72 4T4  T  A43EU   E4WE    6  CP61GL    
20070226001652007022600165CE  2007       2          26         2007001HAGGAN    120070223G57402322330177      SUPPORT BRACKET GARKENYON   26044       LEAR  60    60LEAR      5170707CE  PWA   305   PW305A      52128NE                              ZONE 500        FAILED          B  H51RO   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      NM03252FX5936       0295        196                                     DURING FLAP OPERATION, FLAP ACTUATOR SUPPORT BRACKETS FAILED CAUSING FLAP ACTUATOR TO DAMAGE LEFT WING RIB SEGMENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA10CE   E35NE                
20070807001702007080700170WP  2007       8          7          2007002          120070717G5714                SPAR CAP                                CVAC  PB4Y2 PB4Y2       2421102WP                                                               CENTER WING     CRACKED         B  KGBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM042871G7192                   66302                                   WHILE PERFORMING AD 2003-18-01, CRACKS WERE FOUND UNDER THE LT LOWER, FWD, SPAR CAP DOUBLER IN THE CAP, SPAR WEB AND THE DOUBLER ITSELF.  CRACKS WERE ALSO FOUND IN THE WING SKIN CUTOUTS AT ALL 4 LOWER CENTER WING BELT FRAME CUT-OUTS. RT FWD LOWER SPAR CAP CRACKED IN ONE PLACE UNDER THE DOUBLER.                                                                                                                                                                                                                                                                                                                                                                                                                                         2H74 4R    RT                             
20070409001532007040900153NE  2007       4          9          200701           220070328G7210311300001       GEARBOX                                 ACQCORF22   F22         8850908EA  PWA   JT15  JT15D4      52112NE                              ACCESSORY G/B   MISDRILLED      B  LM1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA09                                                                    ENGINE WAS ROUTED TO OUR FACILITY FOR OVERHAUL AND DURING A FLUSHING PROCESS WE DISCOVERED A WALL IN AN ACCESSORY GEARBOX WITH A MISDRILLED OIL PASSAGE.  THE OIL PASSAGE DID SUPPLY OIL TO THE REQUIRED AREA BUT IT BROKE THROUGH THE WALL DURING THE MANUFACTURING PROCESS RESTRICTING THE OIL SUPPLY. THE ENGINE HAS BEEN OPERATING WITH THIS CONDITION WITH NO APPARENT EFFECT. THE AGB COMPONENTS WAS INSPECTED AND NO DAMAGE WAS FOUND AS A RESULT OF THIS CONDITION.                                                                                                                                                                                                                                                                     1H71 3O4  FNC1A9     E1NE                 
20070129003912007012900391NE  2007       1          29         20070125         220070124G8520                GEAR                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          WORN            B  EVGRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO33622                         10003       L2845148A                   DURING INSPECTION OF THE ENGINE WHILE REPLACING THE CRANKSHAFT IAW SB 569A, IT WAS OBSERVED THAT (PN 13519647) CRANKSHAFT GEAR WAS EXCESSIVELY WORN.  THE GEAR WAS REPLACED WITH A NEW PART.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3O3  O  H11NM   1E4                  
20071101001852007110100185NM  2007       11         1          20073            120071016G6720A3592           ATTACH BRACKET                          ROBSINR22   R22BETA     7640110NM  LYC   O320  O320*       41508EA                              T/R PEDAL       CRACKED         B  LJERA   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             HOHOVERING       1                      NM09721HH12846                  1484                                    TAIL ROTOR PEDALS JAMMED DURING FLARE TO A HOVER. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION IT WAS FOUND THAT THE TAIL ROTOR PEDAL BLOCK SUPPORT BRACKET ON THE RT SIDE HAD CRACKED AT THE AFT PEDAL BLOCK ATTACH POINT ALLOWING THE PEDAL BLOCK TO PIVOT DOWN AND JAM THE PEDALS. REPLACED BRACKET WITH NEW.                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3O3  O  H10WE   E274                 
20070906000212007090600021SO  2007       9          6          2007ADP828001    120070823G3230159SCH1151      SELECTOR VALVE                          GULSTMG159  G159        3952202SO  RROYCEDART  DART5298X   54507EU  ROTOL R4304 R1844304    EU  RT MLG          BYPASSING       C      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      SO11198PA     1253              027                                     AIRCRAFT WAS ENROUTE, FLYING THE APPROACH FOR RUNWAY 03. ONCE THE CREW PERFORMED THE APPROACH CHECKLIST, AND GEAR DOWN WAS SELECTED BEFORE LANDING CHECKLIST THEY GOT THE RT MAIN AND NOSE GEAR LIGHT ONLY. CREW TRY THE EMERGENCY PROCEDURES DESCRIBED ON CHECKLIST. THIS PROCEDURE DID NOT GET THE (3) GREEN GEAR LIGHTS.  AIRCRAFT LANDED WITH (2) GEARS DOWN ON RUNWAY 21, AND SLID INTO THE GRASS.  NO INJURIES TO CREW OR PASSENGERS.                                                                                                                                                                                                                                                                                                     2L72 4T4  T  1A17    E297    6  CP899     
20070821002032007082100203CE  2007       8          21         2007AP080901     120070809G5521043200185       SPAR                                    CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA                              RT ELEVATOR     CRACKED         B  LJERK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM094844015375                  15280910                                RT ELEVATOR SPAR FOUND BROKEN/CRACKED AT OB ATTACH POINT. OB HINGE BRACKET PULLED AWAY FROM SPAR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  ONT3A19    E223                 
20070821002092007082100209CE  2007       8          21         2007AP081001     120070810G27301016100190014   TORQUE TUBE     BEECH                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA                              ELEVATOR        WORN            B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW177166P1195911959 BB482       BB482                                   WHILE UNDERGOING A SCHEDULED INSPECTION, FOUND THE RT ELEVATOR HAD DEVELOPED VERTICAL PLAY WHEN GRASPED FROM THE TRAILING EDGE. FOUND THE ELEVATOR TORQUE TUBE HAD ROTATIONAL WHERE THE 6 EACH OB BLIND RIVETS ATTACH THE TORQUE TUBE TO THE MOUNT PLATE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 4T4  T  A24CE   E4EA                 
20070830000202007083000020CE  2007       8          30         2007AP0821001    120070809G249736153           TERMINAL                                BEECH 200   B200        1152922CE                                                               RT GCU          BROKEN          D      BA  EMER. DESCENT           UNSCHED LANDING                                                         BGHSMOKE/FUMES/ODORS/SPARKS  MULTIPLE FAILURE          ELECT. POWER LOSS-50 PC   CRCRUISE         1                      CE071925P9715                   BB1094                                  WIRE NUMBER P73G16N AT RT ENGINE FIREWALL GROUND POINT GS15 SEPARATED FROM THE WIRE TERMINAL DURING CRUISE FLIGHT. THIS WIRE CONNECTS GROUND TO THE GCU PIN G. THE RT GENERATOR OUTPUT SPIKED AND OPENED THE 325 AMP RT BUSS CURRENT LIMITER, THE 50 AMP RT INVERTER CURRENT LIMITER, AND DAMAGED RADIOS, THE GCU AND SYSTEMS WIRED TO THE RT BUSS. UPON INSPECTION, THE INSULATION OF P73G16N WAS FOUND STRIPPED TOO FAR FROM THE WIRE END THEREBY GIVING NO SUPPORT OF THE WIRE INTO THE TERMINAL AT THE INSULATION CRIMP AREA.                                                                                                                                                                                                               1L72 4T      A24CE                        
20070914002012007091400201EU  2007       9          14         2007F00052       120070904G7714AG34            TACH GENERATOR                          DORNERDO228 DO228202    2992030EU  GARRTTTPE331TPE33110T        WP  HARTZLHCB4T HCB4TN5     GL  LEFT ENGINE     FALSE INDICATIONE      E   ENGINE SHUTDOWN                                                                                 O  OTHER                                                                         CRCRUISE         1                      EA21403VA                       8171                                    LEFT RPM INDICATION ABNORMAL PERFORMED PRECAUTIONARY SHUTDOWN.  INSPECTION FOUND TACH GENERATOR SHAFT BROKEN.  REMOVED AND REPLACED TACH GENERATOR IAW AMM 77-11-03.  ENGINE GROUND PERFORMANCE RUN C/W AND PASSED.  ALL PARAMETERS NORMAL.  AIRCRAFT APPROVED FOR RETURN TO SERVICE.                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA16EU   E4WE    6  CP40EA    
20071130001442007113000144CE  2007       11         30         2007F00064       120071018G322013889           BEARING RACE                            BEECH 100   B100        1152919CE                                                               NLG             CORRODED        B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL25500KD200                    BE79                                    FOUND BOTH NOSE WHEEL BEARINGS PN 13889, AND RACES, PN 13836 TO BE CORRODED.  CHANGED THESE SAME BEARINGS AND RACES AT LAST INSPECTION DUE TO SAME PROBLEM.  BEARINGS HAVE 200 HOURS OR 4 MONTHS ON THEM.  NOSE WHEEL IS AN STC WHEEL AND BRAKE ASSEMBLY.  WE ALSO REPLACED THESE SAME BEARINGS AND RACES 1 YEAR PRIOR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 4T      A14CE                        
20071105000112007110500011SW  2007       11         5          2007F00065       120071016G6320204040016005    TRANSMISSION                            BELL  204   UH1F        1181411SW  GE    T58   T58GE3           NE                              MAIN ROTOR      CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM054040P                       657911                                  CRACK FOUND ON MAIN GEARBOX (TRANSMISSION IN VERTICAL CAST WEBBING ABOVE ENGINE TO TRANSMISSION DRIVE QUILL.  MILITARY TECHNICAL MANUAL ALLOWS .2500 INCH RADIUS/POLISH INTO WEBBING THIS CRACK HAS BEEN FOUND ON THREE (3 EACH) TRANSMISSIONS ON OTHER AC WITH ONE PENETRATING THE GEARBOX AND LEAKING FLUID.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 4U4  U  EXPA1G71                     
20070108001482007010800148CE  2007       1          8          2007FA0000001    120070102G281010092004115     LINE                                    BEECH 200   B200        1152922CE  PWA   PT6   PT6A42      52043NE                              FUEL SYSTEM     CHAFED          C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM08155AV                       BB1216                                  DURING A SCHEDULED PHASE INSPECTION P/N 100-920041-15 ALUMINUM MAIN FUEL LINE WAS FOUND CHAFED IN THE LT MAIN LANDING GEAR WHEEL WELL WHERE IT ENTERS INTO THE BACK OF THE WING. THE EDGES OF THE HOLE THAT THE LINE PASSES THROUGH WAS PROTECTED WITH PLASTIC ANTI CHAFE MATERIAL THAT WE CALL TANK TRACKS, OR RAILROAD TRACK, AND HAS A PN MS21266-1N.  THIS ANTI CHAFE MATERIAL WAS INSTALLED AT THE FACTORY. THIS ANTI CHAFE MATERIAL CAUSED P/N 100-920041-15 ALUMINUM MAIN FUEL LINE TO BE CHAFED ALMOST THROUGH ITS .030 INCH SIDEWALL THICKNESS.  THERE ARE OTHER AC THAT HAVE CHAFED FUEL LINES DUE TO THE CLOSE TOLERANCE OF THE FUEL LINES PASSING THROUGH THE STRUCTURE IN THE MAIN LANDING GEAR WHEEL AREA.                        1L72 4T4  T  A24CE   E4EA                 
20070116000442007011600044EA  2007       1          16         2007FA0000031    220070103G852013B37024        CRANKSHAFT                              PIPER PA28  PA28161     7102803SO  LYC   O320  O320D3G     41508EA  SNSNCH74D   74DM        EA  ENGINE          CORRODED        D  GICRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM015347M2372                   2842136     L1949939A   A59073          THE ENGINE CURRENTLY UNDERGOING ITS FIRST OVERHAUL SINCE NEW.  THE CRANKSHAFT WAS CLEANED, URETHABOND 104 COATING REMOVED AND CORROSION PITTING WAS DISCOVERED BENEATH COATING.  THE PITTING EXCEEDED (SERVICEABLE LIMITS) AS STATED IN SB NR 505B.  THIS CAUSED THE CRANKSHAFT THE BE REMOVED     FROM SERVICE.  THE ENGINE AVERAGED 39.5 HOURS/ MONTH SINCE IT WAS NEW.  MFG AD COVERS THIS SUBJECT WITH THE COMPLIANCE WITH FAR, BEING TERMINATING ACTION FOR THE REPETITIVE INSPECTION.  THE CRANKSHAFT (FROM THE FACTORY) HAD THE COATING AND (PID) STAMPING.  NOTE: DUE TO THE URETHABOND 104 COATING, THIS SHOULD HAVE PREVENTED THE CORROSION PITTING WHICH IS A CONCERN OF THIS AD.  THE ENGINE OVERHAULER STATED THE COATING WAS NOT W1L71 3O3  O  2A13    E274    5  NP88614   
20070125000422007012500042SO  2007       1          25         2007FA0000036    220070102G8520                LIFTER                                  CESSNA206   U206C       2073332CE  CONT  O520  IO520F      17032SO                              NR 6 CYLINDER   DETERIORATED    D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL0329114                       U2061084    1683457                     AFTER DRAINING OIL AND INSPECTING FILTER, LARGE FLAKES OF METAL WERE FOUND.  DISASSEMBLED VALVE TRAIN AND FOUND SPALLING ON CYLINDER NR 6 INTAKE LIFTER.  DAMAGE OCCURRED TO THE CORRESPONDING CAM LOBE AND CLYINDER NR 5 INTAKE LIFTER DUE TO DETERIORATION OF CYLINDER NR 6 INTAKE LIFTER.  UPON INSPECTION IT WAS DETERMINED THAT THE LIFTER HAS BAD METALLURGY.  ALL OTHER LIFTERS NOT NOTED, SHOWED PROPER WEAR, AND HARDNESS TESTING MARKS.  THE CAM SHOWED DAMAGE ON CORRESPONDING LOBE, NOT DETERIORATION, AND OTHER LOBES SHOWED PROPER WEAR.  THE ENGINE HAS 228.06 HOURS SINCE FACTORY REMANUFACTURE.  MFG WAS CONTACTED ABOUT SITUATION, AND NO INTEREST WAS NOTED ON POSSIBLE PROBLEMS.  ENGINE WAS SENT TO LOCAL REPAIR STATION FO1H71 3O3  O  A4CE    E5CE                 
20070125002502007012500250EA  2007       1          25         2007FA0000038    120070115G32332953310095200   SEAL            ROTOL                   CNDAIRCL600 CL6002B16   1900305EA                                                               ACTUATOR PISTON POROUS          B      K   NONE                                                                                            KJ FLUID LOSS                WARNING INDICATION                                  ININSP/MAINT     1                      GL13                DCL28293                                            GREEN TWEED SEAL P/N 295-33100-952-0050 INSTALLED ON PISTON ASSEMBLY IN MFG SIDE BRACE ACTUATOR P/N: 6500-3 HAVE BEEN FOUND WITH VOIDS ON THE INNER RAISED SURFACE CAUSING FLUID LEAK.  THESE VOIDS ARE UNDETECTED AT INSTALLATION OF NEW SEAL AS THE VOIDS ARE NOT ON THE SURFACE AND DO NOT BECOME VISIBLE UNTIL AFTER MONTHS OF OPERATION.  SEAL CONDITION NOTED DURING WARRANTY REPAIR.  SUBJECT ACTUATOR RETURNED FOR WARRANTY REPAIR AFTER 11 MONTHS OPERATION.                                                                                                                                                                                                                                                                           2L72 4F    RTA21EA                        
20070124001832007012400183SO  2007       1          24         2007FA0000039    120070116G2497                WIRE                                    PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA                              UNKNOWN         WORN            C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO17456M                        318152081                               THE WIRING THAT PASSES THROUGH THE NOSE RIB GROMMETS HAVE WORN TO THE EXTENT THAT THE INSULATION IS GONE AT PLACES CAUSING THE METAL CONDUCTOR TO SHOW THROUGH.  IT APPEARS THAT THIS IS WORSE WITH THE GREATER AMOUNT OF CABLES IN THE BUNDLE.  BUNDLES OF ONLY 2 WIRES DO NOT HAVE THIS PROBLEM. APPARENTLY THE BUNDLE IS (SLAPPED) UP AND DOWN WITH VIBRATION.  THIS IS CAUSE FOR CONCERN DUE TO SPARKING NEAR THE FUEL TANK.                                                                                                                                                                                                                                                                                                                1L72 3O3  O  A20SO   E14EA                
20070129003462007012900346SO  2007       1          29         2007FA0000040    120070116G3233400872          CLEVIS BOLT                             PIPER PA28  PA28R201    7102816SO  LYC   O360  IO360A1A    41514EA                              NLG             SHEARED         B      A   UNSCHED LANDING                                                                                 FJ FLT CONT AFFECTED         WARNING INDICATION                                  CRCRUISE         1                      GL21289ND4558                   2844039                                 DURING CRUISE FLIGHT, CREW REPORTED LOUD BANG FOLLOWED BY A NOSE GEAR DOWN AND LOCKED INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION BY MX PERSONNEL NOSE GEAR ACTUATOR ROD END CLEVIS BOLT (AN23-21A) MISSING WITH EVIDENCE OF BOLT FAILURE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3O3  O  2A13    1E10                 
20070126002512007012600251SO  2007       1          26         2007FA0000041    120070116G3233400872          CLEVIS BOLT                             PIPER PA28  PA28R201    7102816SO  LYC   O360  IO360A1A    41514EA                              NLG             SHEARED         B  OG5RA   UNSCHED LANDING                                                                                 FDJFLT CONT AFFECTED         INFLIGHT SEPARATION       WARNING INDICATION        CRCRUISE         1                      GL21289ND4558                   2844039                                 DURING CRUISE FLIGHT, CREW REPORTED LOUD BANG FOLLOWED BY A NOSE GEAR DOWN AND LOCKED INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION BY MX PERSONNEL NOSE GEAR ACTUATOR ROD END CLEVIS BOLT (AN23-21A) MISSING WITH EVIDENCE OF BOLT FAILURE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3O3  O  2A13    1E10                 
20070129003472007012900347SO  2007       1          29         2007FA0000042    120070116G2497                WIRE                                    PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA                              ELECTRICAL SYS  CHAFED          C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO17456M                        318152081                               THE WIRING THAT PASSES THROUGH THE NOSE RIB GROMMETS HAS WORN TO THE EXTENT THAT THE INSULATION IS GONE AT PLACES CAUSING THE METAL CONDUCTOR TO SHOW THROUGH.  IT APPEARS THAT THIS IS WORSE WITH THE GREATER AMOUNT OF CABLES IN THE BUNDLE.  BUNDLES OF ONLY 2 WIRES DO NOT HAVE THIS PROBLEM. APPARENTLY THE BUNDLE IS (SLAPPED) UP AND DOWN WITH VIBRATION.  THIS IS CAUSE FOR CONCERN DUE TO SPARKING NEAR THE FUEL TANK.                                                                                                                                                                                                                                                                                                                 1L72 3O3  O  A20SO   E14EA                
20070126000062007012600006CE  2007       1          26         2007FA0000046    120070105G571305112821        STRINGER                                CESSNA170   170B        2072306CE  CONT  O300  O300*       17022SO                              WING            CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL033436D4200                   26979                                   CRACKED AT FORWARD END AND PROGRESSES AFT.  PROP STRIKE, OUT OF BALANCE PROP.  EXAMPLE FROM C-170B WITH THE ENGINE INSTALLED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  O  A799    E253                 
20070125003462007012500346CE  2007       1          25         2007FA0000047    120070105G57130511282         STRINGER                                CESSNA170   170B        2072306CE  CONT  O300  O300*       17022SO                              WING            CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL033436D4200                   26979                                   CRACKED AT FWD END AND PROGRESSES AFT.  PROP STRIKE, OUT OF BALANCE PROP?  AIRCRAFT HAS A HISTORY OF WING REPAIRS FROM GROUND LOOPS BUT HAS SINCE HAD A ENGINE UPGRADE TO MFG.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  O  A799    E253                 
20070125003472007012500347CE  2007       1          25         2007FA0000048    120070105G57130511282         STRINGER                                CESSNA170   170B        2072306CE                                                               WING            CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03                                                                    CRACKED AT FORWARD END AND PROGRESSES AFT.  PROP STRIKE, OUT OF BALANCE PROP.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O      A799                         
20070125002812007012500281EU  2007       1          25         2007FA0000049    120070104G4980MY20240035005A3 SEAL            MICROTURBO              AMD   FALC20FALCON20F5  2730105EU  GARRTTTFE731TFE731*     01518WP                              APU EXHAUST     DETERIORATED    B  JGVRO   OTHER                                                                                           S  AFFECT SYSTEMS                                                                NRNOT REPORTED   1                      CE09189RB1673       592         262                                     DETERIORATED APU EXHAUST DUCT SEAL BETWEEN THE DUCT FLANGE AND AIRCRAFT SKIN ALLOWED HOT EXHAUST GASSES TO ENTER THE TAILCONE AREA RESULTING IN HEAVY SOOT BUILDUP AND HEAT DAMAGE TO WIRE BUNDLES AND ELECTRICAL CONNECTORS AND STRUCTURAL COMPONENTS ADJACENT TO THE APU EXHAUST OPENING.  ULTRASOUND INSPECTION REVEALED HEAT DAMAGE TO THE AC SKIN ABOVE THE EXHAUST OPENING.  THE APU EXHAUST OPENING DOUBLER AND STRINGERS ADJACENT TO THE OPENING.  PERIODIC INSPECTION OF THE APU INSTALLATION, INCLUDING THIS SEAL, IS REQUIRED EVERY A-CHECK IAW MM.  (K)                                                                                                                                                                             2L72 4F4  FRTA7EU    E6WE                 
20070125001972007012500197SO  2007       1          25         2007FA0000050    120070110G5521510229615       ATTACH ANGLE                            AMRGENAA5   AA5A        3960106SO  LYC   O320  O320*       41508EA                              STABILIZER      CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW179962U3163                   AA5A0362                                DURING INSPECTION, ANGLE PN 5102296-15 AND PN 5102296-16, WERE FOUND CRACKED IN THE UPPER END OF THE ANGLE AS INSTALLED.  CAUSE OF CRACKING IS BELIEVED TO BE DUE TO HIGHT STRESS LOADS IN THIS AREA.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  O  A16EA   E274                 
20070125001982007012500198CE  2007       1          25         2007FA0000051    120070107G5230                DOOR                                    CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              CARGO BAY       OPEN            D      K   NONE                                                                                            O  OTHER                                                                         LDLANDING        1                      WP01480DG5294                   5600015     108029                      RT BAGGAGE DOOR POPPED OPEN ON ROLLOUT WITHOUT WARNING.  COULD NOT DUPLICATE CIRCUMSTANCES, SUGGEST INSPECTING LATCHES AND DOOR WARNING.  ON A MORE REGULAR BASIS.  AIRCRAFT RETURNED WITHOUT PROBLEM.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA22CE   E25EA                
20070129003552007012900355EU  2007       1          29         2007FA0000054    120070102G2435                BEARING         LUCAS       23080005    BRAERODH125 BAE125800A  1500285EU  GARRTTTFE731TFE731*     01518WP                              STARTER GEN     FAILED          C      D   RETURN TO BLOCK                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      EA09180NE     710   95274       NA0401      P91312                      FORWARD BEARING FAILED                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA3EU    E6WE                 
20070125001342007012500134SO  2007       1          25         2007FA0000056    120070110G5521510229615       ATTACH ANGLE                            AMRGENAG5B  AG5B        3990100SO  LYC   O360  O360*       41514EA                              STABILIZER      CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW17119661190                   10121                                   DURING INSPECTION, ANGLE PN 5102296-15 AND PN 5102296-16, WERE FOUND CRACKED IN THE BEND RADIUS OF THE UPPER END OF THE ANGLE AS INSTALLED.  CAUSE OF CRACKING IS BELIEVED TO BE DUE TO HIGH STRESS LOADS IN THIS AREA.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3O3  ONT1L71    E286                 
20070125000632007012500063GL  2007       1          25         2007FA0000057    120070105G5210                ATTACH FITTING                          DIAMONDA40  DA40        2990002GL                                                               AFT CABIN DOOR  BENT            D  GO3SA   UNSCHED LANDING                                                                                 D  INFLIGHT SEPARATION                                                           NRNOT REPORTED   1                      NM07422FP212                    40FC022                                 AFT CABIN DOOR ASSY SEPARATED FROM AC DURING FLIGHT.  CONTROL OF THE AC WAS MAINTAINED AND LANDED SAFELY AT DEPARTURE AIRPORT.  DOOR WAS EVENTUALLY RECOVERED AND UPON VISUAL INSPECTION OF THE DOOR, THE AFT DOOR LATCH PIN WAS NOT ENGAGED.  THE FRONT DOOR LATCH PIN WAS PROPERLY ENGAGED AND THE DOOR LATCH WAS CLOSED.  NO (DOOR OPEN) ANNUNCIATION WAS INDICATED BECAUSE THE DOOR OPEN SWITCH IS ACTUATED FROM THE FRONT DOOR LATCH PIN.  UPON DISASSEMBLY OF THE DOOR, THE AFT DOOR LATCH ROD WAS DETACHED FROM THE LATCH MECHANISM.  THE ATTACHMENT CLIP, (PN AND NAME NOT GIVEN; NR 215 IN THE PARTS BOOK) WAS BENT ALLOWING THE ROD TO BECOME SEPARATED FROM THE LATCH.  A MUCH STRONGER MATERIAL IS RECOMMENDED FOR THE ATTACHMENT CL1L71 3O    NTA47CE                        
20070125003072007012500307EA  2007       1          25         2007FA0000058    220070105G854061098           GEARSHAFT                               DIAMONDA40  DA40        2990002GL  LYC   O360  O360A4M     41514EA                              ENGINE          SEIZED          D  GO3SO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07423FP234                    40FC023     L4037236A                   REMOVED VACUUM DRIVE ASSEMBLY AND FOUND DRIVE GEAR SHAFT SEIZED AND (3) TEETH BROKEN OFF OF DRIVE GEAR.  FURTHER INSPECTION REVEALED NO LUBRICATION PORT FOR PRESSURIZED ENGINE OIL TO LUBRICATE THE DRIVE GEAR SHAFT.  ALL (3) TEETH WER FOUND IN THE OIL PUMP INLET SCREEN.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  ONTA47CE   E286                 
20070125001382007012500138SO  2007       1          25         2007FA0000059    120070110G5521510229615       ATTACH ANGLE                            AMRGENAA5   AA5B        3960105SO  LYC   O360  O360*       41514EA                              STABILIZER      CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW174521A2194                   AA5B1070                                DURING INSPECTION, ANGLE PN 5102296-15 AND PN 5102296-16, WERE FOUND CRACKED IN THE BEND RADIUS OF THE UPPER END OF THE ANGLE AS INSTALLED.  CAUSE OF CRACKING IS BELIEVED TO BE DUE TO HIGH STRESS LOADS IN THIS AREA.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3O3  O  A16EA   E286                 
20070125001492007012500149CE  2007       1          25         2007FA0000063    120070110G573005230294        SKIN                                    CESSNA172   172N        2072434CE                                                               RT WING         MISMANUFACTURED B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      SO09A5OR                                                                DURING AN RECEIVING INSPECTION OF NEW RT OB LEADING EDGE SKIN, IT WAS FOUND TO HAVE BEEN DRILLED UP INCORRECTLY SINCE NONE OF THE NOSE RIBS WOULD LINE UP AND THE SET UP WOULD HAVE LT INSUFFICIENT EDGE DISTANCE ON THE LOWER MAIN WING SPAR RIVET LINE.  THIS IS ZND TIME WE HAVE RECEIVED THIS SAME PART.  WE ASKED THAT THE PART NOT BE PUT BACK INTO MFG STOCK SINCE PART IS NON-CONFORMING.  THE PART CAME WITH 8130-3 AIRWORTHINESS APPROVAL TAG.  RECOMMEND MFG PERFORM CLOSE CONFORMITY INSPECTION OF PARTS.  (K)                                                                                                                                                                                                                      1H71 3O    NT3A12                         
20070125002922007012500292SO  2007       1          25         2007FA0000064    120070109G32136531904         CYLINDER                                PIPER PA28  PA28140     7102802SO  LYC   O320  O320*       41508EA                              LT MLG          DAMAGED         B  A5ORK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO09157153501                   287325144                               DURING AN ANNUAL INSPECTION FO THE LT MLG CYLINDER ASSY PN 6531904, IT WAS FOUND TO BE LOOSE IN THE MAIN WING SPAR.  THE LT MLG WAS REMOVED FOR FURTHER INSPECTION OF THE LT MAIN WING SPAR ASSY GEAR ATTACHING BOLT HOSES AND ATTACH POINTS.  CLOSE INSPECTION FO THE WING SPAR SHOWED THAT THE LOWER (4) BOLTS HOLES HAD BEEN ELONGATED.  THE HOLES IN THE LT LANDING GEAR CYLINDER WERE FOUND TO BE ELONGATED ALSO.  IT APPEARED THAT ALL BOLTS WERE TIGHT AND THIS CONDITION HAD BEEN LOOSE FOR SOME TIME.  AIRCRAFT WING SPAR WS REPAIRED AND THE LT MLG CYINDER WAS REPLACE WITH A LATER MODEL CYLINDER ASSY FROM MFG SINCE THE ORIGINAL PART WAS NO LONGER AVAILABLE.  RECOMMEND CLOSE INSPECTION OF LANDING GEAR ATTACH POINTS DURING AL1L71 3O3  O  2A13    E274                 
20070130001762007013000176EU  2007       1          30         2007FA0000065    120070103G2742                ACTUATOR                                PARTENP68   P68C        6780105EU  LYC   O360  IO360A1A    41514EA                              PITCH TRIM      SEIZED          D      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             NRNOT REPORTED   1                      GL033832Q                       274                                     (REF NR: PT202781) AIRCRAFT ARRIVED WITH PITCH TRIM ACTUATOR SEIZED IN FULL NOSE UP POSITION.  ACTUATOR IS DRIVEN BY TRIM CABLE LOOPED OVER ACTUATOR PULLEY WITH NO MEANS OF PREVENTING CABLE FROM SLIPPING ON THE PULLEY.  IT IS POSSIBLE TO RUN TRIM TO FULL TRAVEL ALLOWING ACTUATOR TO BIND.  WHEN TRIM CONTROL IS REVERSED THE CABLE CAN SLIP OVER PULLEY WITH OUT MOVING ACTUATOR IF PROPER CABLE TENSION IS NO PRESENT.  SUGGEST REVISION TO POH/AFM ADVISING CREW TO VISUALLY CHECK OPERATION OF PITCH TRIM SYSTEM PRIOR TO FLIGHT.  (K)                                                                                                                                                                                                1H72 3O3  O  A31EU   1E10                 
20070131000332007013100033CE  2007       1          31         2007FA0000070    120070108G25205514551129      ATTACH FITTING  CESSNA                  CESSNA500   500CESSNA   2076602CE  PWA   JT15  JT15D1      52060NE                              CABIN           CRACKED         B  ESERO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO11117TW                       5000059                                 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS.  CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 4F4  F  A22CE   E1NE                 
20070201000012007020100001NE  2007       2          1          2007FA0000071    120070110G62207610208051105   TIE BOLT                                SKRSKYS76   S76B        8143007NE  PWA   PT6   PT6*        52043EA                              MAIN ROTOR      BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA17411JW3392                   760357                                  WHILE PERFORMING A ROUTINE INSPECTION OF THE MAIN ROTOR SPINDLES, A SPINDLE TIE BOLT WAS FOUND BROKEN AT THE THREADED END OF THE BOLT WHERE THE NUT ATTACHES.  THE NUT WAS FOUND INSIDE THE SPINDLE CUFF WHERE THE ROTOR BLADE IS ATTACHED.  A BROKEN SECTION OF THE BOLT WAS STILL THREADED INTO THE NUT.  IT IS UNCLEAR WHY THE BOLT BROKE.  THE BOLT AND SPINDLE HAVE BEEN REMOVED AND SENT TO MFG AIRCRAFT FOR FURTHER INVESTIGATION TO DETERMINE CAUSE OF FAILURE.  (K)                                                                                                                                                                                                                                                                    1G72 4U3  T  H1NE    E2NE                 
20070129001202007012900120EU  2007       1          29         2007FA0000072    120070102G2435                BEARING                                 BRAERODH125 BAE125800A  1500285EU  GARRTTTFE731TFE731*     01518WP                              STATER GEN      FAILED          C      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              CRCRUISE         1                      EA09180NE     710   95274       NA0401      P91312                      FORWARD BEARING FAILED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA3EU    E6WE                 
20070129003572007012900357    2007       1          29         2007FA0000073    120070126G8011ES6462751       STARTER                                                                                                                                 ENGINE          LEAKING         C  WS9RO   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      NM07     2                                                              SUBMITTED TO SLC-FSDO BY (WS9R).  STARTER LEAKING OUT OF REAR OF STARTER PLATE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           
20070131000662007013100066SO  2007       1          31         2007FA0000074    120070123G5312624403          BULKHEAD                                PIPER PA28  PA28180     7102808SO  LYC   O360  O360A3A     41514EA  SNSNCH76E   76EM8       EA  FUSELAGE        CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL097095W4309                   28882       L148936C    15028K          THE BULKHEAD, BRACKETS, AND DOUBLERS AT STA. 228.3 WERE SEVERELY CORRODED. THIS BULKHEAD IS THE FRONT SUPPORT FOR THE VERTICAL STABILIZER/RUDDER ASSEMBLY. THE CORROSION COVERED AN AREA APPROXIMATE THE SIZE OF THE FRONT RUDDER ATTACHMENT BRACKET THAT IS PART OF THIS BULKHEAD ASSEMBLY. THE CORROSION WAS FOUND DURING AN ANNUAL INSPECTION AND WAS ONLY VISIBLE, WITHOUT DISASSEMBLY, AS SLIGHT BUBBLING OF THE METAL ON THE BRACKETS FACING REARWARD THAT ARE ATTACHED TO THE AFORE MENTIONED BULKHEAD ASSEMBLY.                                                                                                                                                                                                                         1L71 3O3  O  2A13    E286    5  NP4EA     
20070131000672007013100067SO  2007       1          31         2007FA0000075    120070123G5312624403          BULKHEAD                                PIPER PA28  PA28180     7102808SO  LYC   O360  O360A3A     41514EA  SNSNCH76E   76EM8       EA  FUSELAGE        CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL097095W4309                   28882       L148936C    15028K          THE BULKHEAD, BRACKETS, AND DOUBLERS AT STA. 228.3 WERE SEVERELY CORRODED. THIS BULKHEAD IS THE FRONT SUPPORT FOR THE VERTICAL STABILIZER/RUDDER ASSEMBLY. THE CORROSION COVERED AN AREA APPROXIMATE THE SIZE OF THE FRONT RUDDER ATTACHMENT BRACKET THAT IS PART OF THIS BULKHEAD ASSEMBLY. THE CORROSION WAS FOUND DURING AN ANNUAL INSPECTION AND WAS ONLY VISIBLE, WITHOUT DISASSEMBLY, AS SLIGHT BUBBLING OF THE METAL ON THE BRACKETS FACING REARWARD THAT ARE ATTACHED TO THE AFORE MENTIONED BULKHEAD ASSEMBLY.                                                                                                                                                                                                                         1L71 3O3  O  2A13    E286    5  NP4EA     
20070131000732007013100073SO  2007       1          31         2007FA0000076    120070117G2434635796          COUPLING        CONT                    PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360KB   17025SO  MCAULY3AF32C3AF32C508   GL  ALTERNATOR      FAILED          C      B   EMER. DESCENT                                                                                   HG ELECT. POWER LOSS-50 PC   MULTIPLE FAILURE                                    CRCRUISE         1                      GL09321AK4479 869   B020128     3447021     811403R     960254          ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY.  1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, CAUSING THE ALTERNATORS FAILURES.  PILOTS LOST ELECTRICAL AND DESCENDED THROUGH ICE, UNABLE TO SHED MODERATE TIME ICE ACCUMULATION. TOTAL COMM AND AVIONICS FAILURE, PARTIAL PANEL WITH NO PITOT HEAT AVAILABLE.                                                                                                                                                                                                                                                                                                                                                                1L72 3O3  O  A7SO    E9CE    5  CP22EA    
20070131000752007013100075SO  2007       1          31         2007FA0000077    120070117G2434635796          COUPLING        CONT                    PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360KB   17025SO  MCAULY3AF32C3AF32C508   GL  ALTERNTOR       FAILED          C      B   EMER. DESCENT                                                                                   HG ELECT. POWER LOSS-50 PC   MULTIPLE FAILURE                                    CRCRUISE         1                      GL09321AK4479 869   B020128     3447021     811403R     960254          ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY.  1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, CAUSING THE ALTERNATORS FAILURES.  PILOTS LOST ELECTRICAL AND DESCENDED THROUGH ICE, UNABLE TO SHED MODERATE  RIME ICE ACCUMULATION. TOTAL COMM AND AVIONICS FAILURE, PARTIAL PANEL WITH NO PITOT HEAT AVAILABLE.                                                                                                                                                                                                                                                                                                                                                               1L72 3O3  O  A7SO    E9CE    5  CP22EA    
20070130001792007013000179CE  2007       1          30         2007FA0000081    120070119G3245850X1000        TUBE                                    CESSNA208   208B        2073701CE                                                               TIRE            DAMAGED         C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL211293E4                      208B0537                                RIGHT MAIN GEAR TIRE REPORTED LOW.  REMOVED TIRE TO CHECK THE TUBE.  THE TUBE APPEARED TO LOOK OLD AND CHECKED.  TECHNICIAN REPLACED WITH NEW TUBE.  ONE WEEK LATER TIRE REPORTED LOW AGAIN ON SAME POSITION.  REMOVED THE TIRE AND INSPECTED THE TUBE.  THE TUBE LEAKING ON ONE SIDE AND ALMOST WORN THRU ON THE OPPOSITE SIDE.  AFTER FURTHER INVESTIGATION DETERMINED THAT THE STICKERS INSIDE THIS 8.50 X 10.00 FC III P/N 850T86-2 S/N 62570185 TIRE HAD CAUSED THE FAILURE.  THIS WAS THE SECOND FAILURE ON THE SAME GEAR POSITION WITH THE SECOND NEW TUBE WITHIN 7 WEEKS.  AFTER CONTACTING MANUFACTURER TIRE PRODUCT SUPPORT, SENT A NOTE AND PICTURES ABOUT THE PROBLEM AND THE FAA PMI FROM THE FARGO FSDO.  THE MANUFACTURER RESPOND1H71 3T      A37CE                        
20070131001002007013100100    2007       1          31         2007FA0000082    220070119G7414K3823           DISTRIBUTOR BLK SLICK       6314                                                                                                        MAGNETO         MELTED          B      K   NONE                                                                                            M  OVER TEMP                                                                     ININSP/MAINT     1                      GL21408ND493        05100422                                            DURING TEARDOWN INSPECTION OF 2 SLICK 6314 MAGNETOS THE DISTRIBUTOR BLOCK AND GEAR ASSY PN K3823 WAS FOUND TO BE MELTED TO THE POINT OF EMANATE FAILURE. THE MAGS WERE FROM 2 SEPARATE AIRCRAFT BUT WITH NEAR IDENTICAL TOTAL TIMES ONE AT 493.3 HRS AND THE OTHER AT 498.8.THE MANUFACTURE WAS CONTACTED AND THEY REQUESTED THE MAGS FOR EVALUATION.                                                                                                                                                                                                                                                                                                                                                                                                                                     
20070131001032007013100103CE  2007       1          31         2007FA0000083    120070123G716007520161011     SEAL                                    CESSNA180   180J        2072622CE                                                               INTAKE          MISSING         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NE059986N                       18052641                                INTAKE SEALS FOUND MISSING. AD 77-04-05 PERTAINING TO THIS DEFECT HAD BEEN PREVIOUSLY ACCOMPLISHED IN 1977. DUE TO THE AGE OF THE FLEET I BELIEVE THAT THE ONE TIME INSPECTION IAW THIS AD IS INSUFFICIENT. AS THIS IS NOT THE FIRST TIME I HAVE FOUND THE SAME CONDITION ON OTHER AIRCRAFT I WOULD CONSIDER UPDATING THE AD TO INCLUDE REPETITIVE INSPECTIONS AT ANNUAL/100 HOUR INTERVALS.                                                                                                                                                                                                                                                                                                                                                    1H71 3O      5A6                          
20070131001042007013100104CE  2007       1          31         2007FA0000084    120070119G3245850X1000        TUBE                                    CESSNA208   208B        2073701CE                                                               LANDING GEAR    WORN            C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL211293E4                      208B0537                                RT MAIN GEAR TIRE REPORTED LOW. REMOVED TIRE TO CHECK THE TUBE. THE TUBE APPEARED TO LOOK OLD AND CHECKED. TECHNICIAN REPLACED WITH NEW TUBE. 1 WEEK LATER TIRE REPORTED LOW AGAIN ON SAME POSITION. WE REMOVED THE TIRE AND INSPECTED THE TUBE. THE TUBE LEAKING ON ONE SIDE AND ALMOST WORN THRU ON THE OPPOSITE SIDE.  AFTER FURTHER INVESTIGATION WE DETERMINED THAT THE STICKERS INSIDE THIS 8.50 X 10.00 FC III P/N 850T86-2 S/N 62570185 TIRE HAD CAUSED THE FAILURE. THIS WAS THE SECOND FAILURE ON THE SAME GEAR POSITION WITH THE SECOND NEW TUBE WITHIN 7 WEEKS.  AFTER CONTACTING MFG WHO GAVE ME AN E-MAIL FOR THEIR PRODUCT SUPPORT CONTACT WE GOT INFORMATION VERY QUICKLY. I SENT HIM A NOTE AND PICTURES ABOUT THE PROBLEM AND 1H71 3T      A37CE                        
20070131001062007013100106SO  2007       1          31         2007FA0000085    120070117G2434635796          COUPLING        CONT                    PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360KB   17025SO  MCAULY3AF32C3AF32C509   GL  ALTERNATOR      FAILED          C      B   EMER. DESCENT                                                                                   HG ELECT. POWER LOSS-50 PC   MULTIPLE FAILURE                                    CRCRUISE         1                      GL09321AK4479 869               3447021     812128R     961321          ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATOR, IN IMC SIMULTANEOUSLY. COUPLING FAILURE RESULTED IN TOTAL ELECTRICAL FAILURE, RT ENGINE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 3O3  O  A7SO    E9CE    5  CP22EA    
20070131001072007013100107CE  2007       1          31         2007FA0000086    120070126G32601003810061      DOWNLOCK SWITCH                         BEECH 200   B200        1152922CE  PWA   PT6   PT6A60A     52043NE                              LANDING GEAR    FAILED          E      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 LDLANDING        1                      GL07200EW7169 70                BB1163                                  NOSE LANDING GEAR DID NOT HAVE A DOWN AND LOCKED INDICATION GEAR WARNING SYSTEMS ACTIVATED (LIGHT IN SELECTOR HANDLE AND GEAR HORN). AN UNEVENTFUL LANDING HAS MADE VISUAL CHECK OF NOSE GEAR SHOWED TO BE IN THE DOWN AND LOCKED POSITION. SWITCH REMOVED AND REPLACED WITH A NEW UNIT AND THE SYSTEM CHECKED NORMAL.                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 4T4  T  A24CE   E4EA                 
20070131002562007013100256CE  2007       1          31         2007FA0000090    120070102G2730355246516       CONTROL CABLE                           BEECH 35    V35         1151538CE  CONT  O520  IO520*      17032SO                              ELEVATOR SYS    BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL23767TM2801                   D8556                                   FOUND BROKEN STRANDS ON ELEVATOR CABLE BEHIND INSTRUMENT PANEL ABOUT 10 INCHES ABOVE THE (PN 535521242-13) BOBWEIGHT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  O  3A15    E5CE                 
20070131002572007013100257EA  2007       1          31         2007FA0000091    220070118G7314AC40295         PUMP                                    AMRGENAA5   AA5         0631410SO  LYC   O320  O320E2G     41508EA                              ENGINE          LEAKING         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      SO0124AU      302               AA50588                                 AT ANNUAL FUEL STAINS WERE FOUND ON ENGINE LOWER COWLING.  IN AN ATTEMPT TO FIND THE LEAK THE ELECTRIC FUEL PUMP WAS TURNED ON TO PRESSURIZE THE FUEL SYSTEM BUT NO LEAKAGE WAS FOUND.  WHILE TURNING ENGINE OVER BY HAND DURING THE COMPRESSION CHECK A LARGE FLOW OF GAS WAS FOUND LEAKING OUT THE SIDE OF THE FUEL PUMP ABOVE THE OUTLET PORT BETWEEN THE DIAPHRAGM AND PUMP CASTINGS.  REPAIR STATION WAS CONTACTED AND THY INDICATED THAT THE SCREWS THAT HOLD THE PUMP TOGETHER ARE ASSEMBLED AT 25 INCH LBS TORQUE + OR - 5 INCH LBS .  PUMP SCREWS WERE CHECKED AND THEY WERE FOUND TO BE TIGHTENED TO ONLY 2-3 INCH LBS OF TORQUE.  ALL OF THE SCREWS HAD TORQUE PUTTY ON THEM WHICH INDICATED THE SCREWS HAD NOT BACKED OUT.  GUESS IS1L71 3O3  O  A16EA   E274                 
20070215001692007021500169WP  2007       2          15         2007FA0000092    220070115G725031021069        TURBINE WHEEL                           GULSTM690TP 690B        7630516SW  GARRTTTPE331TPE33110T        WP  HARTZLHCB3T HCB3TN5     GL  ENGINE          DAMAGED         B  IZ2RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW15690LL2245                   11544       P99112C     BVA7239         INSPECTION OF ENGINE REVEALED DAMAGE TO 3RD STAGE TURBINE ROTOR VISIBLE THROUGH ENGINE TAILPIPE.  ENGINE WAS REMOVED FROM AIRCRAFT AND THE TURBINE SECTION MODULE REMOVED TO INVESTIGATE FOR CAUSE OF DAMAGE.  UPON INSPECTION 4 EA PINS WERE FOUND MISSING FROM 2ND STAGE TURBINE ROTOR ASSEMBLY CAUSING SIGNIFICANT DAMAGE TO VARIOUS TURBINE SECTION COMPONENTS, SEVERAL OTHER PINS WERE ALSO FOUND LOOSE AND DAMAGED.  SB ADDRESSES REMOVAL OF 2ND STAGE TURBINE ROTORS PN 310210610 UTILIZING AN IMPROVED PIN DESIGN.  FURTHERMORE MFG HAS INDEPENDENT SERVICE CENTER SPECIAL PROGRAM IN PLACE TO COVER PIN REPLACEMENT ON AFFECTED TURBINE ROTORS AT NO CHARGE, COVERING SECONDARY DAMAGE ON A PRORATED BASIS.  (K)                       1H72 3T4  T  2A4     E4WE    6  CP15EA    
20070213001652007021300165EA  2007       2          13         2007FA0000095    220070109G8520AEL321031       CRANKSHAFT                              CESSNA172   172L        2072432CE  LYC   O320  O320E2D     41508EA                              ENGINE          BROKEN          B  VA1RO   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  DEDESCENT        1                      SW1915RA 410                    17259568    L2207127A                   ENGINE BEGAN RUNNING ROUGH AND BECAME SMOOTH AGAIN DURING DESCENT.  TROUBLESHOOTING FIRST FOUND BRASS METAL PARTICLES IN AIR FILTER AND OIL.  CRANKSHAFT WAS APPARENTLY BROKEN OR CRACKED BUT STILL TOGETHER.  AFTER NUMEROUS GROUND RUSN AND KNOCKING NOISES HEARD, THE CRANKSHAFT BROKEN AND ROD THROWN THROUGH CASE.  THE BREAK WAS BETWEEN NR 3 AND NR 4 ROD JOURNALS.  SENG BACK TO ENGINE COMPONENTS FOR WARRANTY AND ANALYSIS.  (K)                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    E274                 
20070214000832007021400083SO  2007       2          14         2007FA0000096    120070103G3230455180          CONDUIT                                 PIPER PA24  PA24250     7102404SO  LYC   O540  O540*       41532EA                              LT MLG PUSH PULLSEPARATED       D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA636632P3200                   241755                                  THE LT MAIN LANDING GEAR PUSH PULL CONDUIT SEPARATED AT THE BALL END WHERE IT IS ATTACHED TO THE SUPPORT STRUCTURE IN THE WHEEL WELL.  BELIEVE THIS FAILURE OCCURRED AT THE PREVIOUS LANDING GEAR RETRACTION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  1A15    E295                 
20070213001762007021300176    2007       2          13         2007FA0000101    220070124G74146320            MAGNETO                                                                                                                                 ENGINE          FROZEN          B  WS9RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07                                                                    SHAFT IN MAGNETO FROZEN, WOULD NOT MOVE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             
20070213001892007021300189EA  2007       2          13         2007FA0000102    120070109G5755                BRACKET                                 CNDAIRCL600 CL6002B16   1900305EA  GE    CF34  CF343B1          NE                              FLT SPOILER     CRACKED         B  RO3RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE03684TS                       5384                                    WHILE PERFORMING A 96 MONTH AIRFRAME INSPECTION, DISCOVERED THE LT FLIGHT SPOILER TRANSMITTER BRACKET WAS CRACKED.  UPON REMOVING BRACKET, DISCOVERED MATTING SURFACE WITH TRANSMITTER WAS CORRODED.  DECIDED TO REMOVE TO INSPECT RT TRANSMITTER BRACKET AND FOUND THE RT SIDE CORRODED AS WELL.  REMOVED AND REPLACED BOTH BRACKETS.  RT AND LT HAVE THE SAME PN.  (K)                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20070213001642007021300164EA  2007       2          13         2007FA0000103    120070109G5755600913563       BRACKET                                 CNDAIRCL600 CL6002B16   1900305EA  GE    CF34  CF34*            NE                              RT FLT SPOILER  CRACKED         B  RO3RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE03267DW                       5391                                    RT FLIGHT SPOILER POSITION INDICATION WOULD NOT OPERATE PROPERLY.  UPON FURTHER INVESTIGATION, FOUND THE FLIGHT SPOILER TRANSMITTER BRACKET WAS CRACKED AND UNABLE TO HOLD POSITION TRANSMITTER.  REMOVED AND REPLACED BRACKET.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA21EA   E15NE                
20070205000432007020500043CE  2007       2          5          2007FA0000104    120070201G2710S394            CONTROL CABLE                           CESSNA172   172S        2072439CE                                                               AILERONS        FRAYED          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO155275S3179 100               172S9203                                DURING A ROUTINE INSPECTION THE AILERON CONTROL DIRECT CABLE WAS FOUND SERIOUSLY WORN IN THE CABIN OVERHEAD AREA. THE AILERON BALANCE AND DIRECT CABLES ARE SEPARATED AND GUIDED BY 3 PULLIES, P/N-S394, INDEX NR 30, CHAPTER 27-10-00, FIG 3 IN THE CESSNA PARTS MANUAL. THE CENTER CABLE WAS WORN EXTENSIVELY AND HAD BROKEN STRANDS. THE WEAR IS CAUSED BY CONTACT WITH THE PULLEY. IT IS DIFFICULT TO SEE WITHOUT ROTATING THE CABLE AND EXPOSING THAT PORTION OF THE CABLE THAT CONTACTS THE PULLEY DURING LEVEL FLIGHT. THE CABLE AT FIRST APPEARS SHINY, BUT WITH THE AID OF A POWERFUL MAGNIFYING GLASS REVEALS MUCH MORE SERIOUS WEAR. OBVIOUSLY, THE FAILURE OF THIS CABLE WOULD LIKELY RESULT IN THE LOSS OF THE AIRCRAFT WITH LITTLE1H71 3O    NT3A12                         
20070205000302007020500030CE  2007       2          5          2007FA0000105    120070202G571151220311        SPAR CAP                                CESSNA310   T310R       2074246CE  CONT  O520  TSIO520BB   17040SO  MCAULY3AF32C3AF32C87    GL  LT WING         CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA17465DL1132                   310R1622                                LT TOP WING SPAR CAPS AND TOP SKINS SEVERELY CORRODED IN AREA OF FACTORY NACELLE FUEL BLADDERS.  LT-PN 5122031-1.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 3O3  O  3A10    E8CE    5  CP22EA    
20070213001742007021300174GL  2007       2          13         2007FA0000106    120070111G7603                FRICTION LOCK                           AMTR  LANCARLANCAIR     05616TSGL  WALTERM601  M601E            EU                              POWER LEVER     INOPERATIVE     G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW11750TL154                    LIV555      913008                      AIRCRAFT EXPERIENCED LOSS OF POWER DURING TAKEOFF AND LANDED WITH LANDING GEAR RETRACTED DEPARTING RUNWAY FROM WHICH TAKEOFF WAS MADE.  INVESTIGATION REVEALED FRICTION LOCK WAS NOT EFFECTIVE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3O3  TRTEXPA1L71EXPE3T               
20070213000632007021300063EU  2007       2          13         2007FA0000107    120070125G5210333045181       SEAL                                    ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE731*     01518WP                              CABIN DOOR      LEAKING         D      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      SW09300XL9015                   276                                     THE AIRCRAFT DEPARTED, CLIMBING THROUGH 30000.  THE CABIN ALT BEGAN TO CLIMB WITH THE AIRCRAFT.  THE PILOTS REQUESTED TO DESCEND.  CENTER DECLARED EMERGENCY AND GAVE CREW 12000 FT.  AIRCRAFT PRESSURIZED PROPERLY AT THAT ALT.  PILOT REQUESTED DEVIATION AND TO HAVE EMERGENCY CANCELED.  THIS WAS GRANTED BY CENTER.  AFTER LANDING, CREW LOOKED OVER THE AC AND COULD NOT FIND ANYTHING WRONG, PROCEEDED, AT 19000 FT.  AIRCRAFT PRESSURIZED PROPERLY.  IN MAINTENANCE CREW INSPECTED THE AIRCRAFT AND PERFORMED NUMEROUS GROUND PRESSURIZATION RUNS AN COULD NOT DUPLICATE PROBLEM.  PILOT MADE STATEMENT THAT THE DOOR MAY NOT OF SEALED PROPERLY.  MAINTENANCE LOOKED AT THAT ASPECT AND FOUND THAT THE DOOR CAN BE CLOSED IN A MANOR TH2M72 4F4  F  A2SW    E6WE                 
20070213000602007021300060NE  2007       2          13         2007FA0000108    220070101G7200CFM563B1        POWERPLANT                              BOEING737   737300      1384610NM  GE    CFM56 CFM563B1    13802NE                              OIL SYSTEM      CONTAMINATED    B  UOXRA   UNSCHED LANDING                                                                                 RYJPARTIAL RPM/PWR LOSS      ENGINE STOPPAGE           WARNING INDICATION        NRNOT REPORTED   1                      SO19XAMAA449273514                          720721                      ENGINE SUFFERED AN IFSD DUE TO POWER LOSS AND A COMMANDED ENGINE SHUTDOWN WAS CARRIED OUT.  ENGINE RESTART WAS ATTEMPTED, UNSUCCESSFULLY.  FURTHER INVESTIGATION REVEALED THAT NR 10 STRUT ON FAN FRAME (9 O`CLOCK STRUT AFT LOOKING FWD) WHICH RADIAL DRIVE SHAFT IS LOCATED WAS PUNCTURED, BOTH ON UPPER AND LOWER SURFACES OF STRUT.  IT WAS AGREED TO CARRY OUT ENGINE REMOVAL AND RETURN ENGINE TO REPAIR FACILITY.  HYDRAULIC FLUID WAS FOUND IN OIL SYSTEM, AIR STARTER AND CSD OIL SUMPS.  ALL OIL WETTED ITEMS REQUIRE INSP.  ENGINE HAD UNDERGONE TROUBLESHOOTING FOR HIGH OIL CONSUMPTION FOLLOWING REPORTS ON 2 FLIGHTS AND RETURN ON DEC 22, 2006.  LEVELS OF 2.08 GALLON QUARTERS/HOUR WERE REPORTED AND AVERAGE OIL CON WAS 0.15 2L72 4F4  FRTA16WE   E2GL                 
20070213000552007021300055CE  2007       2          13         2007FA0000109    120070131G273050524401        BELLCRANK                               BEECH 90    65A901      1152901CE  PWA   PT6   PT6*        52043EA                              ELEVATOR        FAILED          C  NBFGO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA2787V                         LM130                                   FOUND BROKEN FORK ON ELEVATOR BELLCRANK SUPPORT ARM AT FWD END OF ELEVATOR LT PUSHROD.  FOUND THE PUSH ROD FWD ATTACH BOLT HAD BEEN OVER-TORQUED SO MUCH AS TO CREATE A 0.016 INCH -0.021 INCH DEPRESSION IN EACH (MAGNESIUM) FORK WHERE THEY PRESSED INTO THE ROD END BEARING.  MFG SB2231R2 INCLUDES: INSPECTION FOR CRACKS IN THIS AREA OF ELEVATOR BELLCRANK.  PROPER GAP BETWEEN ROD END AND SUPPORT ARM FORKS (0.00 INCH TO 0.01 INCH GAP) PROPER TORQUE OF PUSHROD ATTACH BOLT (70-108 INCH LBS)  RECOMMEND FOLLOWING PROPER INSPECTION, INSTALLATION AND TORQUE WHEN INSTALLING THE BELLCRANK AND PUSHRODS.  FOLLOW THE INSTRUCTIONS IN THE MM AND SB2231R2.  (K)                                                                       1L72 3T3  T  3A20    E2NE                 
20070209000362007020900036CE  2007       2          9          2007FA0000112    120070108G71601116            AIR FILTER                              CESSNA172   R172K       2072431CE  CONT  IO360 IO360*      17025CE                                              TWISTED         G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15758EJ                       R1723034                                DURING REMOVAL OF THE AIR FILTER THE CENTER WIRE MESH SCREEN WAS FOUND TWISTED AND BENT.  SOME OF THE WELDS WERE BROKEN.  SCREEN DEFORMATION CAN LEAD TO UNFILTERED AIR AND FOD ENTERING THE ENGINE.  APPARENT CAUSE IS EITHER OVERTORQUEING WING NUT AND/OR INSUFFICIENT STRENGTH OF SCREEN.  RECOMMEND UTILIZING A STRONGER MESH/PERFORATED SCREEN OR EVALUATING INSTALLATION INSTRUCTIONS/TORQUEING PROCEDURES.                                                                                                                                                                                                                                                                                                                              1H71 3O3  O  3A17    E1CE                 
20070212001562007021200156GL  2007       2          12         2007FA0000113    120070205G6500E181150P        V-BELT                                  AMTR  ROTWAYEXEC162F    056037TGL                                                               TAIL ROTOR      BROKEN          G      R   AUTOROTATION                                                                                    F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CE07113JD80                     6107                                    V BELT PREMATURELY FAILED. THIS IS A 250 HOUR CHANGE OUT PART.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3O    O EXPA1G71                     
20070312000622007031200062SO  2007       3          12         2007FA0000114    120070206G2820W70120TE        CONNECTOR                               GULSTMGV    GULFSTREAMGV3980116SO                                                               FUEL LINE       LOOSE           C      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      GL1583M                         557                                     FUEL LINE CONNECTOR IN MAIN WHEEL WELL COMING LOOSE, RESULTING IN FUEL LEAKING INTO WHEEL WELL.REFERENCE MFG ILLUSTRATED PARTS CATALOG; 28-26-00, FIGURE 5, PAGE 2, ITEM 205, PN W701-20TE.  WE ARE HAVING THIS PROBLEM ON MORE THAN ONE OF OUR AIRCRAFT.  THERE IS NO WAY TO SAFETY THIS FITTING.  THIS SITUATION COULD RESULT IN FUEL BEING SPRAYED ON A HOT BRAKE RESULTING IN A FIRE.                                                                                                                                                                                                                                                                                                                                                       2L72 4F    RTA12EA                        
20070220000102007022000010CE  2007       2          20         2007FA0000115    120070111G7120                MOUNT                                   BEECH 36    A36         1151604CE  CONT  O550  IO550B           SO  MCAULY3A32C D3A32C*     GL  ENGINE          CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW131562F                       E2857       687034      940159          PERFORMED ANNUAL INSPECTION ON ENGINE, FOUND BLACK (FRETTING) CORROSION BELOW CENTER 2 (LT AFT) ENGINE MOUNT BOLTS.  BOLTS WERE LOOSE IN MOUNT, BUT THE NUTS WERE TIGHT ON BOLTS.  PROBLEM IS THAT THE BOLTS ARE A LITTLE TOO LONG AND THE NUTS WERE RUNNING OUT OF THREADS ON THE BOLTS.  SOLUTION WAS TO ADD ANOTHER WASHER BELOW THE NUTS, THEN RETORQUE BACK TO SPECS.  (K)                                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  O  3A15    E3SO    5  CP21EA    
20070511001442007051100144    2007       5          11         2007FA0000119    120070208G243523085001        STARTER GEN                                                                                                                                             OUT OF TOLERANCEB      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA65603W 36   36                                                        S/G SUSPECTED TO HAVE IMPROPER DRIVE SHAFT INSTALLED. DRIVE SHAFT MEASURES LONGER THAN ANOTHER S/G WITH SAME PN. ENGINE HAVE THEIR STARTER MOUNT BEARING FAIL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            
20070213000672007021300067CE  2007       2          13         2007FA0000120    120070129G3340CM358910        SWITCH                                  CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              TAXI LIGHT      ODOR            B  ODARA   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      APAPPROACH       1                      EA21321ME                       172S8566                                PILOT REPORTED TO APPROACH THAT THERE WAS AN ELECTRICAL SMELL IN CABIN.  AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT.  UPON INSPECTION, FOUND THE TAXI LIGHT CIRCUIT BREAKER/SWITCH WAS SLIGHTLY DISCOLORED, SMELLED BURNED AND IT WAS INOPERATIVE.  THERE WAS NO APPARENT OTHER DAMAGE TO CIRCUIT OR ANY OTHER PART.  (K)                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A12    1E10                 
20070220000162007022000016    2007       2          20         2007FA0000121    420070130G3418C528072         TRANSDUCER                              PIPER PA46  PA46500TP   7104622SO                                                               STALL WARNING   FAILED          G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE075337N320                    4697102                                 THIS UNIT WAS INSTALLED 12 MONTHS AGO.  THIS IS A TYPICAL LIFE SPAN.  CAUSE OF MALFUNCTION IS UNIT BEING OVERHEATED IN FLIGHT.  THEY CAN`T TURN DOWN THE HEAT BECAUSE OF THE WAY IT WAS CERTIFIED.  MOST PILOTS DO NOT KNOW THIS UNIT IS INOPERATIVE.  THE STALL WARNING HORN WILL SOUND EVEN THOUGH THE UNIT IS BAD.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O    RTA25SO                        
20070213000572007021300057EA  2007       2          13         2007FA0000122    220070105G8530                NUT                                     CESSNA172   172N        2072434CE  LYC   O320  O320*       41508EA                              ARM RETAINER    LOOSE           B  ONFRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA055123E1788                   17271722    RL8312761                   THE NR 3 CYLINDER EXHAUST ROCKER ARM RETAINING NUT BECAME LOOSE, REDUCING LIFT ON THE EXHAUST VALVE, NOT ALLOWING SUFFICIENT AIR TO EXIT THE CYLINDER.  PRESSURE IN THE CYLINDER EXCEDED THE STRENGTH OF THE INTAKE VALVE SYSTEM TO OPEN, CAUSING THE INTAKE PUSHROD TO FALL (BEND).  RECOMMEND A SIMPLE LOCKPLATE BE ADDED UNDER THE ROCKER ARM RETAINING NUT WITH A LOCK TAB TO ELIMINATE THIS POSSIBLE FAILURE.  (K)                                                                                                                                                                                                                                                                                                                         1H71 3O3  ONT3A12    E274                 
20070309001262007030900126CE  2007       3          9          2007FA0000141    120070205G28200500106326      FUEL LINE                               CESSNA180   180         2072602CE                                                               FUEL SYS        WORN            D      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      AL05     4000                                                           FLAP CABLE WEARING INTO FUEL LINE.  FUEL LINE WAS INCORRECTLY ASSEMBLED.  VISUAL INSPECTION OF AREA AT ANNUAL OR 100 HR INSPECTIONS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O    NC5A6                          
20070226001852007022600185SO  2007       2          26         2007FA0000144    120070205G32306741102         SWITCH                                  PIPER PA34  PA34200     7103405SO  LYC   O360  IO360C1E6   41514EA                              MLG             FROZEN          C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA171533E                       347350050                               UPON LANDING, GEAR EXTENSION, DURING APPROACH TO LANDING,  PILOT NOTED AN EXCEPTIONALLY LONG TIME BETWEEN GEAR SWITCH ACTUATION AND INDICATION OF ALL DOWN AND LOCKED.  OUTSIDE TEMP +9 F.  BELIEVE THAT SWITCH ARM FOR DOWNLOCK HAD FROZEN IN PLACE (UP) AND REQUIRED TIME TO ACTUATE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  A7SO    1E10                 
20070226000762007022600076CE  2007       2          26         2007FA0000145    120070215G781002R3022406      EXHAUST DUCT                            BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA                              LT ENGINE       CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO09     6162 731                           PCE85441                    WHILE PERFORMING SCHEDULED MAINTENANCE, REMOVED LT ENGINE EXHAUST STACKS TO FACILITATE INSPECTING THE EXHAUST DUCT.  FOUND A 14 INCH CRACK FOLLOWING THE CIRCUMFERENCE OF THE SKI SLOPE WITH A 3 INCHES CRACK PROPAGATING LONGITUDELY AT THE 10 O'CLOCK POSITION FROM THE 14 INCHES CRACK. EXHAUST DUCT HAD PWA SB 3380 COMPLIED WITH 731 HOURS EARLIER. BECAUSE OF THE REMAINING ENGINE TIME, IT WILL BE PULLED FOR OVERHAUL.                                                                                                                                                                                                                                                                                                                  1L72 4T4  T  A24CE   E4EA                 
20070223002882007022300288CE  2007       2          23         2007FA0000147    120070201G2571                HOSE                                    BEECH 95    B95         1153404CE                                                               BATTERY BOX     DISCONNECTED    C      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      NM019631R                       TD314                                   BATTERY ELECTROLYTE RESIDUE FOUND ON LEFT NOSE GEAR DOOR AND LOWER FORWARD FUSELAGE.  INSPECTION REVEALED BATTERY BOX DRAIN HOSE DISCONNECTED AND HANGING IN LOWER NOSE STRUCTURE AREA BELOW THE BAGGAGE FLOOR.  ACCESS IS HINDERED BY NUMEROUS FASTENERS THAT ARE HARD TO REMOVE.  AT SOME TIME IN THE PAST THE ADF ANTENNA MAST, WHICH DOUBLED AS THE BATTERY DRAIN MAST, HAD BEEN REMOVED AND THE BATTERY DRAIN HOSE WAS NOT RECONNECTED TO A SUITABLE DRAIN.  THIS COULD CAUSE CORROSION DAMAGE TO NOSE AREA LOWER STRUCTURE ON TRAVEL AIR AND BARON AIRPLANES, WHICH HAVE SIMILAR DESIGN.  BEECH MODEL 95 PARTS AND SHOP MANUALS CARRY NO REFERENCES ABOUT THE BATTERY DRAIN SYSTEM.  SUGGEST REVIEW OF ANY RAYTHEON SERVICE BULLETINS DISC1L72 3O      3A16                         
20070301002362007030100236SO  2007       3          1          2007FA0000148    120070214G3234761213          LEVER                                   PIPER PA23  PA23250     7102308SO  LYC   O540  TIO540*     41532EA                              COCKPIT         BROKEN          D  F7HSO   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      WP1331PD 7657                   277654016                               LANDING GEAR LEVER BROKE AT THE RIVET DURING TAKEOFF, AFTER RAISING LANDING GEAR LEVER UP TO RETRACT LANDING GEAR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3O3  O  1A10    E14EA                
20070301002012007030100201    2007       3          1          2007FA0000149    220070209G74146310            MAGNETO                                                                                                                                 ENGINE          MALFUNCTIONED   B  WS9RK   NONE                                                                                            R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      NM07                                                                    MAGNETO IS MISSING AT HIGH ALTITUDE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 
20070301002022007030100202    2007       3          1          2007FA0000150    220070209G74146310            MAGNETO                                                                                                                                 ENGINE          MALFUNCTIONED   B  WS9RK   NONE                                                                                            R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      NM07     2                                                              MAGNETO`S MISSING AT HIGH ALTITUDE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  
20070309001522007030900152SW  2007       3          9          2007FA0000151    120070214G5712                FASTENER                                BBAVIA7     7ECA        21101NNSW  LYC   O235  O235*       41505EA                              WING            OUT OF POSITION D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NE055505N                       126678                                  RIB NAILS PULLING OUT IN ALMOST EVERY RIB.  RT TIP RIB HAS ALL NAILS PULLED OUT AND A  SPACE BETWEEN RIBS AND SPARS, BOTH FRONT AND REAR LOCATIONS.  LT WING HAS ONE NAIL THAT IS ABOUT TO FALL OUT AS IT IS PULLED/WORKED OUT .4375 INCH.  80 PERCENT OF RIBS HAVE AT LEAST ONE NAIL OUT OVER .1250 INCH, AND ONLY APPROX 10 PERCENT OF TOTAL NAILS ARE NOT MOVING.  HAVE NOT DISASSEMBLE YET FOR SPAR DAMAGE, BUT HAVE SEEN A FEW NAILS THAT ARE (SMOKING) WHERE THEY CONTACT THE ALUMINUM RIB.  ALL FOUND DURING ROUTINE INSPECTION AT ANNUAL IAW AD AND APPLICABLE SB`S IAW THE AD.  (K)                                                                                                                                                    1H71 3O3  O  A759    E223                 
20070309001142007030900114SO  2007       3          9          2007FA0000155    220070212G8530                CYLINDER                                CESSNA206   U206B       2073322CE  CONT  O520  IO520F      17032SO                              ENGINE          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL034988F                       U2060688                                CRACKED CYLINDER HEAD BETWEEN 4TH AND 5TH FIN IB OF TOP SPARK PLUG.  CRACKS HEADED TOWARD VALVE SEAT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  O  A4CE    E5CE                 
20070329002962007032900296SO  2007       3          29         2007FA0000156    220070212G8530                CYLINDER                                CESSNA206   U206F       2073333CE  CONT  O520  IO520F      17032SO                              ENGINE          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL037711D                       U20603170                               CRACKED CYLINDER LEAD BETWEEN 4TH AND 5TH FIN IB AT UPPER SPARK PLUG.  CRACK NOT VISIBLE INSIDE CYLINDER.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  O  A4CE    E5CE                 
20070309000462007030900046SO  2007       3          9          2007FA0000157    220070212G8530AEC63139        CYLINDER                                CESSNA206   U206F       2073333CE  CONT  O520  IO520F      17032SO                              ENGINE          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL037711D10226                  U20603170                               CRACKED CYLINDER BETWEEN 2ND AND 3RD FIN IB OF UPPER SPARK PLUG ORIENTED DOWN SIDE OF CYL HEAD.  LARGE NEAR SEPARATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  O  A4CE    E5CE                 
20070309001272007030900127SO  2007       3          9          2007FA0000158    220070212G8530AEC631397       CYLINDER                                CESSNA206   U206F       2073333CE  CONT  O520  IO520F      17032SO                              ENGINE          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL037711D                       U20603170                               CYLINDER HEAD CRACKED AT UPPER SPARK PLUG HOLE THRU BEND TO EXHAUST SEAT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  O  A4CE    E5CE                 
20070309003032007030900303CE  2007       3          9          2007FA0000162    120070206G5511233201015       SPAR CAP        LEAR                    LEAR  35    35A         5170602CE  GARRTTTFE731TFE731*     01518WP                              HORIZ STAB      CORRODED        C  BHKRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA2196FN 17284      1187        186                                     VISUAL CONDITION CHECK PERFORMED ON HORIZONTAL STABILIZER AFT SPAR CAP AND ELEVATOR HINGE BRACKETS FOR CORROSION, BROKEN FASTENERS, ETC.  FOUND SEVERE CORROSION ON UPPER SPAR CAP ASSEMBLY ALONG ENTIRE LENGTH.  THIS REQUIRED REMOVAL AND REPLACEMENT OF UPPER SPAR CAP.  CORROSION CAUSED BY OPERATING CONDITIONS, LACK OF CONSISTENT WASHING PROGRAM AND POSSIBLE EXPOSED, UNPROTECTED METAL.  RECOMMENDA CONSISTENT AIRCRAFT WASHING PROGRAM WHEN OPERATIONS ARE IN OR NEAR COSTAL REGIONS AND ENSURING ALL EXPOSED SURFACES ARE PROPERLY TREATED AND PAINTED.  (K)                                                                                                                                                                        2L72 4F4  F  A10CE   E6WE                 
20070309001612007030900161SO  2007       3          9          2007FA0000163    120070201G8120                FITTING                                 PIPER PA32  PA32301T    7103209SO  LYC   O540  TIO540S1AD  41532EA  HARTZLHCE3Y HCE3YR1     GL  TURBOCHARGER    CRACKED         D      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      SW058185Y     522               328024018   L699564A    FM1408B         THIS PART IS BOLTED TO THE TURBOCHARGER ASSY BETWEEN THE HOT AND COLD SECTIONS.  THE HIGH PRESSURE OIL LINE CONNECTS TO THIS PART VIA A FITTING IN THE TOP OF THE PART.  AFTER AN ANNUAL INSP, THE ENG WAS RUN-UP AND SYSTEM CHECKED.  AN OIL SEEP WAS NOTED IN THE TURBOCHARGER AREA.  THE HIGH PRESSURE OIL LINE AND FITTING WAS REMOVED.  PN LW 14465 WAS REMOVED AND CLEANED.  THE CRACK WAS NOTED. THE PART WAS REPLACED WITH NEW.  AFTER RESEARCHING THE AC RECORDS, IT WAS NOTED THAT EXHAUST SYS, INCLUDING TURBOCHARGER WASTE GATE AND CONTROL ROD END WAS NOT OVERHAULED WITH THE ENGINE CORE AS REQUIRED BY MFG.  TURBOCHARGER WAS REPLACED WITH NEW UNIT AT TIME OF O/H.  UNKNOWN IF PN LW-14465 WAS REPLACED AT THAT TIME.  PART IS1L71 3O3  O  A3SO    E14EA   5  CP33EA    
20070329002652007032900265EA  2007       3          29         2007FA0000164    220070206G8500                ENGINE                                  CESSNA206   T206H       2073303CE  LYC   O540  TIO540A1A   41532EA                                              MAKING METAL    D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL213543B                       T20608330   L1123761A                   UNDER NORMAL CONDITIONS AND UNDER OIL SAMPLE PROGRAM, ENGINE HAS HAD (6) HIGH BAD SAMPLES, HIGH IRON, COPPER AND ALUMINUM.  AC IS A PUBLIC USE AIRCRAFT WITH CUSTOMS AND BORDER PROTECTION, BUT AM REPLACING ENGINE WITH NEW/ OVERHAUL.  CONTACTED MFG ABOUT PROBLEM BUT WAS TOLD TO KEEP CHANGING OIL AND FILTERS.  RECOMMEND THA THIS TYPE ENGINE BE INVESTIGATED CLOSER.  THIS ENGINE WAS CHANGED IN 2005 DUE TO SIMILAR PROBLEM.  (K)                                                                                                                                                                                                                                                                                                       1H71 3O3  ORTA4CE    E14EA                
20070312002622007031200262CE  2007       3          12         2007FA0000165    120070206G5511233201015       SPAR CAP                                LEAR  35    36LEAR      5170601CE  GARRTTTFE731TFE731*     01518WP                              HORIZ STAB      CORRODED        C  BHKRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA2112FN 15719                  016                                     VISUAL CONDITION CHECK PERFORMED ON HORIZONTAL STABILIZER AFT SPAR CAP AND ELEVATOR HINGE BRACKETS FOR CORROSION, BROKEN FASTENERS, ETC.  FOUND MODERATE CORROSION ON UPPER SPAR CAP ASSY AT LT OB ELEVATOR HINGE AREA.  THIS REQUIRED REMOVAL AND REPLACEMENT OF UPPER SPAR CAP.  CORROSION CAUSED BY OPERATING CONDITIONS, LACK OF CONSISTENT WASHING PROGRAM AND POSSIBLE EXPOSED, UNPORTECTED METAL.  RECOMMEND A CONSISTENT AC WASHING PROGRAM WHEN OPERATIONS ARE IN OR NEAR COASTAL REGIONS AND ENSURING ALL EXPOSED SURFACES ARE PROPERLY TREATED AND PAINTED.  (K)                                                                                                                                                                     2L72 4F4  F  A10CE   E6WE                 
20070226000302007022600030EU  2007       2          26         2007FA0000166    120070223G62301090110677      FITTING                                 AGUSTAA109  A109A2      0260120EU  ALLSN 250C  250C20      03013GL                              MAIN ROTOR      WORN            D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA35745HA     32                7413                                    MAIN ROTOR DRIVELINK UPPER FITTING STEEL BUSHES (109-0110-70-1) AND UPPER SLEEVE (109-0110-69-1) SEVERELY WORN.  SLEEVE STEPPED TO LESS THAN HALF MANUFACTURED DIAMETER AT BOTH ENDS.  STEEL BUSHES WORN THROUGH COMPLETELY, WEAR EXTENDING INTO FITTING.  HOLE IN BOTH ENDS OF FITTING FOR STEEL BUSHES ELONGATED.  PHOTOGRAPHS AND DISCREPANT PARTS AVAILABLE IF REQUIRED.  DEFECTIVE PARTS REPLACED.                                                                                                                                                                                                                                                                                                                                         1G72 3U3  U  H7EU    E4CE                 
20070309001222007030900122SO  2007       3          9          2007FA0000168    120070206G5711                SPAR                                    PIPER J3    J3C65       7100510SO                                                               WING            CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE056609H2884                   19808                                   DURING REMOVAL OF LT WING FOR INSTALLATION OF WING FUEL TANK, A QUESTIONABLE PREVIOUS REPAIR WAS FOUND AT THE FRONT WOOD SPAR ROOT.  FURTHER INVESTIGATION FOUND LONGNATUDINAL CRACKS OF THE LT AND RT, FOR AND AFT WOOD WING SPARS.  THESE CRACKS WERE VISIBLE WITH A BARE EYE WHEN THE FRONT SPAR CARRY ATTACH INSPECTION PANEL WAS REMOVED AND INSPECTED FROM THE FRONT CABIN AREA.  CRACKS ARE NOT UNCOMMON AFTER 60 YEARS OF HARD SERVICE AND NATURAL DEGRADATION OF THE WOOD.  (K)                                                                                                                                                                                                                                                        1H71 3O      A691                         
20070226001702007022600170SO  2007       2          26         2007FA0000169    120070223G575186562025        AILERON                                 PIPER PA44  PA44180     7104402SO  LYC   O360  O360*       41514EA                              RIGHT           MISREPAIRED     B      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      WP07576ER3598                   4496152                                 DURING POWER OFF (CLEAN CONFIGURATION) STALLS, THE AIRCRAFT WOULD SUDDENLY BREAK LT AND IF NOT IMMEDIATELY STOPPED COULD LEAD TO A SPIN.  AFTER RERIGGING ALL FLIGHT CONTROLS, CHECKING THE AIRCRAFT ALIGNMENT WITH A LASER AND SEVERAL TEST FLIGHTS BOTH BY COMPANY PILOTS AND MFG FACTORY TEST PILOT, IT WAS DETERMINED THAT WE HAD (FAT) AILERONS ON OUR FLEET.  MFG HAS A HISTORY OF AILERON SKIN CRACKING.  (FOR US, IT HAS JUST BEEN THE RT AILERON THAT HAS HAD THE CRACKING PROBLEM.)  ONCE THE CRACK IS PAST A CERTAIN POINT YOU EITHER HAVE TO REPLACE THE AFFECTED SKIN OR REPLACE THE AILERON.  DURING SKIN REPLACEMENT, IF THE PREFORMED FACTORY SKIN IS SPREAD APART EVEN A LITTLE THE T/E TAKES ON A (FAT) CONDITION.  THIS LEADS1L72 3O3  O  A19S0   E286                 
20070227000482007022700048CE  2007       2          27         2007FA0000171    120070220G3230504501033       TORQUE TUBE     CESSNA                  CESSNA340   340A        2076405CE  CONT  O550  IO550*           SO                              MLG             BINDING         D      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      GL15467DB                       340A0467                                DURING REPLACEMENT OF ORIGINAL EQUIPMENT TORQUE TUBE (P/N 5045010-18/19) WITH MFG REPLACEMENT P/N 5045010-32/33 INTERFERENCE BETWEEN THE TORQUE TUBE AND AIRFRAME ATTACHMENT FITTING WAS DISCOVERED.  RIGGING THE MLG TO ACHIEVE A .1250 DROP OFF WAS IMPOSSIBLE DUE TO THE INTERFERENCE BETWEEN THE TORQUE TUBE AND THE ATTACHMENT FITTING. DROP OFF IS ACHIEVED ONCE THE TORQUE TUBE ROTATES FAR ENOUGH OVER CENTER TO ALLOW THE GEAR TO DROP .1250 BACK DOWN FROM ITS MAXIMUM HEIGHT.  MFG TECHNICAL SUPPORT INDICATED THAT THE ORIGINAL TORQUE TUBE (-18/19) HAD A FLAT SPOT BETWEEN THE AFT HINGE ARMS DESIGNED TO CLEAR THE AIRCRAFT STRUCTURE. THIS FLAT SPOT WAS ORIENTED AT A 33 DEGREE OFFSET. THE TORQUE TUBES WERE REDESIGNED IN 1971L72 3O3  O  3A25    E3SO                 
20070227000512007022700051    2007       2          27         2007FA0000173    220070222G74146310            MAGNETO                                                                                                                                 ENGINE          MALFUNCTIONED   C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07     2                                                              MAGNETO CAUSING HIGH ALTITUDE MIS-FIRE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   
20070227000872007022700087CE  2007       2          27         2007FA0000174    120070201G2432                HOSE                                    BEECH 95    B95         1153404CE  LYC   O360  O360*       41514EA                              BATTERY DRAIN   DISCONNECTED    C      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      NM019631R                       TD314                                   BATTERY ELECTROLYTE RESIDUE FOUND ON LT NOSE GEAR DOOR AND LOWER FORWARD FUSELAGE.  INSPECTION REVEALED BATTERY BOX DRAIN HOSE DISCONNECTED AND HANGING IN LOWER NOSE STRUCTURE AREA BELOW THE BAGGAGE FLOOR.  ACCESS IS HINDERED BY NUMEROUS FASTENERS THAT ARE HARD TO REMOVE.  AT SOME TIME IN THE PAST THE ADF ANTENNA MAST, WHICH DOUBLED AS THE BATTERY DRAIN MAST, HAD BEEN REMOVED AND THE BATTERY DRAIN HOSE WAS NOT RECONNECTED TO A SUITABLE DRAIN.  THIS COULD CAUSE CORROSION DAMAGE TO NOSE AREA LOWER STRUCTURE ON TRAVEL AIR AND BARON AIRPLANES, WHICH HAVE SIMILAR DESIGN.  PARTS AND SHOP MANUALS CARRY NO REFERENCES ABOUT THE BATTERY DRAIN SYSTEM.  SUGGEST REVIEW OF ANY MFG SB DISCUSSING BATTERY BOX DRAIN COMPONENTS, 1L72 3O3  O  3A16    E286                 
20070302000332007030200033CE  2007       3          2          2007FA0000175    120070216G1100070507109       PLACARD                                 CESSNA206   206CESSNA   2073302CE  LYC   O540  TIO540AJ1A       EA  MCAULY3D36C B3D36C432   GL  WING            FADED           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA27     150                    T20608291   L1083261A   002324          P/N 0705071-9) FUEL QUANTITY AND TYPE PLACARDS HAVE BEEN REPLACED ABOUT ONCE A YEAR DUE TO FADING.  THIS AIRCRAFT IS HANGARED.  THIS FADING HAS BEEN NOTED WITH OTHER MFG AIRCRAFT.  RETAIL COST LAST YEAR NR 50.00+.  THIS HAS NOW DOUBLED.  OWNERS DON'T PLACARD IMPORTANCE FOR AIRWORTHINESS.                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  O  A4CE    E14EA   5  CP58GL    
20070312000322007031200032CE  2007       3          12         2007FA0000176    120070222G275255651904        ROLL PIN                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              SPROCKET        BROKEN          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW13797CW8177 1200              5500232                                 DURING A PHASE 5 INSPECTION THE FLAPS SEAMED TO BE SLOW AND BINDING. AT CLOSER INSPECTION IT WAS FOUND THAT THE ROLL PIN HAD BROKEN ALLOWING THE SPROCKET TO MOVE FWD. ON THE P/N 5565190-9 BRAZE ASSY-DRIVE THIS CAUSED BINDING AND ALLOWED THE SPROCKET TO EVEN DROP DOWN ON TO THE P/N 6565193-9 CHAIN GUARD-LOWER FWD. THIS IS A HARD AREA TO LOOK AT EVEN WITH A MIRROR. A FEW MORE ACTIONS WITH THE FLAP WOULD HAVE LED TO TOTAL FAILURE OF THIS SYSTEM.                                                                                                                                                                                                                                                                                  1L72 4F4  F  A22CE   E1NE                 
20070302000342007030200034SO  2007       3          2          2007FA0000177    120070223G575186562025        AILERON                                 PIPER PA44  PA44180     7104402SO  LYC   O360  O360*       41514EA                              WING            MISREPAIRED     D      O   OTHER                                                                                           WF INADEQUATE Q C            FLT CONT AFFECTED                                   CRCRUISE         1                      WP07570ER3583                   4496146                                 DURING POWER OFF (CLEAN CONFIGURATION) STALLS, THE AIRCRAFT WOULD SUDDENLY BREAK LT AND IF NOT IMMEDIATELY STOPPED COULD LEAD TO A SPIN.  AFTER RERIGGING ALL FLIGHT CONTROLS, CHECKING THE AIRCRAFT ALIGNMENT WITH A LASER AND SEVERAL TEST FLIGHTS BOTH BY COMPANY PILOTS AND MFG FACTORY TEST PILOT, IT WAS DETERMINED THAT WE HAD (FAT) AILERONS ON OUR FLEET.  MFG HAS A HISTORY OF AILERON SKIN CRACKING.  (FOR US, IT HAS JUST BEEN THE RT AILERON THAT HAS HAD THE CRACKING PROBLEM).  ONCE THE CRACK IS PAST A CERTAIN POINT YOU EITHER HAVE TO REPLACE THE AFFECTED SKIN OR REPLACE THE AILERON.  DURING SKIN REPLACEMENT, IF THE PREFORMED FACTORY SKIN IS SPREAD APART EVEN A LITTLE THE TRAILING EDGE TAKES ON A (FAT) CONDITION.  1L72 3O3  O  A19S0   E286                 
20070308000562007030800056SO  2007       3          8          2007FA0000178    120070223G575186562025        AILERON                                 PIPER PA44  PA44180     7104402SO  LYC   O360  O360*       41514EA                              WING            MISREPAIRED     B      O   OTHER                                                                                           WF INADEQUATE Q C            FLT CONT AFFECTED                                   CRCRUISE         1                      WP07571ER3801                   4496147                                 DURING POWER OFF (CLEAN CONFIGURATION) STALLS, THE AIRCRAFT WOULD SUDDENLY BREAK LT AND IF NOT IMMEDIATELY STOPPED COULD LEAD TO A SPIN.  AFTER RERIGGING ALL FLIGHT CONTROLS, CHECKING THE AIRCRAFT ALIGNMENT WITH A LASER AND SEVERAL TEST FLIGHTS BOTH BY COMPANY PILOTS AND PIPER FACTORY TEST PILOT, IT WAS DETERMINED THAT WE HAD (FAT) AILERONS ON OUR FLEET.  PIPER HAS A HISTORY OF AILERON SKIN CRACKING.  (IT HAS BEEN THE RT AILERON THAT HAS HAD THE CRACKING PROBLEM).  ONCE THE CRACK IS PAST A CERTAIN POINT YOU EITHER HAVE TO REPLACE THE AFFECTED SKIN OR REPLACE THE AILERON.  DURING SKIN REPLACEMENT, IF THE PREFORMED FACTORY SKIN IS SPREAD APART EVEN A LITTLE THE TRAILING EDGE TAKES ON A (FAT) CONDITION.  THIS LEAD1L72 3O3  O  A19S0   E286                 
20070308000572007030800057SO  2007       3          8          2007FA0000179    120070223G575186562025        AILERON                                 PIPER PA44  PA44180     7104402SO  LYC   O360  O360*       41514EA                              WING            MISREPAIRED     A      O   OTHER                                                                                           WF INADEQUATE Q C            FLT CONT AFFECTED                                   CRCRUISE         1                      WP07572ER3160                   4496148                                 DURING POWER OFF (CLEAN CONFIGURATION) STALLS, THE AIRCRAFT WOULD SUDDENLY BREAK LT AND IF NOT IMMEDIATELY STOPPED COULD LEAD TO A SPIN.  AFTER RERIGGING ALL FLIGHT CONTROLS, CHECKING THE AIRCRAFT ALIGNMENT WITH A LASER AND SEVERAL TEST FLIGHTS BOTH BY COMPANY PILOTS AND MFG FACTORY TEST PILOT, IT WAS DETERMINED THAT WE HAD (FAT) AILERONS ON OUR FLEET.  MFG HAS A HISTORY OF AILERON SKIN CRACKING.  (FOR US, IT HAS JUST BEEN THE RT AILERON THAT HAS HAD THE CRACKING PROBLEM.)  ONCE THE CRACK IS PAST A CERTAIN POINT YOU EITHER HAVE TO REPLACE THE AFFECTED SKIN OR REPLACE THE AILERON.  DURING SKIN REPLACEMENT, IF THE PREFORMED FACTORY SKIN IS SPREAD APART EVEN A LITTLE THE TRAILING EDGE TAKES ON A (FAT) CONDITION.  1L72 3O3  O  A19S0   E286                 
20070308000582007030800058SO  2007       3          8          2007FA0000180    120070223G575186562025        AILERON                                 PIPER PA44  PA44180     7104402SO  LYC   O360  O360*       41514EA                              WING            MISREPAIRED     B      O   OTHER                                                                                           WF INADEQUATE Q C            FLT CONT AFFECTED                                   CRCRUISE         1                      WP07573ER3969                   4496149                                 DURING POWER OFF (CLEAN CONFIGURATION) STALLS, THE AIRCRAFT WOULD SUDDENLY BREAK LT AND IF NOT IMMEDIATELY STOPPED COULD LEAD TO A SPIN.  AFTER RERIGGING ALL FLIGHT CONTROLS, CHECKING THE AIRCRAFT ALIGNMENT WITH A LASER AND SEVERAL TEST FLIGHTS BOTH BY COMPANY PILOTS AND PIPER FACTORY TEST PILOT, IT WAS DETERMINED THAT WE HAD (FAT) AILERONS ON OUR FLEET.  MFG HAS A HISTORY OF AILERON SKIN CRACKING.  (FOR US, IT HAS JUST BEEN THE RT AILERON THAT HAS HAD THE CRACKING PROBLEM).  ONCE THE CRACK IS PAST A CERTAIN POINT YOU EITHER HAVE TO REPLACE THE AFFECTED SKIN OR REPLACE THE AILERON.  DURING SKIN REPLACEMENT, IF THE PREFORMED FACTORY SKIN IS SPREAD APART EVEN A LITTLE THE TRAILING EDGE TAKES ON A (FAT) CONDITION.1L72 3O3  O  A19S0   E286                 
20070308000592007030800059SO  2007       3          8          2007FA0000182    120070223G575186562025        AILERON                                 PIPER PA44  PA44180     7104402SO  LYC   O320  O320*       41508EA                              WING            MISREPAIRED     B      O   OTHER                                                                                           WF INADEQUATE Q C            FLT CONT AFFECTED                                   CRCRUISE         1                      WP07577ER3881                   4496153                                 DURING POWER OFF (CLEAN CONFIGURATION) STALLS, THE AIRCRAFT WOULD SUDDENLY BREAK LT AND IF NOT IMMEDIATELY STOPPED COULD LEAD TO A SPIN.  AFTER RERIGGING ALL FLIGHT CONTROLS, CHECKING THE AIRCRAFT ALIGNMENT WITH A LASER AND SEVERAL TEST FLIGHTS BOTH BY COMPANY PILOTS AND MFG FACTORY TEST PILOT, IT WAS DETERMINED THAT WE HAD (FAT) AILERONS ON OUR FLEET.  MFG HAS A HISTORY OF AILERON SKIN CRACKING.  (FOR US, IT HAS JUST BEEN THE RT AILERON THAT HAS HAD THE CRACKING PROBLEM.)  ONCE THE CRACK IS PAST A CERTAIN POINT YOU EITHER HAVE TO REPLACE THE AFFECTED SKIN OR REPLACE THE AILERON.  DURING SKIN REPLACEMENT, IF THE PREFORMED FACTORY SKIN IS SPREAD APART EVEN A LITTLE THE TRAILING EDGE TAKES ON A (FAT) CONDITION.  1L72 3O3  O  A19S0   E274                 
20070227000602007022700060EA  2007       2          27         2007FA0000183    220070211G854013S19646        GEAR                                    CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  CRANKSHAFT      LOOSE           D      A   UNSCHED LANDING                                                                                 Y  ENGINE STOPPAGE                                                               CLCLIMB          1                      GL15242SP1855                   172S8226    L2830651A   SK039           DURING TAKEOFF AT 400 FT AGL ENGINE QUIT FORCING AN OFF AIRPORT EMERGENCY LANDING.  INITIAL INSPECTION FOUND NO MOVEMENT OF ACCESSORIES AND VALVE MOVEMENT.  REMOVED ACCESSORIES CASE AND FOUND DRIVE GEAR ON CRANKSHAFT MOUNT BOLT LOOSE AND PIN SHEARED.  MARKS SHOW THAT BOLT AND GEAR WERE LOOSE FOR SOME TIME ALLOWING WEAR ON PIN UNTIL FAILURE. SUSPECT INCORRECT TORQUE OR INCORRECT SEATING OF GEAR TO FLANGE.  ALSO WITH GEAR LOOSE BOLT COULD BE TURNED IN LOCKING TAB. HOLE IN LOCKING TAB TOO LOOSE ON BOLT.  ENGINE NEW FROM MFG. WITH 1855.3 HOURS.                                                                                                                                                                              1H71 3O3  ONT3A12    1E10    5  NP857     
20070329002952007032900295EA  2007       3          29         2007FA0000185    220070222G7414ESIO357424      BUSHING         BENDIX                  MOONEYM20   M20D        5870210SW  LYC   O360  O360A1D     41514EA                              MAGNETO         LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP176914U31         1060379     246                                     BRONZE BUSHING VERY LOOSE IN DISTRIBUTOR BLOCK AND MAG WOULD NOT OPERATE CORRECTLY.  AN EMERGENCY LANDING WAS MADE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L71 3O3  O  2A3     E286                 
20070309001722007030900172SO  2007       3          9          2007FA0000186    220070222G7414                BUSHING         BENDIX                  CESSNA172   172D        2072410CE  CONT  O300  O300D       17022SO                              MAGNETO         LOOSE           D      K   NONE                                                                                            O  OTHER                                                                         NRNOT REPORTED   1                      WP172948U194                    17250548                                BRONZE BUSHING, VERY LOOSE IN DISTRIBUTOR BLOCK AND DISTRIBUTOR ARM WAS CONTACTING PINS IN BLOCK.  MAG WOULD NOT OPERATE CORRECTLY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A12    E253                 
20070309001402007030900140EU  2007       3          9          2007FA0000187    120070222G2910285683          COUPLING                                AMD   FALC10FALCON10    2730101EU  GARRTTTFE731TFE7312     01518WP                              HYDRAULIC SYS   DEFECTIVE       D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL0343EC 9017                   168                                     THIS COUPLING IS A QUICK-DISCONNECT TYPE FITTING THAT IS IN LINE OF THE ENGINE DRIVEN HYDRAULIC PUMP AND LOCATED IN THE ENGINE PYLON.  THERE IS ONLY ONE ON EACH ENGINE AND ONLY ON THE SUCTION LINE.  THESE FITTINGS HAVE NO TIME CHANGE REQUIREMENT.  WHEN THIS PART WAS CHANGED (DUE TO EXTERNAL LEAKAGE) IT WAS EXTREMELY DIFFICULT TO SEPARATE.  ONCE SEPARATED, THE LOCKING BALLS HAD DUG SO DEEPLY INTO THE LOCK RING THAT PARTIAL UNSEATING OF THE O-RING HAD OCCURRED.  THERE QUICK DISCONNECT COUPLINGS (LT AND RT) SHOULD BE REQUIRED TO BE INSPECTED AT EACH ENGINE REMOVAL AND REPLACED IF WEAR IS DETECTED.  (K)                                                                                                                  2L72 4F4  F  A33EU   E6WE                 
20070329002942007032900294CE  2007       3          29         2007FA0000188    120070215G2510551900922       SEAT            CESSNA                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              COCKPIT         CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE05404BS                       5500403                                 UPPER CHAIR BASE ASSY CRACKED AT CHAIR BACK ATTACH POINTS.  STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE.  CHAIR WAS REPAIRED IAW STC 01042WI STRUCTURAL SEAT REPAIR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 4F4  F  A22CE   E1NE                 
20070326001012007032600101CE  2007       3          26         2007FA0000189    120070226G2750051010593       CONTROL CABLE                           CESSNA172   172N        2072434CE  LYC   O320  O320*       41508EA                              TE FLAPS        FRAYED          B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL0531SZ 1372913729             17267732                                PILOT REPORTED EXCESSIVE MOVEMENT IN LT FLAP DURING PRE-FLIGHT WALK AROUND OF AIRCRAFT.  INITIAL INVESTIGATION BY MAINTENANCE PERSONNEL CONFIRMED FINDINGS.  MAINTENANCE PERSONNEL DISCOVERED THAT CABLE P/N 0510105-93 HAD MULTIPLE BROKEN STRANDS/FRAYING NEAR THE TURNBUCKLE END.   SUSPECTED CAUSE OF DAMAGE TO CABLE IS DUE TO EXCESSIVE FLEXING BETWEEN TURNBUCKLE END AND FLAP POSITION INDICATOR CLAMP, P/N 0560037-1.  AD 80-06-03 HAD BEEN COMPLIED WITH ON 10/11/1982 BY INSTALLATION OF KIT SK172-60A.                                                                                                                                                                                                                              1H71 3O3  ONT3A12    E274                 
20070301002052007030100205GL  2007       3          1          2007FA0000190    320070221G6114C4201C58        HUB             MCAULY                                                                                      MCAULY2A34C D2A34C58    GL  PROPELLER       CRACKED         B  LT4RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO19                720009                              720009          HUB RECEIVED DISASSEMBLED, CLEANED AND ANODIZED WITH NO CERTIVICATION.  BLADE RETENTION THREADS EDDY CURRENT INSPECTED.  NR 1 BLADE RETENTION THREAD, 4 THREADS IN AT APPROXIMATELY 6 O`CLOCK POSITION FOUND CRACKED.  HUB REMOVED FROM SERVICE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        5  CP3EA     
20070309001192007030900119EU  2007       3          9          2007FA0000191    120070227G5730S25WS3001       SKIN                                    BRAERODH125 HS125700A   4230170EU  GARRTTTFE731TFE731*     01518WP                              RT WING         CORRODED        D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP23224EA9121                   257088                                  RT WING LEADING EDGE(S) HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH.  AFTER COMPLETE DISASSEMBLY IT WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR.  RT WING LEADING EDGE HAD BEEN INSPECTED AT MFG 2.5 YEAR PRIOR TO THIS DISCOVERY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  F  A3EU    E6WE                 
20070326001442007032600144EU  2007       3          26         2007FA0000192    120070227G5754S25WS3002       SKIN                                    BRAERODH125 HS125700A   4230170EU  GARRTTTFE731TFE731*     01518WP                              RT WING LE      CORRODED        D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP23224EA9121                   257088                                  RT WING LEADING EDGE(S) HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH.  AFTER COMPLETE DISASSEMBLY, IT WAS DETERMNED TO BE BEYOND ECONOMICAL REPAIR.  RT WING LEADING EDGE HAD BEEN INSPECTED AT MFG 2.5 YEARS PRIOR TO THIS DISCOVERY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  F  A3EU    E6WE                 
20070402001702007040200170    2007       4          2          2007FA0000193    220070213G74146350            ROTOR                                                                                                                                   MAGNETO         BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW99                                                                    ROTOR AT ROTOR GEAR AND BROKEN.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      
20070309001332007030900133EU  2007       3          9          2007FA0000194    120070221G551225TP1001A       SKIN                                    BRAERODH125 HS125700A   4230170EU  GARRTTTFE731TFE731*     01518WP                              HORIZ STAB      CORRODED        C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP01224EA9121                   257088                                  LT AND RT HORIXONTAL STABILIZER LEADING EDGES HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH.  AFTER COMPLETE DISASSEMBLY, IT WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR.  THIS AREA HAD BEEN INSPECTED AT MFG 2.5 YEARS PRIOR TO THIS DISCOVERY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  F  A3EU    E6WE                 
20070329002992007032900299CE  2007       3          29         2007FA0000195    120070129G3233                LIMIT SWITCH                            CESSNA310   310J        2074226CE  CONT  O470  IO470*      17026SO                              NLG ACTUATOR    FAILED          G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO153091L                       310J0091                                UP LIMIT SWITCH FAILED ON LANDING GEAR ACTUATOR, CAUSING OVER EXTENSION OF NOSE GEAR SYSTEM.  THIS CAUSED THE INTERMEDIATE TORQUE TUBE TO BEND.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  3A10    E1CE                 
20070402001682007040200168WP  2007       4          2          2007FA0000196    220070220G72618961051         COVER                                   BEECH 100   B100        1152919CE  GARRTTTPE331TPE3316     01514WP                              LT ENGINE       BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP09241CW                       BE54        P27188                      PILOT REPORTED HIGH OIL CONSUMPTION, INSPECTED LT ENGINE SCAVENGE PUMP AND FOUND THE PUMP COVER BROKEN AND MISSING PIECES.  ALSO FOUND THE SCAVENGE PUMP OIL TUBE COVER BROKEN AND CHAFING A HOLE THROUGH THE OIL TUBE.  RECOMMEND REMOVING EXHAUST PIPE AT INSPECTIONS TO INSPECT PUMP COVER AND TUBE ASSY FOR DEFECTS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A14CE   E4WE                 
20070309001162007030900116CE  2007       3          9          2007FA0000199    120070301G257107120591P       SUPPORT                                 CESSNA182   182T        2072703CE  LYC   O540  IO540*      41532EA                              BATTERY BOX     CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW153539G                       18281039                                FOUND BATTERY SUPPORT CRACKED.  TOTAL AIRFRAME TIME 1075.  THIS IS THE 3RD ONE THAT WE FOUND.  SUPPORTS NEED TO BE BEEFED UP, THEY ARE TOO LIGHT FOR THE APPLICATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A13    1E4                  
20070309001572007030900157CE  2007       3          9          2007FA0000200    120070301G257107120591P       SUPPORT                                 CESSNA182   182T        2072703CE  LYC   O540  IO540*      41532EA                              BATTERY BOX     CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW1565KC                        18281015                                FOUND BATTERY SUPPORT CRACKED.  TOTAL AIRFRAME TIME 1716.  THIS IS THE THIRD ONE THAT WE FOUND SUPPORTS NEED TO BE BEEFED UP, THEY ARE TOO LIGHT FOR THE APPLICATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A13    1E4                  
20070312002542007031200254EA  2007       3          12         2007FA0000201    220070221G8520V53793493       CRANKSHAFT                              CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              ENGINE          CORRODED        B  YYBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03982BT4744 2196              17280307    L1466351A                   THIS CRANKSHAFT WAS LAST INSPECTED AND PID COATED AT THE FACTORY APRIL 23, 2002, YET 6 YEARS AND 2196 HOURS LATER, IT WAS PITTED, AND REQURIED FURTHER MACHINING.  THE PID COATING DOES NOT SEEM TO HOLD UP, OR BLOCK THE CORROSION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  ONT3A12    1E10                 
20070312002532007031200253EA  2007       3          12         2007FA0000202    220070223G8520V537925914      CRANKSHAFT                              CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              ENGINE          CORRODED        B  YYBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03988BC4170 2211              17280472    L2494851A                   DURING SCHEDULED OVERHAUL, THIS CRANKSHAFT WAS FOUND PITTED IN THE INNER BORE.  THIS ENGINE WAS A FACTORY OVERHAUL JULY 2002, AND DID HAVE THE PID COATING.  THE COATING DOES NOT SEEM TO BLOCK THE CORROSION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A12    1E10                 
20070309001542007030900154EU  2007       3          9          2007FA0000203    120070213G8120LW18607         STRUT                                   PARTENP68   P68TCOBS    6780108EU                                                               TURBO           BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW01737                         40004OTC    RL20464A                    UPON REMOVING ENGINE FROM SHIPPING CRATE, FOUND (NEW) TURBO SUPPORT STRUT CRACKED.  THESE BRACKETS CRACK ALL THE TIME ON THE AIRPLANE.  VERY POOR DESIGN!  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H72 3O    RTA31EU                        
20070309001552007030900155EU  2007       3          9          2007FA0000204    120070213G8120LW18607         STRUT                                   PARTENP68   P68TCOBS    6780108EU                                                               TURBO           BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW01737                         40004OTC    RL20364A                    UPON REMOVING ENGINE FROM SHIPPING CRATE, FOUND (NEW) TURBO SUPPORT STRUT, CRACKED.  THESE BRACKETS CRACK ALL THE TIME IN THE AIRPLANE.  VERY POOR DESIGN!  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H72 3O    RTA31EU                        
20070329002922007032900292CE  2007       3          29         2007FA0000205    120070222G36101H1069          MIXING VALVE                            LEAR  60    60LEAR      5170707CE  PWA   305   PW305            NE                              BLEED AIR SYS   INTERMITTENT    C      A   UNSCHED LANDING                                                                                 JB WARNING INDICATION        SMOKE/FUMES/ODORS/SPARKS                            NRNOT REPORTED   1                      GL11500  83                     306                                     SHORTLY AFTER TAKEOFF, AIRCRAFT (L BLEED AIR) WARNING ILLUMINATED, AND (R BLEED AIR) WARNING ILLUMINATED APPROX 5 SEC LATER, SMELLED ODOR IN CABIN.  REDUCED POWER AND WARNING WENT OUT.  AIRCRAFT DIVERTED FOR MAINTENANCE.  UNABLE TO DUPLICATE MALFUNCTION ON GROUND RUN, LT MIXING VALVE WAS SUSPECTED, SO REPLACED.  PERFORMED GROUND RUN FUNCTIONAL TEST OF BLEED AIR SYSTEM, AND FLIGHT TEST.  NO FURTHER BLEED AIR WARNINGS.  (K)                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA10CE   E35NE                
20070308000832007030800083SO  2007       3          8          2007FA0000206    120070223G575186562025        AILERON                                 PIPER PA44  PA44180     7104402SO  LYC   O360  O360*       41514EA                              WING            MISREPAIRED     B  BF8XO   OTHER                                                                                           WF INADEQUATE Q C            FLT CONT AFFECTED                                   CRCRUISE         1                      WP07575ER3448                   4496151                                 DURING POWER OFF (CLEAN CONFIGURATION) STALLS, THE AC WOULD SUDDENLY BREAK LEFT AND IF NOT IMMEDIATELY STOPPED COULD LEAD TO A SPIN.  AFTER RERIGGING ALL FLIGHT CONTROLS, CHECKING THE AIRCRAFT ALIGNMENT WITH A LASER AND SEVERAL TEST FLIGHTS BOTH BY COMPANY PILOTS AND MFG TEST PILOT, IT WAS DETERMINED THAT WE HAD (FAT) AILERONS ON OUR FLEET.  THIS MAKE OF AIRCRAFT HAS A HISTORY OF AILERON SKIN CRACKING.  (FOR US, IT HAS JUST BEEN THE RT AILERON THAT HAS HAD THE CRACKING PROBLEM).  ONCE THE CRACK IS PAST A CERTAIN POINT , YOU EITHER HAVE TO REPLACE THE AFFECTED SKIN OR REPLACE THE AILERON.  DURING SKIN REPLACEMENT, IF THE PREFORMED FACTORY SKIN IS SPREAD APART EVEN A LITTLE, THE TRAILING EDGE TAKES ON A (FAT) CON1L72 3O3  O  A19S0   E286                 
20070309000042007030900004CE  2007       3          9          2007FA0000207    120070301G2432G35             BATTERY                                 CESSNA180   180         2072602CE  CONT  O470  O470*       17026SO                                              LEAKING         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL159198C34                     31297                                   BATTERY ACID LEAKED OR TRANSFERRED TO AFT, LOWEST CELL (AIRCRAFT TAIL WHEEL) AND SPILLED OUT.  CORRODED HOLE IN BATTERY BOX AND SPILLED INTO BELLY OF AIRCRAFT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3O3  ONC5A6     E273                 
20070309000052007030900005CE  2007       3          9          2007FA0000208    120070301G2432G35             BATTERY                                 CESSNA180   180         2072602CE  CONT  O470  O470*       17026SO                                              LEAKING         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL159198C34                     31297                                   BATTERY ACID LEAKED OR TRANSFERRED TO AFT, LOWEST CELL (AIRCRAFT TAIL WHEEL) AND SPILLED OUT.  CORRODED HOLE IN BATTERY BOX AND SPILLED INTO BELLY OF AIRCRAFT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3O3  ONC5A6     E273                 
20070322000252007032200025    2007       3          22         2007FA0000209    420070306G23509903334446      AUDIO CONTROL                           GULSTMG1159 G1159       3953505SO  PWA   530   PW530A           NE                              COCKPIT         SHORTED         C      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      EA21685SF                       94                                      UNIT WAS MANUFACTURED IN AUGUST 06 AND WAS INSTALLED IN DECEMBER 06. THE UNIT POPPED THE CIRCUIT BREAKER ON THE FIRST TRIP. THE UNIT WAS SENT IN FOR REPAIR AND REINSTALLED IN FEBRUARY 07 AND FAILED AGAIN ON THE FIRST FLIGHT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA12EA   E00053EN             
20070309000412007030900041SO  2007       3          9          2007FA0000210    220070220G8530639614639615    ROCKER          CONT        O300D       CESSNA172   172H        2072424CE  CONT  O300  O300D       17022SO                              ENGINE          INCORRECT       D      K   NONE                                                                                            R  PARTIAL RPM/PWR LOSS                                                          CRCRUISE         1                      EA178848Z     110   64805D6D    17255498    64805D6D                    PILOT REPORTED LOSS OF POWER (600 RPM DROP) SIGNIFICANT ENGINE ROUGHNESS DURING CLIMB. ENGINE RECOVERED SHORTLY AFTERWARDS. PILOT ELECTED TO CONTINUE AND HAD SAME PROBLEM AGAIN DURING CRUISE FLIGHT. ENGINE RECOVERED ON ITS OWN ONCE AGAIN. PILOT SAID CARB HEAT DID NOT MAKE ANY IMPROVEMENT DURING BOTH OCCURRENCES. AIRCRAFT WAS TURNED OVER TO MAINTENANCE.  THE ONLY ABNORMALITY DISCOVERED WAS THAT THE EXHAUST VALVES ON 4 OF THE 6 CYLINDERS HAD INCORRECT ROCKER INSTALLED (639614, INTAKE ROCKER). PARTS MANUAL CALLS FOR 639615 (EXHAUST ROCKER) TO BE INSTALLED ON EXHAUST POSITION.                                                                                                                                             1H71 3O3  ONT3A12    E253                 
20070309000732007030900073CE  2007       3          9          2007FA0000214    120070307G801185562020        STARTER                                 CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              ENGINE          SPINNING        G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP05767CL57                     172S9987                                STARTER SPINS AND WILL NOT ENGAGE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A12    1E10                 
20070322000812007032200081CE  2007       3          22         2007FA0000215    120070301G3230MS2764816       BEARING                                 BEECH 90    F90         1152909CE  PWA   PT6   PT6A135     52043NE                              MLG             SEIZED          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO0719RK 9280                   LA12                                    PERFORMING A ROUTINE 6 YEAR LANDING GEAR OVERHAUL, THE LT LANDING GEAR GEARBOX-ACTUATOR TORQUE TUBE HAD A SEIZED MAIN SUPPORT BEARING. THIS MADE THE TORQUE TUBE EXTREMELY HARD TO TURN. THE BEARING WAS FOUND TO BE RUSTED, AND SEIZED. BEARING WAS REPLACED WITH NEW.                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 4T4  T  A31CE   E4EA                 
20070402001692007040200169EA  2007       4          2          2007FA0000218    220070202G855056G23399        BAFFLE                                  PIPER PA32  PA32301     7103207SO  LYC   O540  TIO540AH1A  42003EA                              OIL SUMP        CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM07447KC85                     3255047     L1239361A                   DURING ENGINE OIL CHANGE FOUND RIVET HEAD IN OIL SUMP SCREEN.  REMOVED ENGINE AND OIL SUMP ASSY.  FOUND OIL SUMP BAFFLE ASY RIVETS SHEARED OFF AND ATTACH HOLES BROKEN OUT AND BAFFLE ASSY CRACKED.  RETRIEVED RIVET STEMS AND HEADS.  REMOVED AND REPLACED OIL SUMP BAFFLE ASSY WITH NEW PART.  REASSEMBLED ENGINE AND REINSTALLED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  O  A3SO    E14EA                
20070329002692007032900269EA  2007       3          29         2007FA0000219    220070302G7310                B-NUT                                   CESSNA182   182T        2072703CE  LYC   O540  IO540AB1A5       EA                              FUEL SYSTEM     LOOSE           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO1138AL                        18281450    L2980148A                   IN THIS CASE, FOUND THAT THE B-NUT CONNECTING TO THE FUEL CONTROL FROM THE SPIDER WAS LOOSE.  IT WAS NOT LEAKING, BUT REQUIRED A THIRD OF A TURN TO TORQUE DOWN TO PROPER TORQUE.  NO OTHER WORK HAS BEEN DONE TO THE SPIDER OR FUEL CONTROL BECAUSE I HAVE DONE THE WORK SINCE NEW ON THIS AIRCRAFT.  TT 228.8.  REMEMBER FINDING A LOOSE FIREWALL FITTING ON THE FIRST INSPECTION.  THIS IS THE SECOND INSPECTION DONE ON THIS AIRCRAFT.  IT WAS CERTIFIED 11/11/2004.  (K)                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A13    1E4                  
20070329002802007032900280CE  2007       3          29         2007FA0000220    120070223G2510551900921       SEAT                                    CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              COCKPIT         CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE05630CC                       5500130                                 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS.  STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE.  CHAIR WAS REPAIRED IAW ST01042WI STRUCTURAL SEAT REPAIR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 4F4  F  A22CE   E1NE                 
20070402002372007040200237EA  2007       4          2          2007FA0000221    220070222G8520                CRANKSHAFT                              CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              ENGINE          CORRODED        B  YYBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03          2199                          L130951A                    DURING NORMAL OVERHAUL, CRANKSHAFT FOUND PITTED IN THE INTERNAL BORE.  THIS ENGINE WAS LAST OVERHAULED BY THE FACTORY, JULY 2002..  THE PID COATING DOES NOT SEEM TO PREVENT PITTING OR CORROSION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  ONT3A12    1E10                 
20070504001652007050400165CE  2007       5          4          2007FA0000222    120070215G282199120154        FUEL FILTER                             CESSNA500   500CESSNA   2076602CE  PWA   JD15  JT15D1A          NE                              RT WING         SEPARATED       D  J7BRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW01409S 10045                  5000238                                 THE RT FUEL FILTER ASSY SEPARATED FROM THE STANDPIPE DUE TO THE SNAP-RING BECOMING DISLOGED AND RESULTED IN A SUBSTANTIAL FUEL LEAK.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 4F4  F  A22CE   E25EA                
20070329002732007032900273EA  2007       3          29         2007FA0000223    220070124G7261                OIL FILTER                              PIPER PA32  PA32R300    7103213SO  LYC   O540  IO540*      41532EA                              ENGINE          COLLAPSED       D      K   NONE                                                                                            K  FLUID LOSS                                                                    NRNOT REPORTED   1                      SW99                                                                    OIL LEAK NOTED AFTER OIL CHANGE.  REMOVED OIL FILTER AND DISCOVERED PARTIAL COLLAPSE OF THE OIL FILTER ELEMENT.  IT WAS DETERMINED THAT THE ENGINE MOUNTED INTERNAL BY-PASS VALVES OPERATION.  PREVIOUS TO THIS OCCURRENCE THE SB MENTION HAD NOT BEEN COMPLIED WITH.  AFTER THIS OCCURRENCE, SB WERE COMPLIED WITH AND A NEW OIL FILTER OF THE SAME MAKE AND MODEL WAS INSTALLED AND THE SYSTEM FUNCTIONED PROPERLY.  SUBMITTER SUGGESTS THAT DUE TO THE SIGNIFICANT NR OF OCCURRENCES OF THIS TYPE THAT SB SI-1442 AND 1453 BECOME MANDATORY THROUGH AD FOR ADDED SAFETY.  (K)                                                                                                                                                                1L71 3O3  O  A3SO    1E4                  
20070402001272007040200127CE  2007       4          2          2007FA0000224    120070215G282199120154        FUEL FILTER     PUROLATOR               CESSNA500   500CESSNA   2076602CE  PWA   JD15  JT15D1A          NE                              RT WING         SEPARATED       B  J7BRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW01409S 10045                  5000238     76509                       THE RT FUEL FILTER ASSY SEPARATED FROM THE STANDPIPE DUE TO THE SNAP-RING BECOMING DISLODGED AND RESULTED IN A SUBSTANTIAL FUEL LEAK.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 4F4  F  A22CE   E25EA                
20070329002972007032900297SO  2007       3          29         2007FA0000225    120070215G275062679000        BRACKET                                 PIPER PA28  PA28*              SO                                                               COCKPIT         CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NE03                                                                    THIS BRACKET IS RIVETED IN THE CENTER TUNNEL AND ACCEPTS (2) BOLTS AT THE FORWARD SIDE OF THE FLAP HANDLE SUPPORT MOUNT.  THIS IS A DIFFICULT AREA TO SEE, EVEN WITH A MIRROR.  WE HAVE FOUND (6) CRACKED BRACKETS SO FAR TO DATE.  SUSPECT FATIGUE AND AIR LOADS CAUSING CRACKS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3O      2A13                         
20070402001582007040200158SO  2007       4          2          2007FA0000226    220070220G8500                ENGINE                                  CESSNA404   404         2075901CE  CONT  O520  GTSIO520M   17032SO                                              FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE03442EH                       4040202     604103                      THIS ENGINE FAILED TO THE TERMINOLOGY OF CATASTROPHIC AT THE NR 1 AND NR 2 CYLINDER CONNECTING ROD LOCATIONS DURING A MAINTENANCE TEST FLIGHT WITHIN TEN MINUTES INTO THAT FLIGHT WITH A MECHANIC ON BOARD MONITORING THE ENGINE INSTRUMENTS.  THE OIL PRESSURE SUDDENLY DROPPED TO ZERO, THE PROPELLER STARTED TO FEATHER AND DURING SHUTDOWN AND SECURING, THE ENGINE LOCKED UP.  PRIOR TO THIS, THE OIL FILTER WAS REMOVED, CUT OPEN AND INSPECTED WITH NO DEFECTS NOTED.  AN OIL SOAP SAMPLE WAS TAKEN.  THE OIL PUMP AND AIRCRAFT OIL PRESSURE GAUGE WAS CHECKED FOR A POSITIVE OIL PRIME AND INDICATION.  AN EXTENDED ENGINE GROUND RUN WAS DONE AT LOW AND HIGH POWER SETTINGS WITH NO OIL PRESSURE DISCREPANCIES NOTED.  THESE CHECKS WE1L72 3O3  ORTA25CE   E7CE                 
20070313001972007031300197CE  2007       3          13         2007FA0000227    120070119G801185A34117        STARTER                                 CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              ENGINE          STUCK           G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP05767CL527                    172S9987                                STARTER STUCK IN ENGAGED POSITION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A12    1E10                 
20070504001382007050400138NM  2007       5          4          2007FA0000228    120070306G3260                SENSOR                                  BOEING747   747230B     1384889NM  GE    CF6   CF650*      30018NE                              MLG             MALFUNCTIONED   B  GJPYO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP33760SA                       21221                                   DURING TAKEOFF, THE LANDING GEAR HANDLE WILL NOT GO TO UP OR RETRACT POSITION.  AIRCRAFT RETURNED TO BASE.  PERFORMED TROUBLESHOOTING ON THE LANDING GEAR SYSTEM AND FOUND THAT LT WING GEAR TRUCK ROTATION SENSOR AT FAULT.  ADJUSTED THE LT WING GEAR TRUCK ROTATION SENSOR IAW AMM 32-61-04.  PERFORMED LANDING GEAR SYSTEM EXTENSION AND RETRACTION SEVERAL TIMES IAW AMM 32-32-00/501, TEST NORMAL.  (K)                                                                                                                                                                                                                                                                                                                                   2L74 4F4  F  A20WE   E23EA                
20070412000272007041200027EU  2007       4          12         2007FA0000229    120070308G2820653014          VALVE                                   ISRAEL1124  1124A       4500103EU  GARRTTTFE731TFE731*     01518WP                              RT LWR FUEL CELLCRACKED         B  JGVRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE09328PC8597                   328                                     CRACK IN INTERCONNECT VALVE MOTOR HOUSING.  FOUND DURING BAG REMOVAL AND REINSTALLATION.  CAUSE OF CRACK, UNKNOWN.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2M72 4F4  F  A2SW    E6WE                 
20070329002932007032900293SO  2007       3          29         2007FA0000230    120070220G55214602003         RIB                                     PIPER PA31T PA31T       7103124SO  PWA   PT6   PT6A28           EA                              LT ELEVATOR     BROKEN          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO09112ED                       31T8020060                              1 INCH CRACK NOTED ON LOWER SKIN THRU RIVET.  DRILLED OPEN SKIN AND FOUND 5 INCH OF RIB FLANGE BROKE OFF 2 INCHS FROM TRAILING EDGE.  SKIN AND RIB HAVE TO BE REPLACED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3T4  T  A8EA    E4EA                 
20070329002982007032900298SO  2007       3          29         2007FA0000231    120070215G2910                HYDRAULIC LINE                          PIPER PA23  PA23250     7102308SO  LYC   O540  IO540*      41532EA                              HYDRAULIC SYS   CHAFED          G      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      SO19144CN5200                   278054036                               AIRCRAFT HYDRAULIC SYSTEM RT GEAR DOWN ALUMINUM LINE LOCATED UNDER COCKPIT FLOOR WAS CHAFING AGAINST CONTROL CABLE AND WAS PENETRATED CAUSING LEAK AND DEPLETION OF HYDRO FLUID WHICH RESULTED IN AIRCRAFT LANDING WITH UNSAFE NOSE GEAR AND DAMAGE TO AIRCRAFT NOSE SECTION.  THIS AREA SHOULD BE INSPECTED AT LEAST DURING ANNUAL INSPECTIONS.  (K)                                                                                                                                                                                                                                                                                                                                                                                           1L72 3O3  O  1A10    1E4                  
20070507001862007050700186SO  2007       5          7          2007FA0000232    120070305G2432RG380E44        BATTERY                                 LKHEED1329  1329*              SO  GARRTTTFE731TFE7313     01518WP                              MASTER          FAILED          B  VXWRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA2158TS                        5079        75238                       THESE 2 EA PN RG-380E/44 MAIN SHIP BATTERIES WERE INSTALLED ON 10/30/2006.  THESE BATTERIES WERE REPLACEMENTS FOR 2 EA BATTERIES THAT HAD BEEN IN SATISFACTORY SERVICE IN THIS AC FOR APPROX 48 MONTHS BUT FAILED A CAPACITY CHECK DURING A REGULAR SCHEDULED INSPECTION.  LESS THAN 2 MONTHS AFTER INSTALLATION THE PILOTS WERE UNABLE TO START THE MAIN ENGINES USING THESE BATTERIES.  AT THIS TIME THE BATTERIES HAD A TOTAL FLIGHT TIME OF 16 HOURS AND HAD PERFORMED 26 MAIN ENGINE STARTS AND 8 APU STARTS.  THE MAIN ENGINES WERE STARTED USING A GROUND POWER UNIT.  ALL CHARGING AND ELECTRICAL OPERATIONS APPEARED NORMAL.  THE BATTERIES WERE REMOVED AND GIVEN TO REPAIR STATION FOR TESTING.  BOTH BATTERIES WERE TESTED IAW (INST2L74 4J4  F  2A15    E6WE                 
20070329002902007032900290EA  2007       3          29         2007FA0000233    220070312G7414M3081           SPRING          SLICK                   CESSNA182   T182T       2072738CE  LYC   O540  TIO540AK1A       EA                              RT MAGNETO      BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP295198G658        66LC35SDNP  T18208150   L1121761A                   NEW POINTS (PN M3081) WERE INSTALLED IN BOTH MAGNETOS AT THE ANNUAL INSPECTION ON 2/22/07, TT 649.2.  ON 3/10/07, TT 658.2, PART TT - 9.0 HOURS, THE PILOT/OWNER PERFORMED MAG CHECK AND THE ENGINE QUIT.  A MECHANIC REMOVED THE RT MAG AND FOUND THAT THE SPRING THAT HOLDS HALF THE POINTS HAD SNAPPED OFF.  THE MECHANIC TOLD THE OWNER THAT HE HAD NEVER SEEN POINTS FAIL LIKE THIS IN HIS 30 YEARS OF AC MAINTENANCE.  TOLD HIM THAT I HAD NEVER SEEN THIS TYPE OF MALFUNCTION IN MY 10 YEARS OF MAINTENANCE.  IT APPEARS THAT THE METAL SPRING THAT MAKES UP THE POINT KIT FAILED JUST AFT OF THE AREA WHERE THE METAL IS BENT ON BOTH EDGES FOR STRENGTHING PURPOSE.  THE BREAK IS IN A SEMICIRCLE FRO ONE SIDE TO THE OTHER.  THE METAL1H71 3O3  ONT3A13                         
20070409001622007040900162GL  2007       4          9          2007FA0000234    320070317G6111F8483           BLADE                                                                                                       HARTZLHCC3Y HCC3YR      GL  PROPELLER       MISREPAIRED     B  ME4RO   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      SO19                                                    DY5121B         (REF NR: 38430A) 2 OF 3 PROPELLER BLADES WERE PREVIOUSLY REPAIRED USING AN UNAPPROVED WELD METHOD IN SEVERAL LOCATIONS ON THE BLADE AIRFOIL.  THE BLADES HAVE BEEN SCRAPED PENDING DISPOSITION INSTRUCTIONS FROM MFG.  THE CUSTOMER HAS BEEN CONTACTED FOR HISTORICAL RECORDS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          5  CP25EA    
20070507001832007050700183GL  2007       5          7          2007FA0000235    320070317G6111F8483           BLADE                                                                                                       HARTZLHCC3Y HCC3YR      GL  PROPELLER       MISREPAIRED     B  ME4RK   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      SO19                                                    DY5121B         (REF NR 38430A)  2 OF 3 PROPELLER BLADES WERE PREVIOUSLY REPAIRED USING AN UNAPPROVED WELD METHOD IN SEVERAL LOCATIONS ON THE BLADE AIRFOIL.  THE BLADES HAVE BEEN SCRAPED PENDING DISPOSITION INSTRUCTIONS FROM MFG.  THE CUSTOMER HAS BEEN CONTACTED FOR HISTORICAL RECORDS. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           5  CP25EA    
20070329002842007032900284EU  2007       3          29         2007FA0000236    120070121G2434                TERMINAL                                SOCATATB20  TB20TRINIDAD8680695EU  LYC   O540  IO540C4D5   41532EA                              ALTERNATOR      BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP05711RP                       1081        L1813148A                   FIELD WIRE TERMINAL END BROKEN AT ALTERNATOR TERMINAL LUG CAUSED FAILURE OF ALTERNATOR TO CHARGE BATTERY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 3O3  ORTA51EU   1E4                  
20070402002142007040200214CE  2007       4          2          2007FA0000237    120070301G561010138402524     WINDSHIELD                              BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  COCKPIT         CRACKED         B  AHTRA   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      GL11200VC728                    FL316                                   AT AN ALTITUDE OF 17,000 FT OAT -6 DEGREES C, THE RT WINDSHIELD CRACKED FROM THE CENTER OB FROM THE TOP TO THE BOTTOM ABOUT 2 INCHES OB ON THE OUTER PANE.  RETURNED TO THE DEPARTING AIRPORT WITHOUT ANY PROBLEMS.  WINDSHIELD WAS REPLACED AND NO KNOWN CAUSE FOR THE WINDSHIELD TO CRACK. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T4  T  A24CE   E4EA    6  CP56GL    
20070322000372007032200037CE  2007       3          22         2007FA0000238    120070316G3242RA66109         BRAKE PADS                              CESSNA172   172RG       2072438CE  LYC   O360  O360F1A6    41514EA  MCAULY2D34C B2D34C220   GL  MLG             FRACTURED       D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA076440V49                     172RG0701   L2783136A   951039          DURING A 50 HR OIL CHANGE AND INSPECTION, FOUND BOTH LT AND RT BRAKE PADS FALLING APART, SEVERELY CRACKED WITH LARGE PIECES MISSING.  BOTH SIDES WERE CHANGED AT THE PREVIOUS 100 HOUR INSPECTION.  THIS HAS BEEN A FREQUENT PROBLEM WITH THESE BRAKE PADS ON ALL OF OUR AIRCRAFT (2 C152, 1 C172, 1 C172RG), NEW PADS FAILING WITHIN 200 HOURS OR LESS SINCE WE STARTED USING THEM. PREVIOUSLY, WE USED OTHER MFG PADS WITH VERY FEW PROBLEMS.                                                                                                                                                                                                                                                                                                 1H71 3O3  O  3A17    E286    5  CP7EA     
20070322000922007032200092CE  2007       3          22         2007FA0000243    120070226G5310VP10            ANTENNA                                 BEECH 33    35B33       1151406CE  CONT  O470  IO470*      17026SO                              VHF SYSTEM      MISINSTALLED    B      A   UNSCHED LANDING                                                                                 WD INADEQUATE Q C            INFLIGHT SEPARATION                                 CRCRUISE         1                      CE031768G94   94                CD509                                   THE DOUBLER FOR THE VHF ANTENNA APPEARS TO HAVE BEEN TOO SMALL(SLIGHLY LARGER THAN THE BASE OF THE ANTENNA)AND WAS NOT RIVITED TO THE FUSELAGE,ALLOWING THE ANTENNA TO FLUTTER WHILE AIRBORNE.ON POST FLIGHT INSPECTION THE PILOT DISCOVERED TEARING ON THREE SIDES ON TOP OF THE FUSELAGE AROUND THE BASE OF THE ANTENNA.NOTE THE TACH ONLY READS 94.5                                                                                                                                                                                                                                                                                                                                                                                         1L71 3O3  O  3A15    E1CE                 
20070322000932007032200093CE  2007       3          22         2007FA0000244    120070301G5551071204221       BRACKET                                 CESSNA185   A185F       2072821CE  CONT  O520  IO520*      17032SO                              HORIZONTAL STAB CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM074640E                       18503824                                DURING A DETAILED INSPECTION OF THE EMPENAGE, THE RT HORIZONTAL STABILIZER HINGE BRACKET P/N 0712042-2 WAS FOUND CRACKED AND HAD (2) SHEARED RIVETS.  UPON DISASSEMBLY THE LT BRACKET P/N 0712042-1 WAS FOUND TO HAVE (2) SHEARED RIVETS.  THESE PARTS ARE IN THE MFG 180/185 IPC FIG 32 INDEX NR 36 AND NR 37.THERE IS NOTHING IN THE RECORDS THAT SHOW THESE PARTS CHANGED, HOWEVER THE RT BRACKET DID HAVE (2) NR 5 RIVETS WHERE ALL OF THE REST ON BOTH BRACKETS WERE NR 4S.  LEADING US TO BELIEVE THAT IT MAY HAVE BEEN REPLACED BEFORE.                                                                                                                                                                                                  1H71 3O3  O  3A24    E5CE                 
20070322000982007032200098CE  2007       3          22         2007FA0000246    120070313G2820050011849       LINE                                    CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              FUEL SYSTEM     CHAFED          D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      SW0530LU 847                    17281257                                DURING PREFLIGHT INSP. PILOT FOUND FUEL ON RAMP UNDER CENTER FUSELAGE  MECHANIC INVESTIGATED INSIDE COCKPIT FLOOR AND FOUND ALUMINUM FUEL LINE CHAFING AGAINST RT STEERING TUBE, CAUSING THE FUEL LEAK. MECHANIC INSPECTED 6 OTHER 2005/2006 172R AIRCRAFT IN OUR FLEET AND FOUND CHAFING IN (3) OTHER AIRCRAFT, WITH ANOTHER LEAK IMMINENT. ALL AC UNDER 900 HRS AFTT. OUR AIRCRAFT CAME FROM THE FACTORY WITH THIS FUEL LINE/STEERING TUBE CONFIGURATION. SUBMITTER SUGGESTS IMMEDIATE INSPECTION FOR THIS CONDITION. NOTE: FUEL WAS NOT SMELLED IN COCKPIT.                                                                                                                                                                                  1H71 3O3  ONT3A12    1E10                 
20070322001402007032200140CE  2007       3          22         2007FA0000247    120070227G716011702           CLAMP                                   BEECH 58    58P         1152744CE  CONT  O520  TSIO520L    17040SO                              LT ENGINE       FAILED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL2525RL                        TJ232       0                           LT ENGINE REPORTED TO BE ROUGH RUNNING.  INDUCTION HOSE CLAMP(P/N-RAM 1170-2)FAILED; ALLOWING INDUCTION COUPLER(P/N-632323) TO SEPARATE FROM INDUCTION TUBE. THIS INDUCTION LEAK OCCURRED BETWEEN THE Y AND INTAKE TUBES TO CYLINDERS NR 2, NR 4 AND NR 6.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A23CE   E8CE                 
20070326001072007032600107CE  2007       3          26         2007FA0000253    120070307G272065651412        ACTUATOR                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              ELEVATOR        BINDING         C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW13797CW8177 300               0232                                    WHILE REPLACING TRIM ACTUATOR P/N 6565141-2 WITH WHAT MFG SAID WAS AN APPROVED SUB PART P/N 5565450-92.   IT WAS FOUND THAT THE LOLLIPOPS (JACK SCREWS) WERE 5.5 INCHES LONG AND THE ORIGINAL LOLLIPOPS ARE 5.75 INCHES LONG. IF YOU LOOK AT THE COMPONENT MANUAL FOR THIS ACTUATOR 6565141-2 IT SHOWS 4 DIFF. DASH NUMBERS. -4 AT 5.5 INCHES, -7 AT 5.5 INCHES, -15 AT 4.85 INCHES, AND -21 AT 5.75 INCHES ALL WHICH IS TO THE SAME LOLLIPOP P/N. THE -92 ACTUATORS FITS UNITS 692 TO 924, WHILE OUR UNIT IS 232. MFG NEEDS TO FIX THESE P/NS AND CLEAR THE WAY THESE MANUALS ARE WRITTEN FOR CLARITY. TO MANY ACTUATORS ARE TO ANOTHER P/N WITH INCORRECT JACKSCREW LENGTHS.                                                                  1L72 4F4  F  A22CE   E1NE                 
20070326001162007032600116CE  2007       3          26         2007FA0000256    120070314G7810655503011       DUCT                                    CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              EXHAUST ASSY    MISMANUFACTURED B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      SW13797CW                       5500232                                 DURING INSPECTION MULTIPLE PATCHES WERE FOUND ON EXHAUST DUCT ASSY P/N 6555030-11. A REPLACEMENT WAS ORDERED AND FOUND TO HAVE 2 HOLES MISDRILLED BY 2 DEGREES. MFG WAS CONTACTED AS TO WHAT COULD BE DONE AND AFTER CONFIRMING THAT IN TRUTH 2 HOLES WERE NOT PROPERLY PLACED WE WERE TOLD THAT IN FACT 4 DUCTS WERE FOUND NOT BUILT CORRECTLY AND 1 HAD GOTTEN TO THE FIELD. MFG HAS AGREED TO ACCEPT THE DUCT BACK FOR REPAIR BUT WANTS TO BILL US FOR THE FIX ON A NEW PART. AFTER REPAIR, WE ARE TO SUBMIT FOR FINANCIAL REIMBURSEMENT FOR THERE ENGINEERING REPAIR.                                                                                                                                                                       1L72 4F4  F  A22CE   E1NE                 
20070326001252007032600125EA  2007       3          26         2007FA0000257    220070224G8530                ROCKER SHAFT                            UNIVAR108   1081        9230404NM  FRNKLN6A41506A4150*     27024EA                              NR 3 CYLINDER   BROKEN          G      B   EMER. DESCENT                                                                                   R  PARTIAL RPM/PWR LOSS                                                          CRCRUISE         1                      WP119088K                       1082088                                 THE NR 3 CYLINDER ROCKER ARM SHAFT FAILED (BROKE) AT THE CENTER SUPPORT POSITION.  ADDITIONALLY, (2) OF THE (3) ROCKER ARM BOSS SECURING BOLTS FAILED AND THE THIRD BOLT PULL OUT OF THE HEAD.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  O  A767    E238                 
20070326001272007032600127CE  2007       3          26         2007FA0000258    120070301G3210MS2764816       BEARING                                 BEECH 90    F90         1152909CE  PWA   PT6   PT6A135     52043NE                              LT MLG          SEIZED          B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO0719RK 9280                   LA12                                    PERFORMING A ROUTINE 6 YEAR LANDING GEAR OVERHAUL, THE LT LANDING GEAR GEARBOX-ACTUATOR TORQUE TUBE HAD A SEIZED MAIN SUPPORT BEARING. THIS MADE THE TORQUE TUBE EXTREMELY HARD TO TURN. THE BEARING WAS FOUND TO BE RUSTED, AND SEIZED. BEARING WAS REPLACED WITH NEW.                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 4T4  T  A31CE   E4EA                 
20070326001282007032600128SO  2007       3          26         2007FA0000259    120070301G8000PM1201          STARTER                                 PIPER PA28  PA28236     7102815SO  LYC   O540  O540J3A5    41532EA  HARTZLHCF3Y HCF3YK1     GL  ENGINE          WORN            G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO052177Z28   28                287911154   L2117640A   CM288           THIS AIRCRAFT HAS HAD (5) PM1201 STARTERS INSTALLED SINCE 03-08-2004. THE STARTERS HAD TO BE REPLACED AT THE FOLLOWING INTERVAL: 58 HOURS TIME IN SERVICE, 18 HOURS TIME IN SERVICE, 11 HOURS TIME IN SERVICE, 5 HOURS TIME IN SERVICE, 28 HOURS TIME IN SERVICE.  ALL STARTERS SUFFER THE SAME PROBLEM. AFTER THE ENGINE IS STARTED AND THE AIRCRAFT HAS FLOWN FOR A SHORT PERIOD OF TIME, (LESS THAN ONE HOUR) THE BENDIX GEAR WILL BEGIN TO CREEP OUT AND TRY TO ENGAGE/RUB THE RING GEAR.  IN FEW FLIGHT HOURS THE BENDIX GEAR WILL START SHOWING WEAR ON BOTH THE BENDIX GEAR AS WELL AS THE RING GEAR ON THE FLYWHEEL.  ALL THE STARTERS WERE REPORTED TO HAVE HAD THE SAME PROBLEM.  THE OWNER DECIDED TO REMOVE THE STARTER FROM HIS AIR1L71 3O3  O  2A13    E295    5  CP31EA    
20070403000822007040300082    2007       4          3          2007FA0000260    320070219G61113BLADEWOOD68    PROPELLER                               AMTR  KITFOXKITFOX41200 05626LBGL                                                               PROPELLER       BROKEN          G      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      SW11880BW219  6                 C96010137                               OWNER REPORTED 5 MINUTES AFTER TAKEOFF AT 2500 ASL, ALL 3 PROPELLER BLADES DEPARTED.  THERE WAS ONE VIOLENT SHAKE AND THEN SMOOTH GLIDING TO SAFE LANDING OFF AIRPORT.  PRELIMINARY EXAM INDICATES ENGINE MOVED ENOUGH TO CAUSE CARBURETOR TO SEPARATE PREVENTING OVERSPEED.  SEPARATED BLADES WERE NEVER LOCATED.  PROPELLER TO BE REPLACED BY OWNER, THIS IS AN EXPERIMENTAL HOMEBUILT AIRCRAFT.                                                                                                                                                                                                                                                                                                                                              1H71 3I    NCEXPA1H71                     
20070326000602007032600060CE  2007       3          26         2007FA0000261    120070322G521099120754        SEAL                                    CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              CABIN DOOR SEAL MISMANUFACTURED B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW13797CW8177 300               5500232                                 WHILE INSTALLING THIS FACTORY NEW SEAL IT WAS NOTED THAT THE SEAL WAS VERY TIGHT GOING AROUND THE DOOR. UPON CABIN PRESS TEST THE SEAL WILL NOT INFLATE DUE TO BEING TO TIGHT.  (2) SEAL FROM STOCK WERE TRIED WITH THE SAME AFFECT. THE LAST SEAL WAS INSTALLED AND INFLATED AS SHOULD BE. THE FACTORY NEEDS TO CHECK THERE SEALS CLOSER UPON RECEIPT FROM THERE VENDORS.                                                                                                                                                                                                                                                                                                                                                                      1L72 4F4  F  A22CE   E1NE                 
20070326000852007032600085CE  2007       3          26         2007FA0000262    120070322G7810655503011       DUCT                                    CESSNA500   550         2076604CE                                                               ENGINE          UNKNOWN         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL19797CW8177 300               5500232                                 UPON RECEIVING THE NEW PART P/N 6555030-11 IT WOULD NOT FIT THE ENGINE. THE ORIGINAL DUCT IS 27 .2500 INCH OUTSIDE AND 25.5 INCH INSIDE. THE NEW UNIT IS A FULL .5 INCH SMALLER IN DIAMETER ALL AROUND. THIS IS THE SECOND ISSUE WITH THESE DUCTS THE FIRST WERE MIS-DRILLED BY 2 DEGREES AT THE 1 AND 5 OCLOCK POSITION. THIS NEW DUCT IS NOT EVEN CLOSE TO FITTING.                                                                                                                                                                                                                                                                                                                                                                          1L72 4F      A22CE                        
20070403000372007040300037EU  2007       4          3          2007FA0000263    120070321G7600L810BQ54        SOLENOID                                SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B         NE                              AUTO THROTTLE   UNSERVICEABLE   B  N37RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW15186AE189                    3872        22484                       (REF NR: 186AE-2007-I-0032) WHILE PERFORMING A CHECK OF THE TWIST GRIP SOLENOID, ENGAGED THE SOLENOID BY PLACING THE AUTO/MAN SWITCH TO MAN  MODE FOR A TOTAL OF 10 MINUTES.  AFTER THE 10 MINUTE PERIOD HAD ELAPSED, RETURNED THE AUTO/MAN SWITCH TO AUTO.  AFTER 15 MINUTES MOVED AUTO/MAN SWITCH BACK TO MAN, THE PISTON FROM THE SOLENOID FAILED TO MOVE.  THE PISTON SHOULD HAVE RETRACED IMMEDIATELY.  PROBABLE CAUSE: SOLENOID OVERHEATING AND MALFUNCTIONING.  RECOMMENDATION TO PREVENT RECURRENCE: REPLACING CURRENT PN OF SOLENOID WITH ONE THAT CAN EITHER RUN COOLER OR WITHSTAND THE HEAT.  (K)                                                                                                                                   1G71 3U3  U  H9EU    E00054EN             
20070402001572007040200157SO  2007       4          2          2007FA0000264    120070306G53501159B541014     FAIRING                                 GULSTMGV    GULFSTREAMGV3980116SO  RROYCEBR700 BR700715A130     NE                              FUSELAGE        DEPARTED        G      A   UNSCHED LANDING                                                                                 D  INFLIGHT SEPARATION                                                           NRNOT REPORTED   1                      CE07401HF1300                   5039                                    ON MARCH 6, 2007, DURING A FLIGHT, THE SUBJECT AIRCRAFT EXPERIENCED AN IAPPARENT IN-FLIGHT STRUCTURAL FAILURE OF THE RIGHT WING-TO FUSELAGE FORWARD FAIRING.  THE INCIDENT OCCURRED AT FLIGHT LEVEL 400 AT 90 DME ON THE (LNK) VOR 220 RADIAL AT .85 MACH.  AFTER ONE HOUR AND 45 MINUTES INTO THE FLIGHT (APPROX 2115Z), THE CREW NOTED AN AUDIBLE (THUMP) FOLLOWED BY A (CHANGE IN WIND NOISE).  AS THE AIRCRAFT IS EQUIPPED WITH PROXIMITY CAMERAS, THE FIGHT CREW WAS ABLE TO SEE A (HOLE OF SIGNIFICANT SIZE) IN THE AREA OF THE SINGLE POINT REFUELING ACCESS DOOR USING THE LOWER AFT-FACING FUSELAGE CAMERA.  THE FLIGHT CREW NOTIFIED AND REQUESTED EMERGENCY LANDING, WHERE THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.  THE FSDO WA2L72 4F4  FRTA12EA   E00061EN             
20070402001342007040200134CE  2007       4          2          2007FA0000265    120070322G2910270213          REGULATOR                               LEAR  60    60LEAR      5170707CE                                                               HYD SYS PRESSURELEAKING         C      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      GL11500  105                    306                                     IN-FLIGHT FAILURE OF BOTH ENGINE HYDRAULIC PUMPS, AND LOSS OF MAIN HYDRAULIC SYSTEM FLUID.  AC DIVERTED TO HOME BASE, DECLARED EMERGENCY LANDING, UNEVENTFUL.  FOUND PRESSURE HOSE ON R ENGINE HAD FAILED, DUE TO OVER-PRESSURE.  FOUND RESERVOIR AIR-PRESSURE REGULATOR (PN 2702-12) HAD FAILED, CAUSING LOSS OF HEAD PRESSURE IN RESERVOIR, AND SUBSEQUENT PRESSURE SPIKES IN ENGINE PUMPS, WHICH BURST FLEX LINE ON R ENGINE HYD PUMP, AND DAMAGED FLEX LINE ON L HYD PUMP AS WELL.  REPLACED L AND R ENGINE HYDRAULIC PUMPS, ALL FLEX PRESSURE LINES IN ENGINE HYDRAULIC CIRCUIT, HYDRAULIC FILTERS, RESERVOIR PRESSURE REGULATOR, CHECK VALVE, AND FILTER. BLED AIR FROM HYDRAULIC SYSTEM, PERFORMED FUNCTIONAL TESTS AND GROUND RUN, REPL 2L72 4F    RTA10CE                        
20070507000032007050700003CE  2007       5          7          2007FA0000266    120070315G5510                HINGE BRACKET                           BEECH 23    A23         1151204CE  CONT  O346  IO346A      17033SO  SNSNCH74DC  M74DC       EA  STABILATOR      CRACKED         B  MS2RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE093573R3596                   M756        1002075A    8623            UPON REMOVAL OF THE HORIZONTAL STABILATOR FOR BEARING REPLACEMENT, A CRACK WAS NOTED COMING OUT FROM UNDER THE LEFT HINGE BRACKET THAT IS RIVETED TO THE SPAR OF THE HORIZONTAL STABILATOR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  O  A1CE    E3CE    5  NP88614   
20070402002222007040200222EU  2007       4          2          2007FA0000267    120070228G81204066109031      BEARING                                 SOCATATB20  TB21        8680697EU  LYC   O540  TIO540AB1A  41533EA                              TURBOCHARGER    FAILED          B  BNGRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL19189GT685                    2022        21052261A                   IN FLIGHT, DROP IN MANIFOLD PRESSURE, TROUBLESHOT, FOUND TURBOCHARGER BEARING FAILURE.  FOUND METAL IN OIL FILTER.  ENGINE REMOVED FOR REPAIR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  ORTA51EU   E14EA                
20070329002912007032900291SW  2007       3          29         2007FA0000268    120070308G291020144           B-NUT                                   GULSTM500   500S        0141107SW  LYC   O540  TIO540A1A   41532EA                              LT MLG          LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL19280MB                       3255                                    PILOT NOTICED A FLUCTUATION AND LOSS OF HYDRAULIC PRESSURE IN FLIGHT, AFTER INSPECTION THE FORWARD HYDRAULIC HOSE B-NUT ON THE LT GEAR ACTUATOR WAS FOUND TO BE LOOSE.  THE B-NUT WAS TIGHTENED AND TORQUE SEAL WAS PUT ON THE B-NUT.  SERVICED HYDRAULIC RESERVOIR WITH H-5606.  AC WAS TEST FLOWN AND LEAK CHECK GOOD.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                   1H72 3O3  O  6A1     E14EA                
20070402001292007040200129CE  2007       4          2          2007FA0000269    120070321G6100                NONE                                    BEECH 90    C90         1152913CE  PWA   PT6   PT6A21      52043EA  HARTZLHCD4N3HCD4N3A     GL  PROPELLER       UNKNOWN         B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO13427DM                       LJ804                                   AIRCRAFT  HAS RAISEBECK STC SA3593NM INSTALLED WHICH STATES THE PROPS ARE NOT TO BE OPERATED BELOW THE SET MINIMUM RPM. PRE PHASE INSPECTION RUNS REVEALED THIS CONDITION. IAW MFG SERVICE LETTER 61-254 THIS CAN CAUSE  NO REACTION MODE VIBRATORY RESONANCE AND MAY RESULT IN HIGH STRESS IN THE BLADES. IT WAS RECOMMENDED THAT THE PROPELLERS BE REMOVED AND BE SENT TO A PROPELLER SHOP FOR INSPECTION.  CUSTOMER DECLINED RECOMMENDATION. NO FURTHER ACTION WAS TAKEN AT THIS INSPECTION.  BOTH THE LT AND RT PROPELLERS HAVE A TSO OF 957.9 AND A TT OF 2615.2                                                                                                                                                                           1L72 3T4  T  3A20    E4EA    5  CSTC      
20070403000492007040300049CE  2007       4          3          2007FA0000270    120070326G271035524314        CONTROL CABLE                           BEECH 35    N35         1151528CE  CONT  O470  IO470*      17026SO                              AILERONS        WORN            C      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             NRNOT REPORTED   1                      WP231363Z7541                   D6787                                   (REF MODEL 35 SERIES IPC FIG. 27)  LT AILERON CABLE FOUND RIDING ON PROP CONTROL CABLE SHEATH, ABOUT 2 INCHES AFT OF FIREWALL.  AILERON CABLE WAS WORN ABOUT HALF THROUGH, AND THE PROP CABLE WAS WORN THROUGH THE SHEATH TO THE INNER STEEL CABLE. (VERY DIFFICULT TO ACCESS THIS AREA FOR VISUAL INSPECTION.)  NO INDICATION OF RUBBING OR DRAGGING DURING GROUND CONTROL SYSTEM CHECKS, OR IN FLIGHT.  IT IS RELATIVELY EASY TO HAVE THE PROP CONTROL CABLE DISPLACED INTO CONTACT WITH THE AILERON CABLE WHEN WORKING IN THIS AREA DURING, FOR EXAMPLE, PANEL MODIFICATIONS OR AVIONICS UPGRADES.  RECOMMEND VISUAL AND TACTILE INSPECTION IN THIS AREA TO CONFIRM CLEARANCE.  UPON REMOVAL OF CABLE ASSEMBLY FOR REPLACEMENT, FOUND ADDITIO1L71 3O3  O  3A15    E1CE                 
20070403000392007040300039CE  2007       4          3          2007FA0000274    120070322G2910270213          REGULATOR                               LEAR  60    60LEAR      5170707CE                                                               HYD SYSTEM      LEAKING         C      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      GL11500  105                    306                                     IN-FLIGHT FAILURE OF BOTH ENGINE HYDRAULIC PUMPS, AND LOSS OF MAIN HYDRAULIC SYSTEM FLUID.  AIRCRAFT DIVERTED TO HOME BASE, DECLARED EMERGENCY LANDING, UNEVENTFUL.  FOUND PRESSURE HOSE ON R ENGINE HAD FAILED, DUE TO OVER-PRESSURE.  FOUND RESERVOIR AIR-PRESSURE REGULATOR (PN 2702-12) HAD FAILED, CAUSING LOSS OF HEAD PRESSURE IN RESERVOIR, AND SUBSEQUENT PRESSURE SPIKES IN ENGINE PUMPS, WHICH BURST FLEX LINE ON R ENGINE HYD PUMP, AND DAMAGED FLEX LINE ON L HYD PUMP AS WELL.  REPLACED L AND R ENGINE HYDRAULIC PUMPS, ALL FLEX PRESSURE LINES IN ENGINE HYDRAULIC CIRCUIT, HYDRAULIC FILTERS, RESERVOIR PRESSURE REGULATOR, CHECK VALVE, AND FILTER. BLED AIR FROM HYDRAULIC SYSTEM, PERFORMED FUNCTIONAL TESTS AND GROUND RUN,2L72 4F    RTA10CE                        
20070402001602007040200160GL  2007       4          2          2007FA0000276    120070306G5551                BOLT                                    DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  HORIZ STAB      BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM03921DA                       C0395       650218      AG5429          AC, RETURN FROM FLIGHT WITH BOTH BOLTS BROKEN; ATTACHING THE FORWARD HORIZONTAL STABILIZER MOUNT BRACKETS.  ATT 1) GIVES FLIGHT INFO.  ATT 2 AND 3) SHOW THE IPB BRAKE DOWN OF THE BOLTS AND LOCATION FROM MFG PARTS BOOK.  ATT 4) PICTURES OF BOLTS AND AIRCRAFT.  ATT 5) THE NTSB PAPERWORK.  ATT 6) IS SOME EMAIL TRAFFIC.  WE REMOVED THE RUDDER AND HORIZONTAL STABILIZER TO INSPECT ENTIRE AREA. WE REPLACE THE AFT MOUNT PLATE AND FORWARD MOUNT BRACKET ALONG WITH ALL NEW BOLTS, WASHERS AND NUTS.  WE ALSO INSPECTED OUR OTHER 9 AC AND REPLACED BOTH BOTH ON ALL 9 AC.  NO OTHER ISSUES WERE FOUND ON OUR OTHER AC.  MFG HAS BEEN BRIEFED AND IS WORKING WITH THE NTSB.  (K)                                                         1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20070507000232007050700023SO  2007       5          7          2007FA0000277    220070322G8520A049405N        CRANKSHAFT                                                                 CONT  O360  TSIO360EB   17025SO                              ENGINE          FAILED          B  LU4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO19                                        A049405U                    CRANKSHAFT FAILED NDI SB MSB96-10.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                3  O          E9CE                 
20070409000582007040900058CE  2007       4          9          2007FA0000279    120070228G322045A3952211      UPLOCK                                  BEECH MU300 400A        1155402CE                                                               NLG             OUT OF ADJUST   B  E81RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL03123QS243                    RK486                                   FLIGHT CREW REPORTED RED LANDING GEAR HANDLE WARNING LIGHT STAYING ILLUMINATED AFTER GEAR RETRACTION.  LANDING GEAR CYCLED SEVERAL TIMES, HANDLE WARNING LIGHT STAYED ILLUMINATED.  FOUND NOSE LANDING GEAR UPLOCK NOT FULLY ENGAGING ADJUSTED NOSE LANDING GEAR UPLOCK AS REQUIRED IAW THE MM.  LANDING GEAR RETRACT/ EXTENSION CHECKS OK, NO FAULTS NOTED.  HAVE NOTED THIS FAULT ON LOW TIME AC SEVERAL TIMES, PARTICULARLY DURING COLD WEATHER OPERATION UPLOCK ADJUSTMENT FAULTS USUALLY SHOW UP DURING MM FUNCTIONAL TESTS DURING THE LOW PRESSURE/LOW FLOW TESTS.  (K)                                                                                                                                                                   2H72 4F    RTA16SW                        
20070402001642007040200164    2007       4          2          2007FA0000280    120070312G3230452552          BEARING                                                                                                                                 LANDING GEAR    INACCURATE      D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NE03                                                                    PN 96522-00, CENTERING SPRING ASSY, HAS A ROD END BEARING ON THE END OF THE SHAFT, WHICH BOLTS TO THE IMOVABLE PORTION OF THE NOSE GEAR.  ORIGINAL ROD END BEARING IS .375 INCH THICK WHERE BOLT GOES THRU.  NEW ROD END BEARING THAT COMES WITH PN 96522-00 ASSY, IS .433 INCH THICK AND RELOCATES CLEVIS BOLT PN AN24-20A .0625 INCH DOWNWARD (UNFAVORABLE) AND CONTRADICTS REQUIREMENTS OF MFG MSB 893.  (K)                                                                                                                                                                                                                                                                                                                                                                           
20070504001622007050400162CE  2007       5          4          2007FA0000284    120070317G5740NAS1738B        ATTACH FITTING                          BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE                              WING            LOOSE           B  KX5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL151525C5500                   FL88                                    MANY OF THE BLIND RIVETS, PN NAS1738B6, ATTACHING THE WING SKIN TO THE LOWER FORWARD WING ATTACHMENT FITTING WERE FOUND TO BE LOOSE.  CONDITION EXISTED ON BOTH WINGS.  CONDITION ALSO FOUND ON AC SN FL59 (8100 HRS).  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4T4  T  A24CE   E4EA                 
20070504002052007050400205GL  2007       5          4          2007FA0000285    220070319G732323065121        GOVERNOR                                HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              ENGINE          FROZEN          B  EOORK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03CGPHC     293               180257D                                 DURING AN INSPECTION IT WAS NOTED THAT THE BEAING RETAINING WASHER FOR THE ROD END WAS INCORRECT.  AFTER THE BOLT WAS REMOVED IT WAS THEN DISCOVERED THAT THE THROTTLE ARM WAS SEIZED UP ON THE GOVERNOR, REPLACED GOVERNOR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3U3  U  H3WE    E4CE                 
20070402001592007040200159GL  2007       4          2          2007FA0000286    120070322G712011925003        MOUNT                                   CIRRUSSR    SR20        05628AJGL                                                               ENGINE          BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO11155CD2058                   1058                                    ENGINE MOUNT RT FRONT CROSSOVER TUBE BETWEEN LT AND RT ENGINE SUPPORTS FOUND BROKEN AT THE WELD RT SIDE.  ENGINE WAS CHANGED ABOUT 250 HRS AGO, NO MENTION OF ENGINE MOUNT DAMAGE.  COULD HAVE BEEN A HARD LANDING, BUT NO OTHER SIGNS WERE NOTED.  CONTACT WITH MFG SAYS NO OTHER REPORTS HAVE BEEN FILLED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O    NTA00009CH                     
20070402001662007040200166SW  2007       4          2          2007FA0000287    120070322G7110                RIVET                                   MOONEYM20   M20J        5870219SW  LYC   O360  IO360A1A    41514EA                              COWLING         CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO119156X                       243253                                  OWNER BROUGHT COWLINGS IN FOR REPAIR BECAUSE THE THROUGH SKIN RIVETS WERE CORRODING AND SHEARING OFF AT THE MFG HEAD AS EXHIBITED BY BLISTERING PAINT AT THE RIVET LOCATIONS.  INSPECTION REVEALED MOST OF THE AD TYPE RIVETS WERE SEVERELY CORRODED BECAUSE THE COWLINGS WERE CONSTRUCTED WITH A HYBRID COMPOSITE LAMINATE OF E-GLASS AND CARBON GRAPHITE PLIES.  IT IS STANDARD INDUSTRY PRACTICE TO USE CORROSION RESISTANT FASTENERS SUCH AS RIVETS THROUGH CARBON GRAPHITE STRUCTURE AND IT IS UNKNOWN WHY ALUMINUM RIVETS ARE USED IN THIS CASE.  AFFECTED AREAS: UPPER COWL/ OIL DOOR CUTOUT DOUBLER RIVETS COOLING AIR INLET AFT EDGE RIVETS.  LOWER COWL/ BOTH UPPER CAMLOCK RECEPTACLE GANG STRIPS (SEVERELY CORRODED AND CONCEALED BY1L71 3O3  O  2A3     1E10                 
20070403000322007040300032SO  2007       4          3          2007FA0000288    120070402G532137829007        FLOOR PANEL                             PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360RB   17025CE                              FUSELAGE        DEBONDED        D  IBIRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA27682JK968                    3449154     322291                      FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM.  THE SEAT MOUNTING BRACKETS ARE BOLTED THRU BOTH SHEETS, BUT THIS STILL MAY BE A STRUCTURE ISSUE.  CALLED MFG FOR GUIDANCE, BUT HAVE NOT HEARD ANYTHING AS YET.                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A7SO    E9CE                 
20070403000332007040300033SO  2007       4          3          2007FA0000289    120070402G532137829007        FLOOR PANEL                             PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360RB   17025CE                              ZONE 100        DEBONDED        D  IBIRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA27682JK968                    3449154     322291                      FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING.  THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM.  THE SEAT MOUNTING BRACKETS ARE BOLTED THRU BOTH SHEETS, BUT THIS STILL MAY BE A STRUCTURE ISSUE.  CALLED MFG FOR GUIDANCE, BUT HAVE NOT HEARD ANYTHING AS YET.                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A7SO    E9CE                 
20070403000342007040300034SO  2007       4          3          2007FA0000290    120070402G532137829007        FLOOR PANEL                             PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360RB   17025CE                              ZONE 100        DEBONDED        D  IBIRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA27682JK968                    3449154     322291                      FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM.  THE SEAT MOUNTING BRACKETS ARE BOLTED THRU BOTH SHEETS, BUT THIS STILL MAY BE A STRUCTURE ISSUE.  HAVE CALLED MFG FOR GUIDANCE, BUT HAVE NOT HEARD ANYTHING AS YET.                                                                                                                                                                                                                                                                                                                                                 1L72 3O3  O  A7SO    E9CE                 
20070403000352007040300035SO  2007       4          3          2007FA0000291    120070402G532137829007        FLOOR PANEL                             PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360RB   17025CE                              ZONE 100        DEBONDED        D  IBIRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA27682JK968                    3449154     322291                      FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING.  THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM.  THE SEAT MOUNTING BRACKETS ARE BOLTED THRU BOTH SHEETS, BUT THIS STILL MAY BE A STRUCTURE ISSUE.  HAVE CALLED MFG FOR GUIDANCE, BUT HAVE NOT HEARD ANYTHING AS YET.                                                                                                                                                                                                                                                                                                                                                1L72 3O3  O  A7SO    E9CE                 
20070403000362007040300036SO  2007       4          3          2007FA0000292    120070402G532137829007        FLOOR PANEL                             PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360RB   17025CE                              ZONE 100        DEBONDED        D  IBIRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA21682JK968                    3449154     322291                      FLOORPANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING.  THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED THRU BOTH SHEETS, BUT THIS STILL MAY BE A STRUCTURE ISSUE.  HAVE CALLED MFG FOR GUIDANCE, BUT HAVE NOT HEARD ANYTHING AS YET.                                                                                                                                                                                                                                                                                                                                                  1L72 3O3  O  A7SO    E9CE                 
20070504001352007050400135CE  2007       5          4          2007FA0000293    120070322G7830                LINK                                    CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              THRUST REVERSER CORRODED        D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL15413LC6894                   5600003     PCE108003                   ALL DRIVE LINK PIVOT BOLTS AND OVER CENTER LINKS SEVERELY CORRODED AND WORN.  PROBABLE CAUSE IS INADEQUATE LUBE.  MANUAL STATES TR`S MUST BE TORN DOWN AND LUBED UPON ASSEMBLY AT SPECIFIC INTERVALS.  ENGINEERING STATES THAT TEARDOWN IS NOT NECESSARY AND ON WING LUBRICATION IS ADEQUATE.  THESE FINDINGS INDICATE OTHERWISE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA22CE   E25EA                
20070504001412007050400141CE  2007       5          4          2007FA0000294    120070222G36101H1069          MIXING VALVE                            LEAR  60    60LEAR      5170707CE  PWA   305   PW305            NE                              LT ENGINE       INTERMITTENT    C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL11500  83                     306                                     SHORTLY AFTER TAKEOFF, AIRCRAFT (LT BLEED AIR) WARNING ILLUMINATED, AND (RT BLEED AIR) WARNING ILLUMINATED APPROX 5 SEC LATER, SMELLED ODOR IN MAINTENANCE.  UNABLE TO DUPLICATE MALFUNCTION ON GROUND RUN; LT MIXING VALVE WAS SUSPECTED, SO REPLACED.  PERFORMED GROUND RUN FUNCTIONAL TEST OF BLEED AIR SYSTEM, AND FLIGHT TEST.  NO FURTHER BLEED AIR WARNINGS.  (K)                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA10CE   E35NE                
20070406001602007040600160CE  2007       4          6          2007FA0000295    120070320G8120                BEARING                                 CESSNA414   414A        2075907CE  CONT  O520  TSIO520*    17040SO                              TURBOCHARGER    WORN            D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL133247M1031       FKL00044    414A0828                                FAILURE OF RT TURBOCHARGER SEAL AND CENTER BEARING CAUSED SMOKE OUT OF EXHAUST AND SQUEALING NOISE RESULTING IN THE FLIGHT CREW TO FEATHER PROPELLER AND SHUTDOWN THE ENGINE.  CAUSE OF FAILURE DO TO WEAR. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 3O3  O  A7CE    E8CE                 
20070409000082007040900008SW  2007       4          9          2007FA0000297    120070305G6410HAC473          BLADE                                   BELL  47    47G5        1181032SW  LYC   O435  VO435*      41516EA                              TAIL ROTOR      DAMAGED         B  ECGRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA131202W                       7857                                    THE STAINLESS STEEL ABRASION STRIP ON THE LEADING EDGE OF THE COMPOSITE TAIL ROTOR BLADE SEPARATED FROM BLADE IN FLIGHT.  PILOT NOTED A VIBRATION IN A SPRAY TURN AND ELECTED TO LAND; AND LANDED SAFELY (NO INJURIES).                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3O3  O  2H3     E279                 
20070504001452007050400145SO  2007       5          4          2007FA0000298    120070320G2400100201021346    INVERTER                                GULSTMGVSP  GVSPG550    3980203SO  GE    CF34  CF343A      30066NE                                              SHORTED         D      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      NRNOT REPORTED   1                      GL055PG  1383                   5046                                    WHEN TURNING MAIN BATTERY SWITCHES ON, MECHANIC HEARD A LOUD POPPING SOUND, FOLLOWED BY THE AROMA OF SMOKE IN THE ENTRANCE AREA OF THE AIRCRAFT.  THE FLOORBOARD WAS REMOVED AND FOUND THAT WATER FROM THE FORWARD LAVATORY AREA HAD BEEN RUNNING ONTO THE TOP OF THE EMERGENCY INVERTER CAUSING H2O AND AC VOLTAGE TO MEET (H2O WON).  THE LAV AREA ON BOTH OF OUR AC WERE INSPECTED FOR LEAKS AND FOUND AREAS WHERE WATER HAD BEEN SITTING, EVEN THROUGH THERE WERE NO LEAKS.  IT IS POSSIBLE THAT WHEN STOWING THE SINK (HINGED AND FOLDS UP INTO A CLOSEOUT) RESIDULE WATER IS DUMPING INTO THE CLOSEOUT.  THE INVERTER WAS REPLACED AND WE SHUT THE WATER SUPPLY OFF FOR THE FORWARD LAY SINK ON BOTH.  THERE IS NO PREFLIGHT OR SCHEDULED 2L72 4F4  FRTA12EA   E15NE                
20070504001482007050400148CE  2007       5          4          2007FA0000299    120070326G2820050011849       LINE                                    CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              FUEL SYSTEM     CHAFED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA232470N400                    172S10070                               FOUND FUEL LINE PN 05001( 8-49, FUEL RETURN  LINE TO RESERVOIR WORN BY RUBBING ON NOSE STEERING ROD JUST BEHIND FIREWALL.  INSTALLED NEW LINE SO AS NOT TO RUB ON STEERING.  INSTALLED SPIRAL WRAP ON AREA WHERE RUBBING HAD OCCURRED.  NOTE: FUEL LINE WAS WORN TO POINT OF LEAKING.  RECOMMEND INSPECTING NEW AC FOR PROPER LINE INSTALLATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O3  ONT3A12    1E10                 
20070504001442007050400144CE  2007       5          4          2007FA0000300    120070327G324016011800        HOUSING         CLEVELAND               CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  BRAKE CALIPER   DEFECTIVE       D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP21PKMPS           017         208B0656    PCEPC0548   001276          THE MAIN CASTING, WHICH HOUSES THE BRAKE CALIPER PISTONS LEAKS FLUID UNDER NORMAL BRAKING PRESSURE.  THE LEAKS ARE FROM EXCESSIVE POROSITY IN THE CASTING.  CASTING  THIS IS THE SECOND OCCURRENCE IN OUR OPERATIONS.  THE FIRST WAS NOT REPORTED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20070406001632007040600163CE  2007       4          6          2007FA0000301    120070406G1400                NUT                                     CESSNA172   172S        2072439CE  LYC   O360  IO360A1A    41514EA                                              MISMANUFACTURED B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA07949SP                       172S8145                                WHILE INSTALLING KIT MK172-25-10C TO COMPLY WITH SB 04-25-01 R4 AND AD 2007-05-10, ONE OF THE PARTS IN THE KIT WAS MACHINED IMPROPERLY. THE HEIGHT ADJUSTING NUT HAD THE THRU HOLE FOR THE ULTRALOC WITH MIS FORMED THREADS. THE MINOR DIAMETER OF THE THREAD WAS GREATER THAN THE MAJOR DIAMETER OF THE THREADS ON THE ULTRALOC. THE CROSS HOLE FOR MOUNTING WAS INCORRECTLY LOCATED WITH INSUFFICIENT EDGE DISTANCE, AND THE PILOT HOLE WAS OFFSET GIVING AN EGG SHAPED HOLE.                                                                                                                                                                                                                                                                 1H71 3O3  ONT3A12    1E10                 
20070409000362007040900036CE  2007       4          9          2007FA0000302    120070403G273165651412        ACTUATOR                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              ELEVATOR TRIM   BINDING         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW135314J5592 300               5500663                                 AFTER A PHASE 1-4 INSPECTION THE ELEVATOR TRIM WAS FOUND TO BE BINDING. INSPECTION OF THIS SYSTEM FOUND THAT THE WILKIE BUTTON IN THE BACK OF THE ACTUATOR TRIM JACK SCREWS HAD COME OUT AND WAS BINDING THE TRIM CHAIN AND SPROCKETS. WHEN THE ACTUATORS ARE LUBED THE WILKIE BUTTONS HAVE A TENDENCY TO POP OUT OF THERE PLACE IF YOU DONT LOOK CLOSELY AFTER LUBING THESE ACTUATORS THE GREASE PUSHES THESE PLUGS OUT AND THEY STICK TO THE INTERCONNECT CHAIN CAUSING A BINDING CONDITION. THIS COULD ALSO HAPPEN IN FLIGHT CAUSING A LIKE CONDITION WITH MORE DIRE PROBLEMS. I THINK MFG SHOULD REMOVE THIS PLUG OR MORE SECURELY FIX THIS PLUG IN PLACE.                                                                                  1L72 4F4  F  A22CE   E1NE                 
20070409000372007040900037CE  2007       4          9          2007FA0000303    120070403G273165651412        ACTUATOR                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              ZONE 200        BINDING         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW135314J5592 300               5500663                                 AFTER A PHASE 1-4 INSPECTION THE ELEVATOR TRIM WAS FOUND TO BE BINDING. INSPECTION OF THIS SYSTEM FOUND THAT THE WILKIE BUTTON IN THE BACK OF THE ACTUATOR TRIM JACK SCREWS HAD COME OUT AND WAS BINDING THE TRIM CHAIN AND SPROCKETS. WHEN THE ACTUATORS ARE LUBED THE WILKIE BUTTONS HAVE A TENDENCY TO POP OUT OF THERE PLACE IF YOU DONT LOOK CLOSELY AFTER LUBING THESE ACTUATORS THE GREASE PUSHES THESE PLUGS OUT AND THEY STICK TO THE INTERCONNECT CHAIN CAUSING A BINDING CONDITION. THIS COULD ALSO HAPPEN IN FLIGHT CAUSING A LIKE CONDITION WITH MORE DIRE PROBLEMS. I THINK MFG SHOULD REMOVE THIS PLUG OR MORE SECURELY FIX THIS PLUG IN PLACE.                                                                                  1L72 4F4  F  A22CE   E1NE                 
20070409000202007040900020CE  2007       4          9          2007FA0000308    120070402G3211508103437       PIN                                     BEECH 200   B200        1152922CE                                                               LT MLG          BROKEN          E      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      SW0565TW 6551 6551              BB902                                   UPON EXTENDING THE LANDING GEAR, THE PILOTS GOT A RED GEAR UNSAFE LIGHT IN THE HANDLE, AND THE LT DOWN AND LOCKED LIGHT WAS NOT LIT UP. THE PILOTS TRIED TO EXTEND THE GEAR MANUALLY, BUT THE HANDLE WOULD NOT EXTEND THE GEAR ANY FURTHER, THE PILOTS RETRACTED THE GEAR AND THE RED LIGHT STAYED ILLUMINATED, THE GEAR WAS EXTENDED AGAIN, STILL THE LT DOWN AND LOCKED LIGHT WAS OFF AND THE RED LIGHT IN THE HANDLE WAS ON. THE PILOTS DECLARED AN EMERGENCY AND LANDED THE AIRCRAFT, WITH NO OTHER EVENTS. THE AIRCRAFT WAS JACKED UP, AND THE LANDING GEAR WAS INSPECTED. THE LT MAIN DOWN LOCKING ASSY PIN WAS FOUND TO BE BROKEN AND HANGING OUT OF THE LOCK HOLES, PREVENTING THE GEAR FROM FULLY EXTENDING AND RETRACTING. THE PIN WAS1L72 4T      A24CE                        
20070409000212007040900021CE  2007       4          9          2007FA0000309    120070402G3210508103437       PIN                                     BEECH 200   B200        1152922CE                                                               ZONE 700        BROKEN          E      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      SW0565TW 6551 6551              BB902                                   UPON EXTENDING THE LANDING GEAR, THE PILOTS GOT A RED GEAR UNSAFE LIGHT IN THE HANDLE, AND THE LT DOWN AND LOCKED LIGHT WAS NOT LIT UP. THE PILOTS TRIED TO EXTEND THE GEAR MANUALLY, BUT THE HANDLE WOULD NOT EXTEND THE GEAR ANY FURTHER, THE PILOTS RETRACTED THE GEAR AND THE RED LIGHT STAYED ILLUMINATED, THE GEAR WAS EXTENDED AGAIN, STILL THE LT DOWN AND LOCKED LIGHT WAS OFF AND THE RED LIGHT IN THE HANDLE WAS ON. THE PILOTS DECLARED AN EMERGENCY AND LANDED THE AIRCRAFT, WITH NO OTHER EVENTS. THE AIRCRAFT WAS JACKED UP, AND THE LANDING GEAR WAS INSPECTED. THE LT MAIN DOWN LOCKING ASSY PIN WAS FOUND TO BE BROKEN AND HANGING OUT OF THE LOCK HOLES, PREVENTING THE GEAR FROM FULLY EXTENDING AND RETRACTING. THE PIN WAS1L72 4T      A24CE                        
20070409000322007040900032CE  2007       4          9          2007FA0000310    120070406G140007900072        NUT                                     CESSNA172   172S        2072439CE  LYC   O360  IO360A1A    41514EA                              KIT             MISMANUFACTURED B      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      EA07949SP                       172S8145                                WHILE INSTALLING KIT MK172-25-10C TO COMPLY WITH SB 04-25-01 R4 AND AD 2007-05-10, ONE OF THE PARTS IN THE KIT WAS MACHINED IMPROPERLY. THE HEIGHT ADJUSTING NUT HAD THE THRU HOLE FOR THE ULTRALOC WITH MALFORMED THREADS. THE MINOR DIAMETER OF THE THREAD WAS GREATER THAN THE MAJOR DIAMETER OF THE THREADS ON THE ULTRALOC. THE CROSS HOLE FOR MOUNTING WAS INCORRECTLY LOCATED WITH INSUFFICIENT EDGE DISTANCE, AND THE PILOT HOLE WAS OFFSET GIVING AN EGG SHAPED HOLE.                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    1E10                 
20070409000222007040900022NE  2007       4          9          2007FA0000311    220070305G7314                REGULATOR                               NAMER T6    AT6D        6400416GL  PWA   R1340 R1340AN1    52016NE  HAMSTD12D   12D40       NE  FUEL PUMP       STUCK           P      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      NM038541B                                                               THE PRESSURE REGULATOR (IN THE WOBBLE PUMP) STUCK IN THE (BYPASS) POSITION CAUSING LOSS OF FUEL PRESSURE AND POWER LOSS DUE TO LACK OF FUEL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3R3  R  A2575   5E2     5  CP257     
20070409000812007040900081WP  2007       4          9          2007FA0000313    220070330G721031030351        BEARING                                                                    GARRTTTPE331TPE33110U   01514WP                              IDLER GEAR      MISINSTALLED    B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      WP07          723                           P44218C                     SUBASSEMBLY BEARINGS TO 2ND IDLER GEAR ASSEMBLED BACKWARDS, CAGE FAILED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               4  T          E4WE                 
20070409000282007040900028CE  2007       4          9          2007FA0000315    120070402G36101H1068          MIXING VALVE                            LEAR  60    60LEAR      5170707CE  PWA   305   PW305            NE                              LT BLEED AIR SYSOUT OF TOLERANCEB      C   ABORTED TAKEOFF                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      TOTAKEOFF        1                      GL09706CR                       168                                     DURING TAKEOFF ROLL CREW EXPERIENCED A RUSH OF WARM OILY SMELLING AIR IN THE COCKPIT. CREW ABORTED TAKEOFF AND RETURNED TO BASE. MAINTENANCE CREW RAN AIRCRAFT AND DUPLICATED PROBLEM FINDING THE DUCT OVRHT LIGHT AND LT BLEED LIGHT ON AT FULL POWER. FURTHER TROUBLESHOOTING FOUND THAT THE LT BLEED AIR MIXING VALVE WAS ALLOWING MORE THAN 200PSI OUT PUT OF AIR. LT BLEED AIR MIXING VALVE WAS REPLACED WITH A SERVICEABLE INSPECTED VALVE AND OPS CHECKED GOOD.                                                                                                                                                                                                                                                                          2L72 4F4  FRTA10CE   E35NE                
20070410000352007041000035    2007       4          10         2007FA0000316    420070406G22000111            TRANSDUCER                              CESSNA180   180         2072602CE                                                               AUTO PILOT      MALFUNCTIONED   D      H   DEACTIVATE SYST/CIRCUITS                                                                        J  WARNING INDICATION                                                            CRCRUISE         1                      WP28     460                                                            ALTITUDE HOLD WAS INOP.  WHEN SELECTED THE A/C WOULD PITCH EITHER UP OR DOWN IMMEDIATELY, OR THE A/C WOULD MAINTAIN ALTITUDE FOR A SHORT TIME AND THEN PITCH IN EITHER DIRECTION. COMPUTER AND PRESSURE TRANSDUCER WERE SENT TO STEC OF TESTING. BOTH UNITS WERE RETURNED AS SERVICEABLE. AFTER INSTALLATION THE PROBLEM WAS STILL THERE. REPLACED THE TRANSDUCER WITH A KNOWN GOOD PART AND PROBLEM WAS SOLVED.  STEC ACTED ASTONISHED THAT THEIR BENCH CHECK WOULD NOT FIND THE PROBLEM!                                                                                                                                                                                                                                                      1H71 3O    NC5A6                          
20070410000362007041000036    2007       4          10         2007FA0000317    420070406G22000111            TRANSDUCER      STEC                    CESSNA180   180         2072602CE                                                               AUTO PILOT      MALFUNCTIONED   D      H   DEACTIVATE SYST/CIRCUITS                                                                        O  OTHER                                                                         CRCRUISE         1                      WP28     460                                                            ALTITUDE HOLD WAS INOPERATIVE.  WHEN SELECTED THE A/C WOULD PITCH EITHER UP OR DOWN IMMEDIATELY, OR THE A/C WOULD MAINTAIN ALTITUDE FOR A SHORT TIME AND THEN PITCH IN EITHER DIRECTION. COMPUTER AND PRESSURE TRANSDUCER WERE SENT TO STEC FOR TESTING. BOTH UNITS WERE RETURNED AS SERVICEABLE. AFTER INSTALLATION THE PROBLEM WAS STILL THERE. REPLACED THE TRANSDUCER WITH A KNOWN GOOD PART AND PROBLEM WAS SOLVED.STEC ACTED ASTONISHED THAT THEIR BENCH CHECK WOULDN'T FIND THE PROBLEM!                                                                                                                                                                                                                                                 1H71 3O    NC5A6                          
20070410000372007041000037    2007       4          10         2007FA0000318    420070406G22150111            TRANSDUCER      STEC                    CESSNA180   180         2072602CE                                                               ZONE 200        MALFUNCTIONED   D      H   DEACTIVATE SYST/CIRCUITS                                                                        O  OTHER                                                                         CRCRUISE         1                      WP28     460                                                            ALTITUDE HOLD WAS INOP.  WHEN SELECTED THE A/C WOULD PITCH EITHER UP OR DOWN IMEDIATLEY, OR THE A/C WOULD MAINTAIN ALTITUDE FOR A SHORT TIME AND THEN PITCH IN EITHER DIRECTION. COMPUTER AND PRESSURE TRANSDUCER WERE SENT TO STEC FO TESTING. BOTH UNITS WERE RETURNED AS SERVICEABLE. AFTER INSTALLATION THE PROBLEM WAS STILL THERE. REPLACED THE TRANSDUCER WITH A KNOWN GOOD PART AND PROBLEM WAS SOLVED.STEC ACTED ASTONISHED THAT THEIR BENCH CHECK WOULDN'T FIND THE PROBLEM!                                                                                                                                                                                                                                                          1H71 3O    NC5A6                          
20070410000382007041000038    2007       4          10         2007FA0000319    420070406G22150111            TRANSDUCER      STEC                    CESSNA180   180         2072602CE                                                               ZONE 200        MALFUNCTIONED   D      H   DEACTIVATE SYST/CIRCUITS                                                                        O  OTHER                                                                         CRCRUISE         1                      WP28     460                                                            ALTITUDE HOLD WAS INOPERATIVE.  WHEN SELECTED THE A/C WOULD PITCH EITHER UP OR DOWN IMMEDIATELY, OR THE A/C WOULD MAINTAIN ALTITUDE FOR A SHORT TIME AND THEN PITCH IN EITHER DIRECTION. COMPUTER AND PRESSURE TRANSDUCER WERE SENT TO STEC FOR TESTING. BOTH UNITS WERE RETURNED AS SERVICEABLE. AFTER INSTALLATION THE PROBLEM WAS STILL THERE. REPLACED THE TRANSDUCER WITH A KNOWN GOOD PART AND PROBLEM WAS SOLVED.STEC ACTED ASTONISHED THAT THEIR BENCH CHECK WOULDN'T FIND THE PROBLEM!                                                                                                                                                                                                                                                 1H71 3O    NC5A6                          
20070504001552007050400155GL  2007       5          4          2007FA0000321    220070401G74126870885         EXCITER                                 HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              ENGINE          INOPERATIVE     B  EOORO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL03CGBUY                       6109580     CAE833577                   PILOT WENT TO START THE AIRCRAFT AND THERE WAS NO IGNITION.  FOUND IGNITION EXCITER INOPERATIVE, REPLACED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3U3  U  H3WE    E4CE                 
20070504001522007050400152SO  2007       5          4          2007FA0000322    120070330G5730427             SKIN                                    GULSTMG1159 G1159A      3970109SO  RROYCESPEY  SPEY511*    54523EU                              RT WING         CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW05300WY                       427                                     DURING A WING NDT INSPECTION OF THE UPPER RT WING PLANK AT FS 452 AND BL 33, CORROSION WAS NOTED IN THIS AREA.  ENGINEERING HAS DETERMINED THIS CORROSION IS EXCESSIVE ENOUGH TO REQUIRE ACCOMPLISHMENT OF ASC 229, WHICH REMOVES THE CORROSION ON THE PLANK AND INSTALLS A DOUBLER PLATE AND A NEW STYLE WING ATTACH PIN AS A CORRECTIVE ACTION.  (K)                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  F  A12EA   E2EU                 
20070507000062007050700006SO  2007       5          7          2007FA0000323    120070301G322095829000        DRAG LINK                               PIPER PA34  PA34200     7103405SO  LYC   O360  IO360A1A    41514EA                              NLG             JAMMED          G  R2LSO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO1515338                       347350051                               THE NOSE GEAR LINK ASSEMBLY JAMS INTERMITTENTLY, KEEPING THE FWD AND AFT NOSE GEAR DRAG LINKS FROM LOCKING COMPLETELY.  REFER TO SB NR 1123B.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 3O3  O  A7SO    1E10                 
20070504001402007050400140GL  2007       5          4          2007FA0000324    120070317G3240                PLATE                                   TCRAFTBC    BC12D       8850316GL  CONT  O200  O200A       17020SO  MCAULY1A100 1A100*      GL  LT BRAKE        LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL15433361669                   6995        666377A     G1885           WHEN BRAKES WERE APPLIED AFTER LANDING.  IT APPEARS THAT THE PINS HOLD THE BACK PLATE ALLOW IT TO SHIFT ENOUGH TO HAVE POSSIBLY MADE CONTACT WITH THE BRAKE ACCUATOR ARM AND NOT ALLOW IT TO RELEASE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  O  A696    E252    5  NP918     
20070425002632007042500263CE  2007       4          25         2007FA0000325    120070325G7810                EXHAUST PIPE                            CESSNA182   182A        2072704CE  CONT  O470  O470*       17026SO  MCAULY2A34C 2A34C203    GL  RT EXHAUST      BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE035848B                       33848       668686L     891146          RT EXHAUST BROKE AT ELBOW, PART HAD BEEN REPAIRED 544 HRS AGO.  DID NOT SHOW ANY CRACK 50 HRS EARLIER.  DO NOT REPAIR EXHAUST PARTS THAT HAVE 1000 HRS ON THEM.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A13    E273    5  CP3EA     
20070425002552007042500255EU  2007       4          25         2007FA0000328    120070406G5554T700A5340023100 FITTING                                 SOCATATBM   TBM700      8682000EU  PWA   PT6   PT6A64           EA  HARTZLHCE4N HCE4N3      NE  RUDDER          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA05704QD                       188         PCEPM0073   HH463           DURING A 6000HR/10 YEAR CORROSION INSPECTION AD2007-06-11 WAS BEING COMPLIED IAW AD AND MANDATORY SB70-=104, AMENDMENT 2.  AFTER COMPLETING THE PENETRANT INSPECTION NO CRACKS WERE DETECTED IN THE SPECIFIED AREAS HOWEVER THE FITTINGS LISTED IN BLOCK 5 WERE REMOVED FROM SERVICE FOR LIGHT PITTING CORROSION.  RECENTLY IN OUR FACILITY, THERE WAS A LEVEL 3 NDT RECURRENT COURSE BEING GIVEN AND THE REMOVED FITTINGS WERE CRACK CHECKED USING A ROTARY TOOL FOR BOLT HOLE EDDY CURRENT SET UP ON .030 CORNER EDM NOTCH AS A REFERENCE STANDARD.  AT THIS TIME THERE WERE CORROSION PITTING CRACKS DETECTED IN BOTH FITTINGS.  THE INSPECTION CRITERIA STATED IN AD AND SB ARE INSUFFICIENT FOR CRACK DETECTION IN THIS AREA.  POSSIBLY THE1L71 3T4  TRTA60EU   E4EA    5  CP10NE    
20070504001682007050400168EU  2007       5          4          2007FA0000329    120070406G5510T700A5530072102 FITTING                                 SOCATATBM   TBM700      8682000EU  PWA   PT6   PT6A64           EA  HARTZLHCE4N HCE4N3      NE  STABILIZER      CORRODED        D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA05704QD5980                   188         PCEPM0073   HH463           DURING A 6000HR/10 YEAR CORROSION INSPECTION AD2007-06-11 WAS BEING COMPLIED IAW AD AND MANDATORY SB70-104, AMENDMENT 2.  AFTER COMPLETING THE PENETRANT INSPECTION, NO CRACKS WERE DETECTED IN THE SPECIFIED AREAS HOWEVER THE FITTINGS LISTED IN BLOCK 5 WERE REMOVED FROM SERVICE FOR LIGHT PITTING CORROSION.  RECENTLY IN OUR FACILITY, THERE WAS A LEVEL 3 NDT RECURRENT COURSE BEING GIVEN AND THE REMOVED FITTINGS WERE CRACK CHECKED USING A ROTARY TOOL FOR BOLT HOLE EDDY CURRENT SET UP ON /030 CORNER EDM NOTCH AS A REFERENCE STANDARD.  AT THIS TIME THERE WERE CORROSION PITTING CRACKS DETECTED IN BOTH FITTINGS.  THE INSPECTION CRITERIA STATED IN AD AND SB ARE INSUFFICIENT FOR CRACK DETECTION IN THIS AREA.  POSSIBLY THE1L71 3T4  TRTA60EU   E4EA    5  CP10NE    
20070504001712007050400171GL  2007       5          4          2007FA0000330    220070403G724023031260        COMBUSTION CASE                         HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              ENGINE          CRACKED         B  EOORO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL03CGPHC                       180257D     CAE831562                   PILOT NOTICED CRACK IN COMBUSTION CAN ON PREFLIGHT CHECK REPLACED UNIT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3U3  U  H3WE    E4CE                 
20070504001902007050400190SO  2007       5          4          2007FA0000331    220070404G7200629340          ROD BOLT                                CESSNA310   310R        2074245CE  CONT  O520  IO520MB     17032SO                              LT ENGINE       BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL232641D740                    310R1678    829015R                     PRELIMINARY INSPECTION FINDINGS:  IN FLIGHT, LT ENGINE FAILURE ON CLIMB OUT.  LT ENGINE HAD 737.1 HOURS AND PUT IN SERVICE 05/2003.  LARGE HOLE IN CASE AROUND NR 5 AND 6 CYLINDER.  NR 5 ROD SEPARATED FROM CRANK AND BROKEN IN TWO PIECES A FEW INCHES FROM PISTON PIN.  SUBSEQUENT FINDINGS FROM ENGINE TEARDOWN REPORT PERFORMED BY MFG.  THE SIGNATURES PRESENT ON THE NR 5 CYLINDER BORE AND THE DAMAGE TO THE NR 5 CONNECTING ROD ARE CONSISTENT WITH A HYDROSTATIC LOCK EVENT.  PRELIMINARY INFORMATION WAS BASED ON A SB CE-00-07, AND SDR REPORTS ISSUED BETWEEN 1995 AND PRESENT, ON SAME MODEL ENGINE WITH SIMILAR BOLT FAILURES.  (K)                                                                                              1L72 3O3  O  3A10    E5CE                 
20070504001982007050400198SO  2007       5          4          2007FA0000332    220070401G8500                SNAP RING                               CESSNA180   180A        2072604CE  CONT  O470  IO470*      17026SO                              ENGINE          MISMANUFACTURED D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL034145                        32840       CS76646PF                   SNAP RING USED TO RETAIN PLATE PN 643629 AND COUNTERWEIGHT PIN 643626-101 WAS BEING INSTALLED IN COUNTERWEIGHT.  UPON INSTALLING, THE LAST SNAP RING, IT WAS NOTICED THAT THE SNAP RING DID NOT HAVE ANY RETAINING PROPERTIES.  IT LACKED TEMPER TO SPRING BACK AND COULD BE FORMED INTO ANY POSITION WHICH COULD HAVE ALLOWED THE PLATE AND PIN TO FALL OUT OF THE COUNTERWEIGHT CAUSING ENGINE FAILURE..  THE SNAP RING WAS PURCHASED ON 12 MARCH, 2007.  THE BATCH NR LISTED FOR THE SNAP RING WAS 0000070137 UNDER API`S PO NR 4500018586.  (K)                                                                                                                                                                                             1H71 3O3  O  5A6     E1CE                 
20070504001372007050400137EA  2007       5          4          2007FA0000333    220070406G8530LW15014         ROCKER                                  CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA                              ENGINE CYLINDER BROKEN          B  YYBRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL032994E                       17271398    L717976T                    THE STAMPED EXHAUST STEEL ROCKER ARM WAS FOUND BROKEN THROUGH AT PUSH ROD, AND THE INTAKE ROCKER ARM WAS CRACKED, AND THE PUSH ROD WAS BENT BADLY.  THE ENGINE HAD 120 HR TSO AND NEW FACTORY CYLIDERS WERE INSTALLED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  ONT3A12    E274                 
20070425002582007042500258CE  2007       4          25         2007FA0000334    120070402G531207126161        BULKHEAD                                CESSNA182   182L        2072726CE  CONT  O470  O470*       17026SO                              FUSELAGE        CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP09420534571                   18258832                                SMALL CRACK AT RUDDER CABLE CUTOUT IB, APPROX .2500 INCH, NO CAUSE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A13    E273                 
20070425002572007042500257EA  2007       4          25         2007FA0000335    220070417G7414                SPRING          SLICK                   PIPER PA28  PA28181     7102807SO  LYC   O360  O360A4M     41514EA                              IMPULSE COUPLINGBROKEN          D      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          TXTAXI/GRND HDL  1                      NE05     1603 38                                                        PILOT STARTED AIRCRAFT NORMALLY AND DID RUN UP WITH A BAD MAGNETO CHECK. PILOT DID NOT FLY AIRCRAFT AND RETURNED TO HANGER. AIRCRAFT WOULD NOT RESTART. IMPULSE COUPLE DID NOT MAKE ANY NOISE, TIMING WAS WAY OFF. FOUND IMPULSE COUPLE SPRING BROKEN A TURN AND A HALF FROM OUTER END.                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3O3  O  2A13    E286                 
20070425002732007042500273    2007       4          25         2007FA0000336    420070416G23120464105430      RADIO                                   BOLKMS117   BK117A1     5626010EU  LYC   LTS101LTS101650B1 41560NE                              NR 2 COMM       SHORTED         E  BAQRK   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      AAAIR AMBULANCE  1                      EA03952CJ                       S7052                                   WHILE SHUTTING DOWN AIRCRAFT THE CREW NOTED A WHIFF OF SMOKE AND ELECTRICAL SMELL IN THE COCKPIT.  FOUND THE NR (2) COMM RADIO INTERNALLY SHORTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1G72 3U3  U  H13EU   E5NE                 
20070425002472007042500247GL  2007       4          25         2007FA0000337    120070418G2710                CONTROL SYSTEM                          CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO                              AILERON SYS     OUT OF RIG      B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA07636ST                       2153                                    DURING INSPECTION, FOUND AILERON RUDDER INTECONNECT OUT OF RIG AND CAUSING INTERFERENCE BETWEEN RUDDER AND AILERON. THIS IS THE FOURTH AIRCRAFT WE'VE FOUND WITH THIS PROBLEM AND ONE ACTUALLY HAD THE RUDDER AND AILERON LOCK IN FULL OPPOSITE DEFLECTIONS JUST PRIOR TO TAKEOFF.                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  ONTA00009CHE3SO                 
20070424000852007042400085GL  2007       4          24         2007FA0000339    120070419G2720                ARM                                     CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO                              RUDDER          MISRIGGED       B  LC1RK   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      EA07927SE                       2238                                    EACH AC THAT CAME INTO THE SHOP WAS INSPECTED FOR THE SAME CONDITION WITH THE AILERON/RUDDER INTERFERENCE. INSPECTION FOUND RUDDER/AILERON INTERCONNECT MISRIGGED RESULTING IN THE BOLT CONNECTING THE BUNGEE TO THE RUDDER/AILERON INTERCONNECT ARM HITTING THE  FORWARD CABLE CLAMP AND DEFLECTING THE RT AILERON CABLE. THE CONTROLS DID NOT LOCK BUT THERE WAS DEFINITE INTERFERENCE. IN THE NEUTRAL POSITION, THE DISTANCE FROM THE C/L OF THE ARM IS SUPPOSED TO BE 4.5 INCHES. ON THIS AIRPLANE IT ABOUT 3.75 INCHES. THERE WAS NO EVIDENCE OF ANYONE MOVING THE CLAMP OR THE CLAMP SLIDING. RECORDS SHOW THAT THERE WAS NO FLIGHT CONTROL RIGGING DONE SINCE THE AIRCRAFT LT THE FACTORY.                                               1L71 3O3  ONTA00009CHE3SO                 
20070424000832007042400083GL  2007       4          24         2007FA0000340    120070419G2720                ARM                                     CIRRUSSR    SR20        05628AJGL  CONT  O550  IO550N      17042SO                              RUDDER          MISRIGGED       B  LC1RD   RETURN TO BLOCK                                                                                 F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      EA07636ST                       1720                                    PILOT WAS TURNING ONTO RUNWAY IN CROSSWIND WITH FULL OPPOSITE AILERON AND RUDDER CONTROLS. CONTROLS LOCKED IN CROSSED POSITION AND WOULD NOT RETURN TO NEUTRAL. PILOT RETURNED TO RAMP. INSPECTION FOUND RUDDER/AILERON INTERCONNECT MISRIGGED RESULTING IN THE BOLT CONNECTING THE BUNGEE TO THE RUDDER/AILERON INTERCONNECT ARM LOCKING OVER THE BOLT GOING THROUGH THE FORWARD CABLE CLAMP. IN THE NEUTRAL POSITION, THE DISTANCE FROM THE C/L OF THE ARM IS SUPPOSED TO BE 4.5 INCHES. ON THIS AIRPLANE IT WAS JUST OVER 3 INCHES. THERE WAS NO EVIDENCE OF ANYONE MOVING THE CLAMP OR THE CLAMP SLIDING. RECORDS SHOW THAT THERE WAS NO FLIGHT CONTROL RIGGING DONE SINCE THE AIRCRAFT LEFT THE FACTORY.                                   1L71 3O3  ONTA00009CHE3SO                 
20070425002462007042500246GL  2007       4          25         2007FA0000341    120070416G2750                RELAY                                   CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO                              T/E FLAP        FAILED          P      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      SW01105SR                       1866                                    DURING A TRAINING FLIGHT, THE FLAPS BECAME STUCK IN THE DOWN POSITION.  THE AIRCRAFT RETURNED TO THE AIRPORT WITHOUT INCIDENT AND THE AIRCRAFT WAS SENT TO MAINTENANCE FOR TROUBLESHOOTING.  MAINTENANCE DISCOVERED THE FLAPS DOWN RELAY FAILED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  ONTA00009CHE3SO                 
20070425002592007042500259SO  2007       4          25         2007FA0000342    220070421G8520655910          CONNECTING ROD  CONT        TSIO520E    CESSNA402   402B        207590PCE  CONT  O520  TSIO520E    17040SO  MCAULY3AF34C3AF34C*     GL  RT ENGINE       FAILED          E      E   ENGINE SHUTDOWN                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      NM058FB             176257      402B1372    176257                      DURING CLIMB AFTER THE POWER HAD BEEN REDUCED FROM THE TAKEOFF SETTING, THE RT ENGINE STARTED TO VIBRATE.  THE PILOT COULD SEE OIL SPLASHING FROM AROUND THE OIL ACCESS DOOR AND RUNNING BACK ON THE TOP COWLING.  THE PILOT SHUTDOWN THE ENGINE AND FEATHERED THE RT PROPELLER.  THE PILOT RETURNED TO THE DEPARTURE AIRPORT AND LANDED WITHOUT FURTHER INCIDENT.  UPON INITIAL INVESTIGATION, A LARGE HOLE WAS FOUND IN THE CRANKCASE ABOVE THE NR 4 ROD JOURNAL.  THE NR 4 CONNECTING ROD WAS SEPARATED FROM THE CRANKSHAFT AND PROTRUDING FROM THE HOLE IN THE CASE.  THE NR 4 CONNECTING ROD CAP WAS ALSO SEPARATED FROM THE CONNECTING ROD AND WAS STICKING UP OUT OF THE HOLE.                                                           1L72 3O3  O  A7CE    E8CE    5  CP22EA    
20070504001462007050400146WP  2007       5          4          2007FA0000343    220070411G726131080261        SCAVENGE PUMP                           CESSNA441   441         2076020CE  GARRTTTPE331TPE33110    01514WP                              LT ENGINE       FLUCTUATES      B      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            NRNOT REPORTED   1                      GL25835MA                       4410343     P77725                      COMMANDED IN-FLIGHT SHUTDOWN OF LT ENGINE DUE TO FLUCTUATING OIL PRESSURE.  UNEVENTFUL SINGLE ENGINE LANDING.  ENGINE LOST OIL.  OIL EXITED ENGINE FROM TURBINE AIR/OIL SEAL AS A RESULT OF TURBINE SCAVENGE PUMP FAILURE.  RECOMMEND COMPLIANCE WITH SB 72-2074R1.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T4  TRTA28CE   E4WE                 
20070504001732007050400173EA  2007       5          4          2007FA0000344    220070323G732025765362        SERVO                                   CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  ENGINE FUEL     WORN            B  HUNRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM019522S1938                   17280432    RL30493351A SF010           PILOT REPORTS THAT ENGINE DIED ON FINAL APPROACH.  ADJUSTED IDLE STOP SLIGHTLY AND MIXTURE SLIGHTLY.  RAN ENGINE AND FOUND THAT SLIGHT ADJUSTMENTS MADE TO FUEL SERVO CREATED LARGE CHANGES IN THE ENGINE OPERATION.  UNABLE TO ADJUST THE FUEL SERVO TO MEET PERFORMANCE REQUIREMENTS STATED IN AD2001-06-17, (D)(2).  THIS IS THE SECOND ATTEMPT TO ADJUST THE FUEL SERVO.  THE FUEL SERVO WAS REMOVED FROM THE AIRCRAFT AND FORWARDED FOR REPAIR UNDER THEIR W/O NR 07-00900.  ORIGINAL FUEL SERVO, PN 25765362, SN 70148401, REINSTALLED ON AC UPON COMPLETION OF REPAIR, WITH REFERENCE TO MM, CHAP 73.  IDLE AND MIXTURE ADJUSTMENT COMPLETED WITH REFERENCE TO MM, CHAP 73.  OPERATIONAL/LEAK CHECK GOOD AT THIS TIME.  (K)              1H71 3O3  ONT3A12    1E10    5  NP857     
20070504002042007050400204    2007       5          4          2007FA0000345    420070117G3417702490031304    ADC                                     LEAR  35    35A         5170602CE  GARRTTTFE731TFE731*     01518WP                              LT AVIONICS BAY MALFUNCTIONED   B      O   OTHER                                                                                           N  FALSE WARNING                                                                 NRNOT REPORTED   1                      GL07700SJ                       082                                     WHILE ENROUTE, THE PILOTS ALTIMETER (FROZE UP) AT ABOUT 8000 FT AND THE OVERSPEED HORN WENT OFF.  THE PILOT RECYCLED THE ADC AND ITS OPERATION WAS RESTORED.  THE ADC WAS TESTED AND NO DEFECTS WERE FOUND.  THERE WAS NO EVIDENCE OF WATER OR MOISTURE IN OR AROUND THE ADC.  THE ADC WAS REPLACED AND TESTED.  THERE HAS BEEN NO PREVIOUS REPORTED FAILURES OF THIS SYSTEM IN THIS AIRCRAFT.  (K)                                                                                                                                                                                                                                                                                                                                             2L72 4F4  F  A10CE   E6WE                 
20070426002672007042600267    2007       4          26         2007FA0000346    420070122G3417702490031304    ADC                                     LEAR  35    35A         5170602CE  GARRTTTFE731TFE731*     01518WP                                              MALFUNCTIONED   B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL07813AS                       167                                     DURING PRE-FLIGHT, THE CREW NOTED THAT THE PILOTS ALTIMETER AND ALTITUDE ALERTER WERE FLAGGED.  ATTEMPTS TO RECYCLE THE SYSTEM WERE NOT SUCCESSFUL.  THE CREW GROUNDED THE AIRCRAFT.   AN AVIONICS TECH WAS DISPATCHED TO THE AIRCRAFTS LOCATION AND DETERMINED THAT THE ADC HAD FAILED.  THE ADC WAS REPLACED.  THE SYSTEM WAS TESTED AND INSPECTED AND FOUND TO COMPLY WITH FAR 91.411, PART 43 AND TO REMAIN RVSM COMPLIANT.  (K)                                                                                                                                                                                                                                                                                                            2L72 4F4  F  A10CE   E6WE                 
20070504001862007050400186CE  2007       5          4          2007FA0000348    120070330G3240                LINE                                    CESSNA170   170B        2072306CE  CONT  C145  C145*       17012SO                              BRAKE           CHAFED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP094696C2611                   25640                                   DURING AN ANNUAL INSPECTION, THE RT BRAKE SUPPLY LINE WAS FOUND CHAFED BY THE ELEVATOR CONTROL CABLE.  THE CHAFING OCCURRED WHEN THE ELEVATOR IS OPERATED NEAR THE (UP) LIMIT OF TRAVEL.  THE LOCATION OF CHAFE IS VIEWED DIRECTLY BELOW THE ELEVATOR TRIM WHEEL, LOOKING SLIGHTLY FORWARD.  THE BRAKE TUBE WAS NOT SUPPORTED BY ANY CLAMPING MEANS TO SECURE THE TUBE.  A REPLACEMENT TUBE WAS FABRICATED AND INSTALLED WITH ADEQUATE CLAMPING TO INSURE NO FURTHER CHAFING ACTION.  THE BRAKE WAS SERVICED AND A SATISFACTORY LEAK CHECK WAS ACCOMPLISHED.  THE ELEVATOR CONTROL CABLE WAS CHECKED FOR DAMAGE AND IS ACCEPTABLE FOR SERVICE.  PHOTOS DETAILING THE CHAFED AREA AND MFG IPC FOR INSTALLATION DETAIL. (K)                       1H71 3O3  O  A799    E253                 
20070504001722007050400172SO  2007       5          4          2007FA0000349    120070401G57533087B           SPAR                                    MAULE M4    M4210C      5460112SO  CONT  IO360 IO360*      17025CE                              RT FLAP         LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP099810M5341                   1020C                                   DURING AN ANNUAL INSPECTION, THE RT FLAP IB HINGE/CONTROL BRACKET WAS FOUND TO BE LOOSE.  FURTHER INSPECTION REVEALED THAT THE FLAP SPAR WAS CRACKED AT THE UPPER RIVET ATTACH POINTS.  THE CRACK IS 3.5 INCH LONG AND EXTENDS PAST THE RIVET HOLES IN BOTH DIRECTIONS.  ADDITIONALLY, BOTH CLOSURE RIBS, AT THEIR ATTACH ANGLES TO THE SPAR.  THE SPAR PN IS 3078B, RIB PNS 3046-2 AND 3046-1, RIVET PNS SS/SS 34D AND SS/SS 32D (MFG SUPPLIED).   THE FLAP SPAR AND RIBS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.  (K)                                                                                                                                                                                                             1H71 3O3  O  3A23    E1CE                 
20070504001492007050400149NE  2007       5          4          2007FA0000350    220070401G72501767M75G03      SHAFT           GE                      BOEING777   777224      1385225NM  GE    GE90  GE9090B          NE                              LPT FAN         UNSERVICEABLE   B  QEMYO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA357801736785      T900253     31679       900238                      AIRCRAFT TAKEOFF WAS ABORTED, A 147 KNOTS AFTER ENGINE LOST POWER.  AC WAS STOPPED SAFELY AND ALL PASSENGERS AND CREW DEPLANED SAFELY.  UPON INSPECTION OF THE ENGINE, THE FAN ROTATED FREELY, BUT THE LPT DID NOT ROTATE.  BS1 OF THE ENGINE SHOWED THAT THE HPT WAS CLEAN, BUT THE LPT WAS HEAVILY DAMAGED.  THE ENGINE WAS SHIPPED TO MFG.  INITIAL INSPECTIONS SHOWED THAT THE FAN MID SHAFT WAS SEPARATED IN THE AXIAL PLANE OF THE HPC S3 DISC.  THE CENTER VENT TUBE WAS SEPARATED IN 3 PLACES ALL AFT OF FMS SEPARATION. AND INVESTIGATION IS ON GOING.  (K)                                                                                                                                                                            2L72 4F4  FRTT00001SEE00049EN             
20070507000512007050700051NE  2007       5          7          2007FA0000351    220070424G8560230319303       THRUST BEARING                                                             LYC   LF507 LF5071F          NE                              SUPERCHARGER    FAILED          B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP07                                        LF07712                     NR 8 THRUST BEARING FAILURE RESULTED IN FAN AND SUPERCHARGER ROTORS TO SHIFT FORWARD CAUSING DAMAGE TO SUPERCHARGER 2ND DISK TO CONTACT THE STATORS MACHINING THROUGH THE 2ND SUPERCHARGER DISK WEB,  RESULTING IN  IN-FLIGHT SHUTDOWN OF NR 1 ENGINE.  OPERATIONAL DESCRIPTION OF EVENT DID NOT INDICATE LOW OIL PRESSURE PRIOR TO THE FAILURE.  WARNING SEQUENCE WAS DESCRIBED AS (1) SMELL IN THE CABIN, HIGH VIBRATIONS WARNING AND VISUAL SPARKES COMING FROM ENGINE, THEN SHUT-DOWN.  BEARING APPEARS TO BE STARVED OF OIL UPON DISASSEMBLY, ALONG WITH VERY LOW OIL CONTENT IN ADJACENT NR 9 BEARING AND PLANETARY REDUCTION GEAR CARRIER.  CURRENTLY INVESTIGATING CAUSE OF OIL STARVATION.  LUBE PUMP IS FROZEN, BUT ENGINE NR 2 AND NR       4  F          E6NE                 
20070501001162007050100116SO  2007       5          1          2007FA0000352    220070424G73223801552         CARBURETOR                                                                 CONT  A65   A65*        17003SO                              ENGINE          MALFUNCTIONED   B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA07                                                                    CARBURETOR WAS SENT IN FOR AN OVERHAUL BECAUSE IT WOULD NOT ACCEPT THROTTLE.  THERE WAS VERY LITTLE TIME ON THE CARBURETOR SINCE IT'S LAST OVERHAUL.  UPON DISASSEMBLY, IT WAS FOUND THAT THE CARBURETOR HAD THE WRONG VENTURI INSTALLED AND THERE WAS OLD CORROSION IN THE FLOAT CHAMBER THAT WAS NOT REMOVED DURING THE PREVIOUS OVERHAUL.  IT HAD THE WRONG SEAT INSTALLED FOR THE TYPE NEEDLE THAT WAS BEING USED.  IT WAS OBVIOUS THAT SOMEONE WHO THOUGHT THEY KNEW CARBURETORS HAD ATTEMPTED TO OVERHAUL THE UNIT UNSUCCESSFULLY.                                                                                                                                                                                                               3  O          E205                 
20070504001992007050400199CE  2007       5          4          2007FA0000354    120070402G2697MS24266R12B12SN CONNECTOR                               BEECH 200   B200        1152922CE  PWA   PT6   PT6*        52043EA                              FIRE DETECTION  CORRODED        D  GONRA   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 NRNOT REPORTED   1                      SW01200VU3534                   BB1393                                  THE AIRCRAFT WAS FLYING THROUGH IMC, WITH ALOT OF RAIN ON THEIR WAY TO DESTINATION.  AS THE CREW WAS LETTING DOWN TO LAND THE LT ENGINE FIRE LIGHT LIT UP.  THE CREW SCANNED ALL THE GAGES, AND DETERMINED THAT THIS WAS A FALSE LIGHT.  THE AC LANDED WITHOUT COMPLICATION.  UPON INSPECTION OF THE LT ENGINE FIRE DETECT SYSTEM, THE TECH FOUND SOME VERY LIGHT CORROSION AND MOISTURE ON THE J102 CONNECTOR PLUG, LOCATED ON THE LT ENGINE FIRE WALL.  THE MOISTURE AND CORROSION WAS REMOVED AND THE FIRE DETECT SYSTEM TESTED PROPERLY, THE AC WAS RETURNED TO SERVICE.  APPLING A THIN COATING OF DC-4 GREASE IN THE CONNECTOR PLUG WOULD PREVENT MOISTURE FROM ENTERING THE PLUG AND THEREFORE KEEP THE CORROSION OUT.  (K)              1L72 4T3  T  A24CE   E2NE                 
20070507000052007050700005CE  2007       5          7          2007FA0000355    120070417G7810265401416       EXHAUST DUCT                            CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL014365U                       208B0253                                CRACKING OCCURRED IN A SHORT TIME SPAN, DURING NORMAL OPERATION.  CRACKS WERE OVER AN AREA APPROX 7 INCHES X 7 INCHES.  ONE PIECE APPROX 3 INCHES X 3 INCHES SEPARATED FROM THE PART.  AFTER CRACKING, DEFORMATION OF LOWER TRAILING EDGE OCCURRED BECAUSE IT WAS NO LONGER RIGID.  IF THIS PROBLEM HAD GONE UNNOTICED, HEAT DAMAGE WOULD PROBABLY HAVE OCCURRED TO ADJACENT PARTS.  MATERIAL OR MFG PROCESS COULD BE SUSPECT.  RECENT MFG BULLETIN CAB 07-2 AFFECTS SOME PRIMARY EXHAUST DUCTS DUE TO IMPROPER MFG, BUT IT DOES NOT APPLY TO THIS ONE.  (MFG HAS BEEN MADE AWARE OF THIS PROBLEM, PART WAS RETURNED TO THEM ON REQUEST FOR EVALUATION).  (K)                                                                                   1H71 3T3  T  A37CE   E4EA                 
20070507001852007050700185SO  2007       5          7          2007FA0000356    220070418G8530FRCN68OACA01    CYLINDER HEAD                           CESSNA182   182A        2072704CE  CONT  O470  O470L       17026SO                              NR 1            SEPARATED       D  FO7RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO135162D145                    51262                                   PERFORMED CYLINDER COMPRESSION TEST AND FOUND NR 1 CYLINDER READING 0 PSI AND FOUND LEAKING AROUND CYLINDER HEAD AND BARREL FINS.  UPON REMOVAL THE HEAD IS COCKED SIDEWAYS ON THE BARREL.  THE HEAD WAS SEPARATING FROM BARREL.  THE CYLINDER PN FRCN68.  OACA/01 CL68 CERMINIL FREEDOM.  CYLINDER ONLY HAD 145.6 HRS TIME IN SERVICE OVERHAUL IN DEC 2003.  (K)                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  ONT3A13    E273                 
20070427000042007042700004CE  2007       4          27         2007FA0000357    120070425G3220                LANDING GEAR                            CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  NOSE            BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      WP09757CM10768                  15279633    RL2072615   770307          NOSE LANDING GEAR BROKE AT HARD NOSE LANDING, NO EVIDENCE OF PREVIOUS CRACKS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A19    E223    5  NP50GL    
20070504001542007050400154CE  2007       5          4          2007FA0000359    120070403G551012320131        FITTING                                 CESSNA207   T207A       2073614CE  CONT  O520  TSIO520M    17040SO  MCAULYD3A34 D3A34C401   GL  STABILIZER      CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP07803AN11657                  20700570    248811R     765815          FWD RT STABILIZER FITTING CRACKED.  FOUND CRACKED FITTING UPON ANNUAL INSPECTION OF EMPENNAGE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  O  A16CE   E8CE    5  CP47GL    
20070504002122007050400212EU  2007       5          4          2007FA0000360    120070407G5340N325400A        BRACKET                                 SNIAS 350   AS350B3     8680954EU                                                               FUSELAGE        BROKEN          B  EOORO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL03C6YPN480                    3688                                    DURING 100 HR INSPECTION, THE MECHANIC REACHED TO UNSCREW THE OIL FILTER AND THE BRACKET BROKE OFF IN HIS HAND.  REPLACED UNIT, THE ENTIRE BREAK LOOKED FRESH EVEN WITH 10X MAGNIFICATION.  IT IS A POT METAL BRACKET.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U      H9EU                         
20070504002292007050400229CE  2007       5          4          2007FA0000361    120070419G2420                COUPLING                                CESSNA150   150M        2071830CE  CONT  O200  O200A       17020SO                              ALTERNATOR      WORN            B  YYBRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL0363332                       15077241    250316                      ALTERNATOR DRIVE COUPLING WAS WORN AND SEVERELY LOOSE WITH EXCESSIVE PLAY DUE TO SOFT, UNDERCUT BUSHINGS PN 632050.  IN ADDITION, THE DRIVE HUB KEY WAY WAS SEVERELY WORN CAUSING EXCESSIVE PLAY OF THE HUB ON THE SHAFT.  CONTINUED OPERATION WOULD RESULT IN DRIVE COUPLING RETAINER PN 352030 FAILING AND POTENTIALLY CAUSING CATASTROPHIC ENGINE FAILURE.  THE CURRENT RUBBER BUSHINGS ARE SOFT AND ALLOW THE DRIVE GEAR TO CRUSH AND DEFORM THEM WHICH REDUCES SHOCK ABSORPTION AND LEADS TO DRIVE COUPLING FAILURE WHEN DRIVE GEAR BEGINS TO CONTACT THE RETAINER CUP DIRECTLY.  THIS IS A RECURRING PROBLEM AS FOUND ON OTHER ALTERNATORS USING THIS TYPE OF DRIVE COUPLING AS LISTED IN SB 95-3B.  (K)                                  1H71 3O3  O  3A19    E252                 
20070504002252007050400225CE  2007       5          4          2007FA0000362    120070419G291098811281        POWERPACK                               CESSNA172   172RG       2072438CE  LYC   O360  O360*       41514EA                              HYD SYSTEM      MISREPAIRED     D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW03413EB                       172RG0113                               INSTALLED A NEWLY OVERHAULED COMPLETE HYDRAULIC POWER PACK UNIT AS RECEIVED.  AFTER INSTALLING THE UNIT IN THE AIRCRAFT AND PERFORMING A RETRACT TEST THE NEW OVERHAULED GEAR MOTOR WAS JERKY AND ACTING LIKE IT WAS SHORTING OUT.  REMOVED MOTOR AND INSTALLED ANOTHER NEW OVERHAULED MOTOR AND SYSTEM WORKED FINE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  O  3A17    E286                 
20070504002332007050400233CE  2007       5          4          2007FA0000363    120070411G321005412024        BUSHING                                 CESSNA172   172S        2072439CE  LYC   O360  IO360A1A    41514EA                              RMLG            UNSERVICEABLE   B  NU7RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL13106RA3586                   172S8241                                BUSHING LINER SEPARATED FROM METAL SHELL, SLID OUT OF SHELL CAUSING AC TO LEAN RT WING TIP LOW.  BETTER BONDING ADHESIVE FOR LINER TO SHELL.  NEED TO GO TO A TIME SCHEDULE FOR INSPECTION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A12    1E10                 
20070507001822007050700182CE  2007       5          7          2007FA0000364    120070420G3230                LANDING GEAR                            CESSNA500   S550        2076607CE  PWA   JT15  JT15D4      52112NE                                              MALFUNCTIONED   B  EBVRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL0932TX                        S5500026                                EMERGENCY LANDING GEAR DEPLOYMENT SYSTEM INSPECTED DURING ROUTINE PHASE INSPECTION.  EMERGENCY GEAR CABLES CHECKED FOR CORRECT RIGGING, AND EMERGENCY GEAR SYSTEM FUNCTION TESTED WITH AIRCRAFT ON JACKS.  SYSTEM FUNCTION TESTED PROPERLY.  PILOT ELECTED TO PERFORM IN FLIGHT CHECK OF SAME SYSTEM AND FOUND THAT MAIN GEAR WOULD NOT DEPLOY.  PILOT EXTENDED GEAR USING NORMAL HYDRAULIC SYSTEM OPERATION AND LANDED WITHOUT INCIDENT.  AC WAS FLOWN TO SERVICE CENTER FOR EVALUATION.  (K)                                                                                                                                                                                                                                                  1L72 4F4  FRTA22CE   E1NE                 
20070504002132007050400213CE  2007       5          4          2007FA0000366    120070412G7921652065          GASKET                                  CESSNA421   421B        2076014CE  CONT  O520  GTSIO520H   17032SO                              OIL COOLER      BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE0142776322                    421B0394    607077                      AIRCRAFT DEPARTED ON A CHARTER , PILOT WAS OVER LAKE WHEN HE NOTICED ENGINE OIL COMING OUT OF TOP ENGINE COWLING COOLING LOUVERS.  PILOT NOTIFIED CONTROL HE WAS LOSING OIL.  FEATHERED THE RT ENGINE AND DIVERTED .  PILOT MADE UNEVENTFUL SINGLE ENGINE LANDING AND TAXIED TO MAINTENANCE HANGAR.  DISCOVERED THE ENGINE WAS SEIZED AND THE COWLING AND NACESSE BOTTOM COVERED WITH OIL.  STARTED DISASSEMBLY AND FOUND THE OIL COOLER GASKET, PN 652065, HAD .1250 INCH SECTION MISSING FROM THE UPPER FORWARD AREA OF THE GASKET.  (K)                                                                                                                                                                                                      1L72 3O3  O  A7CE    E7CE                 
20070504002142007050400214CE  2007       5          4          2007FA0000367    120070420G51006213011139      DOUBLER                                 CESSNA650   650         2076802CE                                                               UNKNOWN         FATIGUED        B  CNQRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE07                                                                    THE 6213011139 LT DOUBLER AND THE 6213011140 RT DOUBLER FATIGUE CRACKING ON BOTH.  THE 6213011139 LT DOUBLER AND THE 6213011140 RT DOUBLER, ON MODEL 650 IS PART OF THE NOSE WHEEL WELL ASSY, HAS BEEN FOUND WITH FATIGUE CRACKING ON MULTIPLE SN.  CURRENTLY THE PART IS BEING REMOVED AND REPLACED AS NEEDED AND A SERVICE CONDITION REPORT (SCR) HAS BEEN SUBMITTED TO ENGINEERING FOR REVIEW.  (K)                                                                                                                                                                                                                                                                                                                                          2L72 4F      A9NM                         
20070504002272007050400227CE  2007       5          4          2007FA0000368    120070420G53106213011140      DOUBLER                                 CESSNA650   650         2076802CE                                                               FS 92-94        FATIGUED        D  CNQRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE07                                                                    THE 6213011-139 LT DOUBLER AND THE 6213011-140 RT DOUBLER FATIGUE CRACKING ON BOTH.  THE 6213011-139 LT DOUBLER AND THE 6213011-140 RT DOUBLER, ON MODEL 650 IS PART OF THE NOSE WHEEL WELL ASSY, HAS BEEN FOUND WITH FATIGUE CRACKING ON MULTIPLE SN.  CURRENTLY THE PART IS BEING REMOVED AND REPLACED AS NEEDED, AND A SERVICE CONDITION REPORT (SCR) HAS BEEN SUBMITTED TO ENGINEERING FOR REVIEW.  (K)                                                                                                                                                                                                                                                                                                                                     2L72 4F      A9NM                         
20070504002232007050400223CE  2007       5          4          2007FA0000369    120070404G3210084100097       LANDING GEAR                            CESSNA310   310D        2074212CE  CONT  O470  IO470*      17026SO                              LT MLG          MALFUNCTIONED   D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM036981T                       39281                                   THE PILOT NOTED THAT SOMETHING WAS HANGING DOWN UNDER THE AC IN CRUISE FLIGHT AND THAT THE AC WAS NOT GOING AS FAST AS IT NORMALLY DID.  ANOTHER AC NOTED THAT THE GEAR WAS UP, BUT THAT THE LEFT IB GEAR DOOR WAS HANGING DOWN PART WAY.  THE TOWER CONFIRMED THAT THE GEAR APPEARED TO BE DOWN AND LOCKED, BUT THAT THE LT IB GEAR DOOR WAS PART WAY DOWN.  ALL INDICATIONS OF THE GEAR IN THE AC WERE NORMAL AND THE GREEN LIGHT WAS ON WHEN THE AC LANDED.  THE AIRCRAFT LANDED NORMALLY AND ROLLED ABOUT 800 FT DOWN THE RUNWAY WHEN THE LEFT MAIN GEAR BROKE OUT OF THE WHEEL WELL.  IT WENT STRAIGHT BACK BEHIND THE WING AND THE AC WENT AROUND TO THE LEFT AND OFF THE RUNWAY.  THE LT IB DOOR WILL MOVE SOME BY HAND AND SEEMED TO OPE1L72 3O3  O  3A10    E1CE                 
20070504001332007050400133    2007       5          4          2007FA0000370    420070427G2562MN1300          BATTERY         ACK                     PIPER PA28  PA28236     7102815SO  LYC   O540  O540J3A5    41532EA  HARTZLHCF2Y HCF2YR1     GL  ELT             LEAKING         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA01          12    020150      28791146    L2113440A   CM285           BATTERIES LEAKED ACID/ALKALII, CORRODING CONTACTS SERVERLY AND RENDERING ELT INOPERABLE.  BATTERIES WERE INSTALLED IN 2006. SHELF DATE ON BATTERIES WERE MAR 2011. ELT WAS NOT FOUND ACTIVATED. THIS IS THE THIRD CASE OF THIS I HAVE SEEN IN 2006/2007 AND THERE HAVE BEEN SEVERAL OTHERS IN THE PAST 5 YEARS.  IN ALL CASES THE BATTERIES RENDERED THE ELT INOP PRIOR TO THE REPLACEMENT DATE (HALF OF SHELF LIFE IAW FAR 91.207 (C)). ALL PROBLEMS WERE DETECTED DURING ANNUAL INSPECTIONS OF ELT IAW FAR 91.207 D.                                                                                                                                                                                                                          1L71 3O3  O  2A13    E295    5  CP27EA    
20070504001342007050400134    2007       5          4          2007FA0000371    420070427G2562MN1300          BATTERY         ACK                     PIPER PA28  PA28236     7102815SO  LYC   O540  O540J3A5    41532EA  HARTZLHCF2Y HCF2YR1     GL  ELT             LEAKING         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA01          12    020150      28791146    L2113440A   CM285           BATTERIES LEAKED ACID/ALKALII, CORRODING CONTACTS SERVERLY AND RENDERING ELT INOPERABLE.BATTERIES WERE INSTALLED IN 2006. SHELF DATE ON BATTERIES WERE MAR 2011. ELT WAS NOT FOUND ACTIVATED. THIS IS THE THIRD CASE OF THIS I HAVE SEEN IN 2006/2007 AND THERE HAVE BEEN SEVERAL OTHERS IN THE PAST 5 YEARS. IN ALL CASES THE BATTERIES RENDERED THE ELT INOP PRIOR TO THE REPLACEMENT DATE (HALF OF SHELF LIFE I/A/W FAR 91.207 (C)). ALL PROBLEMS WERE DETECTED DURING ANNUAL INSPECTIONS OF ELT I/A/W FAR 91.207 D.                                                                                                                                                                                                                         1L71 3O3  O  2A13    E295    5  CP27EA    
20070504001532007050400153    2007       5          4          2007FA0000372    420070502G2562MN1300          BATTERY         AMERIKING               CESSNA182   R182        2072734CE  LYC   O540  O540J3C5    41532EA                              ELT             LEAKING         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA01     12   12    353328      01165                                   BATTERIES LEAKED INSIDE ELT UNIT PREVENTING ELT OPERATION AND DESTROYING CONTACTS INSIDE UNIT. THIS IS ONE OF SEVERAL TIMES THIS PROBLEM HAS BEEN SEEN IN THE NEWER OR MORE RECENTLY MANUFACTURED BATTERIES THIS PARTICULAR SET HAD AN EXPIRATION OF 2012 AND HAD ONLY BEEN INSTALLED IN THE UNIT FOR ONE YEAR.  RECOMMEND BAT REPLACEMENT EVERY 6 MONTHS UNTIL THIS PROBLEM IS ADDRESSED BY ELT MANUFACTURES OR THE BATTERY COMPANY NOTE OLDER BATTERIES DID NOT EXHIBIT THIS PROBLEM.                                                                                                                                                                                                                                                         1H71 3O3  ORT3A13    E295                 
20070504001612007050400161GL  2007       5          4          2007FA0000375    120070427G2720                CONTROL CABLE                           CIRRUSSR    SR22        2130001GL  CONT  O550  IO550*           SO                              AILERONS        INTERFERENCE    B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA07220SR                       0391                                    DURING INSPECTION FOUND INTERFERENCE BETWEEN RUDDER/AILERON INTERCONNECT SYSTEM AND RT AILERON CABLE. CHECKED RIGGING AND FOUND CABLE CLAMP ON RT AILERON CABLE OUT OF POSITION. VISUAL INSPECTION INDICATES NO MOVEMENT BETWEEN CABLE AND CLAMP AND RECORDS REVIEW INDICATE THAT NO RIGGING HAS TAKEN PLACE SINCE THE AIRPLANE LEFT THE FACTORY.                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O3  ONTA00009CHE3SO                 
20070504001702007050400170CE  2007       5          4          2007FA0000377    120070426G3232                ROD             GARKENYON               LEAR  60    60LEAR      5170707CE  WRIGHTR3350 R3350*      67040EA                              ACTUATOR        FAILED          D      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      SO09718A            0290        065                                     WHEN LANDING GEAR WAS CYCLED DOWN, THE RT RED IB GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. GEAR DOWN LOCK LIGHTS WERE GREEN. NORMAL LANDING. INSPECTION REVEALED THAT THE ACTUATOR SHAFT HAD UNSCREWED FROM THE PISTON NOT ALLOWING THE DOOR TO CLOSE. FURTHER EXAMINATION REVEALED THAT THE ROLL PIN SECURING THE SHAFT TO THE PISTON WAS SHEARED.  THE LT ACTUATOR WAS INSPECTED AND THE ACTUATOR ROD WAS FOUND TO BE 2.5 TURNS FROM DISENGAGING FROM THE PISTON. 6-7 TURNS BOTTOMS THE ROD IN THE PISTON. REPLACED BOTH DOOR ACTUATORS.                                                                                                                                                                                                     2L72 4F4  RRTA10CE   E272                 
20070504001882007050400188CE  2007       5          4          2007FA0000378    120070426G323266000858        ACTUATOR                                LEAR  60    60LEAR      5170707CE  WRIGHTR3350 R3350*      67040EA                              MLG             FAILED          D      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      SO09718A 4200                   065                                     WHEN LANDING GEAR WAS CYCLED DOWN, THE RT RED IB GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH.  GEAR DOWN LOCK LIGHTS WERE GREEN. NORMAL  LANDING. INSPECTION REVEALED THAT THE ACTUATOR SHAFT HAD UNSCREWED FROM THE PISTON NOT ALLOWING THE DOOR TO CLOSE. FURTHER EXAMINATION REVEALED THAT THE ROLL PIN SECURING THE SHAFT TO THE PISTON WAS SHEARED. THE LT ACTUATOR WAS INSPECTED AND THE ACTUATOR ROD WAS FOUND TO BE 2.5 TURNS FROM DISENGAGING FROM THE PISTON. 6-7 TURNS BOTTOMS THE ROD IN THE PISTON. REPLACED BOTH DOOR ACTUATORS.                                                                                                                                                                                                    2L72 4F4  RRTA10CE   E272                 
20070504002062007050400206CE  2007       5          4          2007FA0000381    120070404G781002R3022406      EXHAUST DUCT                            BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA                              RT ENGINE       CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO09     13510514                           PCE81382                    WHILE PREFORMING SCHEDULED MAINTENANCE, REMOVED LT ENGINE EXHAUST STACK TO FACILITATE INSPECTING THE EXHAUST DUCT. FOUND CRACK FOLLOWING THE CIRCUMFERENCE OF THE SKI SLOPE. THE EXHAUST DUCT HAD SB 3380 COMPLIED WITH 514 HOURS EARLIER.POWER SECTION WAS REMOVED AND SENT FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA                 
20070504002152007050400215SO  2007       5          4          2007FA0000383    120070430G55202039700         HORN                                    PIPER PA24  PA24250     7102404SO  LYC   O540  O540*       41532EA                              STABILIZER      CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP075977P6000                   241070                                  FOUND STABILATOR HORN P/N 20397-00 SEVERELY CRACKED FROM THE INSIDE WHERE THE ATTACH BOLTS CONNECT THE BALANCE WEIGHT TUBE P/N 20398-02 AND STABILATOR TORQUE TUBE ASSEMBLY P/N 20203-03.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  O  1A15    E295                 
20070613002662007061300266    2007       6          13         2007FA0000385    220070501G7320                FADEC                                   DIAMONDA40  DA40        2990002GL                                                                               MALFUNCTIONED   C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW99     103                                                            THE ECU WARNING LIGHTS HAVE COME ON MULTIPLE TIMES NOW.  ACCRODING TO THE MANUFACTURER, EACH TIME THESE ANNUNCIATORS COME ON THE AIRCRAFT MUST BE SERVICED BY AN APPROVED MECHANIC. BY THIELERTS EXPLANATION, IF THE AIRCRAFT GOES INTO A STEEP BANK OR UN-COORDINATED TURN THAN AN AIR BUBBLE CAN GET INTO THE FUEL LINE AND CAUSE UNEVEN PRESSURES BETWEEN THE TWO ENGINES.  THE FADEC SENSES THIS AS A PROBLEM AND THE ECU WANRINGS TRIP.  ACCORDING TO THIELERT THIS HAS BEEN HAPPENING FREQUENTLY ON AIRCAFT WITH THEIR FADEC ENGINES.  THREE TIMES ALREADY ON OUR WITHIN 100 HOURS.  IT IS A NUISANCE BECAUSE AN AIRCRAFT CAN EASILY BE STRANDED IN A LOCATION WITHOUT A THIELERT APPROVED MECHANIC. OR WORSE, IF A GENUINE PROBLEM EXISTE1L71 3O    NTA47CE                        
20070507001842007050700184    2007       5          7          2007FA0000386    220070501G7320                FADEC                                   DIAMONDA40  DA40        2990002GL                                                                               MALFUNCTIONED   C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW03     103                                                            THE ECU WARNING LIGHTS HAVE COME ON MULTIPLE TIMES NOW.  ACCORDING TO THE MANUFACTURER, EACH TIME THESE ANNUNCIATORS COME ON THE AIRCRAFT MUST BE SERVICED BY AN APPROVED MECHANIC. BY THIELERTS EXPLANATION, IF THE AIRCRAFT GOES INTO A STEEP BANK OR UN-COORDINATED TURN THAN AN AIR BUBBLE CAN GET INTO THE FUEL LINE AND CAUSE UNEVEN PRESSURES BETWEEN THE TWO ENGINES.  THE FADEC SENSES THIS AS A PROBLEM AND THE ECU WARNINGS TRIP.  ACCORDING TO MANUFACTURE THIS HAS BEEN HAPPENING FREQUENTLY ON AIRCRAFT WITH THEIR FADEC ENGINES.  THREE TIMES ALREADY ON OUR WITHIN 100 HOURS.  IT IS A NUISANCE BECAUSE AN AIRCRAFT CAN EASILY BE STRANDED IN A LOCATION WITHOUT A THIELERT APPROVED MECHANIC. OR WORSE, IF A GENUINE PROBLEM EX1L71 3O    NTA47CE                        
20070521001462007052100146CE  2007       5          21         2007FA0000388    120070413G323399101368        ACTUATOR                                CESSNA414   414A        2075907CE  CONT  O520  TSIO520*    17040SO                              LT MLG          CORRODED        D      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      EA616672C7623                   414A0053                                LT LANDING GEAR ACTUATOR FAILED WHILE TAXING.  COLLAPSED LT WING.  DAMAGED LT PROP AND WING TIP.  ACTUATOR INSPECTED AND FOUND WATER INSIDE.  ACTUATOR OVERHAULED AND REINSTALLED NOSE AND RT LG ACTUATOR REMOVED FOR INSPECTION AND CHECKED GOOD.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3O3  O  A7CE    E8CE                 
20070521001142007052100114EA  2007       5          21         2007FA0000389    220070420G85305L32006WA1      CYLINDER                                CESSNA172   172N        2072434CE  LYC   O320  O320D2J     41508EA                              ENGINE          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM014801D1400                   17272362                                CRACK FROM EXH STUD AROUND CYLINDER TO UPPER SPARK PLUG.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A12    E274                 
20070514002102007051400210GL  2007       5          14         2007FA0000390    220070412G7323369A7701        BRACKET                                 HUGHES369   369D        4470706WP  ALLSN 250C  250C20      03013GL                              GOVERNOR        DAMAGED         B  EOORK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL035074R                       1151D                                   DURING A PREFLIGHT, THE PILOT NOTICED THE GOVENOR BELCRANK HAD SOME SLOP SUBSEQUENT INSPECTION DISCLOSED THAT THE BELCRANK PIVOT BOLT WAS MOVING  IN THE BRACKET BECAUSE THE HOLE WAS ELONGATED, REPLACED BRACKET.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  U  H3WE    E4CE                 
20070521001472007052100147SO  2007       5          21         2007FA0000391    220070411G74146310            MAGNETO                                 BEECH 33    F33A        1151425CE  CONT  O520  IO520BA     17032SO                              LEFT            FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL1911BX 26                     CE388       814263R                     DURING NORMAL FLIGHT, VFR CONDITIONS, LT MAGNETO FAILED TO CONTINUE FIRING.  AC LANDED WITHOUT INCIDENT.  UPON TROUBLESHOOTING LT MAGNETO FOUND TO ONLY FIRE ON ONE LEAD.  MAGNETO REPLACED WITH NEW UNIT.  DEFECTIVE MAGNETO FOUND TO HAVE LOOSE PARTS RATTLING INSIDE AFTER REMOVAL FROM ENGINE.  MAGNETO NOT DISASSEMBLED DUE TO WARRANTY STATUS OF MAGNETO.  (K)                                                                                                                                                                                                                                                                                                                                                                            1L71 3O3  O  3A15    E5CE                 
20070514001832007051400183    2007       5          14         2007FA0000392    120070301G1430                TAB                                                                                                                                                     CRACKED         B  UO2RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL19                                                                    WHEN TECH WENT TO BEND THE TAB ATTACHED TO THE WASHER AT THE RADIUS OF THE BEND, THEY WOULD CRACK.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   
20070521000842007052100084CE  2007       5          21         2007FA0000393    120070409G7921LW10025         OIL COOLER                              BEECH 60    A60         1153604CE  LYC   O541  TIO541E1C4  41536EA                              LT ENGINE       CRACKED         G      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  NRNOT REPORTED   1                      SO091873W     142               P231                                    ON APRIL 9, 2007, MADE A PRECAUTIONARY LANDING, AL (TCL) DUE TO LOW OIL PRESSURE ON THE LEFT ENGINE.  MAINTENANCE PERSONNEL REPORTED THAT THE OIL COOLER HAD FAILED DUE TO CRACKS, THE OIL LEVEL WAS DOWN (4) QUARTS, AND THE OIL FILTER WAS INSPECTED WITH NO CONTAMINATION FOUND.  ENGINE MAINTENANCE LOG RESEARCH SHOWED THE FAILED OIL COOLER WAS OVERHAULED AND INSTALLED BY FIREWALL FORWARD.  THE COOLER WAS REPLACED WITH A NEW PART ON 4/13/2007 AT 1770.6 HOBBS.  THE FAILED OIL COOLER HAD 142.1 HOURS SINCE OVERHAUL.  NO DETERMINATION COULD BE MADE OF OIL COOLER TOTAL TIME. (K)                                                                                                                                                 1L72 3O3  O  A12CE   E10EA                
20070514002082007051400208CE  2007       5          14         2007FA0000394    120070406G323398820152        ACTUATOR                                CESSNA172   172RG       2072438CE  LYC   O360  O360F1A6    41514EA  MCAULY2D34C B2D34C220   GL  LT MLG          CRACKED         D  H2USO   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      SW119353D                       172RG1131   L1868036A   801202          PILOT REPORTED LOUD POP JUST BEFORE INTERING THE PATTERN AT M89.  WHEN HE EXTENDED THE GEAR THE GREEN GEAR DOWN LIGHT WOULD NOT COME ON.  FLY BY REVEALED THE LEFT GEAR WAS IN TRANSIENT.  GEAR UP LANDING FOLLOWED.  INSPECTION OF LT MAIN GEAR ACTUATOR REVEALED THE ACTUATOR HOUSING WAS CRACKED ACROSS THE FORWARD ATTACH BOLT HOLE.  THE CRACKED HOUSING ALLOWED THE PISTON RACK TO JUMP GEARS ON THE PINION GEAR ATTACHED TO MAIN GEAR LEG.  THIS AREA IS INSPECTED EACH 100 HR FOR CRACKS AND DEFECTS VERY CAREFULLY WITH LIGHTS AND INSPECTION MIRROWS.  TIME SINCE LAST INSPECTION WAS 25 HRS.  AD 2001-06-06 WAS CW 8-13-2001 TACH 497, TOTAL TIME 4516 WITH NO DEFECTS FOUND.  (K)                                                   1H71 3O3  O  3A17    E286    5  CP7EA     
20070514002242007051400224CE  2007       5          14         2007FA0000395    120070423G324613685           BEARING                                 BEECH 1900  1900D       1154162CE                                                               MLG             LACK OF LUBE    B  HY1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA23733DC360                    UE307                                   WHILE PERFORMING ROUTINE PREVENTATIVE MAINTENANCEON THE RT IB WHEEL AND TIRE ASSEMBLY (TO CHANGE A WORN TIRE) ONE OF THE WHEEL BEARING ROLLERS CAME OUT OF THE OUTER WHEEL BEARING ONCE THE WHEEL BEARING WAS REMOVED FROM THE WHEEL ASSEMBLY.  THE WHEEL BEARING CAGE WAS FOUND TO BE DEFORMED WITH ONE PART OF THE CAGE BROKEN ALLOWING THE ROLLER TO FALL OUT.  PIECES OF METAL WERE FOUND IN THE BEARING SEAL.  THE BEARING APPEARS TO HAVE BEEN OVERHEATED.  PROPER LUBRICATION WOULD HAVE PREVENTED THIS BEARING FROM OVERHEATING.  IT IS IMPERATIVE THAT EACH OPERATOR BE AWARE THAT THE INSPECTION AND LUBRICATION REQURIEMENT/INTERVAL FOR THE WHEEL BEARINGS MAY BE LESS THAN THE MFG RECOMMENDATIONS BASED ON THE OPERATORS OWN SPECI2L72 4T    RTA24CE                        
20070514001822007051400182    2007       5          14         2007FA0000396    420070430G3400593250101       SWITCH                                  CESSNA414   414         2075908CE  CONT  O520  TSIO520*    17040SO                              COCKPIT         STUCK           B  YLMRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP2342SG 2972                   4140927                                 AVIONICS MASTER SWITCH STUCK IN THE ON POSITION AD 2005-20-25 WAS PREVIOUSL COMPLIED WITH AND DID NOT APPLY.  DATE CODE OF THE SWITCH WAS 7647.  THERE WAS NO BURNING SMELL WHEN THE SWITCH BECAME STUCK.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3O3  ORTA7CE    E8CE                 
20070521001412007052100141SO  2007       5          21         2007FA0000397    120070331G3210                BEARING                                 PIPER PA24  PA24250     7102404SO  LYC   O540  AEIO540*         EA                              MLG             BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA617178P                       242347      L259640                     BEARING ROD END BROKEN AT THREAD EXP BEARING (452377) CONDUIT BENT. CONTROL ASSY (455180).                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  O  1A15    1E4                  
20070521000752007052100075SO  2007       5          21         2007FA0000398    220070418G74146320            MAGNETO                                 CESSNA210   T210N       2073456CE  CONT  O520  TSIO520R    17040SO  MCAULYD3A34 D3A34C402   GL  ENGINE          CORRODED        G      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            NRNOT REPORTED   1                      EA135361Y525                    21064183    517975      871106          EMERGENCY RETURN TO FIELD:  INSPECTION REQUIREMENTS FOR MAGNETO (PN 6320) ARC NOT ADEQUATE TO INSURE PROPER VENTING (PRESSURIZED MAG).  SB 2-80C SPECIFIES ONLY EXTERNAL INSPECTION IS REQUIRED EVERY 100 HOURS AND AN INTERNAL INSPECTION AFTER 500 HOURS.  THE SUBJECT MAGNETOS WITH 525 AND 438 CONTAINED MOISTURE AND EXCESSIVE CORROSION INTERNALLY BECAUSE THE PREVIOUS REQUIREMENTS TO TEST PRESSURIZED MAGNETOS CONTAINED IN SB 1-88A DO NOT APPLY TO THE 6300 SERIES MAGNETOS.  (K)                                                                                                                                                                                                                                                    1H71 3O3  O  3A21    E8CE    5  CP47GL    
20070521001152007052100115SO  2007       5          21         2007FA0000399    220070418G74146320            MAGNETO                                 CESSNA210   T210N       2073456CE  CONT  O520  TSIO520R    17040SO  MCAULYD3A34 D3A34C402   GL  ENGINE          CORRODED        G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA135361Y438                    21064183    517975      871106          EMERGENCY RETURN TO FIELD:  INSPECTION REQUIREMENTS FOR MAGNETO (PN 6320) ARC NOT ADEQUATE TO INSURE PROPER VENTING (PRESSURIZED MAG).  SB2-80C SPECIFIES ONLY EXTERNAL INSPECTION IS REQUIRED EVERY 100 HOURS AND AN INTERNAL INSPECTION AFTER 500 HOURS.  THE SUBECT MAGNETOS WITH 525 AND 438 CONTAINED MOISTURE AND EXCESSIVE CORROSION INTERNALLY BECAUSE THE PREVIOUS REQUIREMENTS TO TEST PRESSURIZED MAGNETOS CONTAINED IN SB 1-88A DO NOT APPLY TO THE 6300 SERIES MAGNETOS.  (K)                                                                                                                                                                                                                                                      1H71 3O3  O  3A21    E8CE    5  CP47GL    
20070514002002007051400200GL  2007       5          14         2007FA0000400    220070425G7230                BEARING                                 HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              ENGINE          FAILED          B  EOORO   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      AL03511SB504                    1090592D    CAE830001                   DURING FLIGHT THE UPPER CHIP PULL ILLUMINATED, IT WAS CLEANED IAW MM AND RETURNED TO SERVICE.  A COUPLE OF HOURS LATER, A SECOND LIGHT ILLUMINATED.  FOUND LOTS OF FINE CHIPS.  REPLACED ENGINE.  FOUND NR 1 BEARING BAD.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3U3  U  H3WE    E4CE                 
20070615001732007061500173    2007       6          15         2007FA0000401    120070521G510031699042        HOUSING                                                                                                                                 UNKNOWN         CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW99                                                                    CRACK IN PART ID.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         
20070615001742007061500174CE  2007       6          15         2007FA0000402    120070522G2750                CONTROL CABLE                           SYMPHOSA160 SA160       05619SUCE                                                               TE FLAPS        CHAFED          P      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15                                                                    DURING PREFLIGHT INSPECTION, FOUND FLAP CONTROL CABLES CHAFING ON THE FLAP TRACK.  DEPTH OF INTERFERENCE BETWEEN CABLE AND TRACK WAS ABOUT THE DIAMETER OF THE CABLE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O    NTA46CE                        
20070615001752007061500175CE  2007       6          15         2007FA0000403    120070522G5750                CONTROL CABLE                           SYMPHOSA160 SA160       05619SUCE                                                               TE FLAPS        CHAFED          P      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15                                                                    DURING PREFLIGHT INSPECTION, FOUND FLAP CONTROL CABLES CHAFING ON THE FLAP TRACK.  DEPTH OF INTERFERENCE BETWEEN CABLE AND TRACK WAS ABOUT THE DIAMETER OF THE CABLE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O    NTA46CE                        
20070615001762007061500176EU  2007       6          15         2007FA0000404    120070522G5330                SKIN                                    ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE73131G   29003NE                              FUSELAGE        CORRODED        B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL23600NY                       231                                     FOUND SEVERE PITTING CORROSION ON BOTH THE LT AND RT SIDES BETWEEN FRAME, STATIONS 184 AND 194 BELOW EMERGENCY ESCAPE DOORS.  BELIEVE THIS IS DUE TO WATER LEAKING AROUND THE EMERGENCY ESCAPE DOORS AND SOAKING THE SOUND DAMPENING INSULATION.  THE PITTING WAS SO BAD IT CORRODED THROUGH THE SKIN ON THE RT SIDE.  THIS CORROSION WAS FOUND DURING AN RVSM INSTALLATION WHILE WE WERE MARKING OUT THE CRITICAL REGION AROUND THE STATIC PORTS.  WE REPAIRED THE DAMAGE FOLLOWING APPROVED DATA FROM A STRUCTURAL ENGINEER AND RETURNED TO SERVICE IAW FAA FORM 8110-3.                                                                                                                                                                      2M72 4F4  F  A2SW    E6WE                 
20070615001772007061500177EU  2007       6          15         2007FA0000405    120070522G5330                SKIN                                    ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE73131G   29003NE                              FUSELAGE        CORRODED        B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL23600NY                       231                                     FOUND SEVERE (PITTING CORROSION) ON BOTH THE LT AND RT SIDES BETWEEN FRAME, STATIONS 184 AND 194 BELOW EMERGENCY ESCAPE DOORS.  THIS IS DUE TO WATER LEAKING AROUND THE EMERGENCY ESCAPE DOORS AND SOAKING THE SOUND DAMPENING INSULATION.  THE PITTING WAS SO BAD IT CORRODED THROUGH THE SKIN ON THE RT SIDE.  THIS CORROSION WAS FOUND DURING AN RVSM INSTALLATION WHILE WE WERE MARKING OUT THE CRITICAL REGION AROUND THE STATIC PORTS.  REPAIRED THE DAMAGE FOLLOWING APPROVED DATA FROM A STRUCTURAL ENGINEER AND RETURNED TO SERVICE IAW FAA FORM 8110-3.                                                                                                                                                                               2M72 4F4  F  A2SW    E6WE                 
20070614002372007061400237CE  2007       6          14         2007FA0000410    120070110G32450923540         TUBE                                    BEECH 18    D18S        1151004CE  PWA   R985  R985*       52008NE                              TIRE            BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW99500MK50                                                             THIS IS THE THIRD NEW MFG INNER TUBE THAT HAS SPLIT ALONG CIRCUMFERENTIAL WELDED SEAMS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3R3  R  A765    5E1                  
20070615001712007061500171EU  2007       6          15         2007FA0000411    120070515G32105321012110      BOLT                                    PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  LANDING GEAR    BROKEN          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA65624AF1576       AM090       624         PR0499      KX227           DURING A 100 HOUR INSPECTION, A VISUAL INSPECTION FOUND A BROKEN BOLT ON THE RT MLG. THE BOLT ATTACHED THE LOWER PART OF THE SHOCK ABSORBER TO LANDING GEAR LEG. THE PN OF THE BOLT IS MOST LIKELY 532.10.12.110. THERE IS A LATER PN 532.10.12.205 BUT THIS WAS PROBABLY NOT THE PART INSTALLED. THEIR WAS NO MARKING ON THE BOLT ITSELF MAKING IT DIFFICULT TO DETERMINE THE PN. THIS PROBLEM WAS PREVIOUSLY ADDRESSED BY AD 04-06-05 AND SB 32-015, BUT THIS AIRCRAFT AND SN OF THE LANDING GEAR IN QUESTION ARE WELL BEYOND THE AFFECTIVITY OF BOTH THE AD AND THE SB.                                                                                                                                                                      1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070615001922007061500192EU  2007       6          15         2007FA0000412    120070515G32105321012110      BOLT                                    PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  LANDING GEAR    BROKEN          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA65624AF1576       AM090       624         PR0499      KX227           DURING A 100 HOUR INSPECTION, A VISUAL INSPECTION FOUND A BROKEN BOLT ON THE RT MLG. THE BOLT ATTACHED THE LOWER PART OF THE SHOCK ABSORBER TO LANDING GEAR LEG. THE PN OF THE BOLT IS MOST LIKELY 532.10.12.110. THERE IS A LATER PN 532.10.12.205 BUT THIS WAS PROBABLY NOT THE PART INSTALLED. THEIR WAS NO MARKING ON THE BOLT ITSELF MAKING IT DIFFICULT TO DETERMINE THE PN. THIS PROBLEM WAS PREVIOUSLY ADDRESSED BY AD 04-06-05 AND SB 32-015, BUT THIS AIRCRAFT AND SN OF THE LANDING GEAR IN QUESTION ARE WELL BEYOND THE AFFECTIVITY OF BOTH THE AD AND THE SB.                                                                                                                                                                      1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070615001932007061500193EU  2007       6          15         2007FA0000413    120070515G32105321012110      BOLT                                    PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  ZONE 700        BROKEN          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA65624AF1576       AM090       624         PR0499      KX227           DURING A 100 HOUR INSPECTION, A VISUAL INSPECTION FOUND A BROKEN BOLT ON THE RT MLG. THE BOLT ATTACHED THE LOWER PART OF THE SHOCK ABSORBER TO LANDING GEAR LEG. THE PN OF THE BOLT IS MOST LIKELY 532.10.12.110. THERE IS A LATER PN 532.10.12.205 BUT THIS WAS PROBABLY NOT THE PART INSTALLED. THEIR WAS NO MARKING ON THE BOLT ITSELF MAKING IT DIFFICULT TO DETERMINE THE PN. THIS PROBLEM WAS PREVIOUSLY ADDRESSED BY AD 04-06-05 AND SB 32-015, BUT THIS AIRCRAFT AND SN OF THE LANDING GEAR IN QUESTION ARE WELL BEYOND THE AFFECTIVITY OF BOTH THE AD AND THE SB.                                                                                                                                                                      1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070615001942007061500194EU  2007       6          15         2007FA0000414    120070515G32105321012110      BOLT                                    PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  ZONE 700        BROKEN          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA65624AF1576       AM090       624         PR0499      KX227           DURING A 100 HOUR INSPECTION, A VISUAL INSPECTION FOUND A BROKEN BOLT ON THE RT MLG. THE BOLT ATTACHED THE LOWER PART OF THE SHOCK ABSORBER TO LANDING GEAR LEG. THE PN OF THE BOLT IS MOST LIKELY 532.10.12.110. THERE IS A LATER PN 532.10.12.205 BUT THIS WAS PROBABLY NOT THE PART INSTALLED.  THEIR WAS NO MARKING ON THE BOLT ITSELF MAKING IT DIFFICULT TO DETERMINE THE PN. THIS PROBLEM WAS PREVIOUSLY ADDRESSED BY AD 04-06-05 AND SB 32-015, BUT THIS AIRCRAFT AND SN OF THE LANDING GEAR IN QUESTION ARE WELL BEYOND THE AFFECTIVITY OF BOTH THE AD AND THE SB.                                                                                                                                                                     1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070530000022007053000002EA  2007       5          30         2007FA0000416    220070415G7322103103          CARBURETOR                              AMTR  VAN   HATZVAN     0561383GL  LYC   O235  O235C1      41505EA  SNSNCH76AM  M76AM       EA  ENGINE          CONTAMINATED    C      E   ENGINE SHUTDOWN                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  APAPPROACH       1                      GL15899P                        313         335915      12242           DURING INSPECTION OF THE CARBURETOR, DISCOVERED FLAKES OF WHAT APPEARS TO BE METAL IN THE GASCOLATOR SCREEN.  ALSO, OBSERVED SOME SPECS OF RED MATERIAL ABOUT THE SIZE OF PEPPER. WHEN WE PULLED THE CARB APART WE OBSERVED A LINE ON THE BOTTOM OF THE BOWL WHERE SEDIMENT HAD PREVIOUSLY SETTLED IN THE BOWL. HOWEVER, NOTHING SIGNIFICANT WAS NOTED IN THE BOWL DURING OUR INSPECTION.  FURTHER INSPECTION REVEALED THAT ONCE THE NEEDLE VALVE WAS SEATED BY LIGHTLY PRESSING THE FLOAT UPWARD, IT WOULD THEN REMAIN SEATED EVEN IF AIR WAS BLOWN IN THE FUEL INLET  PORT. HOWEVER, IF THE FLOAT WAS MANIPULATED UP AND DOWN A FEW TIMES, THE NEEDLE VALVE WOULD THEN NOTICEABLY POP FREE. AND ALTHOUGH NO OBVIOUS DEBRIS WAS NOTED UPON DISA1H71 3O3  O  EXPA1H71E223    5  N1P210    
20070615001952007061500195CE  2007       6          15         2007FA0000417    120070511G5711                SPAR                                    BBAVIA11    11AC        0191102CE  LYC   O235  O235*       41505EA  SNSNCH76AK  M76AK       EA  LT WING         DELAMINATED     G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL093581E                       11AC1813    108715      11544           DELAMINATION OCCURRING AT LT FRONT WING SPAR / STRUT LOCATION.  CRACK AT BOTTOM EDGE, AT WING ROOT FITTING.  POSSIBLE AGE OF SPAR CAUSING DELAMINATION.  LONGITUDINAL CRACK AT WING ROOT POSSIBLE EARLIER DAMAGE.  REPLACED WITH NEW WOOD SPAR P/N 5146L.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  O  A761    E223    5  N1P210    
20070613002142007061300214CE  2007       6          13         2007FA0000419    120070410G781002R3022406      EXHAUST DUCT                            BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO09     13510365                                                       WHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.THE EXHAUST DUCT SB 3380 HAD BEEN COMPLIED WITH 365 HOURS PRIOR.POWER SECTION WAS REMOVED FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 4T4  T  A24CE   E4EA                 
20070613002052007061300205SO  2007       6          13         2007FA0000420    120070510G2571352020035201    BATTERY BOX                             PIPER PA28  PA28181     7102807SO                                                                               BROKEN          B  LC1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA076151H                       287890211                               PLASTIC BATTERY BOX BROKE INTO SEVERAL PIECES. LID WOULD NO LONGER HOLD SECURLY ON THE BOX ALLOWING BATTERY TO BE UNSECURED IN THE AIRCRAFT. PIPER REPIORTED THAT P/N 35201-00 LID AND 35202-00 WAS NO LONGER AVAILABLE. INSTALLED STC'D BATTERY BOX TO REPLACE THE DAMAGED ONE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O      2A13                         
20070615001972007061500197CE  2007       6          15         2007FA0000425    120070515G55110432001466      RIB                                     CESSNA150   150E        2071812CE  CONT  O200  O200A       17020SO                              HORIZONTAL STAB CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE012586J8600                   15061086                                DURING LT LEADING EDGE SKIN REPLACEMENT OF HORIZONTAL STABILIZER DUE TO BIRD STRIKE FOUND BOTH IB LEADING EDGE RIBS PN 0432001-46/ -6 CRACKED THROUGH UPPER AND LOWER MOUNTING TABS. WORKING RIVETS WERE FOUND AT THE TABS AND 2 RIVETS OB ON FORWARD SPAR. BIRD STRIKE DID NOT CAUSE CRACKS. THESE TABS ARE DIFFICULT TO INSPECT WITHOUT DISASSEMBLY OF TAIL. ANY EVIDENCE OF DEFECTS IN THE TAIL STRUCTURE SHOULD BE INVESTIGATED THOROUGHLY AS THEY ARE PRONE TO CRACKING AND WEAR.                                                                                                                                                                                                                                                          1H71 3O3  O  3A19    E252                 
20070615001982007061500198CE  2007       6          15         2007FA0000426    120070515G55110432001466      RIB                                     CESSNA150   150E        2071812CE  CONT  O200  O200A       17020SO                              HORIZONTAL STAB CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE012586J8600                   15061086                                DURING LT LEADING EDGE SKIN REPLACEMENT OF HORIZONTAL STABILIZER DUE TO BIRD STRIKE FOUND BOTH IB LEADING EDGE RIBS PN 0432001-46/ -6 CRACKED THROUGH UPPER AND LOWER MOUNTING TABS. WORKING RIVETS WERE FOUND AT THE TABS AND 2 RIVETS OB ON FORWARD SPAR. BIRDSTRIKE DID NOT CAUSE CRACKS. THESE TABS ARE DIFFICULT TO INSPECT WITHOUT DISASSEMBLY OF TAIL. ANY EVIDENCE OF DEFECTS IN THE TAIL STRUCTURE SHOULD BE INVESTIGATED THOROUGHLY AS THEY ARE PRONE TO CRACKING AND WEAR.                                                                                                                                                                                                                                                           1H71 3O3  O  3A19    E252                 
20070615001992007061500199CE  2007       6          15         2007FA0000427    120070515G55110432001466      RIB                                     CESSNA150   150E        2071812CE  CONT  O200  O200A       17020SO                              HORIZONTAL STAB CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE012586J8600                   15061086                                DURING LT LEADING EDGE SKIN REPLACEMENT OF HORIZONTAL STABILIZER DUE TO BIRDSTRIKE FOUND BOTH IB LEADING EDGE RIBS PN 0432001-46/ -6 CRACKED THROUGH UPPER AND LOWER MOUNTING TABS. WORKING RIVETS WERE FOUND AT THE TABS AND 2 RIVETS OB ON FORWARD SPAR. BIRDSTRIKE DID NOT CAUSE CRACKS. THESE TABS ARE DIFFICULT TO INSPECT WITHOUT DISASSEMBLY OF TAIL. ANY EVIDENCE OF DEFECTS IN THE TAIL STRUCTURE SHOULD BE INVESTIGATED THOROUGHLY AS THEY ARE PRONE TO CRACKING AND WEAR.                                                                                                                                                                                                                                                            1H71 3O3  O  3A19    E252                 
20070615002002007061500200CE  2007       6          15         2007FA0000428    120070515G55110432001466      RIB                                     CESSNA150   150E        2071812CE  CONT  O200  O200A       17020SO                              HORIZONTAL STAB CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE012586J8600                   15061086                                DURING LT LEADING EDGE SKIN REPLACEMENT OF HORIZONTAL STABILIZER DUE TO BIRDSTRIKE FOUND BOTH IB LEADING EDGE RIBS PN 0432001-46/ -6 CRACKED THROUGH UPPER AND LOWER MOUNTING TABS. WORKING RIVETS WERE FOUND AT THE TABS AND 2 RIVETS OB ON FORWARD SPAR. BIRDSTRIKE DID NOT CAUSE CRACKS. THESE TABS ARE DIFFICULT TO INSPECT WITHOUT DISASSEMBLY OF TAIL. ANY EVIDENCE OF DEFECTS IN THE TAIL STRUCTURE SHOULD BE INVESTIGATED THOROUGHLY AS THEY ARE PRONE TO CRACKING AND WEAR.                                                                                                                                                                                                                                                            1H71 3O3  O  3A19    E252                 
20070615002022007061500202CE  2007       6          15         2007FA0000429    120070515G7820E477001         MUFFLER                                 CESSNA150   150E        2071812CE  CONT  O200  O200A       17020SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE012586J3128                   15061086                                PILOT REPORTED FATIGUE WHILE FLYING. NO OBVIOUS EXTERNAL SIGNS OF MUFFLER FAILURE WERE FOUND, SHROUD REMOVAL REVEALED A TIGHT CRACK FROM NR 2 RISER INTO BODY, 3 INCHES LONG THAT LEFT VERY LITTLE STAINING ON INSIDE OF SHROUD. MUFFLER BODY WAS DEFORMED WHERE RISER IS WELDED INTO BODY, NEW MUFFLER HAD NO DEFORMATION IN THIS AREA.                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  O  3A19    E252                 
20070615002012007061500201CE  2007       6          15         2007FA0000434    120070515G7820E477001         MUFFLER                                 CESSNA150   150E        2071812CE  CONT  O200  O200A       17020SO                              ENGINE          CRACKED         E      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE012586J3128                   15061086                                PILOT REPORTED FATIGUE WHILE FLYING. NO OBVIOUS EXTERNAL SIGNS OF MUFFLER FAILURE WERE FOUND, SHROUD REMOVAL REVEALED A TIGHT CRACK FROM NR 2 RISER INTO BODY, 3 INCHES LONG THAT LT VERY LITTLE STAINING ON INSIDE OF SHROUD.  MUFFLER BODY WAS DEFORMED WHERE RISER IS WELDED INTO BODY, NEW MUFFLER HAD NO DEFORMATION IN THIS AREA.                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  3A19    E252                 
20070613002252007061300225CE  2007       6          13         2007FA0000435    120070209G781002R3022406      EXHAUST DUCT                            BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO09     13502422                                                       WHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE. EXHAUST DUCT SB HAD BEEN COMPLIED WITH 422 HOURS PRIOR. POWER SECTION WAS REMOVED FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA                 
20070530000052007053000005SO  2007       5          30         2007FA0000436    220070410G8530649169          CYLINDER                                                                   CONT  O520  IO520*      17032SO                              ENGINE          CRACKED         C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW17                                                                    PARTIAL HEAD AND BARREL SEPARATION. LARGE CRACK STARTING AT THE FUEL INJECTOR PORT RUNNING INTO THE CYLINDER HEAD COMBUSTION CHAMBER, THROUGH THE INTAKE SEAT BOSS AND CONTINUING AROUND TO THE LOWER SPARK PLUG BOSS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 3  O          E5CE                 
20070615002042007061500204EU  2007       6          15         2007FA0000437    120070522G5330                SKIN                                    ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE73131G   29003NE                              FUSELAGE        CORRODED        B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL23600NY                       231                                     FOUND SEVERE PITTING CORROSION ON BOTH THE LT AND RT SIDES BETWEEN FRAME STATIONS 184 AND 194 BELOW EMERGENCY ESCAPE DOORS.  THIS IS DUE TO WATER LEAKING AROUND THE EMERGENCY ESCAPE DOORS AND SOAKING THE SOUND DAMPENING INSULATION.  THE PITTING WAS SO BAD IT CORRODED THROUGH THE SKIN ON THE RT SIDE.  THIS CORROSION WAS FOUND DURING AN RVSM INSTALLATION WHILE WE WERE MARKING OUT THE CRITICAL REGION AROUND THE STATIC PORTS.  REPAIRED THE DAMAGE FOLLOWING APPROVED DATA FROM A STRUCTURAL ENGINEER AND RETURNED TO SERVICE IAW FAA FORM 8110-3.                                                                                                                                                                                  2M72 4F4  F  A2SW    E6WE                 
20070615002052007061500205GL  2007       6          15         2007FA0000443    320070525G6110                ROD                                     CESSNA208   208         2073702CE                                   MCAULY3AF34C3GFR34C703  GL  PROPELLER       FAILED          B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE09                                                    001922          RECEIVED PROPELLER FOR OVERHAUL. DURING PREFUNCTION TEST FOUND BLADE NR 1 WAS NOT LINKED TO THE PITCH CHANGE ROD. AFTER DISASSEMBLY OF PROPELLER FOUND NR 1 BLADE ACTUATING PIN PN B5072-1 DISCONNECTED FROM BLADE. ACTUATING PIN ATTACHMENT SCREWS WERE SAFETIED AND HAD ANTISABOTAGE ON THE SCREW HEADS. THE THREADS HAD BEEN PULLED OUT OF THE BLADE. THERE WAS NO OBVIOUS SIGNS OF SUDDEN STOPPAGE OR A STRIKE. ALL BLADES SHOWED SIMILAR EROSION FROM ROCK DAMAGE. BLADE TRACK WAS .0625 INCH PLUS OR MINUS AND DIAMETER WAS 106 INCHES.IAW THE RECORD, THIS WAS THE FIRST OVERHAUL EVENT. MANUFACTURE HAS REQUESTED BLADE, ACTUATING PIN AND LINK BE RETURNED TO THEM FOR EVALUATION.                                                     1H71 3T    NTA37CE           5  CP60GL    
20070618001042007061800104    2007       6          18         2007FA0000444    220070421G850012501           ENGINE                                                                                                                                                  MALFUNCTIONED   C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW03620TS                       20                                      AIRCRAFT ECU WARNING LIGHT COME ON FREQUENTLY.  WE SPOKE WITH THIELERT ABOUT THE PROBLEM AND THEY SAY THAT DURING STEEP BANKS OR YAW THE FUEL PRESSURE CAN BE DIFFERENT BETWEEN THE RAILS ON EACH ENGINE.  THE ECU CAN INTERPRET THIS AS A PROBLEM AND TURN ON THE ANNUNCIATOR.  THIS IS MOSTLY A NUISANCE BECAUSE EVERYTIME THE AN ANNUNCIATOR TURNS ON WE MUST BRING THE AIRCRAFT TO A MECHANIC WHO MUST CLEAR THE PROBLEM FORM THE COMMPUTER.  WHILE THE ANNUNCIATOR IS ON WE HAVE NO WAY OF KNOWING IF A REAL PROBLEM DEVELOPS BECAUSE THE ANNUCIATOR IS STILL ON. IN ADDITION AS A FLIGHT SCHOOL IT COSTS US SIGNIFICANT AMOUNTS OF LOST REVENUE EVERY TIME THAT WE MUST TAKE THE AIRPLANE OFF-LINE UNTIL OUR MECHANICE CAN INSPECT IT.   O                                          
20070601001162007060100116EU  2007       6          1          2007FA0000447    120070508G21505700700A        HOSE                                    SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B         NE                              A/C SYSTEM      BURST           D      K   NONE                                                                                            KJ FLUID LOSS                WARNING INDICATION                                  ININSP/MAINT     1                      EA01849BP                       3554        22310                       HIGH PRESSURE AIR CONDITIONER HOSE BURST.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3U3  U  H9EU    E00054EN             
20070530000162007053000016EA  2007       5          30         2007FA0000450    220070328G8530LW19279         CYLINDER                                CESSNA206   206H        2073301CE  LYC   O540  TIO540AJ1A       EA                              ENGINE          SCRATCHED       B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP28     1023 1023              T20608350   172S08719                   SET OF 6 CYLINDERS CAME IN WITH 2 BROKEN CONTROL RINGS. CYLINDERS HAD RING STEPS ON TOP AND BOTTOM OF CYLINDER BARRELS. CORROSION WAS PRESENT IN BARRELS FROM THE MIDDLE UP TO THE HEAD OF THE CYLINDERS. EXHAUST GUIDES WERE FAR OUT OF LIMITS AND DIFFICULT TO REMOVE RESULTING IN HAVING TO OVERSIZE 3 BOSSES TO P05 GUIDES AND THE OTHER 3 TO P10. 2 EXHAUST SEATS FELL OUT DURING THE HEAT SOAK FOR INSTALLING THE EXHAUST GUIDES. BROKEN RINGS DAMAGED 2 PISTONS WHICH HAD TO BE REMOVED FROM SERVICE. 4 OTHER PISTONS WERE DAMAGED IN THE PISTON PIN BOSSES. THE BROKEN RINGS ALSO CAUSED MODERATE SCRATCHING TO THE BARREL OF THE CYLINDERS WHICH WAS REMOVABLE BY POWER HONING. 2 CYLINDERS HAD TO BE OVERSIZED FROM THE CORROSION AND 1H71 3O3  ORTA4CE    E14EA                
20070613001672007061300167EA  2007       6          13         2007FA0000451    220070328G8530LW19279         CYLINDER                                CESSNA206   206H        2073301CE  LYC   O540  TIO540AJ1A       EA                              ENGINE          SCRATCHED       B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP07     1023 1023              T20608350   172S08719                   SET OF 6 CYLINDERS CAME IN WITH 2 BROKEN CONTROL RINGS. CYLINDERS HAD RING STEPS ON TOP AND BOTTOM OF CYLINDER BARRELS. CORROSION WAS PRESENT IN BARRELS FROM THE MIDDLE UP TO THE HEAD OF THE CYLINDERS. EXHAUST GUIDES WERE FAR OUT OF LIMITS AND DIFFICULT TO REMOVE RESULTING IN HAVING TO OVERSIZE 3 BOSSES TO P05 GUIDES AND THE OTHER 3 TO P10. 2 EXHAUST SEATS FELL OUT DURING THE HEAT SOAK FOR INSTALLING THE EXHAUST GUIDES. BROKEN RINGS DAMAGED 2 PISTONS WHICH HAD TO BE REMOVED FROM SERVICE. 4 OTHER PISTONS WERE DAMAGED IN THE PISTON PIN BOSSES. THE BROKEN RINGS ALSO CAUSED MODERATE SCRATCHING TO THE BARREL OF THE CYLINDERS WHICH WAS REMOVABLE BY POWER HONING. 2 CYLINDERS HAD TO BE OVERSIZED FROM THE CORROSION AND 1H71 3O3  ORTA4CE    E14EA                
20070607000072007060700007SO  2007       6          7          2007FA0000453    120070407G56101159SCB31023    WINDSHIELD                              GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6118          EU                              COCKPIT         FAILED          B  JUORO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP27495RS2735                   1161                                    CREW REPORTS WINDSHIELD FAILURE DURING PART 91 MAINTENANCE POSITIONING FLIGHT.  EMERGENCY DECLARED WITH UNEVENTFUL LANDING.  AIRCRAFT CONTINUED TO DESTINATION AIRPORT UNDER CDL RESTRICTIONS.  UNKNOWN CAUSE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA12EA   E25NE                
20070601001072007060100107SO  2007       6          1          2007FA0000454    220070501G7414                BRUSHES                                 CIRRUSSR    SR20        05628AJGL  CONT  O360  IO360ES          SO                              MAGNETO         WORN            B  YYBRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL03154WF423                    1638        360136                      THIS MAGNETO WAS MISFIRING, AND APPEARS TO HAVE CAUSED DETONATION IN THE NR 5 CYLINDER.  PISTON MATERIAL WAS FOUND IN THE OIL FILTER AND OIL COOLER.  ENGINE HAD TO BE REMOVED, INSPECTED, AND REPAIRED DUE TO THE DETONATION.  THE MAGNETO WAS FOUND TO HAVE A SEVERELY WORN BRUSH (K3215), THE BRUSH BLOCK WAS MELTED (K3823), THE COIL WAS BURNED CLOSE TO THE BRUSH CONTACT POINT (K3975), AND THE POINTS WERE BADLY BURNED (M3081).  THIS IS THE (3RD) OCCURRENCE FOUND WITH THIS SAME PROBLEM.  (K)                                                                                                                                                                                                                                       1L71 3O3  ONTA00009CHE1CE                 
20070601001122007060100112CE  2007       6          1          2007FA0000455    120070505G323008940002        GEARBOX                                 CESSNA340   340A        2076405CE  CONT  O520  TSIO520*    17040SO                              MLG             DAMAGED         B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW172745F                       340A0949                                GEAR MOTOR, REDUCTION GEAR BOX AND GEAR TRANSMISSION WERE REMOVED AND SENT OUT TO FOR INSPECTION.  WHEN THEY OPENED GEAR REDUCTION BOX, THEY DISCOVERED THAT ONE OF THE MOUNTING BOLTS HAVE BEEN OF THE IMPROPER LENGTH CAUSING THE THREAD PATTERN.  TBOLT SHOWS SLIGHT WEAR WHERE IT TOUCHED THE GEAR SYSTEM.  ACCORDING TO MFG THERE WAS ONLY A SLIGHT TRANSFER TO GEAR, WHICH THEY FEEL WOULD NOT HAVE CAUSED A PROBLEM.  CANNOT DETERMINE HOW LONG THIS CONDITION EXISTED.  THE BOLTS LOOK TO BE OLD AND THE INTERNAL GEAR BOX SEEMS ALSO TO BE OLD.  THE INSTALLATION CALLED FOR A .8750 INCH BOLT FOR THIS MOUNTING HOLE, AND REMOVED A 1 INCH BOLT.  THE CORRECTIVE ACTION IS TO INSTALL THE REPAIRED GEAR BOX AND THE CORRECT MOUNTING H1L72 3O3  O  3A25    E8CE                 
20070607000312007060700031GL  2007       6          7          2007FA0000456    320070516G6110B24573          FORK                                    BNORM BN2   BN2         1520202EU                                   HARTZLHCC2Y HCC2YK2     GL  PITCH CHANGE    UNSERVICEABLE   B  ME4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO19                                                    AU9949B         STEEL FATIGUE CRACK NDT (MAGNETIC PARTICLE) DETECTED.  PROPELLER ASSY RECEIVED FOR STANDARD OVERHAUL AND DEFECT FOUND IN PROPELLER ASSY (PN C2K00500, DESCRIPTION HC-C2YK-2CUF/FC8477A-4, SN AU9949B), UNDER WO NR 38425A.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H72 3O      A17EU           5  CP920     
20070607000092007060700009GL  2007       6          7          2007FA0000457    320070516G6111F8468A6R        BLADE                                   PZLWARWILGA PZL104W35A  7360104EU  LYC   O540  IO540K1B5   41532EA  HARTZLHCC3Y HCC3YR      GL  PROPELLER       CRACKED         B  ME4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO19424HD                       00030015                DY2965A         ALUMINUM FATIGUE CRACK VISUALLY AND NDT DETECTED.  PROPELLER ASSY RECEIVED FOR OVERHAUL AND BLADE NR 2 OF 3 REMOVED FROM PROPELLER ASSY (HC-C3YR-1RF/ F8468A-6R, UNDER WO NR 38598A.  NOTE: MANDATORY OVERHAUL REQUIRED DUE TO GROUND STRIKE, HOWEVER, BLADE SUBMITTED WAS NOT BENT AND LEAST DAMAGED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3R3  ONCEXPA1H711E4     5  CP25EA    
20070601001132007060100113WP  2007       6          1          2007FA0000458    220070502G7321307080026       FUEL CONTROL                            AMD   FALC90FALCON900B  2730171EU  GARRTTTFE731TFE7315BR        WP                              ENGINE          FAULTY          C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA034MB  5476 1861              146         P101199                     PILOTS REPORTED THAT ENGINE THAT THIS FUEL CONTROL UNIT WAS INSTALLED ON COULD NOT BE CONTROLLED BY NORMAL COMPUTER MODE, AND THAT WHEN THEY WENT TO MANUAL MODE THAT THEY COULD NOT CONTROL ENGINE SPEED FUNCTIONS EITHER.  IT SEEMS THAT THIS FUEL CONTROL HAS SOME INTERNAL FAULT.  REPLACEMENT FUEL CONTROL RESOLVED THIS PROBLEM.  (K)                                                                                                                                                                                                                                                                                                                                                                                                     2L73 4F4  FRT        E6WE                 
20070606000012007060600001CE  2007       6          6          2007FA0000459    120070404G272004140161532     BRACKET                                 CESSNA172   172F        2072414CE  CONT  O300  O300*       17022SO                              RUDDER CONTROL  BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL098879U2961                   17252796                                DURING ANNUAL INSPECTION BRACKET (PN 04140616-1-532).  FOUND BROKEN AND CRACKED IN OTHER LOCATIONS.  LOCATED UNDER FLOOR CENTER SECTION AT FLIGHT CONTROL BELL CRACK.  REPLACED WITH NEW PART.  REQUEST INSPECTORS CHECK THIS AREA OF THE FLIGHT CONTROLS CAREFULLY DURING 100/ANNUAL INSPECTION. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O3  ONT3A12    E253                 
20070601001152007060100115CE  2007       6          1          2007FA0000460    120070430G3297D3899924WD19    CONNECTOR                               RAYTHN390   390         7150030CE  WILINTFJ44  FJ44        66000GL                              ANTI SKID SYS   FAULTY          B  E81RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL03972PF976                    RB38                                    TROUBLESHOT INTERMITTENT ANTI-SKID SYSTEM FAIL ANNUNCIATION, CABIN DOOR SEAL STAYING INFLATED ON GROUND, AND LIFT DUMP HANDLE OPERATION.  FOUND BAD CRIMP ON PIN (L) FOR WIRE G117B24 IN LT MLG SQUAT SWITCH CONNECTOR.  FUNCTIONAL CHECKS OK.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 3F4  FRTA00010WIE3GL                 
20070601001142007060100114SO  2007       6          1          2007FA0000461    220070309G74141051324         SPRING          CONT                    BEECH 58    58          1152740CE  CONT  O550  IO550C           SO                              MAGNETO         BROKEN          E  MKWAO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL037293R827        F02CA139R   TH590       824323R                     WHILE TROUBLESHOOTING ENGINE RUNS ROUGH AND WONT RUN AT ALL OVER 1200 RPM.  WE DISCOVERED THE IMPULSE COUPLING SPRINGS ON BOTH MAGS WERE BROKEN.  (IMPULSE COUPLING , PN 10-400309)  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3O3  O  3A16    E3SO                 
20070607000332007060700033SO  2007       6          7          2007FA0000462    220070309G74141051324         SPRING          CONT                    BEECH 58    58          1152740CE  CONT  O550  IO550C           SO                              MAGNETO         BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL037293R827        F02CA164R   TH590       824323                      WHILE TROUBLESHOOTING ENGINE RUNS ROUGH AND WON`T RUN AT ALL OVER 1200 RPM.  WE DISCOVERED THE IMPULSE COUPLING SPRINGS ON BOTH MAGS WERE BROKEN.  (IMPULSE COUPLING PN 10400309) (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 3O3  O  3A16    E3SO                 
20070606000022007060600002CE  2007       6          6          2007FA0000463    120070514G5711                SPAR                                    BBAVIA11    11BC        0191106CE  LYC   O235  O235*       41505EA  SNSNCH76AK  M76AK       EA  LT WING         CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL093581E                       11AC1813    108715      11544           DELAMINATION OCCURRING AT WING STRUT ATTACH LOCATION.  CRACK AT BOTTOM EDGE AT ROOT FITTING.  POSSIBLE AGE OF SPAR CAUSING DELAMINATION.  LONGITUDINAL CRACK AT WING ROOT POSSIBLE EARLIER DAMAGE REPLACE WITH NEW WOOD SPAR (PN 5146L).  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  O  A761    E223    5  N1P210    
20070615001032007061500103    2007       6          15         2007FA0000464    120070430G6100                BOLT                                                                       LYC   O360  O360*       41514EA  MCAULY1A200 1A200*      GL  PROPELLER       SHORT           D      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      AL05866MM400                                            YI46003         INSPECTING PROPELLER DURING ANNUAL, FOUND PROPELLER BOLTS 0.25 IN SHORT OF BACK SIDE OF FLANGE INSERTS.  ALL BOLT THREAD ENGAGEMENT WAS FORWARD OF INSERT BOSS.  AFT .2500 INC OF INSERT, MATERIAL BEHIND CRANK FLANGE, HAD NO THREAD ENGAGEMENT.  WRONG BOLTS INSTALLED, CORRECTED BY INSTALLING PROP BOLT KIT (PN 76EM8) WHICH PROVIDED (2) THREADS THROUGH INSERT WHEN TROQUED.  (K)                                                                                                                                                                                                                                                                                                                                                                3  O          E286    5  NP874     
20070607000142007060700014EU  2007       6          7          2007FA0000465    120070509G3411                PITOT LINE                              AMD   FALC10FALCON10    2730101EU  GARRTTTFE731TFE731*     01518WP                              NR 2            LOOSE           B  EBVRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE09160FJ                       160                                     WHILE TROUBLESHOOTING A LEAK IN NR 2 STATIC SYSTEM, THE RT SIDE STATIC PLATE HAD TO BE TAKEN LOOSE.  UPON REMOVAL OF THE PLATE, SILICONE RTV WAS FOUND ON THE FITTING FOR THE NR 1 STATIC SYSTE.  WHEN THE FITTING WAS LOOSENED, FOUND A LAGRE AOUNT OF TEFLON PIPE TAPE WRAPPED AROUND THE NIPPLE OF THE STATIC PLATE, AND THE FLARE OF THE ALUMINUM HARD LINE GOING TO THE STATIC PLATE WAS BROKEN OFF AND LAYING LOOSE IN THE ASSY.  A TECH IN THE PAST HAD POSSIBLY EXPERIENCED A LEAK ON THIS SYSEM, AND LOADED THE NIPPLE WITH TEFLON TAPE AND RTV TTO GET THE SYSTEM TO SEAL, INSTAD OF REPAIRING THE HARD LINE.  THESE LINES SHOULD BE REPAIRED IAW STANDARD PRACTICE TO PREVENT PREMATURE FAILURE.  (K)                                2L72 4F4  F  A33EU   E6WE                 
20070605002722007060500272CE  2007       6          5          2007FA0000466    120070201G3310                LIGHT                                   CESSNA340   340A        2076405CE  CONT  O520  TSIO520*    17040SO                              COMPASS         FIRE            D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE03340JH                       340A0771                                COMPASS LIGHT/SOCKET OVERHEATED DURING TAXI AND CAUGHT FIRE BEFORE THE CIRCUIT BREAKER TRIPPED.  PILOT EXTINGUISHED FIRE WITH HANDKERCHIEF.  CAUSE UNKNOWN, NO DAMAGE TO AIRCRAFT INTERIOR OR STRUCTURE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3O3  O  3A25    E8CE                 
20070607000352007060700035CE  2007       6          7          2007FA0000467    120070316G5532                SKIN                                    BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A6       52043EA                              VERTICAL STAB   DAMAGED         B  E81RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL03135YV                       UE135                                   VERTICAL STABILIZER LEADING EDGE SKIN ATTACH RIVETS WORKING.  FOUND THAT THE ORIGINAL UNIVERSAL HEAD RIVETS WERE REPLACED WITH FLUSH RIVETS.  THE SKIN WAS COUNTERSUNK TO ACCOMMODATE THE RIVETS, HOWEVER THE SKIN WAS TOO THIN TO COUNTERSINK AND EVENTUALLY WORKED LOOSE.  SKIN WAS REPAIRED IAW DER ENGINEERING REPORT AND CORRECT RIVETS INSTALLED.  STRICT ADHERENCE TO PUBLISHED DATA WOULD HAVE PREVENTED DAMAGE.  (K)                                                                                                                                                                                                                                                                                                                   2L72 4T3  TRTA24CE   E4EA                 
20070607000342007060700034EU  2007       6          7          2007FA0000468    120070501G5610D25W343001009   WINDSHIELD                              ISRAEL1125  ASTRASPX    4500205EU                                                               COCKPIT         CRACKED         B  UO2RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL19411MM                       080                                     THE WINDSHIELD ON THE PILOT`S SIDE CRACKED DURING FLIGHT AT F/L 41,000 FT ON 4/24/2007.  THE WINDSHIELD HAD 3104.6 TT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F    RTA16NM                        
20070607000262007060700026CE  2007       6          7          2007FA0000469    120070227G3220C611300518      LINK                                    BEECH 90    F90         1152909CE                                                               NLG             DAMAGED         B  E81RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL03189JR                       LA61                                    THIS REPORT IS A RESULT OF REPLACEMENT OF THE FORWARD NOSE GEAR RETRACT CHAIN.  TO REPLACE OR TO REINSTALL THIS CHAIN, A NEW PN C-6113005-18, CONNECTING LINK MUST BE USED.  A NEW LINK SHOULD HAVE FIVE PIECES.  ONE LINK ASSY WITH (2) SHAFTS SWAGED INTO AN END PLATE, TWO CENTER PLATES THAT SHOULD SLIP ONTO THE SHAFTS, ONE END PLATE, AND ONE SPRING CLIP RETAINER.  THE END PLATE SHOULD HAVE SMALLER HOLES IN IT AND REQUIRE PRESSING FOR PROPER ASSY.  THIS PRESSED FIT REQUIRES DISTRUCTION OF THE LINK DURING ASSY.  WHEN INSTALLING THE NEW CHAIN AND INSTALLING THE NEW LINK, FOUND THAT ALL THREE PLATES HAD THE HOLE SIZE THAT WOULD ALLOW THEM TO BE SLIPPED ONTO THE SHAFTS WITHOUT PRESSING.  CHECKED ANOTHER NEW LINK ASSY. 1L72 4T      A31CE                        
20070605002732007060500273CE  2007       6          5          2007FA0000470    120070226G21701013840245      EVAPORATOR                              BEECH 200   B200        1152922CE                                                               AIR CONDITIONER UNSERVICEABLE   D  E81RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL03                                                                    AFT CABIN AIR CONDITIONER EVAPORATOR RECEIVED FROM VENDER IN OVERHAULED CONDITION.  INITIAL INSPECTION REVEALED HARD LINE.  WHICH SHOULD RUN PARALLEL TO HEAT EXCHANGER, WAS INSTALLED APPROXIMATELY 25 DEGREES TO HEAT EXCHANGER.  THE EVAPORATOR COULD NOT HAVE BEEN INSTALLED WITHOUT STRESSING AIRCRAFT HARD LINES.  THIS LINE HAD BEEN REPAIRED (BY WELDING?) HOWEVER, THE INSIDE SURFACE STILL SHOWED SEVERE PITTING.  THE UNIT WAS RETURNED TO VENDER AS WELL AS VENDER SHOULD HAVE CAUGHT THESE DEFECTS.  (K)                                                                                                                                                                                                                           1L72 4T      A24CE                        
20070607000322007060700032SW  2007       6          7          2007FA0000471    120070404G321312984           LOCK NUT                                BBAVIA7     7ECA        21101NNSW  LYC   O290  O290*       41506EA                              MLG LEG         STRIPPED        G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM136096F1642                   7ECA352                                 LOCK NUT THREADS FAILED, MLG STRUT EXTENDED ON TAKEOFF ALLOWING MLG TO SWING FREE.  DURING LANDING, MLG WAS UNDER FUSELAGE CAUSING DAMAGE TO LOWER LONGERONS, CONDITION OF THREADS CANNOT BE DETERMINED WITHOUT DISASSEMBLING THE MLG STRUT ASSY.  THEREFORE, THE THREADS MAY DETERIORATE SIGNIFICANTLY WITHOUT DETECTION.  SUGGEST SPECIAL EMPHASIS INSPECTION ROUTINE AT (5) YEAR INTERVALS TO INCLUDE DISASSEMBLY OF MLG STRUT ASSY.  (K)                                                                                                                                                                                                                                                                                                    1H71 3O3  O  A759    E229                 
20070604000152007060400015    2007       6          4          2007FA0000472    220070510G7322105018          BOWL                                                                                                                                    CARBURETOR      DAMAGED         B  NE2RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE07                A44695                                              RECEIVED CARBURETOR FROM CUSTOMER WITH THE REQUEST (PLEASE INSPECT UNIT FOR PROPER OPERATION, AIRCRAFT ON GROUND.  HAVE BEEN BOMBARDED WITH SERIOUS PROBLEMS TO JUST ABOUT EVERY CARBURETOR WE HAVE) PILOT STATED THAT HE ALMOST CRASHED HELICOPTER DUE TO LACK OF ENGINE RESPONSIVENESS AFTER ROLLING THROTTLE IN AFTER TEST AUTO ROTATION.  INSPECTION OF CARBURETOR REVEALED VENT PORTS IN BOWL AND THROTTLE BODY WERE NOT IN THE NORMAL POSITION NOR THE NORMAL SIDE FOR THIS CARBURETOR MODEL.  COULD NOT POSITIVELY IDENTIFY THE IDLE TUBE AND NOZZLE AS OEM PARTS.  THE ACCELERATOR PUMP DISCHARGE CHECK VALVE DID NOT FUNCTION IN THE MANNER NORMALLY SEEN BY THIS REPAIR STATION.  THROTTLE BODY HAS ECONOMIZER JET INSTALLED WHICH IS                                           
20070606000032007060600003EU  2007       6          6          2007FA0000473    120070511G62101090103019      BLADE                                   AGUSTAA109  A109        0260109EU  ALLSN 250C  250C20B     03013GL                              MAIN ROTOR      CRACKED         D      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              LDLANDING        1                      NM01109CJ2031                   7280                                    SKIN CRACKS WERE DISCOVERED IN THIS BLADE UPON INVESTIGATION OF AN UNUSUALLY HIGH VIBRATION LEVEL AS REPORTED BY THE PILOT.  THE ONE-PER-REV VERTICAL VIBRATION WAS ESPECIALLY NOTICEABLE DURING THE LANDING PHASE OF FLIGHT.  INSPECTION OF THIS BLADE REVEALED CORD-WISE CRACKS IN THE TOP AND BOTTOM SKINS WHICH EXTEND FROM THE TRAILING EDGE AT STA 3135 TO THE AFT EDGE OF THE SPAR AT STA 3123.  THE CRACKS THEN EXTEND SPAN-WISE FROM STA 2940 TO STA 3225.  THE CRACK IN THE LOWER SKIN BISECTS A SKIN REPAIR AT STA 3130, APPROXIMATELY 2 INCHES FORWARD OF THE TRAILING EDGE.  THIS REPAIR WAS ACCOMPLISHED WITH AD 2000-15-20 AND BT 109-111 UNDER WO NR 8-080132-84, DATED 4/24/2006.  BT 109-50, PART I REQUIRES DAILY VISUAL INSP1G72 3U3  U  H7EU    E4CE                 
20070606000042007060600004NE  2007       6          6          2007FA0000474    220070507G7420                IGNITION LEAD                           CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              LT ENGINE       OUT OF POSITION B      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      EA25228PC                       5600310                                 WHILE DEPARTING, ENCOUNTERED A  75 PERCENT THROTTLE SPLIT WITH THE LEFT ENGINE ACHIEVING ONLY 93 PERCENT N1.  A MFG PHASE B INSPECTION WAS PERFORMED ON THE AIRCRAFT ON 5/5/2007.  WHILE PERFORMING THE PHASE B INSPECTION ITEM B742001, TASK 74-31-00-210 (ENGINE IGNITERS OPERATIONAL TEST), IT WAS DETERMINED THAT THE RT IGNITER LEAD ON THE LT ENGINE WAS RE-INSTALLED IN A POSITION THAT AFFECTED THE THROTTLE LINKAGE AND PREVENTED FULL TRAVEL OF THROTTLE LEVER IN THE FLIGHT DECK.  FURTHER INVESTIGATION REVEALED THAT THERE IS NO REFERENCE OR PRECAUTIONS IN THE MM AS TO THE RE-INSTALLATION POSITION OF THE LEAD UPON REMOVAL AND RE-INSTALLATION OF THE IGNITER PLUG.  INSTALLING THE IGNITER LEAD END TO THE IGNITER WITH A 90 2L72 4F4  FRTA22CE   E25EA                
20070607000032007060700003EU  2007       6          7          2007FA0000475    120070430G25204311935         HOUSING                                 AMD   FALC50FALCON900   2730160EU  GARRTTTFE731TFE731*     01518WP                              SEAT ROLLER     MISMANUFACTURED B  UO2RO   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      GL19678CH                       47                                      (8) SEATS, MODEL 5004 (SINGLE) WERE PURCHASED.  THE SEATS HAVE (3 FT) ON EACH CORNER (12 TOTAL) THAT ARE TO FIT INTO THE SEAT RAIL.  SAID PURCHASED SEATS DID NOT FIT INTO THE EXISTING MFG SEAT RAIL.  MFG WAS CONTACTED.  IT WAS DETERMINED BY THE MFG THAT THE (3 FEET) BY THE MFG THAT THE (3 FEET) ON EACH CORNER (12 TOTAL) WERE BEING MFG INCORRECTLY.  THE SEATS ARE DESIGNED TO FIT INTO (2 TRACKS).  THE FRONT 3 AND BACK 3 FEET ON THE LT SIDE OF THE CHAIR ARE PART OF A (ROLLER HOUSING).  EACH CHAIR HAS (2) ROLLER HOUSINGS.  MFG IS PROVIDING 16 REPLACEMENT ROLLER HOUSINGS (PN 431193-5). (K)                                                                                                                                 2L73 4F4  FRTA46EU   E6WE                 
20070613001662007061300166GL  2007       6          13         2007FA0000476    120070504G7160BA24            AIR FILTER                              CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO  HARTZLHCJ3Y PHCJ3YF1    GL  ENGINE INTAKE   DEBONDED        B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA17711KW                       1348        917594      FP3492B         APPEARS THAT THE FOAM AIR FILTER ELEMENT, THAT IS CYLINDER SHAPED AND BONDED TOGETHER, DID NOT HAVE SUFFICIENT GLUEUU OR CAME UNBONDED AND WAS ALLOWING UNFILTERED AIR TO ENTER THE ENGINE INTAKE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  ONTA00009CHE3SO    5  CP36EA    
20070613001682007061300168GL  2007       6          13         2007FA0000477    120070507G2720                BUNGEE                                  CIRRUSSR    SR22        2130001GL                                                               RUDDER          MISRIGGED       B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA07519SR                       2072                                    DURING INSPECTION FOUND RUDDER AILERON INTERCONNECT BUNGEE MISRIGGED AND INTERTFERING WITH THE AILERON CONTROLS. THERE IS NO EVIDENCE THAT THIS AIRCRAFT HAS HAD ANY MAINTENANCE TO THIS SYSTEM SINCE LEAVING THE FACTORY. ANOTHER AIRCRAFT WITH THIS CONDITION HAD THE CONTROL SYSTEM JAM WITH FULL OPPOSITE RUDDER AND AILERON. IT APPEARS THAT THIS CONDITION IS CAUSED BY IMPROPER RIGGING OF THE INTERCONNECT SYSTEM AT THE FACTORY.                                                                                                                                                                                                                                                                                                       1L71 3O    NTA00009CH                     
20070613002042007061300204EA  2007       6          13         2007FA0000478    220070510G8530LW12987         CYLINDER                                                                   LYC   O540  IO540*      41532EA                              ENGINE          ERODED          B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW17                                                                    AFTER REMOVAL OF THE CYLINDER BARREL FROM THE CYLINDER HEAD, SEVER ERROSION WAS NOTED JUST ABOVE THE SEAL BAND AREA. IF THE BARREL HAD NOT BEEN REMOVED, THIS ERROSION WOULD HAVE BEEN UNDETECTED AND WOULD HAVE CAUSED A HEAD AND BARREL SEPERATION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  3  O          1E4                  
20070618001052007061800105CE  2007       6          18         2007FA0000479    120070516G251004101342        SEAT                                    CESSNA150   150F        2071814CE  CONT  E185  E185*       17014SO                              COCKPIT         CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE018095S                       15061695                                SEAT PAN WAS FOUND CRACKED AT THE FORWARD END OF PILOTS OB SEAT RAIL STIFFENER, APPROXIMATELY 1 NR LONG ACROSS SCREW HOLES. STIFFENER PN 0411546-1 WAS ALSO CRACKED AT CUTOUT FOR FUEL LINE. TOTAL AIRFRAME TIME UNKNOWN, BUT GREATER THAN 1300 HOURS. THESE CRACKS ARE SOMEWHAT COMMON ON 3000 TO 5000 HOUR AIRPLANES.                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  3A19    E246                 
20070615002242007061500224SO  2007       6          15         2007FA0000480    120070523G57116707003         SPAR CAP                                PIPER PA28  PA28140     7102802SO  LYC   O320  O320*       41508EA                              RT WING         CORRODED        G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO154579R3465                   2821321                                 FUEL TANK REMOVED DUE TO LEAKING VENT LINES. UPON REMOVAL, DISCOVERED RT WING UPPER SPAR CAP SEVERLY CORRODED. MAJOR EXFOLIATION TO THE SPAR CAP AT THE OB SECTION OF THE FUEL TANK OPENING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3O3  O  2A13    E274                 
20070618001062007061800106CE  2007       6          18         2007FA0000481    120070523G5311051212497       SPAR                                    CESSNA172   172RG       2072438CE  LYC   O360  O360F1A6    41514EA  MCAULY2D34C B2D34C220   GL  FUSELAGE        DAMAGED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW155145U14529100               172RG0258   L2767336A   961976          FOUND SMOKING RIVETS ON TOP OF FUSELAGE IN AREA OF THE REAR CENTER SECTION SPAR.  REMOVED RIVETS (APPROX. EIGHT ON EACH END OF SPAR) AND FOUND RIVET HOLES SEVERELY ELONGATED.  FACTORY ORIGINAL RIVETS WERE .1250 INCH DIA. AND SEVERAL HAD BEEN REPLACED IN THE FIELD WITH .1562 INCH RIVETS.  ALL OF THE AFFECTED RIVET HOLES HAD BECOME OVERSIZED TO AN EXTENT THAT RENDERED THE SPAR AND OVERLAPPING FUSELAGE SKINS UNSERVICEABLE.                                                                                                                                                                                                                                                                                                         1H71 3O3  O  3A17    E286    5  CP7EA     
20070615002132007061500213SO  2007       6          15         2007FA0000482    120070523G57116205401         SPAR                                    PIPER PA28  PA28R180    7102809SO                                                               RT WING         CORRODED        G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO153208R14400                  28R3113                                 RT WING REMOVED DUE TO DAMAGE. WING WAS SCRAPPED AND DEALER WANTED STEEL FITTINGS REMOVED. UPON REMOVAL OF REAR SPAR ATTACH PLATE, SEVERE CORROSION WAS FOUND ON THE SPAR UNDER THE PLATE. CONDITION WAS VERY SERIOUS AND COULD HAVE LEAD TO AN INFLIGHT FAILURE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O      2A13                         
20070615002142007061500214CE  2007       6          15         2007FA0000483    120070525G2400                UNKNOWN                                 BEECH 35    K35         1151524CE  CONT  O470  IO470N      17026SO  MCAULY2A36C 2A36C23     GL                  UNKNOWN         C      H   DEACTIVATE SYST/CIRCUITS                                                                        H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CE076061E                       D5996       096827R     7710181         LOST ELECTRICAL POWER.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3O3  O  3A15    3E1     5  CP880     
20070615002162007061500216EA  2007       6          15         2007FA0000484    220070525G7322MA45            CARBURETOR                              PIPER PA24  PA24        7102402SO  LYC   O360  O360*       41514EA                              ENGINE          WORN            D      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      EA237204P748  748               242374                                  THE ACCELERATOR PUMP IN THE CARBURETOR FAILED.  INSPECTION SHOWED THAT THE PUMP HEAD GLAND HAD SHRUNK, SO THAT IT DID NOT PROVIDE A SEAL BETWEEN THE CARBURETOR BODY AND THE PUMP ITSELF.  THE RESULT WAS THAT ADVANCING THE THROTTLE DID NOT CAUSE FUEL TO BE SQUIRTED FROM THE PUMP EXIT ORIFICE.  REPLACEMENT OF THE PUMP RESOLVED THE PROBLEM.                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  1A15    E286                 
20070615002102007061500210EU  2007       6          15         2007FA0000486    120070530G27521391T1008       ACTUATOR                                ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE731*     01518WP                              FLAP            MISALIGNED      B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE0927TZ                        213                                     INSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T100-8, SN 387AB.  FLAP OPERATION WAS NORMAL.  WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR.  A COVER PLATE ON THE FLAP ACTUATOR HAD BEEN INDEXED INCORRECTLY AND WAS INTERFERING WITH THE AILERON BELLCRANK.  PROBABLE CAUSE WAS INCORRECT ASSEMBLY OF FLAP ACTUATOR.                                                                                                                                                                                                                                                                                                                                             2M72 4F4  F  A2SW    E6WE                 
20070615002112007061500211EU  2007       6          15         2007FA0000487    120070530G27521391T1008       ACTUATOR                                ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE731*     01518WP                              FLAP            MISALIGNED      B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE0927TZ                        213                                     INSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T100-8, SN 387AB.  FLAP OPERATION WAS NORMAL.  WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR.  A COVER PLATE ON THE FLAP ACTUATOR HAD BEEN INDEXED INCORRECTLY AND WAS INTERFERING WITH THE AILERON BELLCRANK.  PROBABLE CAUSE WAS INCORRECT ASSEMBLY OF FLAP ACTUATOR.                                                                                                                                                                                                                                                                                                                                             2M72 4F4  F  A2SW    E6WE                 
20070618001082007061800108    2007       6          18         2007FA0000489    220070530G7414                CAPACITOR                                                                                                                               MAGNETO         FAILED          C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW15                                                                    IN READING AN ALERT FROM APRIL 2007 REFERRING TO SLICK MAGNETO CAPACITOR FAILURE PN M-3984 STATES THAT OIL/DIELECTRIC FLUID LEAKED FROM THE CAPACITOR.  THAT IS A DRY CAPACITOR AND CONTAINS NO FLUID. HAVE CUT OPEN SEVERAL FOR TRAINING AIDS AND NO LIQUID EXISTS IN THAT PART.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         
20070615002182007061500218SO  2007       6          15         2007FA0000490    220070525G8520IO240A          CRANKSHAFT                                                                 CONT  O240  IO240B      17063SO                              ENGINE          CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW17                                                                    CRANKSHAFT  HAD A VERY LARGE, DEEP FORGING LAP ON THE NR 3 CRANK CHEEK. AN EFFORT WAS MADE TO REMOVE THE LAP BY LOCALIZED GRINDING BUT THE IT WAS TOO DEEP TO REMOVE. CRANKSHAFT WAS DETERMINED UNAIRWORTHY BY ENGINEERING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            3  O          E7SO                 
20070615002212007061500221    2007       6          15         2007FA0000491    420070429G2215065001790100    SERVO                                   CESSNA182   182S        2072701CE  LYC   O540  IO540*      41532EA                              AILEONS         BINDING         D      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      SW099875F1056                   18280141                                PILOT/OWNER REPORTED TO MX THAT ON APPROACH AFTER DISENGAGING AUTOPILOT, AILERONS WERE DIFFICULT TO MOVE. NO WINDS AND STABLE APPROACH MINIMIZED PROBLEM. MX NOTED AILERONS WERE EXTREMELY DIFFICULT TO MOVE, AND FURTHER MOVEMENT COULD HAVE CAUSED EVEN GREATER DIFFICULTY OR COMPLETE IMMOBILIZATION OF THE AILERONS. AILERON SERVO WAS REMOVED AND SENT OUT FOR EXCHANGE. IT WAS NOTED ON REMOVAL THE OUTPUT SHAFT SUPPORT BEARING WAS LOOSE AND BINDING.                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A13    1E4                  
20070615002222007061500222CE  2007       6          15         2007FA0000492    120070531G575307620382        BELLCRANK                               CESSNA182   182S        2072701CE  LYC   O540  IO540*      41532EA                              TE FLAPS        BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW099875F1056                   18280141                                DURING ANNUAL INSPECTION, IT WAS NOTED THAT THE (BELLCRANK ASSY) ON THE FLAP FEEDBACK LEVER, BEHIND THE INSTRUMENT PANEL, WAS BROKEN IN TWO, IT CONSIST OF A PLASTIC BLOCK WITH A SLOT IN IT WHICH MOVES THE MICROSWITCH ASSY TO ACTIVATE, OR DEACTIVATE THE FLAP DRIVE MOTOR. THE BLOCK IS ATTACHED WITH 2 RIVETS OF SOME TYPE. THE END OF THE BLOCK IS CRACKED COMPLETELY THROUGH ALLOWING SEPARATION OF THE UPPER AND LOWER HALVES. THIS ALSO STRESSED THE ATTACHING RIVETS CAUSING CRACKS, AND EXCESSIVE MOVEMENT.  (PICS ARE AVAILABLE)  IF PART COMPLETELY FAILED IT COULD ALLOW COMPLETE UNCOMMANDED FLAP DEPLOYMENT OR INABILITY TO RETRACT FLAPS, SUCH AS A BALKED LANDING.                                                            1H71 3O3  ONT3A13    1E4                  
20070615002232007061500223    2007       6          15         2007FA0000493    220070530G7414M3984           CAPACITOR                                                                                                                               MAGNETO         NONE            C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW15                                                                    IN READING AN ALERT FROM APRIL 2007 REFERING TO SLICK MAGNETO CAPACITOR FAILURE PART NR  M-3984 STATES THAT OIL/DIELECTRIC FLUID LEAKED FROM THE CAPACITOR.  THAT IS A DRY CAPACITOR AND CONTAINS NO FLUID.  I HAVE CUT OPEN SEVERAL FOR TRAINING AIDS AND NO LIQUID EXSISTS IN THAT PART.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
20070618002112007061800211    2007       6          18         2007FA0000494    420070604G22166565001197      CABLE                                   CESSNA500   550         2076604CE                                                               AUTOPILOT       FRAYED          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW014614N7737 300               5500659                                 WE HAVE FOUND THE ELEVATOR CABLE AT THIS SERVO P/N 4006719-904 SHOWING EXCESSIVE WEAR ON AIRCRAFT UNDERGOING PHASE 1-4 AND ALSO PHASE 5 INSPECTIONS. THE CABLE WAS FOUND WHERE IT PASSES THROUGH AT FS. 428.50 AND IS DIFFICULT TO SEE. THIS CABLE HAD APROX. 3 STRANDS TO GO TO TOTAL FALURE. THE IPC REFERENCE FOR THE CABLE IS 22-10-00, FIGURE 1, PAGE 3, ITEM 85                                                                                                                                                                                                                                                                                                                                                                           1L72 4F      A22CE                        
20070618002222007061800222NM  2007       6          18         2007FA0000495    120070606G3060SMR2263         HEATER          HARTZL                  LANCARLC40  LC40550FG   5150000NM  CONT  O550  TSIO550C         SO                              PROP BLADES     DEBONDED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW071439C226        LX197B      41618       914411                      INBOARD PORTION OF ALL THREE PROP DEICE BOOTS DEBONDED AGAIN.  ON THIS PROP, NEW BLADES WERE SENT FROM HARTZELL DUE TO DEBOND OF PREVIOUS BOOTS AT 28.4 HRS TT AND AGAIN AT 28.9 HRS TT.  RETAINER STRAP AND BOOT DEBONDS DUE TO CENTRIFUGAL FORCE PULLING DEICE BOOT LEAD ON EACH PROP BLADE.  THIS HAS HAPPENED ON FIVE OR MORE LANCAIR COLUMBIA AIRCRAFT.  THE SEALING PROCESS FOR THE RETAINER STRAP IS LACKING.  SMR TECHNOLOGIES AND HARTZELL NEED A BETTER STRAP OR A GOOD TY-RAP.                                                                                                                                                                                                                                                       1L71 3O3  ORTA00003SAE5SO                 
20070618002242007061800224SO  2007       6          18         2007FA0000496    220070530G8500                STUD                                                                       CONT  O520  TSIO520*    17040SO                              ENGINE CASE     CHAFED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW99                                        532343                      DURING BUILD UP OF A NEW ENGINE FOR INSTALLATION, IT IS ROUTINE FOR US TO R&R THE OIL COOLER TO INSTALL THE GASKET WITH SEALANT AND TO INSPECT THE ADAPTER PLATE MOUNTING STUD HEIGHT.  ON THIS PARTICULAR ENGINE, ALL OF THE STUDS WERE INSTALLED TOO HIGH, SO THAT THEY PROTRUDED ABOVE THE GASKET MOUNTING SURFACE.  TWO OF THEM HAD MADE IMPRESSIONS IN THE COOLER SEALING SURFACE.                                                                                                                                                                                                                                                                                                                                                                3  O          E8CE                 
20070618002652007061800265SO  2007       6          18         2007FA0000497    220070607G8530EC646144CN      CYLINDER                                CESSNA210   210C        2073412CE  CONT  O470  IO470S      17026SO                              ENGING          DAMAGED         G      A   UNSCHED LANDING                                                                                 A  FLAME/FIRE                                                                    CLCLIMB          1                      WP213622Y     501               21058122    CS1024292S                  CYLINDER HEAD DETACHED FROM CYLINDER BARREL CAUSING INJECTOR FUEL LINE TO RUPTURE.  A INFLIGHT FIRE OCCURED CAUSING DAMAGE TO WIREING, MAG.,AND OTHE ENGINE COMPONENTS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  3A21    3E1                  
20070618002662007061800266CE  2007       6          18         2007FA0000498    120070527G5610                WINDSHIELD                              CESSNA421   421C        2076016CE                                                               COCKPIT         BROKEN          G      B   EMER. DESCENT                                                                                   D  INFLIGHT SEPARATION                                                           CRCRUISE         1                      SO15237SM                       421C0237                                MAJOR PORTION OF RT WINDSHIELD SEPARATED FROM AIRCRAFT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3O      A7CE                         
20070618002672007061800267EA  2007       6          18         2007FA0000501    220070607G8520LW13683         MAIN BEARING                            PIPER PA31  PA31350     7103110SO  LYC   O540  LTIO540J2BD 41533EA                              ENGINE          DELAMINATED     B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW99     1100                   318052122   L110868A                    CUSTOMER FOUND METAL IN FILTER DURING ROUTINE MAINTENANCE. TOOK ENG. APART AND FOUND 2 CENTER MAIN BRGS. WHERE DELAMINATED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A20SO   E14EA                
20070627000152007062700015NM  2007       6          27         2007FA0000503    120070618G6510A04111          BEARING                                 ROBSINR22   R22BETA     7640110NM  LYC   O320  O320*       41508EA                              DRIVESHAFT      ROUGH           B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM09461H 161                    1460                                    PILOT REPORTS GRINDING NOISE FROM TAIL ROTOR DRIVESHAFT. REMOVED DRIVESHAFT ASSY AND DISCOVERED ROUGH A041-11 DAMPER BEARING. REPLACED BEARING ASSY.  CLOSER EXAMINATION SHOWED PAINT USED DURING DRIVESHAFT ASSEMBLY ON LIP OF SEAL. OVER TIME THIS DAMAGED THE LIP OF THE SEAL AND ALLOWED GREASE TO PURGE FROM BEARING. THIS IS THE SECOND OCCURRENCE OF THIS IN THE PAST 12 MONTHS. MFG NOTIFIED EACH TIME. SUGGEST BETTER QC DURING DRIVESHAFT BUILD UP AT MFG.                                                                                                                                                                                                                                                                            1G71 3O3  O  H10WE   E274                 
20070711000212007071100021CE  2007       7          11         2007FA0000505    120070504G534024130023        ATTACH FITTING                          CESSNA172   172RG       2072438CE  LYC   O360  O360*       41514EA  MCAULY2D34C B2D34C220   GL  NLG ACTUATOR    CRACKED         B  BGSRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA21169EC1345                   172RG0515   L2843836A   804955          L/W SEB 93-8 ON NOSE GEAR ACTUATOR ATTACH FITTING AND SOUND CRACK ON LT, LOWER, IB BOLT HOLE OF FITTING.  ALSO, BOLT HOLES IN LOWER SKIN WERE IN EXCESS OF .030.  REPLACED ATTACH FITTING, LOWER SKIN AND DOUBLER IAW SK 172-142 AND SK 172-159.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  O  3A17    E286    5  CP7EA     
20070711000222007071100022CE  2007       7          11         2007FA0000506    120070517G575395160000XX      SKIN                                    BEECH 60    B60         1153605CE  LYC   O541  TIO541*     41536EA                              LT TE FLAP      CRACKED         B  HSRRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM06837RJ5859                   P355                                    BOTH FLAPS CRACKED AT ACTUATOR ATTACH POINT.  LT FLAP SKIN AND RIB CRACKED.  RT FLAP RIB CRACKED.  RIGGING WAS OK, PROBABLY AN OPERATOR INDUCED PROBLEM.  BELIEVE THE FLAPS HAVE BEEN LOWERED AT TOO HIGH AN AIRSPEED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A12CE   E10EA                
20070711000292007071100029CE  2007       7          11         2007FA0000507    120070515G2130AN8186D         NUT             BEECH                   BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              TUBE            LOOSE           B  E81RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL03132QS                       RK427                                   CREW REPORTED PRESSURIZATION CONTROL INEFFECTIVE, CABIN RATE CLIMBING AND DESCENDING, WHILE DESCENDING IN AUTOMATIC MODE.  STABILIZED BRIEFLY WHILE IN MANUAL MODE.  TROUBLESHOT IAW FIM 21-30-00, EXCESSIVE LEAK RATE NOTED AT TEST PORT 2.  FOUND LOOSE (B) NUT ON CONTROL LINE TUBE ASSY.  AT TEE FITTING FOR MANUAL CONTROL VALVE.  CORRECTED LOOSE FITTING AND SYSTEM TESTS OK.  RESTORED AC TO NORMAL CONFIGURATION, PRESSURIZATION SYSTEM TESTS SATISFACTORY ON GROUND RUN-UP.  UNKNOWN IF PREVIOUS MAINTENANCE PERFORMED IN THIS AREA.  (K)                                                                                                                                                                                             2H72 4F4  FRTA16SW   E25EA                
20070627000072007062700007WP  2007       6          27         2007FA0000510    120070618G6520269A6029        LOCK NUT                                HUGHES269   269C        4470504WP  LYC   O360  HIO360*     41514EA                              T/R GEARBOX     BACKED OUT      B      C   ABORTED TAKEOFF                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      NM0927YS 1573                                                           DURING GROUND RUNUP, PILOT NOTICED TAIL ROTOR NOT SPINNING. AIRCRAFT SHUTDOWN AND RETURNED TO HANGER. UPON DISASSEMBLY IT WAS NOTED THAT THE NUT PN 269A6029 THAT ATTACHES THE DRIVE COUPLING TO THE GEARBOX HAD BACKED OUT COMPLETELY AND WORN A HOLE THROUGH THE ALUMINUM BUMPER PN 269A5712 THAT IS INSIDE THE TAIL ROTOR DRIVESHAFT. THREADS INSIDE THE TAIL ROTOR GEARBOX INPUT SHAFT PN 269A5626-5 WERE ALSO DAMAGED. PARTS WERE FORWARDED TO MFG FOR EVALUATION.                                                                                                                                                                                                                                                                         1G71 3O3  O  4H12    1E10                 
20070711000622007071100062CE  2007       7          11         2007FA0000511    120070530G5730552275563       PANEL                                   CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              WING            DELAMINATED     B  H00RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA21100DS4430                   5500639                                 DURING COMPLETION OF MFG PROGRAM PHASE 5 INSPECTION, NOTICEABLE DEPRESSION WAS OBSERVED IN UPPER SURFACE OF LT AND RT WING SKINS IN AREA OF MLG UPLOCK HOOK ASSY ATTACHMENT.  DURING COMPLETION OF LANDING GEAR OPERATIONAL CHECK, IT WAS NOTED THAT DEPRESSION AREA SIZE GREW WHILE MLG WAS IN UP AND LOCKED POSITION.  USING THE COIN TAP TEST METHOD CONFORMATION WAS MADE THAT BOTH BONDED PANELS WERE DELAMINATED.  IAW TECH SUPPORT, NO DELAMINATION IS ALLOWED ON THESE PANELS.  OPTIONS AVAILABLE FOR REMEDY WERE REMOVED AND REPLACED, POSSIBLE REPAIR DEFINITION AND ASSOC 8110FORM, OR POSSIBLE TEMPORARY REPAIR WITH FLIGHT EXTENSION.  (K)                                                                                         1L72 4F4  F  A22CE   E1NE                 
20070711000632007071100063CE  2007       7          11         2007FA0000512    120070530G5730552277564       PANEL                                   CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              LT WING         DELAMINATED     B  H00RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA21100DS4430                   5500639                                 DURING COMPLETION OF MFG PROGRAM PHASE 5 INSPECTION, NOTICEABLE DEPRESSION WAS OBSERVED IN UPPER SURFACE OF LT AND RT WING SKINS IN AREA OF MLG UPLOCK HOOK ASSY ATTACHMENT.  DURING COMPLETION OF LANDING GEAR OPERATIONAL CHECK, IT WAS NOTED THAT DEPRESSION ARE SIZE GREW WHILE MLG WAS IN UP AND LOCKED POSITION.  USING THE COIN TAP TEST METHOD.  CONFORMATION WAS MADE THAT BOTH BONDED PANELS WERE DELAMINATED.  IAW TECH SUPPORT, NO DELAMINATION IS ALLOWED ON THESE PANELS.  OPTIONS AVAILABLE FOR REMEDY WERE REMOVED AND REPLACED, POSSIBLE REPAIR DEFINITION AND ASSOC 8110 FORM, OR POSSIBLE TEMPORARY REPAIR WITH FLIGHT EXTENSION.  (K)                                                                                       1L72 4F4  F  A22CE   E1NE                 
20070625000032007062500003    2007       6          25         2007FA0000513    420070608G2562E0109           CONNECTOR       ACK         E01ELT      PIPER PA16  PA16        7101602SO                                                               ELT             MISSING         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO255834H1277 87    021767      16453                                   DURING 100 HOUR INSPECTION IT WAS NOTED THAT THE BNC CONNECTOR ATTACHED TO THE ELT PORTABLE ANTENNA WAS MISSING. AN IN-DEPTH SEARCH OF THE AIRCRAFT BELLY FAILED TO TURN UP THE CONNECTOR. THE CONNECTOR IS ATTACHED TO THE PORTABLE COLLAPSIBLE ANTENNA BY A 6-32 SCREW IN THE BOTTOM OF THE ANTENNA. THERE IS NO PROVISION TO LOCK THIS THREADED ATTACHMENT.                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O      1A1                          
20070625000062007062500006GL  2007       6          25         2007FA0000516    120070612G575313431004        HINGE                                   CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO  HARTZLHCJ3Y PHCJ3YF1    GL  FLAP            CORRODED        G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW13122GH543                    0175                                    FLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGE JUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  ONTA00009CHE3SO    5  CP36EA    
20070625000072007062500007GL  2007       6          25         2007FA0000517    120070612G575313432002        HINGE                                   CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO  HARTZLHCJ3Y PHCJ3YF1    GL  FLAP            CORRODED        G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NE03122GH543                    0175                                    FLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGE JUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  ONTA00009CHE3SO    5  CP36EA    
20070625000252007062500025SO  2007       6          25         2007FA0000524    220070511G8500                ENGINE                                  BEECH 36    A36         1151604CE  CONT  O550  IO550*           SO                              RIGHT           FAILED          G      BA  EMER. DESCENT           UNSCHED LANDING                                                         JYTWARNING INDICATION        ENGINE STOPPAGE           ENGINE CASE PENETRATION   CRCRUISE         1                      SO11814JG     14                E2622       675591                      ON MAY 11, 2007 AT APPROXIMATELY 1815 EST, 2205Z, A BEECH BE-36-A36 BONANZA, N814JG, S/N E-2622, AT CRUISE HAD A DECREASE IN ENGINE CYLINDER TEMPERATURE, FOLLOWED BY A LOSS OF OIL PRESSURE AND ENGINE POWER WITH SUBSEQUENT ENGINE FAILURE. THE AIRCRAFT MADE AN EMERGENCY LANDING. PILOT WALKED AWAY FROM THE AIRCRAFT WITH NO INJURIES. A VISUAL INSPECTION OF THE AIRCRAFT REVEALED A HOLE IN THE UPPER RIGHT HAND ENGINE COWLING APPROXIMATELY 3 INCHES IN DIAMETER WHICH WAS LIMITED TO SHEET METAL DAMAGE. UPON INSPECTION OF THE ENGINE COMPARTMENT THE FORWARD UPPER CASE OF THE ENGINE WAS HEAVILY DAMAGED REVEALING SEVERAL DAMAGED PISTONS, PISTON CONNECTING RODS BROKEN AND NR 6 CONNECTING ROD MISSING, ALONG WITH SEVERAL CRANK1L71 3O3  O  3A15    E3SO                 
20070625000272007062500027EA  2007       6          25         2007FA0000525    220070615G7414M3548           ROTOR           SLICK       4370        PIPER PA28  PA28161     7102803SO  LYC   O320  O320D3G     41508EA  SNSNCH74D   74DM        EA  MAGNETO         SHEARED         C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE01     335  335   06052245                                            RIGHT MAGNETO ROTOR SHEARED DIRECTLY UNDER THE MAGNETO CAM.  SECOND IDENTICAL FAILURE IN 335 HRS ON THE AIRCRAFT.  AIRCRAFT DYNAMIC PROP BALANCE WAS CHECKED AFTER THIS FAILURE AND CHECKED EXCELLENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3O3  O  2A13    E274    5  NP88614   
20070625000282007062500028SO  2007       6          25         2007FA0000526    120070615G2420                TERMINAL        CHRYSLER                PIPER PA28  PA28180     7102808SO  LYC   O360  O360A4A     41514EA  SNSNCH76E   76EM8S5     EA  ALTERNATOR      LOOSE           C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE01                F082472                                             217 HOURS AFTER OVERHAUL, THE  OUTPUT TERMINAL BECAME LOOSE IN THE BUSS STRAP INSIDE THE ALTERNATOR, CAUSING COMPLETE FAILURE.  LIKELY THIS FIT (NORMALLY A PRESS FIT) WAS NOT AS TIGHT AS IT NEEDED TO BE WHEN THIS UNIT LEFT KELLY.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L71 3O3  O  2A13    E286    5  NP4EA     
20070711000612007071100061GL  2007       7          11         2007FA0000530    120070622G322211907005        STRUT                                   CIRRUSSR    SR20        05628AJGL  CONT  O550  IO550N      17042SO                              NLG             CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA07961CD623                    1610                                    NOSE LANDING GEAR STRUT HAS A CRACK AT THE TOP. THE STRUT COMES UP TO A Y FOR MOUNT. AT THE YOKE OF THE Y IS A WELDED REINFORCEMENT, AND THE CRACK IS AT THE TOP WHERE THIS REINFORCEMENT MEETS THE LEGS OF THE Y ON BOTH SIDES.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  ONTA00009CHE3SO                 
20070627000202007062700020EU  2007       6          27         2007FA0000531    120070615G27509450202205      FLEX DRIVE                              PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  TE FLAPS        BROKEN          B      O   OTHER                                                                                           O  OTHER                                                                         DEDESCENT        1                      EA65591AF2329                   591         PR0454      KX164           DURING APPROACH WHEN THE FLAPS WERE SELECTED TO 15 DEGREES THE FLAPS FAILED TO EXTEND AND A FLAP CAUTION ANNUNCITOR WAS DISPLAYED ON THE CAWS PANEL. THE FLIGHT CREW FOLLOWED THE APPROPRIATE POH PROCEDURES AND LANDED UNEVENTFULLY. INVESTIGATION INTO THE FLAP PROBLEM AFTER THE AIRCRAFT LANDED DETERMINED THAT THE LT IB FLAP FLEX DRIVE PN 945.02.02.205, SN S2532, HAD BROKEN JUST IB OF THE LT IB FLAP ACTUATOR.                                                                                                                                                                                                                                                                                                                        1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070711000232007071100023    2007       7          11         2007FA0000532    120070620G3220608200185       TORQUE KNEE     BEECH       T34                                                                                                         NLG             MISMANUFACTURED B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE09                GL210                                               PURCHASED BRAND NEW PART. DURING ASSEMBLY IT WAS FOUND THAT THE TORQUE ARM PIN LUGS ARE OF DIFFERENT THICKNESSES.  THEY ARE SUPPOSED TO BE THE SAME.  THIS DEFECT CAUSED THE HOLES IN THE HOUSING AND THE TORQUE PIN TO NOT ALIGN.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        
20070711000592007071100059GL  2007       7          11         2007FA0000533    120070622G322211907004        STRUT                                   CIRRUSSR    SR20        05628AJGL  CONT  IO360 IO360*      17025CE                              NLG             CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA07217JH562                    1320                                    NOSE LANDING GEAR STRUT HAS A CRACK AT THE TOP. THE STRUT COMES UP TO A Y FOR MOUNT. AT THE YOKE OF THE Y IS A WELDED REINFORCEMENT, AND THE CRACK IS AT THE TOP WHERE THIS REINFORCEMENT MEETS THE LEGS OF THE Y.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  ONTA00009CHE1CE                 
20070627000192007062700019CE  2007       6          27         2007FA0000534    120070619G3246D30257          HUB                                     CESSNA206   U206F       2073333CE                                                               WHEEL           FAILED          C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL031191V           D30         U20602506                               WHEEL-BROKE AT CENTER, CASTING FAILED AT BOLT HOLES-8:00X6 TIRES AND TUBES 190-200" NRS AT CAP SCREWS INSTALLED 7-23-03 TACH 1709 CURRENT TACH 2052.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O      A4CE                         
20070711000732007071100073EU  2007       7          11         2007FA0000535    220070501G7314AN9113D         NIPPLE                                  NANCNGCJ6A  CJ6A        056183NWP  VEDENY      M14P             EU  MUHBR MTV   MTV9*       EU  FUEL PUMP       UNKNOWN         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP07552CY20                     4332008     KR822009                    FUEL INJECTION FUEL SUPPLY FROM FUEL PUMP FITTING THAT COMES OUT OF PUMP.  FIX WOULD BE CHANGE TO STEEL AND SUPPORT LINE WITH BRACKET OR CHANGE TO FIREWALL MOUNT OF FUEL PRESSURE TRANSDUCER.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3R    RTEXPA1L71USSR    5  CP24NE    
20070711000882007071100088CE  2007       7          11         2007FA0000536    120070530G3500510010746       LINE                                    CESSNA441   441         2076020CE  CONT  O520  GTSIO520*   17032SO                              OVERHEAD CABIN  CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW03377CA5341                   4410289                                 DURING INSPECTION, HEARD A FAINT GAS LEAK IN OVERHEAD.   PULLED O2 OUTLETS IN SUSPECTED AREA, AND CHECKED B-NUTS, ALL SECURE.  PULLED HEADLINER FOR A CLOSER INSPECTION.  FOUND O2 LINE JUST FWD OF THE CABIN DOOR CORRODED AND LEAKING.    CORROSION ON THE LINE OCCURRED WHERE THE DUCTING PASSED UNDER IT.    EVERYWHERE THIS DUCTING TOUCHED AN O2 LINE THERE WAS CORROSION.    THE LINES & FLEX DUCTING WAS REPLACED WITH NEW.   (K)                                                                                                                                                                                                                                                                                                       1L72 3T3  ORTA28CE   E7CE                 
20070711000922007071100092NE  2007       7          11         2007FA0000537    220070531G7321312064401       FCU             PWA                     BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE                              LT ENGINE       MALFUNCTIONED   B  VG4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO15609BG403  234   PCEPK0709   FL468       PCEPK0709                   ENGINE POWER LOSS AT ALTITUDE.  ENGINE ROLLED BACK FROM 50 PERCENT.  MFG TECH SUPPORT RECOMMENDS FCU REPLACEMENT.  CAUSE UNKNOWN AT THIS TIME. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4T4  TRTA24CE   E4EA                 
20070711000932007071100093CE  2007       7          11         2007FA0000538    120070604G5320                FLOOR SUPPORT                           CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              FS 151          CRACKED         B  JGVRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE09905CW9359                   5500072                                 CABIN FLOOR SUPPORT WEB CRACKED AND BROKEN, FUSELAGE STATION 151.  FOUND CRACK DURING PHASE INSPECTION.   UNABLE TO FIND PN IN MFG PARTS CATALOG.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 4F4  F  A22CE   E1NE                 
20070711000942007071100094EU  2007       7          11         2007FA0000539    120070530G27521391T1008       ACTUATOR                                ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE731*     01518WP                              TE FLAPS        MISALIGNED      D  JGVRK   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CE0927TZ                        213                                     INSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T1008, SN 387AB.  FLAP OPERATION WAS NORMAL.  WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR.  A COVER PLATE ON THE FLAP ACTUATOR HAD BEEN INDEXED INCORRECTLY AND WAS INTERFERING WITH THE AILERON BELLCRANK.  PROBABLE CAUSE; INCORRECT ASSY OF FLAP ACTUATOR.  (K)                                                                                                                                                                                                                                                                                                                                                2M72 4F4  F  A2SW    E6WE                 
20070711000982007071100098SO  2007       7          11         2007FA0000540    120070625G7500M1213400        RING            ALIDSG                  GULSTMG1159 G1159A      3970109SO  RROYCESPEY  SPEY*            NE                              PRECOOLER       MISSING         C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW092NA                         309                                     THE COMPONENT OEM (REPORT 4-193), THE MM (CHAPTER 36-02-00), IPC (CHAPTER 36-10-00) AND THE CMP WORK CARDS (364040, 364045) ARE MISSING THE REQUIREMENT TO INSPECT AND INSTALL GAMMA RING (PN) M1213-400 DURING THE INSTALLATION OF THE PNEUMATIC SYSTEM PRECOOLER. FAILURE TO INSTALL THE GAMMA RING COULD CAUSE THE HIGH PRESSURE DUCT TO SEPARATE FROM THE PRECOOLER AND CAUSE SIGNIFICANT HEAT DAMAGE TO THE AIRCRAFT SKIN AND STRINGERS.                                                                                                                                                                                                                                                                                                   2L72 4F4  T  A12EA   E2EU                 
20070711000822007071100082SO  2007       7          11         2007FA0000543    220070625G7322                NEEDLE VALVE                            CESSNA182   182Q        2072732CE  CONT  O470  O470U       17026SO                              CARBURETOR      MISSING         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW99          51                                                        AT THE END OF THE FLIGHT, PILOT REPORTED THAT THE ENGINE WOULD NOT IDLE.  DURING INSPECTION OF THE CARBURETOR,  MECHANIC FOUND THE MIXTURE ADJUSTMENT NEEDLE VALVE MISSING.  CARBURETOR WAS REMOVED AND SENT BACK FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A13    E273                 
20070711000262007071100026EU  2007       7          11         2007FA0000547    120070620G276069023617        PULLEY BRACKET                          GLASFLH301  H301LIBELLE 3800337EU  CONT  O360  TSIO360E    17025SO                              SPOILER         CHAFED          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE09301Q 2343                   35                                      ROLL SPOILER CABLE PN:S3779-4P233.7M WAS ROUTED INCORRECTLY OVER LOW FRICTION PULLEY P/N:S3504-4.5  (THROUGH A TOOLING HOLE) IN PULLEY BRACKET P/N:6960236-17.  THIS CAUSED AN INTERFERENCE AND WEAR IN THE PULLEY BRACKET, AND FLAT AREAS TO THE CABLE.  CABLE AND BRACKET WERE REPLACED WITH NEW.                                                                                                                                                                                                                                                                                                                                                                                                                                             1K00   3  O  G12EU   E9CE                 
20070711000272007071100027CE  2007       7          11         2007FA0000548    120070620G2760S37794P2337M    CONTROL CABLE                           CESSNA680   680CE       2076811CE                                                               SPOILER         MISINSTALLED    B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CE09301QS2343                   6800010                                 ROLL SPOILER CABLE P/N S3779-4P233.7M WAS ROUTED INCORRECTLY OVER LOW FRICTION PULLEY. CABLE WAS FOUND ROUTED THROUGH TOOLING HOLE IN BRACKET P/N 6960236-17 RATHER THAN ENGAGING PULLEY.  THE BRACKET TOOLING HOLE EXHIBITED WEAR FROM THE CABLE RIDING (CUTTING) INTO THE TOOLING HOLE.                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F    RCT00012WI                     
20070711000432007071100043CE  2007       7          11         2007FA0000550    120070621G323050410015        BELLCRANK                               CESSNA310   310R        2074245CE  CONT  O520  IO520*      17032SO                              ZONE 700        BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      SO191771G                       310R0040                                LT MAIN GEAR BELLCRANK ASSY BROKE IN MARCH OF 2007. THE PART WAS REPLACED BY A USED SERVICABLE PART WHICH LASTED APPROXIMATLY 58 HRS. THEN FAILED  AT THE SAME LOCATION ON THE PART.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  3A10    E5CE                 
20070711000522007071100052SO  2007       7          11         2007FA0000552    120070622G2910177662          HOSE                                    PIPER PA31T PA31T       7103124SO                                                               HYD SYSTEM      RUPTURED        D      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  NRNOT REPORTED   1                      GL27970PS6349                   31T8020023                              LT MLG IB GEAR DOOR ACTUATOR HYDRAULIC HOSE, HAD A PRESSURE FAILURE, THUS DRAINING HYDRAULIC FLUID IN FLIGHT, RESULTING IN FAILURE OF PROPER GEAR EXTENSION, EMERGENCY GEAR EXTENSION, AND CAUSING AIRCRAFT GEAR UP LANDING.  HYDRAULIC HOSE P/N 17766-2 AND PIPER P/N 465-138.  HOSE IS ORIGINAL EQUIPMENT INSTALL.                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3T      A8EA                         
20070711001162007071100116WP  2007       7          11         2007FA0000553    220070626G720030751604        ENGINE                                  RAYTHNDH125 HAWKER800XP 7150012CE  GARRTTTFE731TFE7315BR        WP                              NR 2            BINDING         C      E   ENGINE SHUTDOWN                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      WP07     1781                   258593      P107918                     IFSD OCCURRED ON JUNE 21ST 2007.  AN EMERGENCY WAS DECLARED WHEN THE NR 2 ENGINE ITT CLIMBED TO 1066C FOR 5 SECONDS AT FL 260 AND A HIGH VIBRATION WAS FELT.  THE PILOT SHUTDOWN THE ENGINE.  ALL PARAMETERS WERE FINE UNTIL THIS EVENT.  AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED ON THE AIRCRAFT WITH NO ABNORMALITIES REPORTED.  DISASSEMBLY FINDINGS OF THE ENGINE REVEALED LPC2 DISC POST SEPARATIONS AS LISTED IN SB TFE731-72-3711.                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA3EU    E6WE                 
20070711001272007071100127    2007       7          11         2007FA0000554    420070628G345712744001        ANTENNA                                 CIRRUSSR    SR20        05628AJGL  CONT  IO360 IO360*      17025CE                              GPS             DISCONNECTED    B      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      EA075959A127                    1526                                    WHILE IN CRUISE FLIGHT THE NR 1 GPS STOPPED RECEIVING A SIGNAL. AFTER LANDING, REMOVED THE MFD AND FOUND THE GLUE HOLDING THE VELCRO TO THE GPS ANTENNA HAD COME UNDONE. BOTH GPS ANTENNAS ARE HELD IN PLACE WITH VELCRO STRIPS AND IN THE HEAT OF SUMMER, THE GLUE SOFTENS AND COMES UNDONE.                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  ONTA00009CHE1CE                 
20070712001202007071200120EA  2007       7          12         2007FA0000555    220070616G8530                EXHAUST VALVE                           AMERACS1    S1AAMERAC          WP  LYC   O235  O235C2C     41505EA  MCAULY1A105 1A105SCM    GL  ENGINE          BENT            G      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CLCLIMB          1                      GL035651L1749 1749              AA10051     L961915     52473           EXHAUST VALVE WAS FOUND STUCK IN THE OPEN POSITION ON TEARDOWN OF THE ENGINE.  VALVE STEM HAD A SLIGHT BEND.  ENGINE TEARDOWN WAS DUE TO AN AIRCRAFT ACCIDENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 3R3  O  ATC521  E223    5  NP918     
20070711001402007071100140EU  2007       7          11         2007FA0000556    120070628G6320305A32031002    GEARBOX                                 SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B1   60056NE                                              UNKNOWN         B      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      EA17808CP161                    4151        23335                       MGB CHIP LIGHT CAME ON IN FLIGHT. INSPECTED CHIP PLUGS IAW AEC MWC AND SPM. NO FURTHER ACTION REQUIRED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  U  H9EU    E00054EN             
20070711001412007071100141EU  2007       7          11         2007FA0000557    120070628G6320305A32031002    GEARBOX                                 SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B1   60056NE                                              UNKNOWN         B  PN1RA   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      EA17808CP161                    4151        23335                       MGB CHIP LIGHT CAME ON IN FLIGHT. INSPECTED CHIP PLUGS IAW AEC MWC AND SPM. NO FURTHER ACTION REQUIRED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  U  H9EU    E00054EN             
20070711001502007071100150CE  2007       7          11         2007FA0000558    120070510G3240                LINE                                    CESSNA185   A185F       2072821CE  CONT  O520  IO520*      17032SO                              BRAKE           LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      GL134845E                       18503887                                RT MAIN BRAKE FAILED ON AIRCRAFT ROLLOUT OF NORMAL CROSSWIND LANDING.  BRAKE LINE B-NUT FOUND COMPLETELY LOOSE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  O  3A24    E5CE                 
20070711001522007071100152CE  2007       7          11         2007FA0000559    120070525G528045A303794       DOUBLER                                 BEECH MU300 400BEECH           CE  PWA   JT15  JT15D5      52112NE                              MLG DOOR        CRACKED         B  E81RO   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      GL03406TS                       RJ6                                     FLIGHT CREW REPORTED RED GEAR UNSAFE INDICATION LIGHT AFTER GEAR EXTENSION FOR APPROACH, ALL (3) LANDING GEARS INDICATING DOWN AND LOCKED.  PERFORMED ALTERNATE GEAR EXTENSION IAW CHECKLIST.  AIRCRAFT FERRIED WITH LANDING GEAR DOWN IAW PERMIT TO FACILITY FOR REPAIRS.  AFTER NORMAL LANDING, RT MLG FUSELAGE DOOR UNLATCHED AND DRAGGED ON TAXIWAY DURING TAXI-IN.  FOUND DOUBLER UNDER RT FUSELAGE DOOR FORWARD HINGE BRACKET CRACKED, ALSO CRACK IN PN 45A30314-6 FRAME ( U-CHANNEL) AT FORWARD HINGE AREA.  SUSPECT CRACKED AREA ALLOWED ENOUGH PLAY IN DOOR ASSY FOR DOOR UPLOCK NOT TO FULLY ENGAGE.  DOOR ASSY APPEARS TO HAVE BEEN REPAIRED PREVIOUSLY.  (K)                                                                        2H72 4F4  FRTA16SW   E25EA                
20070711001922007071100192EU  2007       7          11         2007FA0000560    120070521G5302                STRUCTURE                               SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1     60030NE                              TAIL BOOM       CRACKED         B  QS7RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM09352EV2542                   2555                                    A CRACK APPROXIMATELY 170 MM LONG WAS FOUND ON THE LEADING EDGE, AFT OF FWD MOUNT POINT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H9EU    E19EU                
20070711001962007071100196WP  2007       7          11         2007FA0000561    120070525G7600                BUSHING                                 HUGHES269   269C        4470504WP  LYC   O360  HIO360D1A   41514EA                              THROTTLE LINKAGEWORN            B  NTBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM051666S192                    S1898       L3316351A                   ENGINE MOUNTED THROTTLE LINKAGE BUSHINGS WORN.  FOUND ON INSPECTION WITH EXCESSIVE PLAY.  PROBABLY OCCURRED DUE TO EXCESSIVE VIBRATION OR LACK OF SUBRICATION.  RECOMMENDATION TO PREVENT WOULD BE TO LUBRICATE MORE FREQUENTLY OR DIFFERENT DESIGN OF LINKAGE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3O3  O  4H12    1E10                 
20070711001982007071100198EA  2007       7          11         2007FA0000562    220070629G8550AE3663162J0230  LINE                                    CESSNA182   T182T       2072738CE  LYC   O540  TIO540A1A   41532EA                              ENGINE OIL      CRACKED         B  LJERK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM091328N                       T18208403   L1196661A                   30 DEGREE FITTING HAS CRACK ON WRENCH FLAT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A13    E14EA                
20070711002012007071100201EA  2007       7          11         2007FA0000563    120070507G3240                SHAFT                                   SCWZERG164  G164A       3952704EA                                                               BRAKE           ROUGH           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW155149                        1123                                    ON DISASSEMBLY, THE SHAFT WAS FOUND TO BE QUIET ROUGH, WHERE THE PARKING BRAKE TAB LEVER 149-1 ENGAGES WITH THE SHAFT.  THIS IS NOT APPARENT UNTIL IT IS REMOVED AND TAKEN APART, AS SPRING 02-9 OBSCURES THE NEW OF IT.  TO PREVENT REOCCURRED THE SHAFT SHOULD BE CHECKED AND SMOTHERED OR REPLACED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                     1Q71 3R      1A16                         
20070711002022007071100202CE  2007       7          11         2007FA0000564    120070519G74004370            ARM                                     CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA                              POINTS          BROKEN          D  M90RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL0961953133                    17264910    L4116127A                   POINTS ARM BROKE IB OF POINTS AFTER ONLY 133.1, TIME SINCE INSTALLATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A12    E274                 
20070711002042007071100204CE  2007       7          11         2007FA0000565    120070606G291041344           VALVE                                   CESSNA525   525A        2076615CE  WILINTFJ44  FJ44        66000GL                              HYD SYSTEM      LEAKING         D      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  LDLANDING        1                      CE07301PG                       525A0301                                PERFORMED AN EMERGENCY LANDING DUE TO LOSS OF HYDRAULIC PRESSURE.  THE EMERGENCY BOTTLE WAS USED TO LOWER THE GEAR AND LAND WITHOUT INCIDENT.  THE CAUSE HAS BEEN DETERMINED TO BE THE HYDRAULIC LOADING VALVE (PN 4134-4, SN 781) FAILING IN CLOSED POSITION, RESULTING THE HYDRAULIC FLUID IN THE SYSTEM TO BE DUMPED OUT THE VENT TUBE CAUSING THE LOSS OF HYDRAULIC PRESSURE.  IT IS ALSO SUSPECTED THAT THE LOADING VALVES FAILURE, CAUSED THE PCB N2108 (CIRCUIT BOARD) TO FAIL AS WELL.  THE PCB 2108 WAS REPLACED.  THE AIRCRAFT HYDRAULIC SYSTEM HAS BEEN LEAK CHECKED, OPS CHECKED AND HAS BEEN RETURNED TO SERVICE WITH NO FURTHER INCIDENTS.                                                                                        1L71 4F4  FRTA1WI    E3GL                 
20070711002092007071100209CE  2007       7          11         2007FA0000566    120070608G2800                FUEL                                    CESSNA525   525         2076601CE  WILINTFJ44  FJ44        66000GL                                              CONTAMINATED    C      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      EA6541YP                        5250122                                 PERFORMED AN EMERGENCY LANDING, DUE TO A FUEL BYPASS LIGHT COMING ON IN FLIGHT.  THE AIRCRAFT LANDED AND TAXIED TO THE SERVICE CENTER WITHOUT INCIDENT.  THE CAUSE OF THE LIGHT HAS BEEN DETERMINED TO BE THE FUEL ITSELF.  THE FUEL IS CONTAMINATED WITH VISIBLE DEBRIS AND HAS A CLOUDY TINT TO IT.  THE CAUSE OF THE BYPASS LIGHT IS FROM THE PARTICLES IN THE FUEL CLOGGING THE ENGINE FILTERS.  THE FUEL FILTERS ON BOTH THE LT AND THE RT ENGINES HAVE BEEN REPLACED IAW MM.  THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.  NOTE: THE FUEL WAS NOT PURCHASED FROM SERVICE CENTER.  (K)                                                                                                                                                      1L72 4F4  FRTA1WI    E3GL                 
20070711002102007071100210CE  2007       7          11         2007FA0000567    120070629G61009696001123      LINE                                    BEECH 58    58          1152740CE  CONT  O550  IO550C           SO                              PROPELLER       LEAKING         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO11658RA1501                   TH1892                                  BAD OIL LEAK:  DETERMINED METAL ID PLATE ON MP HOSE WORE HOLE INTO PROP UNFEATHERING ACCUMULATOR TUDE.  NOTE: THIS IS THE SUBJECT OF AD 2007-06-07 AND MANDATORY SB 61-3806 BUT DOES NOT COVER THIS AC SN.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 3O3  O  3A16    E3SO                 
20070711002122007071100212CE  2007       7          11         2007FA0000568    120070629G3260602EN6026       UPLOCK SWITCH                           CESSNA650   650         2076802CE                                                               NLG             DEFECTIVE       B  EWCRO   OTHER                                                                                           N  FALSE WARNING                                                                 CLCLIMB          1                      EA39750CK                       6507015                                 GEAR SELECTED UP AFTER TAKEOFF.  UNSAFE LIGHT WOULD NOT GO OUT AND AIR NOISE FROM NOSE GEAR DOORS OPEN.  2 GEAR CYCLE ATTEMPTS WITH NO CHANGE.  RETURNED TO GSO (PTI) AIRPORT, LANDED WITH NORMAL GREEN LIGHTS.  AIRCRAFT TURNED OVER TO MFG SERVICE CENTER FOR REPAIR.  NOSE GEAR UPLOCK SWITCH FOUND DEFECTIVE.  REPLACED SWITCH OPERATION CHECKED NORMAL.  (K)                                                                                                                                                                                                                                                                                                                                                                               2L72 4F      A9NM                         
20070711002142007071100214EU  2007       7          11         2007FA0000569    120070517G7700642795431       TRANSMITTER                             AMD   FALC90FALCON900EX 2730009EU  GARRTTTFE731TFE73160         NE                              ENGINE          READS LOW       B  UO2RO   OTHER                                                                                           N  FALSE WARNING                                                                 CLCLIMB          1                      GL19127SF5144                   013         P112149                     THE AIRCRAFT WAS CLIMBING AND THE NR 3 ENGINE OIL PRESSURE INDICATION STARTED TO DROP.  AT 46 PSI IT WENT RED AND THE PILOT SHUTDOWN THE ENGINE  AND LANDED THE AIRCRAFT.  THE OIL LEVEL WAS IN LIMITS AND NO EXTERNAL LEAKS WERE FOUND.  A DIRECT READING PRESSURE GAGE WAS INSTALLED AND SHOWED GOOD OIL PRESSURE AND THAT THE INDICATOR WAS READING LOW.  A NEW OIL PRESSURE TRANSMITTER WAS INSTALLED AND CORRECTED THE LOW READING PROBLEM.  (K)                                                                                                                                                                                                                                                                                           2L73 4F4  FRTA46EU   E1NM                 
20070711002152007071100215CE  2007       7          11         2007FA0000570    120070529G53115511118200      FRAME                                   CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              FUSELAGE        DAMAGED         C  JGVRK   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CE09905CW9359                   5500072                                 FUSELAGE FRAME WEB DAMAGED BY DRILL BIT FROM THE BEND RADIUS OF THE OUTER (SKIN) FLANGE.  REPLACEMENT REQUIRED SRM, CHAPTER 53-12-27.  PROBABLE CAUSE:  INCORRECTLY DRILLED AT AIRCRAFT MFG.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 4F4  F  A22CE   E1NE                 
20070711002182007071100218SO  2007       7          11         2007FA0000571    120070531G322067107000        BRACKET                                 PIPER PA28  PA28R200    7102811SO  CONT  IO360 IO360*      17025CE                              NOSE GEAR       FAILED          H      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      SO3356066                       28R7335346                              THE PILOT STATED NOSE GEAR COLLAPSED ON LANDING.  AFTER AIRCRAFT REMOVED FROM RUNWAY AND PUT ON JACKS.  THE NOSE GEAR WOULD NOT EXTEND OR RETRACT.  THE GEAR WAS EXTENDED BY EMERGENCY EXTENSION.  THE NOSE GEAR ALIGNER BRACKET FELL OFF THE GEAR.  AGAIN THE NOSE GEAR WAS EXTENDED AND RETRACTED SEVERAL TIMES. THE TT OF THE NOSE GEAR ALIGNER BRACKET COULD NOT BE DETERMINED.  (K)                                                                                                                                                                                                                                                                                                                                                        1L71 3O3  O  2A13    E1CE                 
20070711002192007071100219CE  2007       7          11         2007FA0000572    120070525G2720S16751          BEARING                                 CESSNA210   T210M       2073451CE                                                               RUDDER PEDAL    BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP23808FS2721                   21061586                                WHILE PERFORMING RUN UP OF AIRCRAFT DURING ANNUAL INSPECTION IT WAS NOTICED THAT PILOT RT RUDDER PEDAL HAD AN UNUSUAL FEEL WHILE BRAKING.  DURING THE INSPECTION OF THE RUDDER PEDALS IT WAS FOUND THT THE EACH OF THE PILOT SIDE S1675-1 RUDDER IB BEARING HALF HAD BROKEN INTO SEVERAL PARTS.  THE S1675-1 BEARING HALFS ARE CONSTRUCTED OF PLASTIC, AND THE LIKELY REASON FOR BREAKING WOULD BE DUE TO THE AGING AND EMBRITTLEMENT OF THE PLASTIC.  I WOULD RECOMMEND THAT THE BEARINGS BE CONSTRUCTED OF A MATERIAL OTHER THAN PLASTIC, OF HAVE A PART REPLACEMENT INTERVAL BEFORE BREAKAGE COULD OCCUR.  (K)                                                                                                                               1H71 3O      3A21                         
20070711002202007071100220CE  2007       7          11         2007FA0000573    120070606G272025137911        PIN                                     CESSNA208   208B        2073701CE  PWA   PT6   PT6*        52043EA                              RUDDER PEDAL    UNSERVICEABLE   B  ES4RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL014365U18129                  208B0253                                ON A ROUTINE INSPECTION, A MECHANIC FOUND THAT THE PILOTS RT RUDDER PEDAL PIN WAS ABOUT TO FALL OUT OF THE RUDDER PEDAL.  FURTHER INSPECTION FOUND THAT THE ROLL PIN PN: NAS561C318 HAD FALLEN OUR OF ITS HOLE CAUSING THE RUDDER PEDAL PIN TO MIGRATE FROM ITS POSITION.  INSPECTION OF RUDDER PEDAL ASSY FOUND THAT THE ROLL PIN HOLE IN THE RUDDER PEDAL HAD BECOME ENLARGED, DUE TO AN UNKNOWN REASON.  RECOMMENDATION TO PREVENT RECURRENCE:  ATTENTION TO ROLL PIN INSTALLATION FOR ADEQUATE PRESS FIT AND ADDITIONAL ATTENTION OF ROLL PIN ON ROUTINE INSPECTION.  (K)                                                                                                                                                                   1H71 3T3  T  A37CE   E2NE                 
20070711002212007071100221CE  2007       7          11         2007FA0000574    120070629G3244265F868         TIRE                                    BEECH B300  B300        1159232CE  PWA   PT6   PT6*        52043EA                              NLG             UNBALANCED      B  FTURK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NE055XM  408                    FL115                                   PILOT REPORTED A NOSE SHIMMY, UPON INVESTIGATION IT WAS DETERMINED THAT THE MFG BALANCE WEIGHT HAD COME LOOSE.  THIS IS THE SECOND OCCURRENCE OF THIS TYPE FOR THE OPERATOR. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T3  TRTA24CE   E2NE                 
20070711002222007071100222NE  2007       7          11         2007FA0000575    220070602G73210292858360      HMU                                     UROCOPEC130 EC130B4     8680989EU  TMECA ARRIELARRIEL2B1   60056NE                              ENGINE          FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE01151AC1609                   3732        23065                       THE PILOT REPORTED A LOUD THUD AND A SUBSEQUENT YAWING OF THE AC, WITH CONTINUED YAWING OF THE AC, AND NO INDICATION ON THE COCKPIT INSTRUMENTATION THAT HE NOTICED.  THE PILOT DECLARED AN EMERGENCY AND PERFORMED AN AUTORATATIVE LANDING AT THE AIRPORT.  THE VEHICLE AND ENGINE MULTIFUNCTION DISPLAY, DISPLAYED FAILURE OF CHANNEL A.  THE EC130 IS EQUIPPED WITH A DUAL CHANNEL FADEC SYSTEM WITH A MECHANICAL BACKUP.  IN THE FOLLOWING TROUBLESHOOTING PROCESS IT WAS FOUND THAT THE RESOLVER MOTOR ON THE FUEL CONTROL (HMU)  HAD A RESISTANCE VALUE THAT WAS OUT OF TOLERANCE.  A FIELD TECH WAS BROUGHT IN FROM MFG TO PERFORM FURTHER TESTING, SINCE THE FAILURE OF ONE CHANNEL OF THE FADEC AND THE SUBSEQUENT SWITCHING TO THE OTH1G72 3U3  U  H9EU    E00054EN             
20070711002322007071100232CE  2007       7          11         2007FA0000576    120070611G5300                STRUCTURE                               BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE                              FUSELAGE        MISINSTALLED    B  BWVRK   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CE077262U                       FL532                                   THE AIRCRAFT ARRIVED NEW FROM THE FACTORY FOR AVIONICS MODIFICATIONS AND DURING OUR INCOMING INSPECTION A TECH NOTED MISSING RIVETS IN (2) STRINGER CLIPS.  THE CLIPS ARE LOCATED AT FS 386 ON THE RT NR3 AND RT NR 5 STRINGERS AS NOTED USING THE UPPER CENTERLINE STRINGER AS STRINGER NR 1.  EACH CLIP WITH (6) RIVETS EACH WERE EITHER MISSING RIVETS AND/OR THE RIVETS WERE NOT BUCKED SITTING IN THE HOLES.  ADVISED MFG OF DISCREPANCY.  (K)                                                                                                                                                                                                                                                                                             2L72 4T4  TRTA24CE   E4EA                 
20070711002332007071100233SO  2007       7          11         2007FA0000577    120070512G32206715003         DOWNLOCK                                PIPER PA28  PA28R200    7102811SO  CONT  IO360 IO360*      17025CE                              NLG             BROKEN          G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL035094S3220                   28R7135094                              THE LOWER LATCH HOOK WAS BROKEN OFF ALLOWING THE NOSE GEAR TO COLLAPSE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3O3  O  2A13    E1CE                 
20070711002462007071100246CE  2007       7          11         2007FA0000578    120070605G5343FMI32345010B    BUSHING                                 CESSNA750   750         2076810CE  ALLSN AE3007AE3007C          GL                              TRUNNION        GOUGED          B  NOZRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP2322NG                        7500204                                 BUSHINGS WHERE OLEO ATTACHES TO TRUNNION.  OLEO ATTACH BOLT WAS SEIZED AND HARD TO REMOVE.  INNER BORE OF BUSHINGS WERE GOUGED.  NO MEANS TO LUBRICATE THESE BUSHINGS EXCEPT AT ASSY.   SUGGEST USE OF ANT SEIZE COMPOUND DURING ASSY INSTEAD OF AEROSHELL 17.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4J4  FRTT00007WITE6CH                
20070711002472007071100247CE  2007       7          11         2007FA0000579    120070605G534367410261        TRUNNION                                CESSNA750   750         2076810CE  ALLSN AE3007AE3007C          GL                              MLG             MISALIGNED      B  NOZRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP2322NG                        7500204                                 AFT TRUNNION ATTACH PIN LOCK PIN HOLE MISALIGNED.  LOCK PIN HOLES DRILLED IN TRUNNION DO NOT LINE UP WITH HOLE DRILLED IN MOUNTING PIN.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4J4  FRTT00007WITE6CH                
20070711002492007071100249CE  2007       7          11         2007FA0000580    120070427G8011MHB4016R        STARTER                                 CESSNA182   R182        2072734CE  LYC   O540  O540*       41532EA                              ENGINE          FAILED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW03182MS                       18200791                                REMOVED THIS STARTER FROM AIRCRAFT DUE TO BENDIX FAILURE.  TIME ON THIS STARTER IS UNKNOWN.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ORT3A13    E295                 
20070711002572007071100257CE  2007       7          11         2007FA0000581    120070518G8011MHB4016R        STARTER                                 CESSNA182   R182        2072734CE  LYC   O540  O540*       41532EA                              ENGINE          MALFUNCTIONED   D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW03182MS62                     18200791                                REMOVED THIS STARTER FROM SAME AIRCRAFT FOR THE 3RD TIME WITH 62.3 HRS SINCE OVERHAUL.  STARTER BENDIX WOULD NOT ENGAGE ANYMORE DURING START UP.  NO PROBLEM COULD BE FOUND WITH AIRCRAFT ELECTRICAL SYSTEM.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  ORT3A13    E295                 
20070711002582007071100258CE  2007       7          11         2007FA0000582    120070430G8011MHB4016R        STARTER                                 CESSNA182   R182        2072734CE  LYC   O540  O540*       41532EA                              ENGINE          FAILED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW03182MS                       18200791                                REMOVED THIS STARTER WITH 3.3 HOURS SINCE OVERHAUL.  STARTER BENDIX STAYED ENGAGED DURING START UP.  NO PROBLEM COULD BE FOUND WITH AIRCRAFT ELECTRICAL SYSTEM.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ORT3A13    E295                 
20070711002592007071100259CE  2007       7          11         2007FA0000583    120070524G8011MHB4016R        STARTER                                 CESSNA182   R182        2072734CE  LYC   O540  O540*       41532EA                              ENGINE          DEFECTIVE       D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW03182MS                       18200791                                REMOVED THIS STARTER FROM SAME AIRCRAFT FOR THE 4TH TIME WITH 11.3 HOURS SINCE OVERHAUL.  STARTER BENDIX WOULD NOT ENGAGE ANYMORE DURING STARTUP.  NO PROBLEM COULD BE FOUND WITH AIRCRAFT ELECTRICAL SYSTEM.  INSTALLED ON ANOTHER AIRCRAFT TO VERIFY PROBLEM AND FOUND THAT THE STARTER WAS DEFECTIVE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ORT3A13    E295                 
20070711002652007071100265CE  2007       7          11         2007FA0000584    120070521G3231HM4             ROD END                                 CESSNA310   310P        2074238CE  CONT  O470  IO470*      17026SO                              NOSE GEAR DOOR  FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      SO155918M                       310P0218                                ROD END FAILED, ALLOWING NOSE GEAR DOOR TO PARTIALLY CLOSE IN FLIGHT.  WHEN GEAR WAS RETRACTED, JAMMED NOSE GEAR ASSY ALONG WITH GEAR DOOR UP IN GEAR WELL.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3O3  O  3A10    E1CE                 
20070711002662007071100266EA  2007       7          11         2007FA0000585    120070507G5100AN837A          BOLT                                    SCWZERG164  G164A       3952704EA  PWA   R1340 R1340AN1    52016NE                              UNKNOWN         BROKEN          C      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      SW155149                        1123                                    THE BOLTS FAILED DUE TO LANDING WITH WHEEL LOCKED.  THINK THE BOLTS WERE FINE BEFORE THIS INCIDENT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1Q71 3R3  R  1A16    5E2                  
20070711002682007071100268NM  2007       7          11         2007FA0000588    120070413G3240                BRAKE DISC                              BOEING727   727200      138407ENM                                                               LT MLG          MALFUNCTIONED   H      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW99HP161                       20780                                   (REG NR: HP1610)  DURING PREFLIGHT INSPECTION, FOUND MAIN TIRE NR 2 WITH FLAT SPOT.  ON THIS AIRCRAFT OP SPECS APPROVED BY THIS DGAC, OPERATING BY DHL OF GUATEMALA UNDER THEM.  REMOVED AND REPLACED MWA AND BRAKE ASSY.  NR 2 DUEL TO DAMAGED , ALSO MAIN WHEEL ASSY NR 1 WAS REPLACED , BECAUSE IT RAN WITH THE TIRE NR 2 DEFLATED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                     2L73 4F    RTA3WE                         
20070712001212007071200121    2007       7          12         2007FA0000589    220070622G74141068256013      GEAR                                                                                                                                    MAGNETO         DAMAGED         G      K   NONE                                                                                            E  VIBRATION/BUFFET                                                              NRNOT REPORTED   1                      CE01          720                                                       REPAIR STATION RECEIVED MAGNETO FOR REPAIR. WHEN THE UNIT WAS DISASSEMBLED IT WAS NOTED BOTH DISTRIBUTOR GEARS TCM PN 10-682016 WERE MISSING TEETH. IT WAS NOTED THAT A PATTERN OF TEETH THAT WERE MISSING COULD BE SEEN. A TOTAL OF 5 TEETH WERE MISSING FROM BOTH GEARS. WHAT SEEMS TO HAPPEN IS WHEN THE IMPULSE SNAPS THE IMPULSE SNAPS THAT TOOTH OFF THE GEAR? WHEN ASSEMBLED TO VIEW THE GEAR POSITION IT WAS NOTED THAT ONE TOOTH WAS MISSING WITH FIVE EACH OF THE SIX TOTAL ENGAGEMENTS OF THE IMPULSE. ITEMS THAT COULD CONTRIBUTE TO THIS PROBLEM CAN BE FOUND IN SB658. IT IS RECOMMENDED TO FOLLOW SB658 AND TO INSPECT THE DISTRIBUTOR GEARS ON ALL IMPULSE D-3000 OR D-2000 UNITS FOR WEAR AT EVERY 100 HRS BY REMOVING THE MAGN                                          
20070712001222007071200122SO  2007       7          12         2007FA0000590    220070527G741410382585        CONTACTOR                   D4LN2021                                       CONT  O360  IO360A      17025SO                              MAGNETO         MELTED          D      EBA ENGINE SHUTDOWN         EMER. DESCENT           UNSCHED LANDING                                 GY MULTIPLE FAILURE          ENGINE STOPPAGE                                     CRCRUISE         1                      NM03134DC114        R2388K                  L1176351A                   AIRCRAFT HAD DEPARTED FOR A SIGHT SEEING TRIP. ON THE RETURN, ALL ENGINE POWER WAS LOST, THE AIRCRAFT WAS LANDED IN A MEADOW WITH MINIMAL DAMAGE TO THE AIRCRAFT.  UPON INSPECTION OF THE ENGINE, FOUND THAT THE MFG DUAL MAGNETO  D4LN-2021 WAS NOT FUNCTIONAL ON EITHER MAG. UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT THE CAM FOLLOWERS OF THE POINTS HAD GOTTEN TOO HOT AND MELTED TO A POINT THAT RENDERED THE CONTACT ASSEMBLY  INOPERATIVE, CAUSING A DUAL FAILURE OF THE MAG. IT WAS NOTED THAT THE SCREW THAT HOLDS THE POINTS CAM IN PLACE HAD A TORQUE CHECK  PAINTED ON IT AND HAD TURNED BLACK FROM HEAT. DUE TO THE FACT THAT THE DUAL MAG HAS MORE POSSIBILITIES TO PRODUCE MORE HEAT JUST FROM THE ELECTRICAL PART OF MA       3  O          E1CE                 
20070712001252007071200125SO  2007       7          12         2007FA0000592    220070703G8530SA10203         CYLINDER                                CESSNA172   172E        2072412CE  CONT  O300  O300D       17022SO  MCAULY1C172 1C172EM     GL  NR 5            SEPARATED       G      E   ENGINE SHUTDOWN                                                                                 D  INFLIGHT SEPARATION                                                           CRCRUISE         1                      EA635436T850                    17251336    34640D6D    78634           CYLINDER BARREL SEPARATED APPROXIMATELY 2 NR ABOVE THE CYLINDER BASE FLANGE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  ONT3A12    E253    5  NP910     
20070712001322007071200132NM  2007       7          12         2007FA0000593    120070703G575125W171124       SUPPORT FITTING                         ISRAEL1125  1125               NM  GARRTTTFE731TFE731*     01518WP                              AILERONS        DAMAGED         B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CE0949MN 7037                   019                                     AFTER REMOVAL OF AILERON AND SERVICE SUPPORT FITTING AT BL 9R FUSELAGE STATION 199.579.  FOUND SEVERAL MISSED DRILLED/ELONGATED /FILLED FASTENER HOLES IN  T CASTING P/N:25W17124, ANGLE P/N:25W171126 AND AILERON AND SERVICES SUPPORT FITTING CASTING P/N:25W353216                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA16NM   E6WE                 
20070717000122007071700012NM  2007       7          17         2007FA0000594    120070703G575125W171124       SUPPORT FITTING                         ISRAEL1125  1125               NM  GARRTTTFE731TFE731*     01518WP                              AILERON         MISMANUFACTURED B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CE0949MN 7037                   019                                     AFTER REMOVAL OF AILERON AND SERVICE SUPPORT FITTING AT BL 9R FUSELAGE STATION 199.579. FOUND SEVERAL MISSED DRILLED/ELONGATED /FILLED FASTENER HOLES IN T CASTING P/N:25W17124, ANGLE P/N:25W171126 AND AILERON AND SERVICES SUPPORT FITTING CASTING P/N:25W353216                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA16NM   E6WE                 
20070718002192007071800219EU  2007       7          18         2007FA0000599    120070616G2701103B4411        CONTROL COLUMN                          GROB  103TWNG103ATWINII 1660206EU                                                               COCKPIT         FRACTURED       D      BA  EMER. DESCENT           UNSCHED LANDING                                                         F  FLT CONT AFFECTED                                                             CLCLIMB          1                      NM074446Y2650                   3825                                    ON SECOND FLT OF DAY, & WHILE STILL ON AERO-TOW, PILOT WHO WAS FLYING FROM THE REAR SEAT WITH A NON-PILOT PASSENGER IN FRONT,  NOTICED THAT IT REQUIRED APPROXIMATELY 20 DEGREES OF RT-STICK CORRECTION TO MAINTAIN LEVEL FLT. PILOT ALSO OBSERVED AILERONS TO BE IN A NEUTRAL POSITION WITH THIS RT-STICK CORRECTION. PILOT RELEASED FROM TOW, & RETURNED TO AIRPORT & EXECUTED A SUCCESSFUL, UNEVENTFUL LANDING USING MINIMAL, LIGHT CONTROL STICK INPUTS. POST FLT INSPECTION OF AFT CONTROL STICK REVEALED CONTROL COLUMN BASE UNIT TUBING STUB OVER WHICH DETACHABLE REAR CONTROL STICK MOUNTS, TO BE FRACTURED, APPROXIMATELY 80 PERCENT OF ITS TOTAL CIRCUMFERENCE. IT REQUIRED ONLY MINIMUM FURTHER (BENDING) OF THE CONTROL STICK TO AC1K00 3O    0 G39EU                        
20070718002352007071800235SO  2007       7          18         2007FA0000601    120070710G2910MS21911D6       FITTING                                 GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              HYD LINE        CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILIARY HYDRAULIC SYSTEM FILTER RETURN LINE. CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER.  REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM. OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA12EA   E25NE                
20070718002372007071800237SO  2007       7          18         2007FA0000602    120070710G2910MS21911D6       FITTING                                 GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              HYD LINE        CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILIARY HYDRAULIC SYSTEM FILTER RETURN LINE. CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER. REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM. OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA12EA   E25NE                
20070718002382007071800238SO  2007       7          18         2007FA0000603    120070710G2910MS21911D6       FITTING                                 GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              HYD LINE        CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILLIARY HYDRAULIC SYSTEM FILTER RETURN LINE. CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER. REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM. OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA12EA   E25NE                
20070717000132007071700013SO  2007       7          17         2007FA0000604    120070710G2910MS21911D6       TEE FITTING                             GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              HYD SYSTEM      CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILIARY HYDRAULIC SYSTEM FILTER RETURN LINE. CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER. REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM. OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA12EA   E25NE                
20070717000142007071700014SO  2007       7          17         2007FA0000605    120070710G2910MS21911D6       TEE FITTING                             GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              HYD SYSTEM      CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILIARY HYDRAULIC SYSTEM FILTER RETURN LINE.  CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER.  REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM. OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA12EA   E25NE                
20070717000182007071700018EU  2007       7          17         2007FA0000606    120070712G2913350A35109221    SHAFT                                   SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                              HYD PUMP        WORN            B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW15186AE545                    3872        22484                       DURING DAILY INSPECTION DISCOVERED EXCESSIVE PLAY IN HYDRAULIC PUMP DRIVE PULLEY. HYDRAULIC PUMP DRIVE WAS THEN REMOVED FOR FURTHER INSPECTION. IT WAS DISCOVERED THAT THE DRIVE PULLEY SHAFT HAD WORN EXCESSIVELY WHERE THE DRIVE BEARING HAD BEEN SPINNING AROUND IT. THE DRIVE BEARING APPEARED TO BE FINE WITH NO BINDING NOTICED. IT APPEARS THAT THE FIT OF THE BEARING ONTO THE PULLEY WAS NOT TIGHT ENOUGH TO KEEP THE BEARING RACE FROM SPINNING.                                                                                                                                                                                                                                                                                      1G71 3U3  U  H9EU    E00054EN             
20070717000192007071700019EU  2007       7          17         2007FA0000607    120070712G2913350A35109221    PULLEY                                  SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                              HYD PUMP        WORN            B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW15186AE545                    3872        22484                       DURING DAILY INSPECTION DISCOVERED EXCESSIVE PLAY IN HYDRAULIC PUMP DRIVE PULLEY. HYDRAULIC PUMP DRIVE WAS THEN REMOVED FOR FURTHER INSPECTION. IT WAS DISCOVERED THAT THE DRIVE PULLEY SHAFT HAD WORN EXCESSIVELY WHERE THE DRIVE BEARING HAD BEEN SPINNING AROUND IT. THE DRIVE BEARING APPEARED TO BE FINE WITH NO BINDING NOTICED. IT APPEARS THAT THE FIT OF THE BEARING ONTO THE PULLEY WAS NOT TIGHT ENOUGH TO KEEP THE BEARING RACE FROM SPINNING.                                                                                                                                                                                                                                                                                      1G71 3U3  U  H9EU    E00054EN             
20070717000152007071700015SO  2007       7          17         2007FA0000608    120070710G2910MS21911D6       TEE FITTING                             GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              HYD SYSTEM      CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILIARY HYDRAULIC SYSTEM FILTER RETURN LINE. CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER. REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM. OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA12EA   E25NE                
20070717000162007071700016SO  2007       7          17         2007FA0000609    120070710G2910MS21911D6       TEE FITTING                             GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              HYD SYSTEM      CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILIARY HYDRAULIC SYSTEM FILTER RETURN LINE.  CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER.  REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM.  OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA12EA   E25NE                
20070717000172007071700017SO  2007       7          17         2007FA0000610    120070710G2910MS21911D6       TEE FITTING                             GULSTMG1159 GIV         3980115SO                                                               HYD SYSTEM      CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILIARY HYDRAULIC SYSTEM FILTER RETURN LINE. CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER. REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM. OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F    RTA12EA                        
20070718002392007071800239SO  2007       7          18         2007FA0000611    120070710G2910MS21911D6       FITTING                                 GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              HYD LINE        CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA23177BB                       1073                                    FOUND CRACKED HYDRAULIC TEE FITTING, PN MS21911D6, IN AUXILIARY HYDRAULIC SYSTEM FILTER RETURN LINE. CRACK WAS FOUND AT THE MALE END WHERE END AND TEE BODY COME TOGETHER. REPLACED FITTING AND PRESSURIZED AND LEAK CHECKED SYSTEM. OP'S CHECK WAS GOOD, NO LEAKS NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA12EA   E25NE                
20070718002462007071800246EU  2007       7          18         2007FA0000612    120070711G2741EM40112         ACTUATOR                                PIAGIOP180  P180        6960204EU  PWA   PT6   PT6A66      52043NE                              PITCH TRIM      FAILED          C      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      WP155166P61                     1129                                    ON APPROACH PITCH TRIM ACTUATOR FAILED TO MOVE.  AIRCRAFT LANDED WITH PARTIAL FLAPS WITHOUT FURTHER INCIDENT.  ONE HOUR LATER TRIM ACTUATOR GROUND TESTED REVEALING NO DEFECTS.  ACTUATOR SENT TO MFG FOR INVESTIGATION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H72 3O4  TRTA59EU   E26NE                
20070718002702007071800270CE  2007       7          18         2007FA0000613    120070713G3350                BATTERY                                 BEECH B300  B300        1159232CE                                                               EMERGENCY LIGHT MELTED          B      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      NE05122RG                       FL448                                   AIRCRAFT WAS IN MAINTENANCE FOR AN INSPECTION AND 12 MONTH EMERGENCY LIGHT BATTERY CHANGE.  FOUND BATTERIES SEVERELY CORRODED AND HEAT DAMAGED.  BATTERIES INSTALLED WERE  P/N MN1400. THESE BATTERIES HAVE A TEST STRIP EFFECTIVELY SHORTS THE BATTERY TO CHECK THE CHARGE CONDITION.  THE BATTERY HOLDER IN THE EMERGENCY LIGHT ASSEMBLY CLAMPS THE BATTERY. THE BATTERIES WERE INSTALLED SO THE TEST STRIP WAS CLAMPED SHORTING THE BATTERIES CAUSING THE BATTERIES TO MELT AND CORROD IN THE HOLDERS, DESTROYING THE LIGHT ASSEMBLIES. THE P/N FOR THE BATTERIES FOR THE EMERGENCY LIGHT IS 14A, BATTERIES WHICH HAVE NO TEST STRIP.   USE THE CORRECT P/N BATTERIES.                                                                       2L72 4T    RTA24CE                        
20070719001202007071900120CE  2007       7          19         2007FA0000617    120070718G2731556545098       ACTUATOR                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              RT STAB         WORN            B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW13264949131 1200              0605                                    AT THE PHASE 5 INSPECTION THE ELEVATOR FAILED THE FREE PLAY CHECK. A OVERHAULED UNIT P/N 5565450-98 S/N 0320-63 WAS INSTALLED AND COULD NOT GET THE UP AND DOWN LIMITS TO COME IN TO SPECS. ON CLOSER INSPECTION IT WAS FOUND THAT THE PRIMARY DRIVE GEAR HAS 16 TEETH AND THE ORIGINAL UNIT HAS 14 TEETH. THIS UNIT WAS OVERHAULED 6/8/2007. AS OF THIS WRITING WE ARE IN THE PROCESS OF INSTALLING ANOTHER UNIT WITH THE CORRECT NUMBER OF TEETH.                                                                                                                                                                                                                                                                                             1L72 4F4  F  A22CE   E1NE                 
20070719001422007071900142CE  2007       7          19         2007FA0000618    120070717G270007136242        ANCHOR          CESSNA                  CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  MASTER CYLINDER WORN            D      K   NONE                                                                                            O  OTHER                                                                         UKUNKNOWN        1                      SO09     3140                   172S9480    L1306651A   XB23004         ANCHOR PN 0713624-2, FOUND WORN ALMOST THROUGH BY THE STEEL PIN USED TO HOLD MASTER CYLINDER. ANCHOR IS ALUMINUM WHICH WAS QUICKLY WORN OUT BY THE STEEL PIN.  IF PIN BREAKS FREE FROM THE ANCHOR THE MASTER CYLINDER CAN STOP MOVEMENT OF THE RUDDER PEDAL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  ONT3A12    1E10    5  NP857     
20070719001442007071900144NM  2007       7          19         2007FA0000619    120070717G5714F13147LR        SKIN                                    UNIVAR415   415C        0420302NM  CONT  A75   A75*        17005SO                              CENTER WING     CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE012048H2500 10                2671                                    (5) MISSING AN426-3 RIVET HEADS ON LOWER CENTER SECTION SKINS PN F13147-L/-R PROMPTED INSPECTION HOLE INSTALLATION IAW SB-31 FOR REPAIR ACCESS. LIGHT SURFACE CORROSION WAS FOUND ON LOWER SKINS AND STIFFENERS. BOTH SIDES WERE CLEANED AND TREATED FOR CORROSION.  DURING CLEANING FOUND A 2 INCH SKIN CRACK IN AFT SECTION OF F13147-L AND A .5 INCH CRACK AT THE LOWER FWD TAB OF RIB PN F13016L, BOTH REPAIRED IAW AC 43.13-1B GUIDELINES. FUEL TANKS WERE REMOVED IAW SB-31 REQUIREMENTS AND 4 SMALL PATCHES OF LIGHT SURFACE CORROSION WERE FOUND ON THE RT OB END OF FWD FACE OF MAIN SPAR. CORROSION CLEANED AND TREATED. INSPECTION HOLE INSTALLATION ALLOWS MUCH BETTER VISUAL ACCESS FOR THE INSPECTION OF THE CENTER SECTION THAN W1L71 3O3  O  A718    E213                 
20070719001492007071900149SO  2007       7          19         2007FA0000620    120070525G2820MILH25579       LINE                                    PIPER PA44  PA44180     7104402SO  LYC   O360  IO360E1A    41514EA                              FUEL SYSTEM     LEAKING         D      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      SW13255ER5                      448195004   L47872T                     HOSE LEAK, ENGINE CAUGHT FIRE NOT DUE TO HOSE.  FUEL FED FIRE OFTEN STARTING AT NR 1 EXHAUST PORT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3O3  O  A19S0   1E10                 
20070719001502007071900150WP  2007       7          19         2007FA0000621    220070611G726131011607        SEAL                                    SCWZERG164  G164B       3952802EA  GARRTTTPE331TPE33143    01514WP                              COMPRESSOR      LEAKING         B  G6CRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW0948429                       19B                                     THE COMPRESSOR SEAL WAS LEAKING AND THE REAR SCAVENGE PUMP GEAR SHEARED OFF CAUSING IT TO FAIL.  THIS CAUSED MAJOR OIL LOSS AND THE PROP TO FEATHER.  HAVE REPLACED THE COMPRESSOR SEAL AND REAR PUMP TO PREVENT RECURRENCE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1Q71 3R4  T  1A16    E2WE                 
20070719001252007071900125WP  2007       7          19         2007FA0000622    220070611G7261                GEAR                                    SCWZERG164  G164B       3952802EA  GARRTTTPE331TPE33143B   01514WP                              SCAV PUMP       SHEARED         B  G6CRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW0948429                       19B         P80151                      THE COMPRESSOR SEAL WAS LEAKING AND THE REAR SCAVENGE PUMP GEAR SHEARED OFF CAUSING IT TO FAIL.  THIS CAUSED MAJOR OIL LOSS AND THE PROP TO FEATHER.  HAVE REPLACED THE COMPRESSOR SEAL AND REAR PUMP TO PREVENT RECURRENCE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1Q71 3R4  T  1A16    E2WE                 
20070719002662007071900266SO  2007       7          19         2007FA0000623    120070616G2810                FUEL                                    PIPER PA25  PA25        7102502SO  LYC   O320  O320A2B     41508EA  SNSNCH74D   74DM        EA  UNKNOWN         CONTAMINATED    D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA176195Z                       25229                   A61128          WATER IN FUEL.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  O  2A10    E274    5  NP88614   
20070719001482007071900148CE  2007       7          19         2007FA0000625    120070622G323008421022        BELLCRANK                               CESSNA310   T310Q       2074244CE  CONT  O520  TSIO520*    17040SO                              MLG             FAILED          B  MYNRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL11372CC4771                   310Q1071                                FAILED DUE TO MECHANICAL OVERLOAD, NOSE GEAR JAMMED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3O3  O  3A10    E8CE                 
20070719001522007071900152CE  2007       7          19         2007FA0000626    120070606G2910EM9159REVC      VALVE                                   RAYTHN390   390         7150030CE                                                               HYDRAULIC SYS   STICKING        B  E81RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL0318RF 85                     RB127                                   PILOT REPORTED RT HYDRAULIC SHUTOFF VALVE INITIALLY STUCK DURING PREFLIGHT TEST, THEN OPENED.  REPLACED VALVE WITH NEW UNIT, FUNCTIONAL TESTS, OK.  REMOVED VALVE ASSY, PN 39045AS65014-003, MANUFACTURED 11/2005.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3F    RTA00010WI                     
20070719001542007071900154SO  2007       7          19         2007FA0000627    120070606G3230455180          CONDUIT                                 PIPER PA24  PA24250     7102404SO  LYC   O540  O540A1D5    41532EA                              RT MLG          SEPARATED       G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA617178P                       242347      L359640                     RT MLG EXTEND/RETRACT CONDUIT PUSH-PULL TUBING SEPARATED AT THE SWEDGE CONNECTION JUST OB OF THE LANDING GEAR CONTROL SUPPORT BRACKET.  THERE WERE NO INDICATIONS OF IMPROPER INSTALLATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  O  1A15    E295                 
20070807001562007080700156CE  2007       8          7          2007FA0000628    120070718G5711                NUT PLATE                               CESSNA340   340A        2076405CE  CONT  O520  TSIO520*    17040SO                              SPAR            DAMAGED         G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW11345BK                       340A0113                                WHILE UNDERGOING A ANNUAL INSPECTION INVESTIGATION OF NOISE COMPLAINT FROM THE LANDING GEARBOX IT WAS DISCOVERED THAT THE FOUR AN3-6A BOLTS THAT ATTACH THE PART 5011013-3 (BRACKET ACUATOR MOUNTING) & GEARBOX TO THE FRONT SPAR WAS LOOSE.  AN ATTEMPT AT TIGHTEN THEM REVEALED THAT THE NUT PLATES BUILT INSIDE THE SPAR WERE STRIPPED.  ALLOWED THE GEARBOX TO MOVE BACK FROM THE SPAR BY 1/8" AND REAR BULKHEAD FLEXING THE 1/8". (FS152.75)                                                                                                                                                                                                                                                                                               1L72 3O3  O  3A25    E8CE                 
20070719001172007071900117CE  2007       7          19         2007FA0000629    120070718G5340                NUT PLATE                               CESSNA340   340A        2076405CE                                                               SPAR            LOOSE           G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW1160WH                        340A0083                                WHILE UNDERGOING A ANNUAL INSPECTION INVESTIGATION OF NOISE FROM THE LANDING GEARBOX, IT WAS DISCOVERED THAT THE (4) AN3-6A BOLTS THAT ATTACH THE PN 5011013-3 (BRACKET ACTUATOR MOUNTING) AND GEARBOX TO THE FRONT SPAR WAS LOOSE.  AN ATTEMPT AT TIGHTEN THEM REVEALED THAT THE NUT PLATES BUILT INSIDE THE SPAR WERE STRIPPED.  ALLOWED THE GEARBOX TO MOVE BACK FROM THE SPAR BY .1250 INCH AND REAR BULKHEAD FLEXING THE .1250 INCH.                                                                                                                                                                                                                                                                                                       1L72 3O      3A25                         
20070807001592007080700159EU  2007       8          7          2007FA0000630    120070524G7921369D25830101    BLOWER                                  HUGHES369   369FF       4470709EU  ALLSN 250C  250C30      03013GL                              OIL COOLER      DAMAGED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP1397FF 475                    0097F                                   OIL COOLER BLOWER APPEARS TO BE FOD`D OUT.  ONE BLADE WAS FOUND ENABLED IN THE HOUSING.  THE OUT OF BALANCE SITUATION BROKE ALL (4) BEARING CARRIER LEGS.  DAMAGED BLOWER WAS REPLACED AND AC WAS RETURNED TO SERVICE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  H3WE    E1GL                 
20070807001622007080700162SW  2007       8          7          2007FA0000631    120070628G57115262            SPAR                                    BBAVIA7     7GCAA       21101N8SW  LYC   O320  O320A2B     41508EA                              RT WING         CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP1111666                       23572       L31251278                   (2) LONGITUDINAL CRACKS AT SPAR HINGE FITTING.  SHAKING AND EXPANDING OF WOOD FIBERS DUE TO MOISTURE OR LACK OF.  RECOMMEND USING ALUMINUM SPARS OF SUFFICIENT SIZE AND STRENGTH.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3O3  O  A759    E274                 
20070807001642007080700164CE  2007       8          7          2007FA0000632    120070629G7830545300319       LINK ROD                                RAYTHNDH125 HAWKER800XP 7150012CE  GARRTTTFE731TFE731*     01518WP                              THRUST REVERSER CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL09245SM                       258567                                  PERFORMED EDDY CURRENT INSPECTION OF 8 EA THRUST REVERSER LINK ROD.  FOUND A CRACK IN (1) LINK ROD.  VERIFIED FINDING USING MAGNETIC PARTICLE INSP METHOD.  DURING MP INSP, NOTED ANOTHER CRACK, NOT DETECTED USING EDDY CURRENT.  DECIDED TO PERFORM MP INSP OF ALL RODS AND FOUND 3 MORE CRACKED.  CRACKS APPEAR TO BE ON THE INNER SURFACE AND WOULD NOT BE DETECTABLE WITH NDT INSP PRESCRIBED IN THE MM.  CURRENT INSPECTION REQUIREMENTS ARE NOT ADEQUATE FOR FINDING THESE TYPES OF DEFECTS.  CRACKS IDENTIFIED ARE ORIENTED LONGITUDINALLY O THE RODS AND VARY IN LENGTH FROM .500 IN TO 3.0 INCH.  IT SHOULD BE NOTE THAT MAG PARTICLE INSP IS NOT A REQUIREMENT OF AIR FRAME MFG.  (K)                                                2L72 4F4  FRTA3EU    E6WE                 
20070807001692007080700169CE  2007       8          7          2007FA0000634    120070520G71600750288         SUPPORT                                 CESSNA182   182E        2072712CE  CONT  O470  O470R       17026SO                              AIRBOX          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO112803Y                       18253803                                MECH DISCOVERED ON A 50 HR INSP, THE SUPPORT COLLAR ON THE AIRBOX MOUNTED TO THE CARBURETOR WAS CRACKED.  THIS COULD LEAD TO THE SEPARATION OF THE AIRBOX FROM THE CARBURETOR AND LOSS OF POWER.  PN 0750288 WAS REPLACED WITH NEW SUPPORT COLLAR PN 0750288-1 IAW SRM.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  ONT3A13    E273                 
20070807001712007080700171GL  2007       8          7          2007FA0000635    120070629G2420646843          ALTERNATOR                              CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO  HARTZLHCJ3Y PHCJ3YF1    GL  ENGINE          FAILED          B  T9ZRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM09769PC                       1619                    FP3952B         UPON RECEIPT OF CURRENT ALTERNATOR, NOTICED THAT SLIP-RING HOUSING WAS CLOCKED 180 DEGREES OUT OF ALIGNMENT OUT OF THE BOX.  THIS PLANE HAS HAD SEVERAL REPAIRED ALTERNATORS INSTALLED ON IT.  THE MOST RECENT ALTERNATOR HAD ONLY 131.1 HOURS BEFORE IT FAILED AND THE ONE PREVIOUS TO THAT ONE HAD 67.2 HOURS ON IT BEFORE IT FAILED.   (K)                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  ONTA00009CHE3SO    5  CP36EA    
20070807001722007080700172SW  2007       8          7          2007FA0000636    120070701G6410206016201127M   BLADE                                   BELL  206   206B        1181511SW  ALLSN 250B  250B*            GL                              TAIL ROTOR      DEPARTED        D      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           CRCRUISE         1                      SO15357DC                       1803                                    THE CENTER TIP WEIGHT SLUNG OUT OF SUBJECT TAIL ROTOR BLADE DURING FLIGHT, CAUSING A VIOLENT VIBRATION.  THE VIBRATION CAUSED (3) OF THE TAIL ROTOR GEAR BOX STUDS TO SHEAR BEFORE THE AIRCRAFT COULD AUTO ROTATE TO THE GROUND.  IF THE HELICOPTER HAD NOT MADE IT TO THE GROUND WHEN IT DID THE OTHER STUD WOULD HAVE SHEARED AND THE TAIL ROTOR GEAR BOX WOULD HAVE LEFT THE AIRCRAFT AND THE RESULTS WOULD HAVE BEEN DISASTROUS.  RECOMMEND THE TIP BLOCKS BE MFG FROM MATERIAL THAT CAN WITHSTAND THE CENTRIFUGAL FORCES THAT ARE APPLIED TO THE TIP WEIGHTS DURING FLIGHT. RECOMMEND THAT HELICOPTER TAIL ROTOR BLADE TIPS BE INSPECTED AS SOON AS POSSIBLE AND EVERY 100 HR INSPECTION.  (K)                                             1G71 3U3  T  H2SW    E10CE                
20070807001732007080700173SO  2007       8          7          2007FA0000637    220070613G8520SA640518        PISTON                                  CESSNA182   182H        2072718CE  CONT  O470  O470R       17026SO  MCAULY2A34C 2A34C66     GL  NR1 CYLINDER    FRACTURED       D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA171858X           4765K06552  18255958    1308944R    733700          AFTER INSTALLING NEW CYLINDER ASSY SA47006S-A20P WITH NEW PISTON ASSY PN SA640518, WE WERE PERFORMING BREAK IN RUN AT LOW POWER, FIRST AT 800 RPM FOR 2 MIN.  SHUTDOWN ENGINE, CLEANED FOULED PLUGS DUE TO OIL IN CYLINDER FROM ASSY.  RAN ENGINE AT 1000 RPM FOR 3 MIN.  SHUTDOWN AND CLEANED SPARK PLUGS AGAIN.  RESTARTED ENGINE AND ADVANCED TO 1200 RPM, THE CYLINDER CLEARED OUT AND THEN STOPPED AFTER A FEW SECONDS.  AFTER REMOVING THE OIL PAN AND NR 1 CYLINDER THE PISTON APPEARED TO HAVE FRACTURED ALONG A CASTING FAULT IN THE PISTON PIN BOSS.  THE RESULTING DEBRIS BENT THE CAM SHAFT, BROKE BOTH CRANKSHAFT HALVES.  (K)                                                                                                     1H71 3O3  ONT3A13    E273    5  CP3EA     
20070807001742007080700174NE  2007       8          7          2007FA0000638    220070625G7250                BLADES                                  UROCOPEC135 EC135P1     8680990EU  PWA   PW206 PW206B      0    NE                              ENGINE          DAMAGED         B  HDNRA   UNSCHED LANDING                                                                                 ERYVIBRATION/BUFFET          PARTIAL RPM/PWR LOSS      ENGINE STOPPAGE           CRCRUISE         1                      SW03911SV                       0015        BB0113                      DURING FLIGHT, A LOUD BANG WAS HEARD AND THEN ALL ENGINE INSTRUMENTS SHOWED AN INDICATION OF A TOTAL ENGINE FAILURE.  THE ENGINE WAS SECURED AND A SINGLE ENGINE LANDING WAS INITIATED WITHOUT INCIDENT.  UPON INSPECTION, IT WAS NOTICED THAT THE EXHAUST AREA OF THE ENGINE, THERE WERE PT ROTOR BLADES MISSING OR DAMAGED.  THE ENGINE WILL BE SENT BACK TO THE MFG FOR EVALUATION.  (K)                                                                                                                                                                                                                                                                                                                                                     1G72 3U3  UO H88EU   E42NE                
20070807001752007080700175CE  2007       8          7          2007FA0000639    120070507G323312810013        HOUSING                                 CESSNA172   172RG       2072438CE  LYC   O360  O360*       41514EA  MCAULY2D34C B2D34C220   GL  MLG ACTUATOR    CRACKED         C      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      GL094604V                       172RG0337   L2232D38A   801046          ON A DUAL TRAINING FLIGHT, STUDENT AND INSTRUCTOR HEARD A NOISE WHEN LANDING GEAR WAS RETRACTED.  LT LANDING GEAR REMAINED IN A PARTIALLY RETRACTED/ EXTENDED POSITION, UNABLE TO ACTUATE UP OR DOWN.  THE LT LANDING GEAR ACTUATOR BODY HAD FAILED (CRACKED) AT THE FWD MOUNTING BOLT HOLE, ALLOWING THE ACTUATOR BORE TO OPEN ENOUGH SO THAT  PISTON WOULD NOT ENGAGE THE LANDING GEAR PIVOT SECTOR GEAR SUFFICIENTLY TO MOVE THE LANDING GEAR.  (K)                                                                                                                                                                                                                                                                                          1H71 3O3  O  3A17    E286    5  CP7EA     
20070807001762007080700176SW  2007       8          7          2007FA0000640    120070702G3250                SOLENOID VALVE                          SWRNGNSA226 SA226T      8780122SW  GARRTTTPE331TPE33110U   01514WP                              NLG STEERING    FAILED          B  O9IRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM09749L                        T306                                    THE NOSE WHEEL STEERING WAS TESTED PRIOR TO FLIGHT, AD TESTED SATISFACTORY.  AT AROUND 60 TO 70 KNOTS DURING THE TAKEOFF ROLL, THE AC STEERING FAILED IN A MANOR THAT RESULTED IN THE AC PULLING HARD TO THE LEFT.  USING HARD RT BRAKE AND RT REVERSE THRUST THE AC WAS STOPPED BEFORE RUNNING OFF THE RUNWAY.  WHEN THE SPEED LEVER WAS RETARDED THE STEERING , RE-ENGAGED, AS IT SHOULD HAVE, AND THE AC OPERATED NORMALLY.                                                                                                                                                                                                                                                                                                                  2L72 4T4  TRTA5SW    E4WE                 
20070808000152007080800015CE  2007       8          8          2007FA0000641    120070706G282016864           LINE                                    CESSNA210   T210N       2073456CE  CONT  O520  TSIO520R    17040SO                              FUEL SYSTEM     MISMANUFACTURED D      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      SW134631C394                    21063582                                NEW FUEL INJECTOR LINE NR 5 CYL RAM PMA REPLACEMENT.  INSTALLED ON ENGINES, WELD DEFECT ALLOWED DEVIPER END BAIL TO COME LOOSE FROM LINE.  NOTED FUEL LEAN ON TOP OF ENGINE AT ANNUAL 100 HR INSP.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  3A21    E8CE                 
20070808000162007080800016CE  2007       8          8          2007FA0000642    120070703G2820L2891948A       LINE                                    CESSNA182   182T        2072703CE  LYC   O540  IO540*      41532EA                              FUEL SYSTEM     LEAKING         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA21818CP923                    18281258    L2891948A                   FOUND HEAVY FUEL STAIN FROM OIL COOLER NR 5 INTAKE PIPE AND ON FIREWALL APPROVED TO BE NR 5 INTAKE PIPE.  FURTHER INSPECTION FOUND NR 5 FUEL INJECTION LINE LOOSE AT INJECTOR.  FOUND AND SNUGGED SEVERAL OTHER INJECTOR LINES AT INJECTOR AND FLOW DIVIDER AD-02-01, AD LAST C/W 5-3-07. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A13    1E4                  
20070808000172007080800017CE  2007       8          8          2007FA0000643    120070613G3246G129            WHEEL                                   CESSNA172   R172K       2072431CE                                                               NLG STRUT       MISREPAIRED     G      O   OTHER                                                                                           O  OTHER                                                                         TOTAKEOFF        1                      GL13736MV120                    R1722642                                DURING TAKEOFF FROM A GRASS STRIP AS THE AIRCRAFT APPROACHED 30 TO 40 KNOTS, BOTH NOSE WHEELS INSTALLED ON THE FLOATS FAILED, CAUSING THE AIRCRAFT TO FLIP ON TO ITS BACK.  UPON EXAMINATION OF THE FLOAT NOSE WHEEL STRUTS THE FAILURE OCCURRED AT THE WELD JOINT OF BOTH LT AND RT WHEEL STRUTS.  IT APPEARS THAT THE WELDS DID NOT HAVE ADEQUATE PENETRATION.  INVESTIGATION OF MFG IN PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                         1H71 3O      3A17                         
20070807001632007080700163CE  2007       8          7          2007FA0000646    120070719G271005232182        PUSHROD                                 CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              AILERON         BENT            B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA072277T                       172S9958                                AILERON PUSHROD WAS FOUND BENT DURING PREFLIGHT.  REMOVED PUSHROD AND WENT TO INSTALL NEW ROD AND FOUND THAT ALL FOUR RODS IN STOCK HAD BAD THREADS- PD WAS OVERSIZED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3O3  ONT3A12    1E10                 
20070808000102007080800010EA  2007       8          8          2007FA0000647    220070720G8520AE75089         PISTON                                  CESSNA172   172M        2072418CE  LYC   O360  O360A4M     41514EA                              NR 2 CYLINDER   CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP27208581522                   17263857    L4988127A                   PISTON SKIRT CRACKED ON 2 CYLINDERS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A12    E286                 
20070808000262007080800026    2007       8          8          2007FA0000648    420070720G3457GNS530W         DISPLAY                                 CESSNA414   414A        2075907CE                                                               GPS             MALFUNCTIONED   C      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      WP05     25                                                             SETTING AN EVENT IN THE AUX PAGE FOR A FUTURE TIME CAUSES AUX EVENTS PAGE TO NO LONGER FUNCTION.  SELECTING THIS PAGE CAUSES THE NAV6, GPS SATELLITE STATUS PAGE TO DISPLAY FOR 1 SECOND, THEN NAV2 PAGE(MAP) TO BE SELECTED.  AS A SIDE EFFECT, THE FLIGHT TIMER IS RESET EVERY TIME THE AUX PAGE IS ATTEMPTED TO BE SELECTED.  IT APPEARS THAT THE FIRMWARE BECOMES LOST, BUT RECOVERS.                                                                                                                                                                                                                                                                                                                                                       1L72 3O      A7CE                         
20070808000272007080800027CE  2007       8          8          2007FA0000651    120070722G2810                FUEL CAP                                CESSNA185   185F        2072820CE  CONT  O520  IO520D      17032SO                              WING            LEAKING         P      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      SW13     5                      18503193                                FUEL LEAKING FROM BASE OF NEWLY INSTALLED PREMIUM FUEL CAPS. LOCATION ON WINGS IRRELEVANT. LEAK FROM BOTH IB AND OB CAPS. COMPLIED WITH MFG INSTRUCTIONS IAW VENT LOCATION WITHOUT EFFECT.  EVIDENTLY NOT UNCOMMON PROBLEM, AS BLOGS ON MFG CLUB FORUM AND PILOTS ASSOC. FORUM WILL ATTEST. MFG SENT NEW O-RINGS, BUT HAVEN'T TRIED THEM. NEVERTHELESS, CAPS SHOULD BE FOOL-PROOF FROM FACTORY. HARDLY AN IMPROVEMENT OVER MY OLD MFG RAISED INLET CAPS.                                                                                                                                                                                                                                                                                        1H71 3O3  O  3A24    E5CE                 
20070808000492007080800049SO  2007       8          8          2007FA0000657    120070629G2720480572          ROLL PIN                                PIPER PA42  PA421000    7104225SO                                                               RUDDER PEDAL    SHEARED         B  GW1RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA03411BG5362                   425527004                               PILOTS RT RUDDER PEDAL ROLL PINS SHEARED.  REFERENCE IPC PN 761792, FIG. 103, INDEX 14, PN 480572.  FAILURE MAY CAUSE LOSS OF DIRECTIONAL CONTROL OR BRAKING ACTION DURING GROUND OPERATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 4T    RTA23SO                        
20070808000502007080800050CE  2007       8          8          2007FA0000658    120070612G2820052355912       VENT            CESSNA                  CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA                              LT WING TANK    OBSTRUCTED      D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW07521199458       0301        17274418    L1058239A                   ENGINE QUIT IN FLIGHT WITH HALF TANK OF FUEL REMAINING.  UPON VISUAL INSPECTION OF LT WING, FOUND THE FUEL VENT LINE PN 052355912 OBSTRUCTED WITH INSET REMAINS (WASP).  PHYSICALLY REMOVED OBSTRUCTION AND OPS TESTED ENGINE ON ALL TANK SETTINGS.  UPON SUCCESSFUL OPS CHECK OF FUEL SYSTEM, MADE LOG ENTRY AND RETURNED THE AIRCRAFT TO SERVICE.  AIRCRAFT HAS SUCCESSFULLY FLOWN 50 HRS SINCE 6/12/07 WITH NO FURTHER INCIDENT.                                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A12    E274                 
20070808000512007080800051CE  2007       8          8          2007FA0000659    120070712G3230HMXL6G          ROD END                                 BEECH 58    58          1152740CE  CONT  O520  IO520*      17032SO                              NLG             UNSERVICEABLE   G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL01820GW                       TH13                                    DURING EXAMINATION OF AIRCRAFT POST INCIDENT, IT WAS DISCOVERED THAT ROD END (PN HMXL6G) ATTACHED TO THE NOSE GEAR RETRACT ARM (PN 35825172-2) WAS SHEARED OFF BELOW THE BEARING.  IT APPEARS THE FAILURE STARTED IN A CRACK IN THE THREADS.  THIS MOST LIKELY RELEASED THE OVER CENTER TENSION ON THE NOSE GEAR DOWNLOCK ALLOWING THE NOSE GEAR TO RETRACT AND SUBSEQUENTLY THE MAIN LANDING GEAR.  RECOMMEND ANNUAL PENETRANT INSPECTION OF ALL LANDING GEAR RETRACTION ROD ENDS.  (K)                                                                                                                                                                                                                                                        1L72 3O3  O  3A16    E5CE                 
20070808000522007080800052EA  2007       8          8          2007FA0000660    220070526G8530                EXHAUST VALVE                           PIPER PA28  PA28140     7102802SO  LYC   O320  O320E2A     41508EA                              NR 4 CYLINDER   BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO137342J3339 941               2824671     L2283027A                   NR 4 EXHAUST VALVE BROKE DURING FLIGHT, DAMAGING PISTON CAUSING OIL TO LEAK OUT EXHAUST PORT CREATING OIL SMOKE.   (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3O3  O  2A13    E274                 
20070808000572007080800057SO  2007       8          8          2007FA0000661    120070701G1210                FUEL                                    MAULE M5    M5210C      5460134SO  CONT  O360  IO360A      17025SO                                              CONTAMINATED    D      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      AL0562045     3                 6078C                                   WHILE PERFORMING BI-ANNUAL REVIEW.  ON LAST TAKEOFF, THE ENGINE BEGAN TO RUN ROUGH.  ENGINE DRIVEN FUEL PUMP FAILED AND INSTALLED A FRESHLY OVERHAULED PUMP.  ATTEMPTED A RUN UP WITH THE SECOND PUMP AND FOUND THE COVER PLATE AT THE MIXTURE CONTROL LEVER TO BE LEAKING.  REMOVED SECOND PUMP.  OVERHAUL SHOP  FOUND EVIDENCE OF WATER IN THE FUEL SYSTEM, LIGHT RUST IN THE ORIGINAL PUMP BODY, AND A WHITE FILM UNDER THE PRESSURE VALVE SEAT THAT DISINTEGRATED INTO A WHITE POWDER WHEN IT DRIED.  THE PUMP WAS NOT ABLE TO PRODUCE THE PROPER PRESSURE WITH THIS FILM HOLDING THE VALVE OPEN.  DECIDED TO FLUSH THE FUEL SYSTEM AND TRY TO DETERMINE THE SOURCE OF CONTAMINATION.   FLUSHED ALL OF THE FUEL LINES.     THERE WAS LIGHT S1H71 3O3  O  3A23    E1CE                 
20070808000582007080800058    2007       8          8          2007FA0000662    120070628G8011MZ422           STARTER                                                                                                                                                 BURNED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW99                                                                    STARTER BURNED UP ON TEST CELL RUN.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  
20070808000612007080800061CE  2007       8          8          2007FA0000664    120070628G321307416302        SPRING ASSY                             CESSNA182   182R        2072731CE  CONT  O470  O470*       17026SO                              AXEL FITTING    CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO095544N14045                  18267782                                DURING NDI OF MAIN LANDING GEAR SPRING ASSY, THE RT FITTING WAS FOUND CRACKED.  DURING WFPT FOR ASTM E1417.  PART WAS REPLACED WITH A SERVICEABLE UNIT.  SUSPECT CRACK WAS DUE TO CORROSION BETWEEN THE SPRING AND ALUMINUM FITTING.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  ONT3A13    E273                 
20070808000642007080800064CE  2007       8          8          2007FA0000665    120070726G1100                PLACARD                                 CESSNA172   172S        2072439CE                                                               CABIN           INCORRECT       C      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      EA07                                                                    AIRCRAFT WITH AVIONICS: LOCATION OF INTERIOR ELT PLACARD IN BAGGAGE COMPARTMENT INDICATES THAT THE ELT IS BEHIND THE LOWER ACCESS PANEL TO THE AFT FUSELAGE.  THAT IS INCORRECT.  THE ELT ACCESS IS FROM THE UPPER PANEL.  REMOVED PLACARD AND FABRICATED NEW PLACARD AND PLACED IT ON THE UPPER ACCESS PANEL.                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O    NT3A12                         
20070808000662007080800066EA  2007       8          8          2007FA0000667    220070726G8530AEL85099        CYLINDER HEAD                           HUGHES269   269C1       8059504SW  LYC   O360  HO360C1A    41514EA                              NR 2 CYLINDER   SEPARATED       B      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      WP272021G1046                   0095        L3725036A                   NR 2 CYLINDER HEAD SEPARATED FROM CYLINDER BARREL IN FLIGHT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3O3  OO 4H12    E286                 
20070808000682007080800068EU  2007       8          8          2007FA0000669    220070710G7200DN3351053050    DAMPER                                                                     CFMINTCFM56 CFM563C1    13802EU                              ENGINE          FAILED          B  UOXRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO19                                        ESN725219                   WAS NOTIFIED BY TEST CELL OPERATOR THAT DAMPER ASSY PN DN335-105-305-0 CAME APART DURING ENGINE TEST CELL OPERATIONS OF ENGINE DURING ENGINE TEST AND AFTER POST ENGINE ADJUSTMENT.  THE DAMPER ASSY WAS DISCOVERED IN THE ENGINE INLET AREA. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      4  F          E21EU                
20070808000692007080800069CE  2007       8          8          2007FA0000670    120070309G2460IN31X100050CM358MASTER SWITCH                           CESSNA402   402C        207590RCE                                                                               FAILED          C      O   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      SW99J8VBL                       0640                                    LOST POWER TO THE AVIONICS BUSS.  CARRIED OUT THE REQUIRED CHECKS AND TRIED REPEATEDLY TO RESTORE POWER TOT THE AVIONICS BUSS VIA THE EMERGENCY AVIONICS BUSS SWITCH, TO NO AVAIL.  LANDED, CONTACTED MAINTENANCE, WHO CONFIRMED THE AVIONICS BUSS FAILURE.  (K) INVESTIGATE AVIONICS BUSS SYS FAILURE AND FOUND AVIONICS MASTER SWITCH DEFECTIVE.  MASTER SWITCH REMOVED AND REPLACED WITH NEW ITEM IAW MEB 05-1.  FUNCTION CHECK OF MASTER AVIONICS SWITCH AND EMERGENCY AVIONICS BUSS SWITCH CARRIED OUT SATISFACTORY.  (K)                                                                                                                                                                                                                  1L72 3O      A7CE                         
20070807000332007080700033EU  2007       8          7          2007FA0000671    120070727G5310A741210N        BRIDGE                                  LET   L23   L23         1360308EU                                                                               CRACKED         B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM03431BA1693                   029013                                  DURING A ROUTINE DYE-PENETRANT INSPECTION ON TG-10B CRACKS WERE DISCOVERED AT SEVERAL WELDS ON THE A741 210N BRIDGE ASSEMBLY.    A REPLACEMENT BRIDGE ASSY CANNIBALIZED FROM ANOTHER TG-10B IN AN EFFORT TO PLACE THE FIRST NOTED AIRCRAFT BACK IN SERVICE.  AS A PRECAUTIONARY STEP, DECIDED TO DYE-PENETRANT THE CANNIBALIZED ASSEMBLY AND DISCOVERED IT TOO WAS CRACKED.   DECIDED TO INSPECT THE REST OF THE ACFT.  12 OUT OF 12 ACFT REVEALED CRACKS.                                                                                                                                                                                                                                                                                      1K00       RCG24EU                        
20070808000932007080800093EU  2007       8          8          2007FA0000672    120070727G5101A741210N        BRIDGE                                  LET   L23   L23         1360308EU                                                               ZONE 100        CRACKED         B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM03431BA1693                   029013                                  ON JULY 23, 2007 DURING A ROUTINE DYE-PENETRANT INSPECTION ON TG-10B (L-23 SUPER BLANIK, S/N 029013) CRACKS WERE DISCOVERED AT SEVERAL WELDS ON THE A741 210N BRIDGE ASSEMBLY.  IT IS A MAINTENANCE MANUAL REQUIREMENT THAT THIS PART BE DYE-PENETRANT INSPECTED EVERY 1000 HOURS.  A REPLACEMENT BRIDGE ASSEMBLY WAS CANNIBALIZED FROM ANOTHER TG-10B (L23, S/N 029015) IN AN EFFORT TO PLACE THE FIRST NOTED AIRCRAFT BACK IN SERVICE.  AS A PRECAUTIONARY STEP, WE DECIDED TO DYE-PENETRANT THE CANNIBALIZED ASSEMBLY AND DISCOVERED IT TOO WAS CRACKED.  AT THIS POINT IT WAS DECIDED TO INSPECT THE REST OF THE AIRCRAFT HERE AT USAFA.  12 OUT OF 12 AIRCRAFT REVEALED CRACKS.                                                            1K00       RCG24EU                        
20070808000962007080800096CE  2007       8          8          2007FA0000674    120070717G2910SA7670024001    LINE                                    RAYTHNDH125 HAWKER800XP 7150012CE                                                               HYD SYSTEM      RUPTURED        C      H   DEACTIVATE SYST/CIRCUITS                                                                        KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      EA2750AE 1848                   258650                                  FLEXIBLE HYDRAULIC LINE TO THE RT MAIN GEAR IB DOOR ACTUATOR RUPTURED IN FLIGHT. CREW EXTENDED LANDING GEAR AND FLAPS USING THE AUXILIARY HYDRAULIC SYSTEM AND LANDED WITHOUT INCIDENT. DURING INSPECTION BY MAINTENANCE DEPARTMENT NO APPARENT CAUSE WAS DETERMINED FOR THE LINE FAILURE. MFG HAS BEEN ADVISED OF THE DEFECT. NEW HYDRAULIC LINE WAS INSTALLED, SYSTEM WAS SERVICED WITH FLUID AND BLED, AIRCRAFT WAS RETURNED TO SERVICE.                                                                                                                                                                                                                                                                                                     2L72 4F    RTA3EU                         
20070808001132007080800113CE  2007       8          8          2007FA0000675    120070712G573008220009        SKIN                                    CESSNA340   340A        2076405CE  CONT  O520  TSIO520*    17040SO                              LT WING         CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE078647K6580                   340A0605                                CRACK IN THE TOP SKIN OF THE LT WING AT THE LANDING GEAR SIDE BRACE ATTACHMENT LOCATION, APPROXIMATELY WS 63.45.  THE SKIN IS 2024-T63 ALUMINUM, .032 THICK.  THE CRACK IS ABOUT 3 INCHES LONG OR LONGER.  CANNOT DETERMINE THE TOTAL LENGTH OF THE CRACK.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 3O3  O  3A25    E8CE                 
20070808001112007080800111EA  2007       8          8          2007FA0000677    220070715G8530AEL85099IR      CYLINDER HEAD                           HUGHES269   269C1       8059504SW  LYC   O360  HO360C1A    41514EA                              ENGINE          SEPARATED       G      A   UNSCHED LANDING                                                                                 EDKVIBRATION/BUFFET          INFLIGHT SEPARATION       FLUID LOSS                CLCLIMB          1                      WP272021G1046 1046              0095        L3725036A                   2 NR CYLINDER HEAD ASSEMBLY APPEARS TO HAVE FAILED DURING FLIGHT RESULTING IN A SEVERE ENGINE VIBRATION AND A FORCED LANDING. EXAMINATION OF UPPER HALF OF FAILED CYLINDER ASSEMBLY REVEALS THAT A CRACK OCCURRED AND PROPAGATED SYMMETRICALLY AROUND THE CYLINDER APPROXIMATELY .3750 BENEATH WHERE THE CYLINDER BARREL MEETS THE CYLINDER HEAD. NO INTERNAL CYLINDER /PISTON DAMAGE WAS VISUALLY OBSERVED.                                                                                                                                                                                                                                                                                                                                    1G71 3O3  OO 4H12    E286                 
20070808001102007080800110GL  2007       8          8          2007FA0000678    120070624G32301956750         SHUTTLE VALVE                           BLANCA17    1730A       1220433GL  CONT  O520  IO520K      17032SO  HARTZLHCC3Y HCC3YF1     GL  MLG             MALFUNCTIONED   G      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      SW018847V1527 4                 30359                                   THE AIRCRAFT LOST ELECTRICAL POWER AND PILOT TRIED TO EXTEND THE LANDING GEAR USING THE EMERGENCY LEVER.  THE EMERGENCY LOWERING OF THE LANDING GEAR DID NOT TAKE PLACE AND THE PILOT HAD TO LAND THE AIRCRAFT WITH THE LANDING GEAR IN THE FULL UP POSITION.  DAMAGE; PROP STRIKE, LOWER FUSELAGE SKIDDING DAMAGE, LOWER FUSELAGE FUEL DRAIN GROUND OFF, SUDDEN STOPPAGE OF THE ENGINE.                                                                                                                                                                                                                                                                                                                                                        1L71 3O3  O  A18CE   E5CE    5  CP25EA    
20070821000242007082100024SW  2007       8          21         2007FA0000680    120070729G793335C155103       SENSOR                                  ECLIPSEA500 ECLIPSEEA5003350000SW              PW610FA                                          OIL TEMP        FAULTY          C      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      EA27116DJ32                     000021      LA0009                      RT ENG HIGH OIL TEMPERATURE CAS MESSAGE UPON LANDING. EXCEEDANCE (OIL TEMP) AFTER LANDING-ENGINE SHUTDOWN DURING TAXI. FOUND FAULTY MOT/MOP SENSOR REPLACED WITH NEW UNIT AND OPERATIONALLY CHECKED SATISFACTORY IAW EMM 79-30-04.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 4J    RTA00002AC                     
20070808001092007080800109NE  2007       8          8          2007FA0000681    220070731G856013814           SEAL                                                                       PWA   R1340 R1340AN1    52016NE                              SUPERCHARGER    LEAKING         B      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      SW15                                                                    DISASSEMBLY OF THE ENGINE AND OR REAR SECTION AFTER CUSTOMERS REPORTED SMOKING AND INCREASE IN OIL CONSUMPTION. DURING THE DISASSEMBLY IT WAS FOUND THAT BLOWER SEALS HAVE FAILED AND BEEN LEAKING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    3  R          5E2                  
20070821000642007082100064CE  2007       8          21         2007FA0000683    120070712G573008220009        SKIN                                    CESSNA340   340CESSNA   2076404CE  CONT  O520  TSIO520*    17040SO                              RT WING         CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE075152J                       3400542                                 CRACK IN THE TOP SKIN OF THE RT WING AT THE LANDING GEAR SIDE BRACE ATTACHMENT LOCATION, APPROX WS 63.45.  THE SKIN IS 2024-T3 ALUMINUM, .032 THICK.  THE CRACK IS ABOUT 4.5 INCHES LONG.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3O3  O  3A25    E8CE                 
20070821000652007082100065EA  2007       8          21         2007FA0000684    220070712G8520                CRANKSHAFT                              CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              ENGINE          CORRODED        B  YYBRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03175AF4363                   17281175    L3097351A                   FOUND CRANKSHAFT TO BE PITTED, LAST INSPECTION WAS DONE BY MFG (4) YEARS AGO.  THIS ENGINE HAD HIGH UTILIZATION AND FREQUENT OIL CHANGES.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    1E10                 
20070821000672007082100067SO  2007       8          21         2007FA0000685    220070712G8550ES48109         OIL FILTER                                                                 CONT  O520  IO520M      17032SO                              ENGINE          CONTAMINATED    C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL11                                        560171                      THE ENGINE OIL SYSTEM WAS CONTAMINATED BY OIL FILTER SEAL DEBRIS. (K) ON DISASSEMBLY OF THE ENGINE RUBBER DEBRIS WAS FOUND:  IN THE OIL PASSAGE THAT FEEDS THE STARTER ADAPTER WITH THE ADAPTER PILOT BEARING PLUGGED.  UPON SPLITTING OF THE ENGINE CASE DEBRIS WAS FOUND IN THE OIL PASSAGE TO THE NR 3 MAIN BEARING.  BOTH OIL COOLING JETS TO NR 3 MAIN BEARING WERE PLUGGED WITH RUBBER DEBRIS.  THE RIGHT WAS PLUGGED WITH A PIECE .6250 INCH LONG AND THE LT WITH A PIECE .1875 INCH LONG.  ONE PIECE OF RUBBER DEBRIS WAS LOCATED IN THE OIL PASSAGE TO THE NR 5 BEARING.  (K)                                                                                                                                                                 3  O          E5CE                 
20070821000682007082100068CE  2007       8          21         2007FA0000686    120070713G551045A2110422      RIB                                     BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              HORIZONTAL STAB CRACKED         B  KX5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL1552AW 4500                   RK115                                   HORIZONTAL STABILIZER LEADING EDGE IB RIBS ARE CRACKED AT THE ROLLER BRACKET ATTACHMENT POINTS.  SAFETY COMMUNIQUE NR 70 IS ONLY PUBLISHED CRITERIA CONCERNING THIS PROBLEM.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4F4  FRTA16SW   E25EA                
20070821000702007082100070GL  2007       8          21         2007FA0000687    120070724G3230105932B         POWERPACK                               BLANCA17    1731A       1220435GL  LYC   O540  IO540K1E5   41532EA                              MLG             BURNED OUT      D      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      SW151474618                     7532156                                 THIS COMPONENT WAS INSTALLED FRESHLY OVERHAULED ON APRIL 6, 2006 AND HAS A TOTAL IN USE TIME OF 18.0 HOURS.  AFTER TAKEOFF THE PILOT NOTICED THE LANDING GEAR WOULD NOT RETRACT.  TROUBLESHOOTING OF THE LANDING GEAR SYSTEM FINDS THE HYDRAULIC POWER PACK MOTOR WINDINGS ARE OPEN, MOTOR WILL NOT RUN.  UNIT WAS OVERHAULED UNDER WO NR AH-16326.  (K)                                                                                                                                                                                                                                                                                                                                                                                        1L71 3O3  O  A18CE   1E4                  
20070808001142007080800114WP  2007       8          8          2007FA0000688    120070710G2400                BRACKET                                 HUGHES269   269C        4470504WP  LYC   O360  HIO360D1A   41514EA                              ALTERNATOR      LOOSE           C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP059988F                       S1791       RL2203051A                  ALTERNATOR BRACKET LOOSE AT ENGINE BOSS.  BOLT CAUSES DAMAGE TO ENGINE CRANKCASE WHEN LOOSE.  FRETTING OF ARM AND ENGINE CRANKCASE OCCURS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3O3  O  4H12    1E10                 
20070821000722007082100072CE  2007       8          21         2007FA0000689    120070701G2497S159660L        CIRCUIT BREAKER                         CESSNA172   172M        2072418CE  LYC   O320  O320*       41508EA                              COCKPIT         FAILED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE0180213                       17266449                                PILOT STATED SMOKE IN COCKPIT.  INSPECTION REVEALED ALTERNATOR OUTPUT C/B FAILED, ALTERNATOR HAD BROKEN AND LOOSE PARTS INTERNALLY, AND VOLTAGE REGULATOR FAILED.  OPENED C/B AND FOUND INTERNAL PARTS HAD MELTED CAUSING SMOKE.  NO SIGNS OF WIRE OVERHEATING, OR SECONDARY DAMAGE WAS FOUND.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A12    E274                 
20070821000742007082100074CE  2007       8          21         2007FA0000690    120070707G531207126161        BULKHEAD                                CESSNA182   182K        2072724CE  CONT  O470  O470*       17026SO                              BS 230          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP282787Q4575                   18257987                                DURING INSPECTION OF THE AFT TAILCONE BULKHEAD (STATION 230.187) A CRACK APPROX .375 INCH LONG WAS DISCOVERED.  THE CRACK LOCATION WAS ON THE LT SIDE EMANATING FROM THE RUDDER CUTOUT HOLE AND PROGRESSING TOWARD THE BULKHEAD FLANGE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  ONT3A13    E273                 
20070821000762007082100076CE  2007       8          21         2007FA0000691    120070625G2420991059111RX     ALTERNATOR                              CESSNA182   182T        2072703CE  LYC   O540  IO540AB1A5       EA                              ENGINE          FAILED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW03232AF573                    18281180    L2860348A                   AC ARRIVED AT 1R4 WITH A FAILED ALTERNATOR.  SYSTEM WAS TESTED TO CONFIRM THAT THE ALTERNATOR WAS THE PROBLEM.  ON 6/25/07 THE ALTERNATOR IN QUESTION WAS REMOVED FROM THE AC.  UPON REMOVING THE ALTERNATOR THE TECHNICAN FOUND THE SAFETY LOCK WIRE FOR THE ALTERNATOR HOUSING HALVES WAS BROKEN AND ONE OF THE FOUR CAP SCREWS WAS MISSING AND THE OTHER (3) WERE LOOSE.  THE AC WAS INSPECTED AGAIN TO DETERMINE IF ANY OTHER PART COULD HAVE COME IN CONTACT WITH THE ALTERNATOR TO CAUSE THE SAFETY LOCK WIRE TO BREAK.  NO CONFLICTS WERE NOTED DURING THIS INSPECTION.  DIGITAL PICTURES HAVE BEEN TAKEN FOR RECORD AND ARE AVAILABLE UPON REQUEST.  (K)                                                                                1H71 3O3  ONT3A13    1E4                  
20070808001162007080800116SW  2007       8          8          2007FA0000692    120070706G5302206020123048    RIB                                     BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              TAIL BOOM       CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW05245AR                       4398                                    DURING THE COURSE OF A SCHEDULED INSPECTION, THE RT HORIZONTAL STABILIZER WAS REMOVED TO TROUBLESHOOT A PROBLEM WITH AN AUXILIARY STROBE LIGHT THAT IS ATTACHED TO THE STABILIZER.  DURING REMOVAL, THE FLANGE ON THE IB RIB THAT ATTACHES THE STABILIZER TO THE TAILBOOM WAS FOUND CRACKED AND SEPARATED INTO 2-PIECES.  DUE TO THE LOCATION OF THE CRACK IT WAS NOT VISIBLE WITH THE STABILIZER INSTALLED.  (K)                                                                                                                                                                                                                                                                                                                               1G71 3U3  U  H2SW    E4CE                 
20070824001382007082400138EA  2007       8          24         2007FA0000693    320070621G6110                BOLT                                    PIPER PA18  PA18150     7101828SO  LYC   O360  O360*       41514EA  SNSNCHW80   W80CM8      EA  PROPELLER       LOOSE           H      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL17530AK                       184385                  AF5140          PILOT REPORTED SLIGHT VIBRATION DURING FLIGHT OF APPROX (1) HOUR.  WHEN POWER WAS REDUCED FOR LANDING, VIBRATION BECAME MORE EVIDENT.  INITIAL INSP FOUND (1) PROP BOLT HAD COME OUT FWD AND THROUGH SPINNER AND PROP WAS LOOSE.  WITH REMOVAL OF SPINNER, FOUND (2) BOLTS BACKED OUT, (1) THROUGH THE SPINNER AND (1) NEXT TO IT.  (2) BOLTS REMAINED SAFETIED, BUT NOT TIGHT.  THE REMAINING PAIR OF BOLTS, THE SAFETY WIRE WAS BROKEN BETWEEN THE BOLTS AND THE BOLTS WERE BACKED OUT APPROX (1) INCH.  AFTER COMPLETE REMOVAL OF PROP, WHICH REQUIRED CUTTING THE HEAD OFF OF (1) BOLT, THE ATTACHMENT BUSHING FOR THIS BOLT WAS BROKEN OFF FLUSH WITH THE CRANKSHAFT FLANGE.  ANOTHER ATTACHMENT BUSHING WAS ALSO BROKEN OFF, FLUSH WITH TH1H71 3O3  O  1A2     E286    5  NP27NE    
20070821001422007082100142CE  2007       8          21         2007FA0000695    120070718G5311                SPAR                                    CESSNA340   340A        2076405CE  CONT  O520  TSIO520NB   17040SO                              MLG WW          DAMAGED         G  W1NRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW1160WH                        340A0083                                WHILE INVESTIGATING A NOISE IN THE LANDING GEAR ACTUATOR GEARBOX, IT WAS DISCOVERED THA THE AN3-6A BOLTS ATTACHING THE ACTUATOR MOUNTING BRACKET, PN 50110133, TO THE FRONT CENTER SPAR WERE LOOSE.  AN ATTEMPT TO TIGHTEN THE BOLTS REVEALED THAT THE NUTPLATES INSIDE THE SPAR WERE STRIPPED.  THE NUTPLATES ARE NOT REFERENCED IN THE IPM AND APPEARS HAVE BEEN INSTALLED INSIDE THE SPAR DURING THE MFG PROCESS (INACCESSIBLE).  AS A RESULT OF THE ABOVE CONDITION, WHEN THE GEAR IS RAISED OR LOWERED, THE BRACKET AND GEARBOX PULL AWAY FROM THE FWD CENTER SPAR AND TRANSMIT ALL THE FORCES TO THE AFT ATTACHMENT BULKHEAD, FLEXING THAT BULKHEAD BY MORE THAN .1250 INCH.  NO INSTRUCTIONS FOR REPLACEMENT OF NUTPLATES IN MM.  (K)    1L72 3O3  O  3A25    E8CE                 
20070821002672007082100267EA  2007       8          21         2007FA0000697    220070711G7414M3816           CONDENSER       SLICK                   HUGHES269   269C        4470504WP  LYC   O360  HIO360D1A   41514EA                              LT MAGNETO      DISCONNECTED    B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM057508H           63008049    S1628       2594851A                    SPRING CLIP ON TERMINAL WIRE CAME OFF ALLOWING WIRE TO DISCONNECT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3O3  O  4H12    1E10                 
20070821002682007082100268SO  2007       8          21         2007FA0000698    220070730G8530TISN712ACA      CYLINDER                                BEECH 55    D55         1152730CE  CONT  O520  IO520CB     17032SO                              NR 6            CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW0569RP 744                    TE766                                   NR 6 CYLINDER WAS NEW ECI REV 3 E SERIES CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR.  THIS IS 6TH ECI REV 3 E SERIES TO CARCK IN THE SAME LOCATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  3A16    E5CE                 
20070821002692007082100269CE  2007       8          21         2007FA0000699    120070703G2910EM0159          SHUTOFF VALVE                           RAYTHN390   390         7150030CE                                                               HYD SYSTEM      JAMMED          B  E81RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL0318RF                        RB127                                   PILOT REPORTED RT ENGINE HYDRAULIC SHUTOFF VALVE WOULD NOT CLOSE FOLLOWING PREFLIGHT CHECKS.  FOUND VALVE ASSY STUCK OPEN.  REPLACED VALVE ASSY WITH NEW VALVE ASSY, OPERATIONS NORMAL.  VALVE ASSY (PN 45AS65014003) HAVE NOTICED THESE VALVE ASSY TENDING TO FAIL WITH SHORT TIE SINCE NEW IN MFG INSTALLATIONS.  VALVE ASSY SEEMS FAIRLY RELAIBLE WHEN USED IN OTHER INSTALLATIONS.  (K)                                                                                                                                                                                                                                                                                                                                                     1L72 3F    RTA00010WI                     
20070821002702007082100270CE  2007       8          21         2007FA0000700    120070711G322004425037        FORK                                    CESSNA150   152         2071835CE  LYC   O235  O235*       41505EA                              NOSE GEAR       CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO0568246                       15282208                                DURING INSPECTION, FOUND NOSE GEAR FORK CRACKED (1.5 INCH LONG) ON LT UPPER RADIUS OF FORK.  AIRCRAFT IS USED FOR TRAINING.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A19    E223                 
20070821002722007082100272EU  2007       8          21         2007FA0000701    120070709G3233                ROD                                     ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE731*     01518WP                              MLG ACTUATOR    CRACKED         B  X6URO   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      SW1540TA 11851                  194         75131                       (REF CNTRL NR WW1045)  RECOVERED AIRCRAFT FROM TAXI WAY AFTER A LANDING WITH NO MLG GREEN LIGHTS.  LT GEAR STARTED RETRACTING DURING TAXI.  FOUND LT AFT GEAR RETRACT ACTUATOR PISTON ROD BROKEN INSIDE PISTON WHICH HAD CAUSED A MIS-DIRECT OF GEAR DOWN FLOW TO ROUTE INTO RETURN AND UNLOCKING THE GEAR JURY BRACE.  THE PISTON ROD HAD BEEN CRACKED FOR A PERIOD OF TIME APPROX .3333 THROUGH PRIOR FAILURE.  (K)                                                                                                                                                                                                                                                                                                                           2M72 4F4  F  A2SW    E6WE                 
20070821001462007082100146SW  2007       8          21         2007FA0000702    120070803G3250S18233          BEARING                                 BBAVIA7     7GCB        2110130SW  LYC   O320  O320*       41508EA                              STEERING ROD    CRACKED         G      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      AL012423 3342                   7GCB55                                  NOSE LANDING GEAR STEERING ROD END BEARING (P/N S-1823-3) FAILED IN THREADED PART OF ROD, ALLOWING NOSE GEAR TO TURN SIDEWAYS, RESULTING IN EXCESSIVE SIDE LOAD ON NOSE LANDING GEAR ASSEMBLY, CAUSING IT TO FAIL AND SEPARATE FROM THE AIRCRAFT RESULTING IN MINOR DAMAGE TO COWLING, PROPELLER, EXHAUST PIPES.  THIS ROD END BEARING SHOWS SIGNS OF CORROSION, PITTING AND IS PROBABLY THE ORIGINAL 1963 PART.                                                                                                                                                                                                                                                                                                                                1H71 3O3  O  A759    E274                 
20070821001712007082100171CE  2007       8          21         2007FA0000703    120070806G3411                STATIC LINE                             LEAR  35    35A         5170602CE  GARRTTTFE731TFE731*     01518WP                              COCKPIT         MISINSTALLED    B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE09621RB                       211                                     THIS RVSM AIRCRAFT HAD AN ALTIMETRY SYSTEM SPLIT. CONTACTED STC GROUP HOLDER FOR PROPER ROUTING OF STATIC SYSTEM PLUMBING. FOUND CO-PILOTS STATIC SYSTEM INSTALLATION WAS NOT CROSS-COUPLED WITH PILOTS SYSTEM. INSTALLED FABRICATED HOSES TO THE CO-PILOTS SYSTEM TO MEET THE INTENT OF STC NR ST00563DE-D IAW MASTER DOCUMENT LIST.  CO-PILOTS STATIC SYSTEM NOT INSTALLED CORRECTLY AT STC INSTALLATION OR SYSTEMS HAVE BEEN ALTERED/MODIFIED POST-STC AND DID NOT FOLLOW APPROVED DRAWINGS.                                                                                                                                                                                                                                                 2L72 4F4  F  A10CE   E6WE                 
20070821001942007082100194NE  2007       8          21         2007FA0000704    220070809G7310                LINE                                    BOEING737   7373T0      1384582NM  GE    CFM56 CFM563B1    13802NE                              FUEL CONTROL    LEAKING         D      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  NRNOT REPORTED   1                      SO191732      320               23372                                   FLOAT STICKS, CAUSING FUEL TO COME OUT OF CARBURETOR SPLIT LINE. LEAKING FUEL FROM GASKET.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA16WE   E2GL                 
20070821001952007082100195SO  2007       8          21         2007FA0000705    120070809G2434KELLY4111810    ALTERNATOR                              PIPER PA28  PA28161     7102803SO  LYC   O320  O320*       41508EA                              ENGINE          FAILED          D      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       NRNOT REPORTED   1                      SO191732417                     287916050                               ALTERNATOR FAILED AFTER 17.6 HOURS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  O  2A13    E274                 
20070821001972007082100197SO  2007       8          21         2007FA0000706    120070809G2434KELLY4111810    ALTERNATOR                              PIPER PA28  PA28161     7102803SO  LYC   O320  O320*       41508EA                              ENGINE          FAILED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO1917324     174               287916050                               ALTERNATOR FAIL AFTER 174 HOURS OF NORMAL OPERATION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3O3  O  2A13    E274                 
20070906000302007090600030WP  2007       9          6          2007FA0000708    120070813G5250                LOCK                                    DOUG  DC8   DC8*               WP                                                               COCKPIT DOOR    MALFUNCTIONED   C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW99                                                                    NOTIFY BY AIR SECURITY REPORT THAT OUR COCKPIT LKD SYSTEM INFORMS US ONLY IF IT'S ARMED OR NOT, BUT NOT IF THE DOOR IS CORRECTLY CLOSED AND LOCKED.  DURING ONE OF THE LAST FLT'S MY COCKPIT DOOR HAS BEEN OPENED BY THE PURSER WITHOUT MY PERMISSION.  THE DOOR SEEMED CLOSED BUT IT WASNT AND HE COULD OPEN IT EASILY.  IT IS UNSAFE FOR US ON BOARD AND FOR ALL PEOPLE THAT WE FLY OVER.EUROPEAN AVIATION SAFETY AGENCYPOSTFACH 10 12 53D-50452 KOELN, GERMANYI'M  MD80 CPT OF ALITALIA , I NOTIFY BY AIR SECURITY REPORT THAT OUR COCKPIT LKD SYSTEM  INFORMS US ONLY IF IT'S ARMED OR NOT, BUT NOT IF THE DOOR IS CORRECTLY CLOSED AND LOCKED.DU                                                                                          2L74 4J    F 4A25                         
20070821002892007082100289EA  2007       8          21         2007FA0000710    220070603G732230804           FLOAT                                   AMTR  COZY  COZY        05613R8GL  LYC   O290  O290*       41506EA                              CARBURETOR      SATURATED       B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA11369CZ                                                               ENGINE FAILED ON SHORT FINAL DUE TO CARB FLOODING FLOAT IN CARB HALF FULL OF GAS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1M71 3O3  ONTEXPA1M71E229                 
20070824002472007082400247GL  2007       8          24         2007FA0000711    120070710G2497                RESISTOR                                DIAMONDA40  DA40        2990002GL  CONT  IO360 IO360*      17025CE                              ALTERNATOR      DAMAGED         D  MZERK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL15187DS169                    40574                                   MFG FABRICATED AN IN-LINE RESISTOR FROM THE ALTERNATOR TO THE VOLTAGE REGULATOR.  THE RESISTOR WAS LOCATED APPROXIMATELY 2 INCHES FROM AUX TERMINAL ON ALTERNATOR.  IT WAS STRENGTHENED WITH MULTIPLE LAYERS OF HEAT-SHRINK AND TERMINAL WAS CRIMPED ON THE SOLID WIRE LEAD OF THE RESISTOR.  THE AIRCRAFT HAD INTERMITTENT ALT FAIL WARNING BUT HAD NORMAL, POSITIVE SYSTEM CHARGING.  UPON DISCOVERY OF THE FAULT, THE RESISTOR LEAD WAS HELD IN THE TERMINAL CRIMP BY THE HEAT SHRINK BUT THE SOLID WIRE WAS BROKEN, MOMENTARILY MAKING CONTACT CAUSING THE FAULT.  THE PROBLEM WAS CORRECTED BY SOLDERING A SMALL SECTION OF WIRE TO THE RESISTOR AND INSTALLING A NEW TERMINAL TO WIRE.  MFG CUSTOMER SUPPORT WAS CONTACTED AND THEY WERE A1L71 3O3  ONTA47CE   E1CE                 
20070824002662007082400266CE  2007       8          24         2007FA0000712    120070727G2621                SQUIB                                   BEECH 300   300BEECH    1152930CE                                                               FIRE BOTTLE     GROUNDED        B  ML2RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL11350RK                       FL516                                   DURING COMPLETION OF THE INITIAL 200 HOUR PHASE 1 INSPECTION, THE RT ENGINE FIRE BOTTLE SQUIB WAS FOUND TO BE IN A GROUNDED CONDITION.  THE TERMINALS WERE WIRED TOGETHER WITH SAFETY WIRE AND A TAG THAT STATED (DISCONNECT AT INSTALLATION, THE AIRCRAFT SQUIB WIRING WAS ATTACHED OVER THE SAFETY GROUND WIRE.  THIS GROUNDED CONDITION IS TYPICALLY FOUND ON SQUIBS THAT ARE PACKAGED FROM THE VENDOR FOR SHIPPING.  DURING INSTALLATION OF THE SQUIB ONTO THE FIRE BOTTLE, THE SAFETY GROUND IS REMOVED.  IN THIS CONDITION, THE SQUIB CANNOT DETONATE TO PUT OUT AN ENGINE FIRE.  LOG BOOKS WERE NOT AVAILABLE FOR RESEARCH AT THE TIME THE DISCREPANCY WAS DISCOVERED, ALTHOUGH THE AIRCRAFT WAS NEW ENOUGH THAT IT WAS UNLIKELY ANY ENGI2L72 4T      A24CE                        
20070824002692007082400269SO  2007       8          24         2007FA0000713    220070731G8530                CYLINDER                                CESSNA310   T310Q       2074244CE  CONT  O520  TSIO520NB   17040SO                              NR 6            LEAKING         B  FTURK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NE057714Q                       310Q0214    521496                      WHILE PERFORMING OTHER MAINTENANCE A FUEL STAIN WAS NOTICED BETWEEN THE SECOND AND THIRD COOLING FIN AFT OF THE FUEL INJECTOR ON THE NR 6 CYLINDER OF THE RT ENGINE.  THIS CONDITION PROMPTED A CLOSER INSPECTION OF THE ENGINE RESULTING IN THE DISCOVERY OF SIMILAR STAINING ON THE NR 1 AND NR 5 CYLINDERS.  EACH CYLINDER WAS INDIVIDUALLY PRESSURIZED AND LEAK CHECKED WITH A SOAPY WATER SOLUTION, NR 6 CYLINDER PRODUCED LARGE BUBBLES.  THE CYLINDERS ARE ECI CASTING NR AEC65385 AND THERE WAS (A) STAMPED ON THE ROCKER BOX FLANGE WHICH REQUIRES NO FURTHER ACTION IAW AD 04-08-10.  BY THE PILOTS STATEMENT THEY BELIEVE THERE IS APPROX. 1000 HOURS ON THESE CYLINDERS.  RECOMMEND THAT A GOOD VISUAL INSPECTION BE PERFORMED AT 101L72 3O3  O  3A10    E8CE                 
20070824002982007082400298SW  2007       8          24         2007FA0000714    120070726G57115146R           SPAR                                    BBAVIA7     7FC         2110124SW  CONT  C90   C90*        17009SO                              WING            CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM049032B3177                   123                                     AIRCRAFT WAS BEING MODIFIED TO INCLUDE THE INSTALLATION OF WING SPAR INSP HOLE KITS AS SUPPLIED IAW STC NR SA00527SE.  A PORTION OF THE WING LEADING EDGE SKIN WAS REMOVED AND THE WING SPAR WAS VISUALLY INSPECTED AS SPECIFIED IN THE INSTALLATION INSTRUCTIONS SUPPLIED WITH THE STC.  DURING THIS VISUAL INSPECTION, A CRACK WAS OBSERVED ON THE TOP SURFACE OF THE RT WING FRONT SPAR.  THE CRACK WAS OBSERVED ON THE TOP SURFACE OF THE RT WING FRONT SPAR.  THE CRACK ORIGINATES AT THE IB END OF THE AFT PLYWOOD REINFORCEMENT PLATE.  REINFORCEMENT PLATE IS LOCATED ON THE AFT SIDE OF THE FRONT SPAR, UNDER THE LIFT STRUT ATTACHMENT FITTING.  THE CRACK PROGRESSES OB ALONG THE TOP SURFACE OF THE SPAR AT A SLIGHT FWD ANGLE (CRAC1H71 3O3  O  A759    E252                 
20070824003072007082400307CE  2007       8          24         2007FA0000715    120070807G29108907021         ACCUMULATOR                             BEECH 76    76          1153005CE  LYC   O360  LO360A1G6   41514EA  HARTZLHCM2Y HCM2YR      GL  HYS SYS         RUPTURED        C  XPTSA   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      SO19612651440                   ME135                                   DURING TRAINING FLIGHT IN PREP FOR COMMERCIAL/AMEL, PILOT PERFORMED INTENTIONAL SHUTDOWN OF LT ENGINE (FEATHERED).  WAS UNABLE TO RESTART WITH ACCUMULATOR AND BEGAN PROCEDURE TO RESTART WITHOUT ACCUMULATOR WHICH WAS UNSUCCESSFUL.  PILOT RETURNED TO DEPARTURE AND LANDED.  AN INVESTIGATION OF THE ACCUMULATOR REVEALED A RUPTURED DIAPHRAGM.  REPLACED LT ACCUMULATOR AND RT ACCUMULATOR WAS REPLACED AS A PRECAUTIONARY METHOD.  (K)                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A29CE   1E10    5  CP43GL    
20070824003082007082400308NE  2007       8          24         2007FA0000716    120070801G3340SB4580          LAMP                                    SKRSKYS76   S76C        8143008NE  TMECA ARRIELARRIEL2S1   60057NE                              SEARCH LIGHT    BURNED OUT      C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA25554L                        760567                                  POSSIBLE MFG PARTS NOT TO SPECIFICATIONS.  MFG OF ORIG UNKNOWN. (GENERIC) LESS THAN 7 FLT HOURS IAW LAMP (AVERAGE) FROM INSTALLATION TO REPLACEMENT.  HAVE REPLACED AT LEAST 5 LAMPS IAW AIRCRAFT IN LESS THAN 30 FLIGHT HOURS EACH.  NO CIRCUIT BREAKERS POPPING.  TROUBLESHOOTING SHOWS NO DISCREPANCIES ON EITHER AIRCRAFT.  NO MFG INFORMATION ON PARTS BOX OR ON THE PART.  (K)                                                                                                                                                                                                                                                                                                                                                            1G72 3U4  UNCH1NE    E00054EN             
20070824003092007082400309NE  2007       8          24         2007FA0000717    120070801G3340SB4580          LAMP                                    SKRSKYS76   S76C        8143008NE  TMECA ARRIELARRIEL2S1   60057NE                              LANDING LIGHT   BURNED OUT      C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA25552J                        760518                                  POSSIBLE MFG PARTS NOT TO SPECIFICATIONS.  MFG OF ORIGIN UNKNOWN. (GENERIC) LESS THAN 7 FLT HOURS PER LAMP (AVERAGE) FROM INSTALLATION TO REPLACEMENT.  HAVE REPLACED AT LEAST 5 LAMPS PER AC IN LESS THAN 30 FLIGHT HOURS EACH.  NO CIRCUIT BREAKERS POPPING.  TROUBLESHOOTING SHOWS NO DISCREPANCIES ON EITHER AC.  NO MFG INFO ON PARTS BOX OR ON THE PART COPY OF ORIGINAL CERTIFICATION ATTACHED.  (K)                                                                                                                                                                                                                                                                                                                                     1G72 3U4  UNCH1NE    E00054EN             
20070824002492007082400249    2007       8          24         2007FA0000718    220070821G732225765362        FUEL CONTROL                            CESSNA172   172S        2072439CE                                                               ENGINE          OUT OF LIMITS   B      D   RETURN TO BLOCK                                                                                 R  PARTIAL RPM/PWR LOSS                                                          TOTAKEOFF        1                      SO15471ER134  61                172S10511                               DURING PRE TAKEOFF RUN UP, THE MAG DROP (BOTH MAGS) WAS BEYOND LIMITS. THIS AIRCRAFT HAD A RECENT HISTORY OF RICH SERVO OPERATION FOLLOWED BY ADJUSTMENTS, WHICH WOULD NOT STABILIZE. THE SERVO WAS CHANGED. THIS PROBLEM IS COMMON ON MANY OF THE AIRCRAFT IN THIS FLEET AND HAS CAUSED FLEET-WIDE ADJUSTMENTS WHEN SUBSTANTIAL CHANGES IN ATMOSPHERIC TEMPERATURE OCCUR. IN MANY CASES THE SERVO MUST BE CHANGED WITH ONLY A FEW HOURS SINCE NEW.                                                                                                                                                                                                                                                                                             1H71 3O    NT3A12                         
20070824002652007082400265EA  2007       8          24         2007FA0000719    220070821G730025765362        FUEL CONTROL                            CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              ENGINE          OUT OF LIMITS   B      C   ABORTED TAKEOFF                                                                                 R  PARTIAL RPM/PWR LOSS                                                          TOTAKEOFF        1                      SO15471ER134  61                172S10511   L3340351E                   DURING PRE TAKE OFF RUN UP, THE MAG DROP (BOTH MAGS) WAS BEYOND LIMITS. THIS AIRCRAFT HAD A RECENT HISTORY OF RICH SERVO OPERATION FOLLWED BY ADJUSTMENTS, WHICH WOULD NOT STABILIZE. THE SERVO WAS CHANGED. THIS PROBEM IS COMMON ON MANY OF THE AIRCRAFT IN THIS FLEET AND HAS CAUSED FLEET-WIDE ADJUSTMENTS WHEN SUBSTANTIAL CHANGES IN ATMOSPHERIC TEMPERATURE OCCUR. IN MANY CASES THE SERVO MUST BE CHANGED WITH ONLY A FEW HOURS SINCE NEW.                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A12    1E10                 
20070824002682007082400268CE  2007       8          24         2007FA0000720    120070821G27100510105364      CONTROL CABLE                           CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              AILERONS        FRAYED          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15454ER987                    172S10256   L3283951E                   DURING A ROUTINE INSPECTION, THE AILERON BALANCE CABLE WAS FOUND BADLY WORN IN THE LT WING AT STATION 71.125. THE CABLE IS DIRECTED OVER A FAIRLEAD AT THIS LOCATION AND TYPICALLY WEARS VERY BADLY AT THIS CONTACT POINT. BECAUSE THE WEAR PATTER IS OVER A STRAIGHT RUN OF CABLE THERE IS NO BENDING OF THE CABLE WHICH WOULD CAUSE THE STRANDS TO FRAY OUTWARD. BECAUSE OF THIS, THE CABLE CAN BE WORN THROUGH MANY STRANDS AND YET APPEAR NORMAL. ONCE THE CABLE IS REMOVED FROM THE AIRCRAFT AND BENT AS SHOWN IN THE AC43.13-1B, PAGE 7-35, FIGURE 7-16, THE BROKEN STRANDS BECOME READILY APPARENT. THIS HAS BEEN AN ISSUE FOR A LONG TIME ON THIS MODEL AIRCRAFT. IF NOT INSPECTED CAREFULLY THE CABLE CAN DETERIORATE TO A DANGEROUS CO1H71 3O3  ONT3A12    1E10                 
20070824003202007082400320GL  2007       8          24         2007FA0000721    120070822G2497                CABLE                                   DIAMONDA40  DA40        2990002GL                                                               ALTERNATOR      BROKEN          G      A   UNSCHED LANDING                                                                                 H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      WP05541AJ265                    40541                                   ALTERNATOR CABLE INSTALLED AT THE FACTORY WAS TOO SHORT.  CABLE CONNECTS TO ALTERNATOR CIRCUIT BREAKER.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3O    NTA47CE                        
20070824003212007082400321SO  2007       8          24         2007FA0000722    120070812G5520                HORN            PIPER                   PIPER PA18  PA18180     7101880SO  LYC   O320  O320*       41508EA                              ELEVATOR        DAMAGED         D      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      WP234363Z     39                188682                                  AFTER DEPARTURE PILOT NOTED UNUSUAL STICK RESTRICTION AND ABORTED TOW OF GLIDER. RETURNED FOR LANDING. UPON INSPECTION THE LOWER ARM/HORN OF THE RT ELEVATOR HORN HAD BROKEN. ALL (3) OTHER ARMS WERE UNDAMAGED AND SHOWED NO SIGN OF CRACKS. BOLTS WERE INTACT AND HOLDING CONTROL CABLE.                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  O  1A2     E274                 
20070824003222007082400322SO  2007       8          24         2007FA0000723    220070823G8550S23611          CHECK VALVE                             CESSNA206   TU206C      2073334CE  CONT  O520  TSIO520C    17040SO                              ENGINE OIL      WORN            D      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      EA17719244839                   U2061226    178337R                     AFTER FLIGHT A/C SITTING ON RAMP DEVELOPED LARGE OIL LEAK FROM TURBOCHARGER.  FOUND OIL CHECK VALVE FLAPPER VALVE SEVERELY WORN.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  O  A4CE    E8CE                 
20070906000882007090600088CE  2007       9          6          2007FA0000725    120070808G2410CS3100          SENSOR                                  CESSNA172   172R        2072401CE  LYC   O360  IO360A1A    41514EA                              MASTER CNTRL BOXINTERMITTENT    B  MYNRO   OTHER                                                                                           N  FALSE WARNING                                                                 TXTAXI/GRND HDL  1                      GL119424F658                    17280390                                CURRENT SENSOR INDICATES 60A AND WHEN MASTER IS TURNED ON FUNCTIONS NORMALLY FROM TIME TO TIME, TAP ON UNIT AND IT FLUCTUATES THEN ACTS PROPERLY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3O3  ONT3A12    1E10                 
20070906000872007090600087CE  2007       9          6          2007FA0000726    120070703G3260903610373       DOWNLOCK SWITCH                         RAYTHNC90   C90GT       7150062CE                                                               MLG             FALSE INDICATIONB  E81RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL03106ML203                    LJ1757                                  PILOT REPORTED LT MAIN LANDING GEAR DOWN AND LOCKED INDICATION WITH LANDING GEAR RETRACTED.  FOUND SWITCH ASSY INDICATOR SHOWING GREEN DOWN AND LOCKED INDICATION IN GEAR RETRACTED POSITION.  REPLACED SWITCH ASSY WITH NEW UNIT.  LANDING GEAR RETRACTION/ EXTENSION SYSTEM TESTS NORMAL.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3T    RT3A20                         
20070906000732007090600073NE  2007       9          6          2007FA0000727    320070620G61116533A12         BLADE           HAMSTD                  AIRTRCAT300 AT301       0390103SW  PWA   R1340 R1340AN1    52016NE  HAMSTD22D   22D40       NE  PROPELLER       BROKEN          G      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      GL1523667           84119       3010410     20788       PP810268        (9 INCHES) OF PROP BLADE BROKE OFF IN FLIGHT.  THE SEVERE VIBRATION CAUSED PILOT TO LAND IN MUDDY FIELD.  AIRCRAFT WAS TOTALED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3R3  R  A9SW    5E2     5  CP736     
20070906000782007090600078CE  2007       9          6          2007FA0000728    120070731G2420DOFF10300B      ALTERNATOR                              CESSNA182   182R        2072731CE  CONT  O470  O470U       17026SO  MCAULY2A34C C2A34C204   GL                  SHORTED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM099628X88                     18268567    470887      851589          ALTERNATOR SHORTED, THIS UNIT IS (1) OF (3) REPLACED IN THE LAST MONTHS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  ONT3A13    E273    5  CP3EA     
20070906000702007090600070CE  2007       9          6          2007FA0000729    220070803G8520538684          BUSHING         CONT                    PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360RB   17025CE                              CONNECTING ROD  MISINSTALLED    D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NE0319WE                        3449037     819271R                     DURING THE PROCESS OF INSPECTING (6 EA) CONNECTING RODS IAW SB 07-1 AND SB 00-3, IT WAS FOUND THAT ALL WRIST PIN BUSHINGS WERE INSTALLED NOT IAW THEIR POSITIONS AS REQUIRED IN THE APPLICABLE SB AS REFERENCED.  SPLIT LINE OF BUSHING ON WRONG SIDE OF CENTERLINE.  PARTS AS RECEIVED FROM MFG.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3O3  O  A7SO    E9CE                 
20070906000362007090600036    2007       9          6          2007FA0000730    420070813G3444ADS430101AC     ANTENNA                                 PIAGIOP180  P180        6960204EU                                                               FUSELAGE        SEPARATED       B  KKQRO   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      GL11395KT3985                   1044                                    RADAR ALTIMETER REPORTED INOPERATIVE.  FOUND ANTENNA SENSOR GONE FROM THE BASE, LEAVING .2500 INCH HOLE THROUGH THE COAX CONNECTION.  THE FLAT ANTENNA MOUNTS TO A CURVED FUSELAGE WITHOUT CONTOUR ADAPTATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H72 3O    RTA59EU                        
20070906000902007090600090SW  2007       9          6          2007FA0000731    120070625G21202784187019      PIPE                                    SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE331*     01514WP                              RT WING BLEED AIARCED           G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW11160WA                       TC399                                   IB OF RT NACELLE, BLEED AIR PIPE (PN 2784187019), CHAFED OR BURNED THROUGH THE ASBESTOS SLEEVE SURROUNDING THE STARTER RELAY WIRING, WHICH THEN ARCED A HOLE IN THE BLEED PIPE, WHICH THEN BURNED THE SHIELDING FROM THE STARTER RELAY WIRES, WHICH THEN ARCED A HOLE IN A HYDRAULIC LINE (PN 2781032403), RESULTING IN A FIRE.                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4T3  TRTA8SW    E2WE                 
20070906000552007090600055CE  2007       9          6          2007FA0000732    120070517G24326041H274        RELAY                                   CESSNA310   T310R       2074246CE  CONT  O520  TSIO520*    17040SO                              BATTERY         FAILED          D  A8XRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO0516EZ                        310R1277                                AIRCRAFT EMERGENCY LANDED WITH COMPLETE ELECTRICAL FAILURE, LG EMERGENCY EXTENDED AND LANDED SAFELY.  FOUND BATTERY RELAY FAILURE.  UNIT REMOVED 200 AMP FOUND TO BE INCORRECT (PN).  SB MEB99-4 ADDRESS THIS PROBLEM, HAD NOT BEEN COMPLIED WITH, CORRECT RELAY 100 AMP PN 0850469-1 (6041H193) INSTALLED, OPS CHECK OK.  (200 AMP RELAY HAD TO HAVE BEEN REPLACED PRIOR TO 1999 WHEN AC IPC REVERSED BATTERY AND STARTER RELAY PN COMPLIANCE WITH SB WOULD HAVE PREVENTED THIS PROBLEM.  (K)                                                                                                                                                                                                                                                  1L72 3O3  O  3A10    E8CE                 
20070906000562007090600056GL  2007       9          6          2007FA0000733    320070810G6114PHCC3YF1RF      HUB             HARTZL                  CESSNA207   207         2073602CE  CONT  O550  IO550F      17042SO  HARTZLHCC3Y PHCC3YF1    GL  PROPELLER       CRACKED         B  LU4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO19                EE2379A                                             HUB, NDI SHOWS RELEVANT INDICATION OF CRACK.(K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3O3  O  A16CE   E3SO    5  CP25EA    
20070906000502007090600050CE  2007       9          6          2007FA0000735    120070809G249736153           GROUND WIRE                             BEECH 200   B200        1152922CE  PWA   PT6   PT6A6       52043EA                              GCU             BROKEN          D      BA  EMER. DESCENT           UNSCHED LANDING                                                         BGHSMOKE/FUMES/ODORS/SPARKS  MULTIPLE FAILURE          ELECT. POWER LOSS-50 PC   CRCRUISE         1                      CE071925P9715                   BB1094                                  WIRE NR P73G16N AT RT ENGINE FIREWALL GROUND POINT GS15 SEPARATED FROM THE WIRE TERMINAL DURING CRUISE FLIGHT. THIS WIRE CONNECTS GROUND TO THE GCU PIN G. THE RT GENERATOR OUTPUT SPIKED AND OPENED THE 325 AMP RT BUSS CURRENT LIMITER, THE 50 AMP RT INVERTER CURRENT LIMITER, AND DAMAGED RADIOS, THE GCU AND SYSTEMS WIRED TO THE RT BUSS. UPON INSPECTION, THE INSULATION OF P73G16N WAS FOUND STRIPPED TOO FAR FROM THE WIRE END THEREBY GIVING NO SUPPORT OF THE WIRE INTO THE TERMINAL AT THE INSULATION CRIMP AREA.                                                                                                                                                                                                                   1L72 4T3  T  A24CE   E4EA                 
20070906000532007090600053CE  2007       9          6          2007FA0000736    120070823G3246178K481         TIRE                                    LEAR  60    60LEAR      5170707CE                                                               LT MLG          DEFLATED        D      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      WP27903AM                       269                                     NOTIFIED BY FLIGHT CREW LT MAIN LANDING GEAR IB AND OB TIRES SEPARATED FROM WHEELS DURING TAXI.  TIRES DETACHED FROM WHEEL ASSEMBLIES BUT DID NOT SEPARATED FROM AIRCRAFT.  TIRES WERE NOT BLOWN.  DAMAGED TIRES AND WHEELS ASSEMBLIES WERE REMOVED.  UPON INSPECTION, NO OTHER DAMAGES NOTED ON LANDING GEAR OR SURROUNDING STRUCTURE.  NO FOD DAMAGE TO AIRCRAFT.  REPLACED WITH SERVICEABLE WHEELS/TIRES ASSEMBLIES.                                                                                                                                                                                                                                                                                                                         2L72 4F    RTA10CE                        
20070912000032007091200003NM  2007       9          12         2007FA0000741    120070828G3246AN535A          BOLT            PARKERHANFIN            COLUMBLC41  LC41550FG4005150011NM                                                               WHEEL ASSY      BROKEN          B      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              LDLANDING        1                      EA251469W143  143   MFG406      41733                                   ON LANDING PILOT FELT AND HEARD A VIBRATION AND BUMPING SOUND.  REMOVED RT LANDING GEAR FAIRING AND INSPECTED BRAKE ASSY.  ON THE WHEEL FOUND ONE WHEEL HALF ATTACH BOLT MISSING AND ONE BROKEN AND EXTENDING OUT OF THE WHEEL TO THE EXTENT OF CAUSING A GOUGE IN THE BRAKE MASTER CYLINDER AND TORQUE PLATE.  ONE BOLT OUT OF THREE WAS HOLDING THE WHEEL HALVES TOGETHER.                                                                                                                                                                                                                                                                                                                                                                    1L71 3O    NTA00003SE                     
20070906000222007090600022NE  2007       9          6          2007FA0000747    220070817G73103011849         TUBE                                    BEECH 90    F90         1152909CE  PWA   PT6   PT6A135     52043NE                              LT ENGINE       CRACKED         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA0350AW 15                     LA142       PCE92358                    FUEL LEAK NOTED ON SHUTDOWN OF LT ENGINE.  FUEL TUBE P/N 3011849 CRACKED AT CONNECTION TO START CONTROL UNIT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A31CE   E4EA                 
20070906000352007090600035EA  2007       9          6          2007FA0000748    220070718G73103011849         TUBE                                    PIPER PA31T PA31T       7103124SO  PWA   PT6   PT6A28           EA                              LT ENGINE       CRACKED         B      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA03100CM5                      31T8020073                              FUEL LEAK NOTED ON SHUTDOWN.  FUEL TUBE P/N 3011849 WAS CRACKED AT CONNECTION TO START CONTROL UNIT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3T4  T  A8EA    E4EA                 
20070906000592007090600059CE  2007       9          6          2007FA0000749    120070829G7810K99102991       EXHAUST PIPE                            CESSNA414   414         2075908CE  CONT  O520  TSIO520NB   17040SO  MCAULY3AF32C3AF32C93    GL  ENGINE          CRACKED         B  W99RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP0922MG      1900              4140533                                 DURING COMPLIANCE WITH AD 2000-01-16 THE TAIL PIPE ON THE RT ENGINE WAS FOUND WITH A 6 INCH CRACK.  THE LAST INSPECTION WAS 40 HRS PRIOR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3O3  ORTA7CE    E8CE    5  CP22EA    
20070906000122007090600012NE  2007       9          6          2007FA0000752    220070725G7200                ENGINE                                  BEECH 90    E90         1152914CE  PWA   PT6   PT6A60A     52043NE                              LEFT            FAILED          D      A   UNSCHED LANDING                                                                                 RXJPARTIAL RPM/PWR LOSS      ENGINE FLAMEOUT           WARNING INDICATION        CRCRUISE         1                      SW1371WB                        LW127                                   AIRCRAFT IN CRUISE AT 22,000 WITH ALL ENGINE INDICATIONS NORMAL.  A LOUD NOISE FOLLOWED BY POWER LOSS AND REDLINE ITT ON THE LT ENGINE.  THE CT BLADES, ITT PROBES, PT VANE AND PT BLADES ALL MELTED AND WENT THROUGH THE EXHAUST STACKS.  COMPRESSOR STATOR AND SPACER RUB.  POSSIBLE COMPRESSOR UNSTACK FAILURE.  THIS IS THE FIRST COMPLETE MELT DOWN FAILURE HAVE EVER SEEN AT ALTITUDE.  (K)                                                                                                                                                                                                                                                                                                                                               1L72 3T4  T  3A20    E4EA                 
20070906000582007090600058EU  2007       9          6          2007FA0000753    120070724G2910704A34412938    LINE                                    SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              HYD SYSTEM      LEAKING         B  PG9RO   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  LDLANDING        1                      WP19170PA                       2637                                    AC HAD HYDRAULIC LIGHT, PILOT PERFORMED A PRECAUTIONARY LANDING AT THE AIRPORT.  UPON INSP FOUND HYDRAULIC LINE FROM PUMP TO MANIFOLD LEAKING AT THE BOTTOM OF THE SWEDGE FITTING.  HYDRAULIC LINE WAS REPLACED WITH NEW LINE.  HYDRAULIC SYSTEM WAS SERVICED, GROUND RUN, AND LEAK CHECK NORMAL.  FLIGHT CONTROL CHECK NORMAL.  AC WAS RETURNED TO SERVICE.  (K)                                                                                                                                                                                                                                                                                                                                                                               1G71 3U3  U  H9EU    E19EU                
20070906000572007090600057EA  2007       9          6          2007FA0000754    120070803G2740604923063       MOTOR                                   CNDAIRCL600 CL6002B16   1900305EA  GE    CF34  CF34*            NE                              HORIZ STAB TRIM UNSERVICEABLE   C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL1343R                         5334                                    WHILE OPERATING HORIZ STAB TRIM ON CHANNEL NR 2 ONLY THE FOLLOWING OCCURS.  PUSHING BUTTON ON CONTROL WHEELS TO NOSE UP, HORIZONTAL ACTUALLY WENT DOWN THEN DISCONNECTED.  REPEATED ATTEMPTS, KEPT TRIMMING TO NOSE DOWN POSITION.  COULD NOT GET HORIZONTAL TO TRIM NOSE UP ON JUST CHANNEL NR 2.  ONCE CHANNEL NR 1 WAS ENGAGED HORIZONTAL STAB TRIM WORKED CORRECTLY.  THIS PART WAS SENT TO THE MFG BY THE PREVIOUS OPERATOR  FOR THIS EXACT PROBLEM.  MFG REPLACED PARTS AND RETURNED IT TO SERVICE.  PROBLEM REOCCURRED, UNIT REMOVED AND SENT BACK TO MFG.  (K)                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20070906000022007090600002CE  2007       9          6          2007FA0000755    120070802G801185070213        STARTER                                 CESSNA172   172S        2072439CE  LYC   O360  IO360A1A    41514EA                              ENGINE          FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA05865SP                       172S8124                                STARTER WAS INTERMITTENT AND FAILED COMPLETELY.  AVERAGE LIFE FOR THE LAST (2) STARTERS HAS BEEN 115 HRS EACH.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A12    1E10                 
20070906000762007090600076NE  2007       9          6          2007FA0000758    220070828G7314                DRIVE SHAFT     SUNDSTRANDEM            BEECH 200   B200        1152922CE  PWA   PT6   PT6A42      52043NE                              FUEL PUMP       SHEARED         D      E   ENGINE SHUTDOWN                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      SO11544P      1340  9489        BB1265      PCE94081                    WHILE AT CRUISE FLIGHT, LT ENGINE SHUTDOWN WITHOUT WARNING. LANDED WITHOUT INCIDENT. FOUND HIGH PRESSURE FUEL PUMP SHAFT SPLINES SHEARED ON INSIDE OF DRIVE COUPLING RENDERING FUEL PUMP AND FUEL CONTROL INOPERABLE. INSPECTION WOULD NOT BE POSSIBLE WITHOUT PUMP REMOVAL AND DISASSEMBLY OF DRIVE COUPLING.                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 4T4  T  A24CE   E4EA                 
20070906000382007090600038NE  2007       9          6          2007FA0000759    220070831G7220BRR40289        FAIRING         RROYCE                  GULSTMGV    GULFSTREAMGV3980116SO  RROYCEBR700 BR700710A110     NE                              LP FAN          CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL1573M  3889                   547         11204                       DURING INSPECTION OF THE AIR INTAKE ROTATING FAIRING, WE FOUND A CRACK BETWEEN THE MOUNT BOLT HOLE AND THE ADJACENT ALIGNMENT PIN HOLE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA12EA   E00057EN             
20070917000202007091700020EA  2007       9          17         2007FA0000760    220070716G8550LW13383         BAFFLE          LYC                     FOUND FBA   FBA2C1      3640103EA  LYC   O540  IO540L1A5   41532EA                              OIL SUMP        CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03796  600                    50          L2947748A                   ENGINE OIL SUMP BAFFLE CONTACTED BOTTOM OF OIL SUMP CRACKING BAFFLE SUPPORT ATTACH POINTS AND SHEARING RIVETS ATTACHING BAFFLE CENTER REINFORCEMENT.  SHEARED RIVET LODGED IN OIL PRESSURE RELIEF VALVE CAUSING LOSS OF OIL PRESSURE.  ENGINE REMOVED FOR OVERHAUL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  ONCA7EA    1E4                  
20070917000242007091700024EA  2007       9          17         2007FA0000761    220070716G8550LW13383         BAFFLE                                  FOUND FBA   FBA2C1      3640103EA  LYC   O540  IO540L1A5   41532EA                              OIL SUMP        CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03794  500                    51          L29544548A                  ENGINE OIL SUMP BAFFLE CONTACTED BOTTOM OF OIL SUMP CRACKING BAFFLE SUPPORT ATTACH POINTS AND SHEARING RIVETS ATTACHING BAFFLE CENTER REINFORCEMENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONCA7EA    1E4                  
20070917000252007091700025GL  2007       9          17         2007FA0000768    120070804G2810                CAP                                     AMTR  SKRAIDSKYRAIDER   05610GIGL  ROTAX 447   ROTAX447    55555EU                              FUEL TANK       OUT OF ADJUST   G      A   UNSCHED LANDING                                                                                 WJ INADEQUATE Q C            WARNING INDICATION                                  DEDESCENT        1                      GL253171135                     SK1966                                  AT CONCLUSION OF 2 HOUR FLIGHT, APPROXIMATELY 2 MILES FROM DESTINATION AIRPORT, PILOT REPORTED AN UNCOMMANDED SIGNIFICANT POWER REDUCTION.  A PRECAUTIONARY LANDING WAS EXECUTED ON A COUNTY ROAD.  SUBSEQUENT INVESTIGATION FOUND 1.5 GALLON FUEL IN RT TANK, NONE IN LT TANK.  EVIDENCE OF FUEL SIPHONING FROM RT FUEL CAP.  PILOT STATED WHEN LT FUEL CAP WAS REMOVED, HISSING NOISE WAS HEARD.  PROBABLE THAT COMBINATION OF SIPHONING RT TANK/CAP AND NO VENTING OF LT TANK/CAP CAUSED A FUEL IMBALANCE AND INTERRUPTION OF FUEL FLOW TO HEADER TANK/ENGINE, RESULTING REDUCTION OF ENGINE OPERATION.  RECOMMEND ANY EXPERIMENTAL AIRCRAFT USING FUEL CAPS WITH THREADED CENTER STEM/(O) RING ASSEMBLY FOR VENTING BE MODIFIED TO INCLUDE A1H71   3  I  EXPA1H71EXPE3I               
20070917000702007091700070SW  2007       9          17         2007FA0000769    120070905G5711                SPAR                                    BBAVIA7     7GCBA       21101PHSW  LYC   O320  O320*       41508EA                              RT WING         FRACTURED       D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA239902Y1480 9                 7GCBA8                                  RT WING MAIN SPAR FOUND FRACTURED IB OF STRUT ATTACH. CURRENT AD INADEQUATE TO PREVENT FURTHER FAILURES. THIS AIRCRAFT HAS LESS THAN 14 HR SINCE LAST ANNUAL INSPECTION..                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  O  A759    E274                 
20070917000082007091700008SW  2007       9          17         2007FA0000770    120070905G5711                SPAR                                    BBAVIA7     7GCBA       21101PHSW                                                               RT WING         BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA239902Y1480 9                 7GCBA8                                  RT WING MAIN SPAR FOUND FRACTURED IB OF STRUT ATTACH. CURRENT AD INADEQUATE TO PREVENT FURTHER FAILURES. THIS AIRCRAFT HAS LESS THAN 14 HR SINCE LAST ANNUAL INSPECTION..                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O      A759                         
20070917000592007091700059CE  2007       9          17         2007FA0000772    120070401G3210NAS464P426      BOLT                                    CESSNA320   320E        2074514CE  CONT  O520  TSIO520B    17040SO  MCAULY3AF32C3AF32C*     GL  RT MLG          SHEARED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP173424Q                       320E0024                                AIRCRAFT HAS EXPERIENCED A RT LANDING GEAR FAILURE UPON LANDING.  PRIOR TO THIS INCIDENT, THE LANDING GEAR HAD BEEN CHECKED DURING THE AIRCRAFT ANNUAL INSPECTION AND FOUND TO BE OUT OF RIG IAW SERVICE MANUAL D508-3-13 STANDARDS. THE AIRCRAFT EXPERIENCED A PARTIAL POWER FAILURE UPON THE FIRST FLIGHT AFTER THE AIRCRAFT HAD BEEN RIGGED.  SUSPECT THE LANDING GEAR WAS NOT LOCKED PROPERLY UPON LANDING ON THE FIRST FLIGHT DUE TO THE PARTIAL ELECTRICAL POWER FAILURE.  UPON THE THIRD FLIGHT LANDING, THE RT GEAR COLLAPSED.  PROBABLE CAUSE MAY HAVE BEEN FROM THE FIRST LANDING WHERE GEAR MAY NOT HAVE BEEN ALL THE WAY DOWN.  THE BOLT TO THE LANDING GEAR STRUT SHEERED AT THE ATTACH POINT OF THE STRUT, AND ONE ATTACH POINT BR1L72 3O3  O  3A25    E8CE    5  CP22EA    
20070917000232007091700023CE  2007       9          17         2007FA0000778    120070906G28203011849         LINE                                    BEECH 90    F90         1152909CE  PWA   PT6   PT6A135     52043NE                              FUEL SYS        CRACKED         B      A   UNSCHED LANDING                                                                                 KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            TXTAXI/GRND HDL  1                      EA0350AW 6848                   LA142       PCE92358                    FUEL TUBE CRACKED AT BACKSIDE OF B-NUT SLEEVE LOCATION, CAUSING FUEL TO LEAK UNDER PRESSURE INTO ENGINE NACELLE AREA FORWARD OF FIREWALL.  TUBE FAILED IN FLIGHT CAUSING INITIAL CHANGES IN FUEL FLOW INDICATIONS TO BE NOTICED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 4T4  T  A31CE   E4EA                 
20070917000032007091700003CE  2007       9          17         2007FA0000780    120070812G2910AE1011889G0116  LINE                                    CESSNA750   750         2076810CE  ALLSN AE300 AE3007A          GL                              HYDRAULIC SYS   RUPTURED        B  CNQ3O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      GL13912QS7516                   7500012                                 THE NOSE WHEEL STEERING CENTERING FLEXIBLE HYDRAULIC HOSE RUPTURED WHERE THE HOSE BODY IS SWEDGED TO A 45 DEGREE FITTING WHICH ATTACHES TO A BULKHEAD FITTING IN THE NOSE WHEEL WELL.  THIS CONDITION ALLOWED THE LOSS OF HYDRAULIC FLUID IN THE (A SYSTEM).  AIRCRAFT LANDED WITHOUT INCIDENT.  THIS HOSE IS CURRENTLY CONSTRUCTED OF KEVLAR AND IS BEING REPLACED WITH STAINLESS STEEL BRAIDED VERSION ALONG WITH OTHER HOSES WHICH ATTACH TO THE NOSE GEAR.  (K)                                                                                                                                                                                                                                                                             2L72 4J4  FRTT00007WITE6CH                
20070917000692007091700069SO  2007       9          17         2007FA0000781    220070810G8520                CRANKSHAFT                                                                 CONT  O520  GTSIO520L   17032SO                              ENGINE          FAILED          B  LU4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO19                                        A511M2                      CRANKSHAFT FAILED NDI SB MSB96-10.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                3  O          E7CE                 
20070917000192007091700019GL  2007       9          17         2007FA0000782    320070810G6114                HUB             HARTZL                  CESSNA207   207         2073602CE  CONT  O550  IO550F      17042SO  HARTZLHCC3Y PHCC3YF1    GL  PROPELLER       CRACKED         B  LU4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO19                EE2379A                             EE2379A         HUB, NDI SHOWS RELEVENT INDICATION OF CRACK. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  O  A16CE   E3SO    5  CP25EA    
20070917000722007091700072SO  2007       9          17         2007FA0000783    120070816G273062701153        CONTROL CABLE                           PIPER PA44  PA44180     7104402SO  LYC   O360  O360*       41514EA                              ELEVATOR        BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO0530521                       447995076                               AFT LOWER ELEVATOR CONTROL CABLE BROKE AT TURN BUCKLE BETWEEN CRIMPED BARREL AND END THREADS.  SENT CABLE ASSY TO NTSB FOR LAB REPORT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A19S0   E286                 
20070917000262007091700026EA  2007       9          17         2007FA0000784    220070708G732230804           FLOAT           PRECISION               AMTR  VANS  RV9A        05614C3GL  LYC   O320  O320D2A     41508EA  SNSNCH70C   70CM6       EA  CARBURETOR      FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO0312HE 33         75992004    91367       L2005739A   38893K          THE ENGINE DIED ON FINAL TO AIRPORT, PUMPED THE THROTTLE, AND THE ENGINE STARTED RUNNING AGAIN, RETARDED THROTTLE, AND THE ENGINE DIED AGAIN.  LANDED WITHOUT INCIDENT.  COULD NOT GET THE ENGINE TO RESTART ON THE GROUND.  ENGINE WAS STARTED THE NEXT DAY, THE FUEL FLOW WAS SHOWING 11 TO 12 GPH AT IDLE.  REMOVED THE CARBURETOR AND ONE PONTOON OF THE PLASTIC FLOAT WAS 90 PERCENT FULL OF FUEL.  (K)                                                                                                                                                                                                                                                                                                                                    1L71 3O3  ONTEXPA1L71E274    5  NP28NE    
20070917000342007091700034CE  2007       9          17         2007FA0000785    120070807G261261423473275     SENSOR                                  BEECH 200   A200        1152921CE  PWA   PT6   PT6A41      52043EA  MCAULY4HFR344HFR34C752  NE  FIRE DETECTION  FAULTY          E      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA05636B 754                    BC61                                    AT APPROXIMATELY 1635 LOCAL, IN CLOUDY CONDITIONS, ON A MAINTENANCE TEST FLIGHT, THE NR 1 ENGINE FIRE LIGHT BRIEFLY ILLUMINATED, THEN EXTINGUISHED.  ALL ENGINE GAUGES INDICATED NORMALLY.  ALREADY IN DESCENT, THROUGH 4,500 FT, AND CONTINUED TO A SAFE LANDING.  MAINTENANCE DISCOVERED FAULTY LOWER AFT SENSOR AND REPLACED IT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA    6  C3PNE     
20070917000102007091700010GL  2007       9          17         2007FA0000786    120070516G7160D4F732612001    AIR BOX                                 DIAMONDA40  DA40        2990002GL  LYC   O360  O360A4M     41514EA                              ENGINE          BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07425FP357                    40FC025                                 CARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  ONTA47CE   E286                 
20070917000672007091700067GL  2007       9          17         2007FA0000787    120070521G7160D4F732612001    AIR BOX                                 DIAMONDA40  DA40        2990002GL  LYC   O360  O360A4M     41514EA                              ENGINE          BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07422FP383                    40FC022                                 CARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE WHILE IN FLIGHT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  ONTA47CE   E286                 
20070917000322007091700032NE  2007       9          17         2007FA0000788    220070810G73208168776007      EEC                                     UROCOPEC135 EC135P1     8680990EU  PWA   PW206 PW206B      0    NE                              ENGINE          FAILED          B  HDNRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW03911KB                       0013        BB0027                      EEC CAUSED ENGINE TO DROP FROM FULL POWER TO IDLE IN CRUISE FLIGHT WITH AN ENGINE FAILURE AND ENGINE MANUAL HORN AND LIGHT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G72 3U3  UO H88EU   E42NE                
20070917000062007091700006SO  2007       9          17         2007FA0000789    220070809G8520530196A1        CRANKSHAFT                                                                 CONT  C85   C8512       17008SO                              ENGINE          DESTROYED       G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL13                                        21407612                    DURING LEVEL FLIGHT THIS AIRCRAFT SUSTAINED LOSS OF PROPELLER.  AIRCRAFT LANDED ON A COUNTY HIGHWAY SATISFACTORILY WITH NO DAMAGE OR INJURIES.  INVESTIGATION REVEALED THE ENGINE CRANKSHAFT FAILED IMMEDIATELY AFT OF THE PROPELLER ATTACH POINT (THIS CRANKSHAFT HAS A TAPERED SHAFT, NOT A FLANGE).  THE PROPELLER WAS LOCATED AT A LATER TIME BY A HIKER IN A STATE PARK.  INSPECTION OF THE ENGINE AND PROPELLER INDICATES THE PROBABILITY THAT THE ENGINE HAD SUSTAINED SUDDEN STOPPAGE AT A PRIOR TIME.  THIS MAY HAVE RESULTED IN A MINUTE CRACK/FRACTURE THAT EVENTUALLY PROPAGATED INTO THE TOTAL FAILURE OF THIS CRANKSHAFT.  SINCE THERE WAS NO DAMAGE TO THE AIRCRAFT OR OCCUPANTS, THIS SITUATION HAD BEEN DETERMINED TO BE AN INC       3  O          E233                 
20070917000132007091700013SW  2007       9          17         2007FA0000790    120070901G36102784187015      PIPE                                    SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE331*     01514WP                              BLEED AIR       DAMAGED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW11226AM                       TC229                                   NOTE: AIRCRAFT HAS BEEN PARKED FOR 2 YEARS AFTER BEING DAMAGED IN HURRICANE.  AIRCRAFT WAS BEING DISASSEMBLED FOR SALVAGE.  IB OF RT NACELLE, BLEED AIR PIPE, PN: 27-84187-015, HAS CHAFED/BURNED THROUGH THE ASBESTOS SLEEVE SURROUNDING THE STARTER RELAY WIRING AND HAS ARCED A HOLE IN THE BLEED PIPE, WHICH THEN ALLOWED BLEED AIR TO MELT THE SHIELDING FROM ONE OF THE WIRES.  (K)                                                                                                                                                                                                                                                                                                                                                       2L72 4T3  TRTA8SW    E2WE                 
20070917000332007091700033WP  2007       9          17         2007FA0000794    120070901G5730                SKIN                                    DOUG  DC9   DC915       3022036WP  PWA   JT8   JT8D7       52053NE                              WING            DAMAGED         D      C   ABORTED TAKEOFF                                                                                 O  OTHER                                                                         TOTAKEOFF        1                      SO17305PA                       45740                                   BIRD STRIKE ON LT LEADING EDGE, CAUSING DEEP DENT AMD A TEAR 5 INCHES VERTICAL AND 4 INCHES HORIZONTAL, FOUND ON POST FLIGHT INSPECTION. REPAIRED IAW SRM CHAPTER 57-06.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  F  A6WE    E2EA                 
20070917000362007091700036CE  2007       9          17         2007FA0000797    120070809G2810FC100           FUEL CAP                                CESSNA182   182P        2075816CE  CONT  O470  O470*       17026SO                              FUEL CELL       VENTING         G      B   EMER. DESCENT                                                                                   YJ ENGINE STOPPAGE           WARNING INDICATION                                  DEDESCENT        1                      GL155877640   40                18262288                                FUEL CAPS WERE INSTALLED ON AIRCRAFT IAW STC SA2376CE AND HAD BEEN IN SERVICE FOR ABOUT 40 HOURS IN A 4 MONTH PERIOD. THEY BEGAN VENTING FUEL FROM BOTH TANKS RESULTING IN A FORCED EMERGENCY LANDING DUE TO FUEL STARVATION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONTTA13    E273                 
20070918001022007091800102EA  2007       9          18         2007FA0000798    220070603G732230804           FLOAT                                   AMTR  COZY  COZYIII     05605BKGL  LYC   O290  O290        41506EA                              CARBURETOR      SATURATED       B  JULRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW01369CZ40                     1517                                    ENGINE FAILED ON SHORT.  FINAL DUE TO CARB: FLOODING FLOAT IN CARB, HALF FULL OF GAS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1M71 3O3  ORTEXPA1M71E229                 
20070917000072007091700007SO  2007       9          17         2007FA0000799    120070905G7820                MUFFLER                                 PIPER PA18  PA18150     7101828SO  LYC   O320  O320*       41508EA                              EXHAUST         BROKEN          G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL157066B36                     185140                                  ENGINE EXHAUST TAIL PIPE FAILED AT THE MUFFLER WELD.  WITH 36 HOURS TOTAL TIME SINCE NEW.  LEADING EDGE EXHAUST SYSTEM WAS INSTALLED BY STC SA02200AK.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3O3  O  1A2     E274                 
20070917000272007091700027EU  2007       9          17         2007FA0000800    120070809G3233485034          ACTUATOR                                BRAERODH125 BAE125800A  1500285EU  GARRTTTFE731TFE7315BR        WP                              RT MLG          UNSERVICEABLE   D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP01919SS                       NA0473                                  RT MLG ACTUATOR CRACKED ATTACH HOUSING DISCOVERED DURING WHEEL WELL INSPECTION, PART WAS NOT LEAKING BUT COULD SEPARATE AT ANY MOMENT AND CAUSE SEVERE DAMAGE TO AIRCRAFT DATE OF ASSY OF ACTUATOR 1/92.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA3EU    E6WE                 
20070917000182007091700018EU  2007       9          17         2007FA0000801    120070809G534325FC5801A       SUPPORT                                 BRAERODH125 BAE125800A  1500285EU  GARRTTTFE731TFE7315BR        WP                              LT MLG          CORRODED        D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP01919SS5860                   NA0473                                  LT MLG DOOR IB AFT SUPPORT REMOVED FOR OTHER MAINTENANCE AND SEVERE INTERGRANULAR CORRODION DISCOVERED FROM LAVATORY LEAKAGE AS INDICATED BY STAINING ON PART LOCATION WHERE BONDING STRAP ATTACHES.  CORROSION SEVERE AND IS ENOUGH TO CAUSE PART TO FAIL.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA3EU    E6WE                 
20070917000742007091700074    2007       9          17         2007FA0000802    120070910G32456006            TUBE                                                                                                                                    TIRE            DEFECTIVE       D      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      NE03                                                                    6.00 X 6 TIRE TUBES WILL NOT FIT IN 6.00 X 6 WHEEL. STEM APPEARS TO NOT BE IN CENTER AND SIZE OF TUBE IS SMALLER THAN NORMAL.  (2) TUBES FOUND TO BE IN THIS CONDITION.  WHEN WE ATTEMPTED TO RETURN THE TUBES TO OUR VENDOR, WOULD NOT ACCEPT A RETURN AND THAT THE TUBES WERE NOT DEFECTIVE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            
20070917000402007091700040NM  2007       9          17         2007FA0000805    120070911G291082970009325     LINE                                    DHAV  DHC8  DHC8106     2809020NM  PWA   PW121 PW121       52124NE                              HYDRAULIC SYS   LEAKING         H      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      SW99387BC                       351                                     PILOT NOTED LOSE HYDRAULIC LINE. DECLARED EMERGENCY AND LANDED. NO NOSE WHEEL STEERING ON GROUND.  INSPECTED ALL HYDRAULIC LINES AND FITTINGS. NOTED EDP LINE GOING TO PRESSURE MANIFOLD B NUT WAS ABLE TO GET HALF A TURN. SYSTEM SERVICED AND FUNCTIONAL CHECKED SERVICEABLE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA13NM   E20NE                
20070917000632007091700063    2007       9          17         2007FA0000809    120070912G322013022101        TAIL WHEEL                                                                                                                                              WORN            G      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW17912S                                                                TAILWHEEL SPRING P/N 13022.101 SHOWED EVIDENCE OF LOOSENESS AND ELONGATION OF THE FORWARD ATTACH POINT HOLE.  THE ATTACH BOLT P/N AN5-22A EXHIBITED SIGNS OF FRETTING WEAR CONTRIBUTING TO THE TAILWHEEL LOOSENESS.  IT WOULD APPEAR THAT THIS CONDITION COULD INDUCE A SIGNIFICANT SIDE LOAD ON THE TAILWHEEL SPRING AFT ATTACHMENT CLAMP AND HARDWARE.  THIS CONDITION WOULD BE DIFFICULT TO DETECT WITH THE WEIGHT OF THE AIRCRAFT ON THE TAILWHEEL.  IT IS RECOMMENDED THAT THE CONDITION INSPECTION INCLUDE SUPPORTING THE FUSELAGE FORWARD OF THE TAILWHEEL SPRING FORWARD ATTACHMENT POINT AND CHECKING THE TAILWHEEL ASSEMBLY FOR SECURITY AND TIGHTNESS.                                                                                                                         
20070925001842007092500184CE  2007       9          25         2007FA0000810    120070731G3222                STRUT                                   CESSNA182   182T        2072703CE  LYC   O540  IO540*      41532EA                              NLG             LEAKING         B  AQHRO   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      WP115348E                       18281212                                FOUND NOSE STRUT ASSEMBLY LEAKING.  REMOVED STRUT ASSEMBLY FROM AIRCRAFT.  ASSEMBLED WITH PN TCNS-1 SEAL KIT IWA SRM AND MM.  RELEASED TO AC OWNER.  OWNER FOUND FLUID NR 4 ON WHEEL FAIRING AFTER TAXI TO HANGAR.  INSPECTION FOUND FLUID COMING FROM BEHIND NOSE GEAR STEERING ASSEMBLY.  CONTACTED TECH SERVICE, RECOMMENDED THA WE REPLACE THE STRUT TUBE (PN 07430901).  REMOVED LEAKING STRUT TUBE FROM AIRCRAFT.  INSTALLED NEW 07430901 TUB USED NEW SEAL KIT TCNC-1 AND SERVICED.  INSPECTED OLD TUBE FOR DAMAGE.  FOUND THA THE TUBE WAS LEAKING BETWEEN THE INNER TUBE AND THE OUTER-MACHINED PART.  FOUND PINHOLE IN BRAZING OF THE PARTS.  (K)                                                                                     1H71 3O3  ONT3A13    1E4                  
20070925001812007092500181NM  2007       9          25         2007FA0000811    120070906G2410B1731           BELT                                    ROBSINR22   R22BETA     7640110NM  LYC   O360  O360C1F     41514EA                              ALTERNATOR      BROKEN          D      HA  DEACTIVATE SYST/CIRCUITSUNSCHED LANDING                                                         D  INFLIGHT SEPARATION                                                           CRCRUISE         1                      WP238372G852                    2782                                    ALTERNATOR LIGHT CAME ON DURING CRUISE FLIGHT.  FOLLOWED HELICOPTER FLIGHT MANUAL PROCEDURES AND RETURNED TO LANDING.  UPON INSPECTION IT WAS DISCOVERED THAT THE ALTERNATOR BELT HAD BROKEN AND DEPARTED THE AIRCRAFT IN FLIGHT.  NO OTHER DAMAGE RESULTED                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3O3  O  H10WE   E286                 
20070925002492007092500249SW  2007       9          25         2007FA0000812    120070919G632020401077503     QUILL ASSY                              BELL  204   UH1H        1181407SW  LYC   T53   T53*        41549NE                                              WORN            B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP173053Q     82                661104                                  QUILL INTERNAL SPLINES WORN AND DAMAGED IN QUILL TUBE CONTACT AREA                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1G71 4U4  U  EXPA1G71E1EA                 
20070925000892007092500089SO  2007       9          25         2007FA0000813    120070920G57127847504         RIB                                     PIPER PA28  PA28R200    7102811SO  LYC   O360  IO360A1A    41514EA                              WING            CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO132702R6441                   28R35252                                CRACKS FOUND DURING INSPECTION.  CRACKS FOUND IN LOWER RELIEF EDGE MADE USE OF REPAIR KIT P/N: 767 - 397 NOT POSSIBLE. THE CRACK REQUIRED REPLACEMENT OF ENTIRE RIB ASSY WITH NEW PART 78475-004 (AN IMPROVED PART). HAVE DIGITAL PHOTOS OF THE CRACKED RIB, THE CRACKS ARE CAUSED BY FLEXING OF THE SPAR BY THE LANDING GEAR SIDE BRACE DUE TO SIDE LOADS DURING LANDING. IF NO REPLACED I DON'T SEE AN INFLIGHT FAILURE, BUT COULD SEE POSSIBILITY OF LANDING GEAR COLLAPSE.                                                                                                                                                                                                                                                                  1L71 3O3  O  2A13    1E10                 
20070925001102007092500110SO  2007       9          25         2007FA0000815    120070920G57127847504         RIB                                     PIPER PA28  PA28R200    7102811SO  LYC   O360  IO360A1A    41514EA                              WING            CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO132702R6441                   28R35252                                CRACKS FOUND DURING INSPECTION, CRACKS FOUND IN LOWER RELIEF EDGE MADE USE OF REPAIR KIT P/N: 767 - 397 NOT POSSIBLE. THE CRACK REQUIRED REPLACEMENT OF ENTIRE RIB ASSY. WITH NEW MFG PART 78475-004 (AN IMPROVED PART).  HAVE DIGITAL PHOTOS OF THE CRACKED RIB, THE CRACKS ARE CAUSED BY FLEXING OF THE SPAR BY THE LANDING GEAR SIDE BRACE DUE TO SIDE LOADS DURING LANDING. IF NO REPLACED I DON'T SEE AN INFLIGHT FAILURE, BUT COULD SEE POSSIBILITY OF LANDING GEAR COLLAPSE.                                                                                                                                                                                                                                                             1L71 3O3  O  2A13    1E10                 
20070925001422007092500142SO  2007       9          25         2007FA0000816    120070917G381091000106        SOCKET                                  GULSTMGV    GULFSTREAMGV3980116SO  RROYCEBR700 BR700710A110     NE                                              BURNED          B      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      LDLANDING        1                      GL1523M  3606                   579                                     THE SOCKET ON ONE OF THE (2) LAMPS BURNED CAUSING AN ELECTRICAL ODOR IN THE BAG BIN WHERE THE STERILIZER IS LOCATED.  THE 2 AMP CIRCUIT BREAKER WHICH CONTROLS THE POWER TO THE STERILIZER DID NOT POP.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA12EA   E00057EN             
20070925001452007092500145CE  2007       9          25         2007FA0000817    120070917G2434DOFF10300B      ALTERNATOR                              CESSNA210   T210M       2073451CE  CONT  O520  TSIO520*    17040SO                                              FAILED          D      D   RETURN TO BLOCK                                                                                 H  ELECT. POWER LOSS-50 PC                                                       TXTAXI/GRND HDL  1                      SW15732YK     458               21061879                                OVERHAULED DOFF10300B ALTERNATOR FAILED AFTER 458 HOURS IN 35 MONTHS OF USE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  O  3A21    E8CE                 
20070925001632007092500163SO  2007       9          25         2007FA0000818    220070919G8530639614639615    ROCKER                                  CESSNA172   172H        2072424CE  CONT  O300  O300D       17022SO                              VALVE ROCKER    MISINSTALLED    D      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      EA254960R     287               17256296    025668R                     ROCKER COVERS REMOVED DURING 100 HOUR INSPECTION TO INSPECT INTAKE AND EXHAUST ROCKERS FOR CORRECT INSTALLATION. FOUND NR1 AND NR6 CYLINDERS HAD INTAKE ROCKER (P/N 639614) INSTALLED IN THE EXHAUST VALVE POSITION. PARTS MANUAL CALLS FOR P/N 639615 ROCKER TO BE INSTALLED IN EXHAUST VALVE POSITION. THIS IS THE SECOND ENGINE DISCOVERED WITH THE SAME ABNORMALITY AFTER RECENT OVERHAULS FROM SAME OVERHAUL FACILITY.                                                                                                                                                                                                                                                                                                                     1H71 3O3  ONT3A12    E253                 
20070925001702007092500170EA  2007       9          25         2007FA0000819    220070924G7414LW14227         BEARING         LYC                     PIPER PA28  PA28180     7102808SO  LYC   O360  O360A4A     41514EA                              MAGNETO         DESTROYED       D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL195147L857  857               284432      L3421136A                   BEARING LW14227 CAGE DESTROYED AND APPROXIMATELY 50 PERCENT MISSING.  THIS IS THE ENGINE SIDE BEARING OF THE LW15416 MAGNETO DRIVE ADAPTER (MAGNETO ISOLATION DRIVE FOR RT MAGNETO)ENGINE HAS 857 HOURS SINCE FACTORY OVERHAUL IN 2000.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3O3  O  2A13    E286                 
20070925001712007092500171EA  2007       9          25         2007FA0000820    220070924G8540LW14227         BEARING                                 PIPER PA28  PA28180     7102808SO  LYC   O360  O360A4A     41514EA                              ENGINE          DESTROYED       D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL195147L857  857               284432      L3421136A                   BEARING LW14227 CAGE DESTROYED AND APPROXIMATELY 50 PERCENT MISSING.  THIS IS THE ENGINE SIDE BEARING OF THE LW15416 MAGNETO DRIVE ADAPTER (MAGNETO ISOLATION DRIVE FOR RIGHT HAND MAGNETO).  ENGINE HAS 857 HOURS SINCE FACTORY OVERHAUL IN 2000.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  2A13    E286                 
20070925002502007092500250CE  2007       9          25         2007FA0000822    120070904G3210AN39227         PIN                                     BEECH 36    A36         1151604CE  CONT  O550  IO550*           SO                              MLG             SHEARED         G      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         LDLANDING        1                      GL13998PL848  100               E3036                                   THE LOWER IB BUSHING ON THE LOWER TORQUE LINK KNEE WAS DRY AND THE PIVOT PIN WHICH RIDES IN THE BUSHING WAS VERY TIGHT POSSIBLY DUE TO A PLUGGED GREASE ZERK FITTING. THIS APPARENTLY CAUSED THE CLEVIS RETAINING PIN TO SHEAR (AS EVIDENCED BY THE SHEAR MARKS ON THE REMAINING PORTION OF THE PIN), THE PIVOT PIN TO FALL OUT AND THE GEAR TO EXTEND TO THE POINT WHERE IT WAS ONLY BEING HELD BY THE BRAKE LINE. ONCE THE AIRCRAFT TOUCHED DOWN THE UNRESTRAINED WHEEL ASSEMBLY TURNED AND WAS TORN FROM THE REST OF THE GEAR.                                                                                                                                                                                                               1L71 3O3  O  3A15    E3SO                 
20071002000502007100200050EA  2007       10         2          2007FA0000823    220070824G7414M3548           ROTOR                                   CESSNA172   172N        2072434CE  LYC   O360  O360A4M     41514EA                              SHAFT           FAILED          C  E92RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL09733XN367        05120929    17268632                                PILOT DEPARTED ON A VFR, DAY FLIGHT.  DURING THE CLIMB FROM DEPARTURE, THE PILOT NOTICED A SLIGHT ENGINE ROUGHNESS THAT LASTED ONLY A SECOND.  THE ENGINE SMOOTHED OUT UNTIL THE AC WAS LEVELED OUT AT CRUISE ALTITUDE AND CRUISE POWER SETTINGS THE ENGINE BEGAN RUNNING ROUGH.  THE PILOT PERFORMED A MAGNETO CHECK IN FLIGHT FINDING THE RT MAGNETO INOPERATIVE.  THE PILOT SWITCHED TO LT MAGNETO AND RETURNED TO LAND AT DEPARTURE WITHOUT INCIDENT.  UPON OPENING THE MAGNETO, THE ROTO GEAR PN M3827 AND THE GEAR IN THE DISTRIBUTOR BLOCK ASSY PN K3822 WERE NOT DAMAGED AND WERE FREE OF OBSTRUCTION AND MOVED WITHOUT BINDING.  THE SHAFT BROKE JUST BELOW THE SLOT IN THE SHAFT THAT HOLDS THE CAM WHICH OPENS THE CONTACTS.  THERE D1H71 3O3  ONT3A12    E286                 
20071002000522007100200052CE  2007       10         2          2007FA0000824    120070826G534305430161        FITTING                                 CESSNA172   172P        2072436CE  LYC   O320  O320*       41508EA                              NLG             CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL259787311305                  17276236                                AC WAS BEING TAXIED FROM THE RAMP TO THE TAXIWAY, AND DURING TAXI, THE PILOTS REPORTED THAT THE NOSE GEAR STEERING SEEMED TO BE MALFUNCTIONING.  UPON INSPECTION, THE NOSE GEAR STRUT APPEARED TO BE PRESSED UP AGAINST THE REAR HALF OF THE LOWER COWLING.  THE LOWER NOSE GEAR FITTING (PN 0543016-1) WAS INSPECTED AND FOUND TO BE CRACKED COMPLETELY OFF ON THE RT SIDE.  THE LT SIDE OF THE NOSE GEAR FITTING WAS STILL INTACT.  THE CAP PN 05430181 WHICH CLAPS THE NOSE GEAR STRUT TO THE LOWER NOSE GEAR FITTING WAS FOUND TO BE MISSING FROM THE AIRCRAFT.  THE HARDWARE WHICH ATTACHED THE LT SIDE OF THE CAP TO THE LOWER NOSE GEAR FITTING WAS FOUND TO BE MISSING ALONG WITH THE CAP.  (K)                                         1H71 3O3  ONT3A12    E274                 
20071002000582007100200058SO  2007       10         2          2007FA0000825    220070821G731464936849A1      PUMP                                    DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  FUEL SYSTEM     FAILED          C  B4VSO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP07708DC                       C0408       650211      AG9712          THE MIXTURE CONTROL SHAFT ON THE ENGINE DRIVEN FUEL PUMP FROZE UP AT HALF TRAVEL BETWEEN FULL RICH AND IDLE CUT OFF.  THIS CREATED A LEAN MIXTURE CONTROL WAS DISCONNECTED FROM THE FUEL PUMP, THEN THE FUEL PUMP CONTROL SHAFT HAD TO BE FREED UP.  THE MIXTURE CABLE WAS COMPLETELY FREE WITH NO BINDING ONCE DISCONNECTED FRO THE FUEL PUMP.  THE FUEL PUMP WAS REPLACED AND SENT BACK TO MFG.  (K)                                                                                                                                                                                                                                                                                                                                          1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20071002000862007100200086CE  2007       10         2          2007FA0000826    120070808G2731NAS302261510    CONTROL CABLE                           BEECH 300   300BEECH    1152930CE                                                               ELEVATOR TRIM   FRAYED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NE05122RG389                    FL448                                   DURING SCHEDULED INSPECTION OF THE AC, THE MECHANIC FOUND THE LT ELEVATOR PITCH TRIM CONTROL CABLE CHAFING ON THE ELEVATOR CABLE PASS THROUGH HOLE LOCATED IN SKIN PN 101-620000-3.  THE ELEVATOR CABLE PASS THROUGH HOLE REQUIRED TRIMMING TO ALLOW PROPER CLEARANCE.  ADJUSTMENTS TO PASS THROUGH HOLE ACCOMPLISHED IAW IAW MFG.  (K)                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4T      A24CE                        
20071002000872007100200087CE  2007       10         2          2007FA0000827    120070814G75004536102150V431  MANIFOLD                                LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE731*     01518WP                              LT ENGINE       DAMAGED         B  KKQRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL11858MK2402                   141                                     LT PYLON OVERHEAT INDICATION OCCURRED IN FLIGHT.  FOUND HIGH PRESSURE BLEED AIR MANIFOLD MATING FLANGE DEFORMED.  REPLACED ASSY 4536102150V43-1 WITH NAV ASSY 45361020228-001.  CAUSE MAY BE AGE OR REPEATED CLAMPING.  ORIGINAL PART HAS BEEN SUPERSEDED BY THE MFG.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTT00008WIE6WE                 
20071003000042007100300004SO  2007       10         3          2007FA0000828    220070906G8530SA52000A20P     CYLINDER                                CESSNA206   U206G       2073356CE  CONT  O520  IO520F      17032SO                              NR 2            CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL034891Z1790                   U20606044   818885R                     CYLINDER HEAD HAS A CRACK.  BEGINNING AT INTAKE PORT AND EXTENDING TO UPPER SPARK PLUG HOLE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  O  A4CE    E5CE                 
20071002000902007100200090WP  2007       10         2          2007FA0000829    120070831G6720369D21800501    CONTROL SYSTEM                          HUGHES369   369D        4470706WP                                                               T/R PITCH       ROUGH           B  EOORO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL03C6DCM     1181                                                      DURING 100 HR INSPECTION, PLAY WAS NOTICED BETWEEN THE ROTATING AND NOT-ROTATING SWASH PLATES OF THE TAIL ROTOR PITCH CONTROL AFTER REMOVAL, IT WAS NOTED THAT THE BEARING WAS DRY AND ROUGH.  RECORDS INDICATE IT WAS REGREASED IN DEC OF 2006.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3U      H3WE                         
20071003000062007100300006CE  2007       10         3          2007FA0000830    120070912G5755                COVER                                   BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              SPOILER MIXER   CORRODED        B  KX5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL15156DH                       RK36                                    WHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND SPOILER MIXER ASSEMBLY BOX COVER NOT SEALED.  REMOVED COVER AND FOUND CORROSION ON ACTUATOR AND MIXER ASSEMBLY.  RECOMMEND THAT THE SPOILER MIXER AREA BE INSPECTED THOROUGHLY THE BOX COVER REMOVED.  INSTALLED THE BOX COVER WITH THE APPROPRIATE SEALANT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4F4  FRTA16SW   E25EA                
20071003000072007100300007CE  2007       10         3          2007FA0000831    120070912G212045A63517073     AIR DUCT                                BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              BLEED AIR       CRACKED         B  KX5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL15156DH                       RK36                                    WHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND THE LEFT AFT FUSELAGE BLEED AIR LINE BELLOWS BLOWN APART PN 45A63517-073 AND THE RT AFT FUSELAGE BLEED AIR LINE BELLOWS BRAIDING FRAYING PN 45A63517-075.  WHEN THE LT BLEED AIR LINE BLEW APART IT CRACKED A FUSELAGE BULKHEAD AT UPPER FRAME STATION 329.92 AND BP 29.92L.  WOULD RECOMMEND THAT DETAILED INSPECTIONS OF THESE BLEED AIR LINES BE PERFORMED AT SCHEDULED INTERVALS AND THE UPPER FRAME STATION IN THE AREA AROUND THE BLEED AIR LINES BE CAREFULLY INSPECTED FOR DAMAGE.  IT IS SUSPECTED THAT BOTH THE BLEED AIR LINES FAILED DUE TO FATIGUE OR TIME IN SERVICE.  (K)                                                                                                      2H72 4F4  FRTA16SW   E25EA                
20071003000082007100300008CE  2007       10         3          2007FA0000832    120070912G561045AS3101012     WINDOW                                  BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              COPILOT         CRACKED         B  KX5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL15141DR                       RK184                                   WHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND COPILOT COCKPIT SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD.  THE D-INSPECTION REQUIRES THAT BOTH WINDSHIELDS BE INSPECTED BY REMOVING THE WINDSHIELD RETAINERS OR USING OPTICAL PRISM INSPECTION METHOD.  THERE IS NO STATEMENT IN THE AC MM OR IN THE A-D INSPECTION CHECKLIST THAT REQURIES YOU TO INSPECT THE COCKPIT SIDE WINDOWS IN THE SAME MANNER AS THE WINDSHIELDS.  ALL OF THE WINDOWS IN THE COCKPIT AREA ARE INSTALLED OR FASTENED IN THE SAME MANNER AS THE WINDSHIELDS.  IT IS SUSPECTED THAT THE COPILOT SIDE WINDOW CRACKED FROM FATIGUE, OR TOTAL TIME INSTALLED.  THE WINDOW WAS MFG MAY OF 1997.  WOULD RECOMMEND THAT INSPECTION OF ALL COCKPIT WINDOWS WITH A 2H72 4F4  FRTA16SW   E25EA                
20071003000102007100300010CE  2007       10         3          2007FA0000833    120070912G5510                STRUCTURE                               BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              HORIZONTAL STAB DAMAGED         B  KX5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL15141DR                       RK184                                   WHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND 6 SHEARED RIVETS AND 2 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A21183-11 ON THE BOTTOM OF THE HORIZONTAL STABILIZER.  IT IS SUSPECTED THAT THE MISSING RIVETS FAILED FROM FATIGUE.  RECOMMEND INSPECTING AREA THOROUGHLY AT EACH INSPECTION, CONTACTING MFG FOR REPAIR OPTIONS.  THIS IS SECOND AC THAT THE SAME DISCREPANCY HAS BEEN FOUND.  (K)                                                                                                                                                                                                                                                                                                         2H72 4F4  FRTA16SW   E25EA                
20071003000112007100300011CE  2007       10         3          2007FA0000834    120070912G5510                STRUCTURE                               BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              HORIZONTAL STAB DAMAGED         B  KX5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL15156DH                       RK36                                    WHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND 8 SHEARED RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A21183-11 ON THE BOTTOM OF THE HORIZONTAL STABILIZER.  IT IS SUSPECTED THAT THE MISSING RIVETS FAILED FROM FATIGUE.  RECOMMEND INSPECTING AREA THOROUGHLY AT EACH INSPECTION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4F4  FRTA16SW   E25EA                
20071003000122007100300012CE  2007       10         3          2007FA0000835    120070802G27603321209         ADJUSTER        LEAR                    LEAR  25    25D         5170514CE                                                               BRAKE VALVE     DAMAGED         B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE09                9711105                                             UPON VISUAL INSPECTION OF THE POWER BRAKE VALVE PN 60810741-804, SN 9711105, IT WAS FOUND THAT THE ADJUSTMENT SCREW HAD BEEN GROUND DOWN AND MODIFIED.  AS WE BEGAN TO LOOK THROUGH SB 23/24/25-32-12 AND FOUND THAT  THIS UNIT PN WAS NOT IN THIS SB.  WE THEN FOUND THAT THIS UNIT WAS FOR A LEAR 60.  WE THEN LOOKED INTO THE MFG PARTS BREAKDOWN AND FOUND THAT THE LEVER AS WELL AS THE MODIFIED ADJUSTMENT SCREW, THE STOP SCREW AND PIN DID NOT BELONG ON THIS PN OF POWER BRAKE VALVE.  THISE PARTS ARE FOR A PN 2380002 OR PN 2381443 OR PN 3321200-3 POWER BRAKE VALVE.  WE CONTACTED OUR CUSTOMER AND FOUND THAT THIS UNIT WAS REMOVED FROM LEAR 25D.                                                                                2L72 4J      A10CE                        
20071003000132007100300013CE  2007       10         3          2007FA0000836    120070806G3411                STATIC SYSTEM                           LEAR  35    35A         5170602CE  GARRTTTFE731TFE731*     01518WP                                              MISINSTALLED    B      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      CE09621RB                       211                                     THIS RVSM AIRCRAFT HAD AN ALTIMETRY SYSTEM SPLIT.  CONTACTED STC GROUP HOLDER FOR PROPER ROUTING OF STATIC SYSTEM PLUMBING.  FOUND CO-PILOTS SYSTEM WAS NOT CROSS COUPLED WITH PILOTS SYSTEM.  INSTALLED FABRICATED HOSES TO THE CO-PILOTS SYSTEM TO MEET STC NR ST 00563DE-D.  PROBABLE CAUSE: CO-PILOTS STATIC SYS NOT CROSS-COUPLED AT STC INSTALLATION OR SYSTEM WAS MODIFIED/ ALTERED POST-STC WITHOUT APPROVED DATA.  (K)                                                                                                                                                                                                                                                                                                                 2L72 4F4  F  A10CE   E6WE                 
20071003000142007100300014NE  2007       10         3          2007FA0000837    220070822G7230                BLADE                                   BOEING737   737800*            NM  CFMINTCFM56 CFM567B26US      NE                              HPC             DAMAGED         B  QEMYO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA35EIDCN           XAEF2436                892123                      ENGINE SURGED ON WING AND WAS INDUCTED INTO SHOP FOR I/V.  DURING STRIP IT WAS NOTED THAT 1 OFF HPC STAGE 3 BLADE HAD BEEN LIBERATED TOGETHER WITH A SECTION OF THE DOVETAIL FROM THE STG 3 DISK.  SECONDARY DAMAGE WAS ALSO NOTED ON THE HPC ROTOR AND STATORS.  INSPECTION OF THE FRONT STATOR CASES REVEALED THAT A VSV STAGE 3 LEVER ARM WAS MISSING AND APPEARED NOT TO HAVE INSTALLED.  NB ESN 892123 INPUTTED AS 1ST SV SINCE NEW.  (K)                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA16WE   E00055EN             
20071003000152007100300015GL  2007       10         3          2007FA0000838    220070815G72306898607         BEARING                                 SCWZER269   269D        8059501EA  ALLSN 250C  250C20      03013GL                              NR 1            FAILED          C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW03411HV                       0040A       CAE845096                   PILOT REPORTED CHIP LIGHT CAME ON DURING TRAINING FLIGHT.  LANDED AS SOON AS POSSIBLE AND PROBE REMOVED AND CLEANED.  GROUND RUN MADE IAW MM AND CHIP PULLED AND INSPECTED.  MORE METAL FOUND SO ENGINE REMOVED FROM AC AND INSPECTED.  FOUND NR 1 BEARING OF COMPRESSOR ASSY FAILING.  NO EVIDENCE OF OVERHEATING OR OIL STARVATION.  PILOT REPORTED NO LOSS OF OIL PRESSURE DURING FLIGHT.  (K)                                                                                                                                                                                                                                                                                                                                               1G71 3U3  U0 4H12    E4CE                 
20071003000182007100300018SO  2007       10         3          2007FA0000840    220070818G73221048931         CARBURETOR                              CESSNA182   182G        2072716CE  CONT  O470  O470R       17026SO                              ENGINE          FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP192347R                       18255447    1316145R                    PILOT REPORTED THAT AFTER A NORMAL START, HE WAS UNABLE TO ADVANCE THE THROTTLE CONTROL TO CRUISE OR TAKEOFF POWER.  A PARTIAL DISASSEMBLY OF THE CARBURETOR REVEALED THAT THE AIR METERING PIN/AIR METERING JET WAS BLOCKING THE THROTTLE SHAFT TRAVEL.  THE CARBURETOR WAS SENT FOR REPAIR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A13    E273                 
20071003000192007100300019EA  2007       10         3          2007FA0000841    220070818G8530AEL65102        CYLINDER                                CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA                              NR 4            FAILED          D      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      GL139815L                       17276618                                DURING CRUISE FLIGHT, THE PILOT REPORTED A LOUD BANG FOLLOWED BY EXCESSIVE VIBRATION, INCREASED POWER TO FULL TO MAINTAIN ALTITUDE AND MADE A WELL-EXECUTED,, PRECAUTIONARY LANDING.  AFTER SHUTDOWN THERE WAS A LARGE OIL PUDDLE DEVELOPING UNDER THE AIRCRAFT.  AIRPLANE COWL REMOVED AND NR 4 CYLINDER WAS FOUND TO HAVE THE TOP HALF SEPARATED FROM THE BOTTOM.  THIS CYLINDER REPORTED TO BE IN SERVICE LESS THAN A YEAR.  THE CYLINDER HAS THE CASTING NR AEL85099 WHICH IS NOT SUBJECT TO AD2006-12-07 OR SB NR 05-8.  ENGINE HAS (3) OTHER CYLINDERS WITH THE SAME CASTING NUMBER INSTALLED.  IT IS ESTIMATED THAT ENGINE LOST 2.5 QUARTS OF OIL DURING THE FEW MINUTES BETWEEN THE SEPARATION AND THE SHUTDOWN.  MECHANIC SUGGEST FAA L1H71 3O3  ONT3A12    E274                 
20071003000202007100300020SO  2007       10         3          2007FA0000842    220070907G8530654375          ROCKER SHAFT                                                               CONT  O200  O200*       17020SO                              CYLINDER        LOOSE           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO03977CC                                   256314                      IAW OWNERS REQUEST, REMOVED ALL (4) ROCKER COVERS TO INSPECT THE ROCKER SHAFT AND SET SCREWS.  AFTER REMOVING THE ROCKER COVERS. FOUND ALL(4) SET SCREWS LOOSE AND ALL (4) SHAFTS MOVED TOWARD THE INTAKE SIDE OF THE BOSSES.  NONE HAVE CUT THE ROCKER COVERS YET, IN ANOTHER 20 HOURS OR SO THEY WOULD.  NOTE: THE NEW ENGINE HAVE A FLAT CUT INTO THE ROCKER SHAFT, AND A SET SCREW IN THE CENTER BOSS, TO RETAIN THE SHAFT.  ALSO, THE SHAFT IS SHARP ON THE END, UNLIKE THE OLD STYLE, AND HAVE A CUT MARK ACROSS THE END OF THE SHAFT FOR USE IN ALINING THE FLAT FOR THE SET SCREW.  THE SET SCREW IS A MS51963-64, AND USES NO LOCKTITE, OR MECHANICAL TYPE LOCK.  THE FLAT IN THE ROCKER SHAFT IS NOT DEEP ENOUGH TO PROVIDE ADEQUATE L       3  O          E252                 
20071003000222007100300022GL  2007       10         3          2007FA0000844    120070813G2731700232          CABLE                                   WACO  YMF   YMFF5C      9600425GL  JACOBSR755  R7557       35003EA  HAMSTD2B    2B20        NE  PITCH SERVO     INOPERATIVE     C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL09919TT                       F5C111      22353       31606           THE PITCH SERVO BRIDLE CABLE WAS FOUND TO BE LOOSE AND NOT CONNECTED TO THE CAPSTAN.  IT WAS WOUND BETWEEN THE BOTTOM END OF THE CAPSTAN AND THE CAPSTAN END PLATE WITH THE CLAMP TO THE ELEVATOR CABLE HAVING BEEN SLIDING ON THE ELEVATOR CABLE.  THE ELEVATOR WAS FOUND TO BE FREE TO MOVE NORMALLY IT IS NOT KNOWN HOW THIS MALFUNCTION OCCURRED.  IT IS POSSIBLE THAT THE BRIDLE CABLE CLAMP WAS NOT SUFFICIENTLY TIGHT ALLOWING THE BRIDLE CABLE TO BECOME SLACK AND COMING LOOSE IN THE CAPSTAN.  (K)                                                                                                                                                                                                                                    1Q71 3R3  R  ATC542  5E11    5  CP255     
20071003000232007100300023SO  2007       10         3          2007FA0000845    220070817G74146314            MAGNETO                                 CIRRUSSR    SR20        05628AJGL  CONT  O360  IO360ES          SO                              ENGINE          ARCED           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO05814RA444                    1663        FP4677                      DURING ANNUAL INSPECTIO, 500 HR MAG INSP COMPLIED WITH EARLY DUE TO NR OF HOURS PREVIOUSLY FLOWN.  BOTH MAGNETOS SHOWED SAME INTERNAL ARCING, SO SEVERE, THAT BRUSH HOLDER PN K3823 WAS MELTED/ BURNED UP, CONTACTED SLICK TECH SUPPORT 904-739-4360, OUR MAG S/N`S WERE MATCHED TO PROBLEM MAGS WHICH SLICK WAS AWARE OF CARBON USED IN MFG OF BRUSHES TOO SOFT, CARBON DUST CAUSED ARCING.  IT IS A WONDER THIS CUSTOMERS ENGINE CONTINUED TO RUN.  (K)                                                                                                                                                                                                                                                                                       1L71 3O3  ONTA00009CHE1CE                 
20071003000262007100300026CE  2007       10         3          2007FA0000846    120070913G552005341221        HORN                                    CESSNA172   172S        2072439CE  LYC   O360  IO360A1A    41514EA                              ELEVATOR        LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NE05672EB1827                   172S8672                                ELEVATOR HORN BEARING LOOSE IN BORE OF HORN, PN 0534122-1, BEARING ITSELF IS NOT WORN OUT BUT THERE IS PLAY BETWEEN THE TWO PARTS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A12    1E10                 
20071003000172007100300017GL  2007       10         3          2007FA0000849    120070926G535018583002        FAIRING                                 CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO                              RT WING ROOT    SEPARATED       D      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           NRNOT REPORTED   1                      EA21631SR200  200               2442                                    LOWER SECTION OF RT WING ROOT FAIRING SEPARATED FROM AIRCRAFT IN FLIGHT.  FAIRING IS RETAINED WITH JUST A FEW SCREWS AND AN AREA OF THE LOWER PORTION OF FAIRING IS RETAINED WITH DOUBLE SIDED TAPE AND AN AREA OF DOUBLE SIDED TAPE CAME DEBONDED AND AIR GOT UNDER IT AND IT RIPED OFF.                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  ONTA00009CHE3SO                 
20071003000252007100300025CE  2007       10         3          2007FA0000850    120070927G781002R3022406      EXHAUST DUCT                            BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA                              RT ENGINE       CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW99     12033280                           PCE85195                    WHILE PERFORMING SCHEDULED MAINTENANCE, REMOVED RT EXHAUST STACKS TO FACILITATE INSPECTING THE EXHAUST DUCT.  FOUND A 1 INCH CRACK IN THE SKI SLOPE.  SB 3380 WAS COMPLIED WITH 711 HOURS EARLIER.  POWER SECTION WAS PULLED AND SENT OFF FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 4T4  T  A24CE   E4EA                 
20071011002082007101100208CE  2007       10         11         2007FA0000851    120071001G3250S11073          ROD END                                 CESSNA182   182A        2072704CE  CONT  O470  O470*       17026SO                              MLG             BROKEN          G      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      SO152145G                       51445                                   ROD END AT STEERING COLLAR SHEARED CAUSING LOSS OF DIRECTIONAL CONTROL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  ONT3A13    E273                 
20071011002112007101100211NE  2007       10         11         2007FA0000852    320070924G6114MS24665134      COTTER PIN                              RKWELLOV10  OV10A       6402512GL                                   HAMSTD33LF  33LF        NE  PROP SPINNER    MISSING         G      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      SO15614V                        33813                                   SPINNER WAS LOST FROM RT ENGINE WHILE IN A RT TURN AT 7000 FT DAMAGING ONE PROPELLER BLADE. SPINNER NOT RECOVERED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H72 4T    RTEXPX1H72        5  CP20EA    
20071011002202007101100220CE  2007       10         11         2007FA0000853    120070920G7810310103901       FLANGE                                  BEECH 90    E90         1152914CE  PWA   PT6   PT6A135     52043NE                              EXHAUST         CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL1590XS                        LW342                                   (2) NEW ENGINES WERE INSTALLED IAW MFG MODIFICATIONS, WITH 938.0 HRS SINCE NEW.  AIRCRAFT WAS IN FOR A PHASE INSPECTION AND FOUND 3 OUT OF L1 EXHAUST FLANGES ON THE ENGINE CRACKED.  ACCORDING TO THE MFG PARTS MANUAL, EXHAUST STIFFENERS ARE NOT USED ON THIS SN AC AND ARE NOT USED WITH MFG INSTALLATION INSTRUCTIONS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3T4  T  3A20    E4EA                 
20071015002272007101500227CE  2007       10         15         2007FA0000854    120070809G781040B22318        EXHAUST STACK                           CESSNA206   T206H       2073303CE  LYC   O540  TIO540AJ1A       EA  MCAULY3D36C B3D36C432   GL  ENGINE          LOOSE           B  Z08RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE07168JS98                     T20608735   L1266161E                   DURING AN INSPECTION, FOUND THE EXHAUST STACK AT NR 2 CYLINDER, PULLED DOWN .0625 INCH APPROX.  FURTHER INVESTIGATION FOUND THE NR1, NR3, NR5 AND NR 6 ENGINE CYLINDERS EXHAUST STACKS PULLED DOWN, BUT NOT AS MUCH.  AFTER RECOMMENDATIONS FROM ENGINE MFG ALSO, THE SUPPLIER EXHAUST SYSTEM (WHICH IS ONE IN THE SAME).  DURING THE ENGINE CYLINDER REMOVAL PROCESS FOUND LOWER FWD, .7500 INCH STUD NUT UNDER TORQUED.  FURTHER INVESTIGATION REVEALED THE FORWARD 2 STUDS BOTH BELOW, MFG RECOMMENDED DRIVING TORQUE OF CYLINDER HOLDDOWN STUDS IN CASE.  INSTALLED NEW OVERSIZE (.003) STUDS IAW ENG MFG RECOMMENDATIONS.  INSTALLED NEW NR 2 ENGINE CYLINDER AND NEW EXHAUST CROSSOVER PIPE AS REQUIRED.  TIGHTENING THE EXHAUST FLANGE NU1H71 3O3  ORTA4CE    E14EA   5  CP58GL    
20071015002292007101500229GL  2007       10         15         2007FA0000855    220070906G732023072790        FADEC                                   BELL  407   407         1182206SW  ALLSN 250C  250C47B          GL                                              FAILED          B  VK1RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW19509PD350                    53703       CAE847760                   AIRCRAFT WAS STARTED IN A NORMAL MANNER.  JUST PRIOR TO LIFT OFF THE (FADEC FAIL), (AUTO RELIGHT) WARNING LIGHTS ILLUMINATED AND THE FADEC FAIL HORN SOUNDED.  NO LIMITATIONS WERE RECORDED OR OBSERVED.  THE FADEC CONTROL ASSY WAS RETURNED TO MFG FOR ANALYSIS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  UO H2SW    E1GL                 
20071015002332007101500233    2007       10         15         2007FA0000856    420070911G3457066011480102    RECEIVER                                CESSNA208   208B        2073701CE  PWA   PT6   PT6*        52043EA                              GPS             SMOKE           D      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      GL2524MG      1664              208B0850                                SHORTLY AFTER TAKEOFF FROM ISP THE PILOT NOTICED SMOKE IN THE COCKPIT.  THE PILOT IMMEDIATELY RETURNED TO DEPARTURE AND LANDED.  THE PILOT REPORTED THAT THE SMOKE APPEARED TO BE CAUSED BY AN ELECTRICAL PROBLEM.  THE PILOT REPORTED THAT THE GPS NO LONGER OPERATED.  ON 9/12/2007, MECHANIC INSPECTED THE AIRCRAFT, REMOVED THE GPS AND FOUND THAT IT SMELLED OF ELECTRICAL SMOKE, THE MECHANIC EXAMINED THE RADIO RACK, WIRING HARNESSES AND ENTIRE INSTRUMENT PANEL AREA AND FOUND NO PROBLEM.  THE ENGINE COMPARTMENT AND ELECTRICAL EQUIPMENT BOX WERE INSPECTED WITH NO PROBLEMS FOUND.  THE AIRCRAFT WAS GROUND RUN AND ALL ELECTRICAL EQUIPMENT WAS OPERATIONAL TESTED WITH THE GPS UNIT REMOVED AND ALL OPERATED NORMALLY.  THE GPS 1H71 3T3  T  A37CE   E2NE                 
20071023000582007102300058CE  2007       10         23         2007FA0000858    120070427G57111369            SPAR                                    BBAVIA11    11CC        9140404CE  CONT  C85   C85*        17008SO                              RT WNG          DETERIORATED    D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM054546E                       11CC249                                 REPORT IAW AD 200-25-02R1 PARAGRAPH D (4) LOOSE, MISSING AND RUSTED NAILS IN RIBS ALLOWING RUSTY MOISTURE INTO SPAR, FRETTING ON TOP CAP GREATER THAN .0625 INCH ON LOOSE RIBS, CRACKS AT AILERON BELLCRANK BRACKET, CAUSED FROM OVER TORQUING OF BOLTS, PREVIOUS WING TIP DAMAGE, LOGS MISSING HISTORY, SPARS REPLACED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  O  A796    E233                 
20071016000012007101600001SW  2007       10         16         2007FA0000859    120070726G57115146R           SPAR                                    BBAVIA7     7FC         2110124SW  CONT  C90   C90*        17009SO                              RT WING         CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM069032B3177                   7FC123                                  AC WAS BEING MODIFIED TO INCLUDE THE INSTALLATION OF WING SPAR INSPECTION HOLE KIT IAW STC NR SA005278E.  A PORTION OF THE WING LEADING EDGE SKIN WAS REMOVED AND THE WING SPAR WAS VISUALLY INSPECTED AS SPECIFIED IN THE INSTALLATION INSTRUCTIONS SUPPLIED WITH THE STC.  DURING THIS VISUAL INSPECTION, A CRACK WAS OBSERVED ON THE TOP SURFACE OF THE RT WING FRONT SPAR.  THE CRACK ORIGINATES AT THE IB AND OF THE AFT PLYWOOD REINFORCEMENT PLATE.  REINFORCEMENT PLATE IS LOCATED ON THE AFT SIDE OF THE FRONT SPAR, UNDER THE LT STRUT ATTACHMENT FITTING.  THE CRACK PROGRESSES OB ALONG THE TOP SURFACE OF THE SPAR AT A SLIGHT FORWARD ANGLE (CRACK ANGLE TOWARD THE FORWARD PLYWOOD REINFORCEMENT PLATE).  THE SURFACE OF THE CRAC1H71 3O3  O  A759    E252                 
20071016000022007101600002SO  2007       10         16         2007FA0000860    120070815G3297                CONNECTOR                               GULSTMGV    GULFSTREAMGV3980116SO  RROYCEBR700 BR700710A110     NE                              NLG STEERING    CORRODED        D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA11509QS6740                   637                                     EXCESSIVE CORROSION AT CONNECTOR PINS CAUSING NWS FAIL MSG.  SUGGEST PERIODIC INSPECTION AND CLEANING OR IMPROVED CONNECTOR SEALING FROM MOISTURE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA12EA   E00057EN             
20071016000032007101600003GL  2007       10         16         2007FA0000861    120070820G781015070001        EXHAUST HEADER                          CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO                              NR 5            CRACKED         D  UV4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO15516CR306                    1309                                    NR 5 EXHAUST HEADER HAS CRACKED OFF AT FLANGE, JUNE 6/06 AT 440.6, NOV 18/06 AT 636.1 HOBBS, MAY 18/07 AT 746.7 HOBBS AND AGAIN AUG 20/07 HOBBS NOT AVAILABLE.  AFTER INSPECTING HEADER IT WOULD SEEM THAT A HEAVER GAUGE PIPE WOULD RESOLVE THE PROBLEM.  THE LAST HEADER WAS INSTALLED WITH BACK UP FLANGES WELDED TO PIPE AT FLANGE SECTION WITH NO EFFECT.  (K)                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  ONTA00009CHE3SO                 
20071016000042007101600004GL  2007       10         16         2007FA0000862    220070815G7230672332390       RETAINING RING  RROYCE                                                     ALLSN 250C  250C20B     03013GL                              COMPRESSOR      FRACTURED       C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO05     2                                  CAC37235                    OPERATOR REPORTED ENGINE CHIP LIGHTS AND A PRECAUTIONARY LANDING WAS MADE.  INSPECTION OF ENGINE CHIP DETECTORS REVEALED ONE SMALL PIECE OF THE FAILED RETAINING RING HAD CAUSED THE LIGHT.  THE COMPRESSOR WAS REMOVED FROM THE ENGINE AND FURTHER INVESTIGATION REVEALED THE RETAINING RING HAD FRACTURED INTO 5 PIECES.  3 PIECES WERE CONTAINED IN THE RETAINING RING GROOVE OF THE IMPELLER, 1 PIECE WAS IN THE GEARBOX SUMP AREA AND THE 5TH PIECE WAS RECOVERED FROM THE CHIP DETECTOR.  THE FAILED RETAINING RING SCORED THE SPUR ADAPTER GEAR ADJACENT TO THE RETAINING RING GROOVE IN THE IMPELLER.  NO FURTHER DAMAGE WAS NOTED.  A NEW SPUR ADAPTER GEAR AND RETAINING RING WERE INSTALLED AND THE COMPRESSOR RETURNED TO SERVICE.         3  U          E4CE                 
20071016000092007101600009GL  2007       10         16         2007FA0000863    120070814G272030730501        RUDDER PEDAL                            AVIAT A1    A1B         2210406GL  LYC   O360  O360*       41514EA                              COCKPIT         FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL03304C                        2113                                    RUDDER PEDAL OPERATION CAN LEAD TO NO BRAKE OPERATION AT FULL TRAVEL OF RUDDER.  SENDING IN THIS FIELD APPROVAL REQUEST FOR A VERNIER MIXTURE CONTROL. BELIEVE THAT THE LT RUDDER PEDAL WHEN PRESSED FULLY ALLOWS YOU TO DEPRESS THE RT BRAKE OVER CENTER THUS GIVING YOU NO BRAKE AND DILEMMA WHEN APPLYING THE BRAKE.  THE SAME THING HAPPENS IN REVERSE WHEN THE RT PEDAL IS DEPRESSED FULLY AND THEN THE LT BRAKE WILL GO OVER CENTER AND BECOME USELESS.  THIS AC, AS AN EXAMPLE WAS GROUND LOOPED AT 68 HRS TT.   IF THIS CONDITION CAN BE ACHIEVED EASILY ON THE GROUND THEN IT COULD HAPPEN ON LANDING, IN A CROSSWIND OR TURN.  FURTHER MORE THE BRAKE PEDAL IN THE OVER CENTER CONDITION WILL BE POINTED FORWARD AND AT A 90 DEGREE AN1H71 3O3  ONCA22NM   E286                 
20080114001992008011400199EU  2008       1          14         2007FA0000864    220070809G853002722001002R1   CYLINDER HEAD                           DIAMONDA42  DA42        2990004EU  THIELTTAE125TAE12501    59300EU                              ENGINE          FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW99240TS                       42072                                   ENGINE BEGAN LOSING COOLANT BY PRESSURIZING THE COOLING SYSTEM WITH COMBUSTION PRESSURE AND BLOWING COOLANT OVERBOARD.  WHEN CYLINDER HEAD WAS REMOVED, EACH CYLINDER HAD A CRACK BETWEEN THE GLOW PLUG AND EXHAUST VALVE RECESS.  THE ENGINE HAD PASSED A COMPRESSION CHECK AND IT IS SUSPECTED THAT THE CRACKS WOULD ONLY LEAK WHEN THE ENGINE WAS WARMED TO OPERATING TEMPERATURE.  THE RESULTANT COOLANT LOSS ONLY INCREASES THE PROBABILITY OF FURTHER TEMPERATURE EXCURSIONS.  A PROBABLE CAUSE WOULD BE INADEQUATE DISTANCE IN THE CASTING OF THE CYLINDER HEAD BETWEEN THE EXHAUST VALVE RECESS AND THE GLOW PLUG.  ALTERNATE CAUSES INCLUDE INADEQUATE COOLING PROVIDED BY THE AIRFRAME MFG, INADEQUATE WATER JACKETING IN THE ENGINE R1L72 3I3  BRTA57CE   E00069EN             
20080114002002008011400200EU  2008       1          14         2007FA0000865    220070809G853002722001002R1   CYLINDER HEAD                           DIAMONDA42  DA42        2990004EU  THIELTTAE125TAE12501    59300EU                              ENGINE          FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM11350TS                       42061                                   ENGINE BEGAN LOSING COOLANT BY PRESSURIZING THE COOLING SYSTEM WITH COMBUSTION PRESSURE AND BLOWING COOLANT OVERBOARD.  WHEN CYLINDER HEAD WAS REMOVED, EACH CYLINDER HAD A CRACK BETWEEN THE GLOW PLUG AND EXHAUST VALVE RECESS.  THE ENGINE HAD PASSED A COMPRESSION CHECK AND IT IS SUSPECTED THAT THE CRACKS WOULD ONLY LEAK WHEN THE ENGINE WAS WARMED TO OPERATING TEMPERATURE.  THE RESULTANT COOLANT LOSS ONLY INCREASE THE PROBABILITY OF FURTHER TEMPERATURE EXCURSIONS.  A PROBABLE CAUSE INCLUDE INADEQUATE COOLING PROVIDED BY THE AIRFRAME MFG, INADEQUATE WATER JACKETING IN THE ENGINE RESULTING IN HOT SPOTS WHICH COULD LEAD TO CRACKING, AND ENGINE RUNNING AT A HIGHER RPM THAN THE COOLING SYSTEM COULD HANDLE.            1L72 3I3  BRTA57CE   E00069EN             
20071016000102007101600010CE  2007       10         16         2007FA0000866    120070907G2497691835432       BUSS BAR                                CESSNA680   680CE       2076811CE  PWC   PW306 PW306C      52169NE                              LT JBOX         LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA03227DH655                    6800086                                 THE AIRCRAFT WENT TO START ENGINES, 6 CAS MESSAGES APPEARED ON THE DISPLAY.  TROUBLESHOT PROBLEM AND FOUND MOUNTING STUD FOR EMERGENCY BUSS BAR WAS LOOSE CAUSING ARCING AND WELDING OF THE STUD.  THIS STUD WAS LOOSE FROM FACTORY.  DO AN INSPECTION OF ALL STUDS TORQUE CHECK) (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRCT00012WIE35NE                
20071016000112007101600011CE  2007       10         16         2007FA0000867    120070911G6100AN520C8R6       SCREW                                   BEECH 58    58          1152740CE                                                               PROPELLER       UNSAFETIED      B  EHHRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA17755P 63                     TH2162                                  HAVE SEEN THIS ATTACHMENT ARRANGEMENT ON MANY AC.  FOUND NON SAFETIED SCREWS ATTACHING PROPELLER DEICE BRUSH ASSY TO MOUNTING.  REMOVED NON SAFETIED SCREWS WITHOUT LOCKING DEVICES WITH MS35265-44 SCREW THAT CAN BE LOCKED WITH SAFETY WIRE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 3O      3A16                         
20071016000122007101600012EU  2007       10         16         2007FA0000868    120070911G621010901030115     BLADE                                   AGUSTAA109  A109        0260109EU  ALLSN 250C  250C20B     03013GL                              MAIN ROTOR      CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM012MF  663                    7277        CAE834542                   EXCESSIVE 1 PER REVOLUTION VIBRATION NOTICED IN MAIN ROTOR SYSTEM.  THE AIRCRAFT WAS LANDED WITHOUT INCIDENT.  INVESTIGATION REVEALED CORD WISE CRACKS IN UPPER AND LOWER SKINS AT STATION 1979 EXTENDING FROM THE TRAILING EDGE TO THE AFT SIDE OF THE SPAR.  THE HONEYCOMB CORE OF THE BLADE IS ALSO SEPARATED AND DAYLIGHT CAN BE SEEN THROUGH CRACKS IN THE BLADE.  THE CRACKS IN BOTH SKINS THEN EXTEND SPAN-WISE ALONG THE SPAR FROM STA 1925 TO STA 2075.  THESE CRACKS ARE EXACTLY AS DESCRIBED IN TECH BULLETIN 109-50, PART 1 REQUIRES DAILY VISUAL INSPECTIONS OF BLADES WITH GREATER THAN 500 HOURS OF OPERATION BETWEEN STATIONS 1550 AND 3100.  BT 109-50, PART II REQUIRES INSPECTION OF THIS AREA WITH A 3X MAGNIFYING GLASS EVE1G72 3U3  U  H7EU    E4CE                 
20071016000132007101600013GL  2007       10         16         2007FA0000869    120070801G5542                SKIN                                    DIAMONDA40  DA40        2990002GL                                                               RUDDER          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP07469JP654                    40469                                   FOUND 3 INCH CRACK AFT OF RUDDER BALANCE WEIGHT IN COMPOSIT SKIN FWD OF UPPER ATTACH POINT.  AIRCRAFT WAS BASED OUT OF A HEAT RELATED AREA.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O    NTA47CE                        
20071016000142007101600014NE  2007       10         16         2007FA0000870    220070912G720030606266        BLADE                                   AMD   FALC50FALCON50MYST2730106EU  GARRTTTFE731TFE73140    29001NE                              3RD STG ROTOR   BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL11115SK1855                   330                                     BROKEN TURBINE BLADE.  ENGINE SENT TO MFG FOR INVESTIGATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L73 4F4  F  A46EU   E1NM                 
20080114002012008011400201EU  2008       1          14         2007FA0000871    220070809G853002722001002R1   CYLINDER HEAD                           DIAMONDA42  DA42        2990004EU  THIELTTAE125TAE12501    59300EU                              ENGINE          DAMAGED         C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM11240TS421                    42072                                   ENGINE BEGAN LOSING COOLANT BY PRESSURIZING THE COOLING SYSTEM WITH COMBUSTION PRESSURE AND BLOWING COOLANT OVERBOARD.  WHEN THE ENGINE WAS REMOVED AND THE OIL DRAINED, COOLANT WAS FOUND IN THE OIL AND FILLING UP CYLINDER NR 3.  IT IS SUSPECTED THAT IF THE CYLINDER HEAD WOULD HAVE BEEN REMOVED, EACH CYLINDER WOULD HAVE HAD A CRACK BETWEEN THE GLOW PLUG AND EXHAUST VALVE RECESSES.  THE ENGINE HAD PASSED A COMPRESSION CHECK AND IT IS SUSPECTED THAT THE CRACKS WOULD ONLY LEAK WHEN THE ENGINE WAS WARMED TO OPERATING TEMPERATURE.  THE RESULTANT COOLANT LOSS ONLY INCREASES THE PROBABILIITY OF FURTHER TEMPERATURE EXCURSIONS.  A PROBABLE CAUSE WOULD BE INADEQUATE DISTANCE IN THE CASTING OF THE CYLINDER HEAD BETWEEN THE1L72 3I3  BRTA57CE   E00069EN             
20071016000152007101600015CE  2007       10         16         2007FA0000872    120070719G5730                SKIN                                    CESSNA421   421C        2076016CE  CONT  O520  GTSIO520*   17032SO                              WINGS           CORRODED        D  BX4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM03648SB                       421C0648                                LT AND RT WING UPPER SKINS UNDER THE NACELLE FUEL BLADDER TANKS HAD CORROSION PRESENT TO THEM AND RELATED AREA AROUND THE BLADDER BAYS.  WO NR 10688.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A7CE    E7CE                 
20071016000162007101600016EA  2007       10         16         2007FA0000873    220070827G74146361            MAGNETO                                 PIPER PA32  PA32R301T   7103220SO  LYC   O540  TIO540AH1A  42003EA                              LT              DAMAGED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO03691MA                       3257291                                 THIS AIRCRAFT HAD A SET OF MAGS INSTALLED AT APPROXIMATELY 400 HRS TT, AT 596 HRS TT, INSTALLED ANOTHER O/H MAG ON THE LT, DUE TO AN OVERHEAT SITUATION.  IT APPEARS THAT THE COIL HAS BROKEN DOWN DUE TO EXCESS HEAT, DURING NORMAL OPERATION.  NEW AC SHOULD HAVE AIR BLAST TUBES INSTALLED FOR EACH MAGNETO, AS WELL AS A COOLING KIT FOR THE VACUUM PUMP.  THE MAGS, NOR THE VACUUM PUMP CAN OPERATE UNDER THESE CONDITIONS WITHOUT AN OUTSIDE AIR SUPPLY.  SB 1157A AFFECTS AC FOR THE TACHOMETER SENSOR ALLOWING MOISTURE TO DAMAGE THE MAGNETO.  (K)                                                                                                                                                                                     1L71 3O3  O  A3SO    E14EA                
20071016000212007101600021CE  2007       10         16         2007FA0000874    120070728G3250MC05430221      ROD END                                 CESSNA172   172D        2072410CE  CONT  O300  O300*       17022SO                              NLG STEERING    BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL012423U                       17250023                                LT SIDE STEERING ROD WITH 215.92 HRS SINCE NEW HAD THE REAR BALL END THAT ATTACHES TO THE RT RUDDER BAR ASSY BREAK.  THE BALL ROD END BROKE AND LEFT THE T/R STEERING ROD AS THE ONLY STEERING FOR THE NOSE GEAR.  THE RODS ARE NOT SOLID RODS, THEY ARE DESIGNED TO PUSH AND NOT TO PULL THAT SLIP INSIDE WHEN PULLED ON.  IT REQUIRES BOTH RODS TO STEER THE RT PEDAL AND LT ROD WILL TURN NOSE TO THE RT AND LT PEDAL AND RT ROD WILL TURN IT TO THE LT.  ON LANDING ROLL OUT, THE PLANE STARTS TO DRIFT TO THE LT AND WITH THE LT RUDDER PEDAL TO NOSE GEAR DISCONNECTED. NOSE GEAR WOULD NOT RESPOND AND THE PLANE WAS SLOWING UP TO THE POINT OF LOSING ENOUGH AIR FLOW OVER THE RUDDER FOR IT TO CONTROL THE PLANE.  THE PILOT STARTED TO1H71 3O3  ONT3A12    E253                 
20071016000182007101600018SO  2007       10         16         2007FA0000875    120071003G5530                BOLT                                    PIPER PA28  PA28181     7102807SO  LYC   O360  O360*       41514EA                              VERTICAL STAB   LOOSE           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP096365C1776 1776              287890366                               LOSE VERTICAL ATTACH BOLTS ON AFT BULKHEAD.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L71 3O3  O  2A13    E286                 
20071016000412007101600041GL  2007       10         16         2007FA0000876    120070919G7931PT100GA         TRANSMITTER                             RYAN  NAVIONNAVION      6150160GL  CONT  O520  IO520B      17032SO                              ENGINE OIL PRESSUNRELIABLE      D      K   NONE                                                                                            N  FALSE WARNING                                                                 ININSP/MAINT     1                      NM044131K                       NAV41131    1212867B                    AIRCRAFT LANDED WITH ZERO OIL PRESSURE INDICATION. AFTER TESTING WITH DIRECT READING GAUGE IT WAS DETERMINED THAT THE ACTUAL ENGINE OIL PRESSURE WAS WITHIN LIMITS SPECIFIED BY THE MFG.  FURTHER TESTING REVEALED PRESSURE INDICATING SYSTEM WOULD OPERATE NORMALLY AFTER ENGINE TEMPERATURES HAD COOLED BUT WOULD PROVIDE FALSE INDICATIONS WITH ENGINE AT OPERATING TEMPERATURE.  FEEL THIS IS A SERIOUS PROBLEM BECAUSE THIS SYSTEM IS STC APPROVED AS A PRIMARY INSTRUMENT AND ITS MALFUNCTION COULD CAUSE UNNECESSARY AND DANGEROUS OFF AIRPORT LANDINGS.                                                                                                                                                                                 1L71 3O3  ORTA782    E5CE                 
20071016000732007101600073NM  2007       10         16         2007FA0000877    120070807G2420LC41550FG       ALTERNATOR                              COLUMBLC41  LC41550FG4005150011NM  CONT  O550  TSIO550A    41516SO                              ENGINE          FAILED          F      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      NM09376PD350                    41018                                   A FLIGHT TEST WAS BEING CONDUCTED ON 07/30/07 ON A REWORKED THERMAL SYSTEMS (KATS) EVADE SYSTEM, WHEN THE SYSTEM WENT UNSTABLE CAUSING THE ALTERNATOR TO GO OFF LINE.  THE TECHNICIAN MONITORING THE SYSTEM ON A DIAGNOSTIC LAPTOP COMPUTER ANNOUNCED TO THE PILOT THAT THE SYSTEM WAS FAILED BUT THE PILOT DID NOT HAVE A "FAILED" ANNUNCIATION ON THE INSTRUMENT PANEL.  KATS CONFIRMED THAT THERE WAS A PROBLEM WITH THE FAULT DETECTION SOFTWARE THAT WOULD ALLOW THIS UNDER VERY SPECIFIC CONDITIONS.  KATS STATED THAT THEY DO NOT BELIEVE THIS TO BE A SERIOUS SITUATION SINCE THE SYSTEM IS CERTIFIED INADVERTENT ICING ONLY.                                                                                                           1L71 3O3  ONTA00003SEE5SO                 
20071023000672007102300067    2007       10         23         2007FA0000878    420070629G3455TDR906221270001 TRANSPONDER                                                                GARRTTTFE731TFE731*     01518WP                              TAILCONE        FAILED          B  BSYRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL0756EM                        144                                     ON 6/27/2007 WHILE ENROUTE, THE PRIMARY TRANSPONDER FAILED WHILE THE AIRCRAFT WAS OPERATING IN AIRSPACE.  THE CREW WAS ABLE TO SWITCH TO THE SECONDARY TRANSPONDER AND CONTINUE THEIR FLIGHT TO LOCK WITHOUT FURTHER INCIDENT.  UPON ARRIVAL, THE PRIMARY TRANSPONDER WAS CONFIRMED FAILED AND WAS REPLACED WITH A SERVICEABLE TRANSPONDER.  THE SYSTEM WAS TESTED IAW FAR PART 43, APPENDIX F AND APPENDIX E, SUB PARA C, AND ICA NR 30A05002, REVISION C.  THE SYSTEM WAS FOUND TO BE OPERATING NORMALLY AND THE AIRCRAFT WAS RETURNED TO SERVICE.  (K)                                                                                                                                                                                              4  F          E6WE                 
20071023000682007102300068CE  2007       10         23         2007FA0000879    120070909G282312161001        SELECTOR VALVE                          CESSNA207   T207A       2073614CE  CONT  O520  TSIO520M    17040SO  MCAULYD3A34 D3A34C401   GL  FUEL SYSTEM     MISMANUFACTURED D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP07803AN161                    20700570    248811R     765815          WHEN THE FUEL SELECTOR VALVE IS SELECTED TO THE RT TANK, FUEL IS BEING DELIVERED FROM THE LT TANK, VISE VERSA.  THIS WAS DISCOVERED DURING A SHORT FLIGHT IN WHICH THE PILOT NOTICED THE RT TANK FUEL GAUGE WAS DROPPING WHEN THE LT TANK WAS SELECTED.  THIS WAS LATER CONFIRMED DURING AN INSPECTION IN WHICH FUEL WAS DRAINED FROM BOTH TANKS.  IN FACT THE SELECTOR VALVE IS PUT TOGETHER INTERNALLY BACKWARDS.  (K)                                                                                                                                                                                                                                                                                                                        1H71 3O3  O  A16CE   E8CE    5  CP47GL    
20071023000692007102300069CE  2007       10         23         2007FA0000880    120070917G2420DOFF10300JR     ALTERNATOR                              CESSNA172   172M        2072418CE  LYC   O320  O320*       41508EA                                              INOPERATIVE     D  UT2RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP239531H46                     17266205                                THIS ALTERNATOR WAS OVERHAULED, OPERATED LESS THAN 50 HOURS, FAILED.  THE STUD THAT HOLDS THE DIODE PLATE IN THE ALTERNATOR WAS BROKEN, AND THE SECOND STUD WAS LOOSE.  THIS HAS BEEN AN ONGOING PROBLEM WITH OVERHAULS.  WE ARE A SMALL SHOP, YET WE HAVE HAD MANY FAILURE WITH THIS PRODUCT IN THE PAST 2 YEARS.  APPROXIMATELY 70 PERCENT OF THE OVERHAULS WE HAVE INSTALLED HAVE GONE BACK FOR WARRANTY.  PROBLEMS INCLUDE LOOSE DRIVE PULLEYS, LOOSE HARDWARE, SHORT CIRCUITS, DEAD FIELD WINDINGS, DEFECTIVE BRUSHES.  MY SUPPLIERS STATE THAT THEY HAVE HAD MANY COMPLAINTS ABOUT THIS REPAIR.                                                                                                                                           1H71 3O3  ONT3A12    E274                 
20071023000702007102300070    2007       10         23         2007FA0000881    420070918G830023066678        PINION GEAR     ALLSN                                                      ALLSN 250C  250C47B          GL                              GEARBOX         FRACTURED       B  YKERO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA17                CAG47225                CAE847225                   RECEIVED THE ENGINE FOR REPAIR DUE TO VIBRATIONS, AND METAL IN OIL.  UPON DISASSEMBLY OF THE GEARBOX FOUND THE ROLLER RETAINER OF THE NR 3 BEARING FRACTURED IN (4) PLACES.  ALSO FOUND THAT THE NR 1 TURBINE WHEEL BLADE TIPS HAD BEEN RUBBING THE BLADE TRACK WHICH CAUSED THE VIBRATION.  TECH SUSPECTS THE FRACTURED RETAINER MAY HAVE BEEN A RESULT OF THE VIBRATION. (K)                                                                                                                                                                                                                                                                                                                                                                         3  U          E1GL                 
20071023000712007102300071GL  2007       10         23         2007FA0000882    120070831G782020559002        MUFFLER                                 CIRRUSSR    SR20        05628AJGL  CONT  O360  IO360ES          SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA07824ZB559                    1674                                    CHECK MUFFLER IAW MFG SB, SB2X-78-07, ISSUED JUNE, 2007.  FOUND SPOT WELDS ON EXTERNAL BAFFLE CRACKED.  REPLACED MUFFLER.  THIS SB APPLIES ONLY TO SR20`S SN 1005 THRU 1797.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O3  ONTA00009CHE1CE                 
20071023000722007102300072SO  2007       10         23         2007FA0000883    120070807G32137873804         AXLE                                    PIPER PA32  PA32300     7103212SO  LYC   O540  IO540K1A5   41532EA  HARTZLHCC2Y HCC2YK1     GL  LT MLG          BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL038905N10353                  3240690     L2683048E   CH35831B        ON TAXI TO TAKEOFF, AC TURNED AROUND AFTER BACK TAXI.  PIVOTING ON LT M/G.  SIDE LOAD BROKE AXLE AT END OF DRILLED OUT CENTER.  EVIDENCE OF PREVIOUS CRACKING FROM INSIDE OB.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  A3SO    1E4     5  CP920     
20071023000742007102300074CE  2007       10         23         2007FA0000884    120070717G324007516800        PLATE                                   CESSNA208   208         2073702CE  PWA   PT6   PT6A6       52043EA                                              CRACKED         C  FE4RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL039602F15966                  20800103                                FOUND TORQUE PLATE CRACKED DURING ROUTINE INSPECTION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3T3  TNTA37CE   E4EA                 
20071023000752007102300075EU  2007       10         23         2007FA0000885    120070910G5753257WF101A       VANE                                    BRAERODH125 BAE125800A  1500285EU  GARRTTTFE731TFE731*     01518WP                              TE FLAP         CORRODED        B  JGVRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE09150SB5758                   258197                                  LT IB FLAP VANE, UPPER SKIN CORRODED BEYOND LIMITS.  POSSIBLE CAUSE: DISSIMILAR METAL CORROSION AS TRAILING EDGE IS MAGNESIUM AND SKIN IS ALUMINUM OR ENVIRONMENT IN WHICH THE VANE OPERATES. IT IS LOCATED BEHIND THE MLG.  ASSURE THE SKIN IS PROPERLY TREATED IAW CORROSION PREVENTION PROCEDURES AND PAINTED WITH EPOXY PRIMER BEFORE INSTALLATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA3EU    E6WE                 
20071023000782007102300078EA  2007       10         23         2007FA0000886    220070817G8500                ENGINE                                  BEECH 60    A60         1153604CE  LYC   O541  TIO541E1C4  41536EA                                              MAKING METAL    D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM0198KA                        P212        RL79259                     DURING ROUTINE OIL CHANGE, METAL SHAVINGS WERE FOUND IN OIL FILTER AND SCREEN.  SHAVINGS WERE MAGNETIC.  THESE ENGINES DO HAVE WEAR ISSUES ON CAM AND LIFTERS.  AFTER REMOVING OIL PAN, FOUND CAM BAD AND LIFTER WEAR.  OIL ANALYSIS DIDN`T PICK UP LARGER MICRON IN OIL.  RECOMMEND INSPECTION OF CAM AND LIFTER BEFORE 1000 HOUR.  REMOVED OIL PAN ON RT ENGINES AND FOUND BEAD WEAR AS WELL.  NO METAL IN FILTER.  (K)                                                                                                                                                                                                                                                                                                                       1L72 3O3  O  A12CE   E10EA                
20071023000802007102300080GL  2007       10         23         2007FA0000887    220070803G7250                TURBINE WHEEL                           CESSNASTC   STC206C     1182107CE  ALLSN 250C  250C30P     03013GL                              ENGINE          FAILED          C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM055746N1654 13                45461       890629                      AFTER 13 HOURS OF OPERATION SINCE OVERHAUL, DURING A POWER CHECK, THE TURBINE ASSY FAILED CAUSING THE FORCED LANDING OF THE HELICOPTER.  FORCED LANDING CAUSED SUBSTANTIAL DAMAGE TO THE AIRCRAFT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  UNTA4CE    E1GL                 
20071023000832007102300083CE  2007       10         23         2007FA0000888    120070830G3246C163003102      WHEEL                                   CESSNA172   172M        2072418CE  LYC   O360  O360A4M     41514EA  SNSNCH76E   76EM8       EA  LT MLG          FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM019898Q                       17265842    L3551036A   31674R          WHEEL IS A 3 PIECE CONSTRUCTION, OUTER RIM AND THE INNER SPACER.  BROKE APART ON TAXIING OF AIRCRAFT. JACKED AIRCRAFT AND INSTALLED SERVICEABLE UNIT, THREADS STRIPPED OUT OF CENTER SECTION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A12    E286    5  NP4EA     
20071023000862007102300086SO  2007       10         23         2007FA0000889    220070911G8530                ROCKER                                  CUBCFTCC11  CC11100     060002HCE  CONT  O200  O200A       17020SO                              NR 4 CYLINDER   MISINSTALLED    D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM01787AK118                    CC1100006   256113                      FOUND THE ROCKER ARMS REVERSED, INTAKE EXHAUST ROCKERS IN CYLINDER NR 4 LEADING TO POSSIBLE EXHAUST GUIDE AND VALVE DAMAGE DO TO THE  EXHAUST ROCKER ARM HAS AN OILING PORT FOR THE EXHAUST VALVE AND THE INTAKE ROCKER ARM DOES NOT HAVE THE OILING PORT.  THE ROCKER ARMS WERE REMOVED AND INSTALLED CORRECTLY.  DAMAGE TO VALVE AND GUIDE UNKNOWN AT THIS TIME, WILL HAVE TO CONTACT MFG.  (K)                                                                                                                                                                                                                                                                                                                                               1H71 3O3  ONC        E252                 
20071023000882007102300088SO  2007       10         23         2007FA0000890    220070911G8530MS5196364       SETSCREW                                CUBCFTCC11  CC11100     060002HCE  CONT  O200  O200A       17020SO                              CYL ROCKER BOSS DAMAGED         C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM01787AK118                    CC1100006   256113                      IN THE NEW STYLE CYLINDER ASSY PN 655482 FOR THE ENGINE, THE ROCKER ARM PIN PN 654375 IS RETAINED BY A SET SCREW PN MS51966364 IN THE CENTER ROCKER BOSS SUPPORT.  FOUND IN THIS ENGINE (2) SET SCREWS LOOSE AND A THIRD FOUND RATTLING AROUND AND LODGED UNDER THE INTAKE ROCKER ARM BETWEEN THE CYLINDER HEAD.  THE ROCKER SHAFTS ARE MOVING OFF CENTER AND ROTATING AND WITH A MACHINED SHARP CUT IN THE END OF THE ROCKER SHAFT TO INDICATE WERE SET SCREW IS TO LINE UP WITH THE ROCKER SHAFT, IT IS CUTTING THROUGH THE VALVE COVERS AND WILL LEAD TO LOSS OF ENGINE OIL AND OPERATION OF THE ENGINE AND POSSIBLE LOSS OF PERSONAL LIFE.  (K)                                                                                             1H71 3O3  ONC        E252                 
20071023000912007102300091SO  2007       10         23         2007FA0000891    220070914G8530O200D           SETSCREW                                AMCNLGAL3   AL3         060002KCE  CONT  O200  O200*       17020SO                              ROCKER ARM BOSS MISMANUFACTURED D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO0565LC 42                     AL1083                                  CHECKING ROCKER ARM SHAFT SET SCREWS AND TO ASSURE INTAKE AND EXHAUST ROCKER ARMS NOT SWITCHED IAW INFORMATION TO OWNERS FORM INTERNET OWNERS AIRCRAFT FORUM. CYLINDER NR 1, SN AC06HB070, SET SCREW AND ROCKER ARMS, OK.  CYLINDER NR 2, SN AC06FA543, SET SCREW LOOSE ENOUGH TO ALLOW SHAFT TO MOVE, ROCKER ARMS, OK.  CYLINDER NR 3, SN AC06HA911, SET SCREW OK, INTAKE AND EXHAUST ROCKER ARMS SWITCHED.  CYLINDER NR 4, SN AC06HA935, SET SCREW AND ROCKER ARMS, OK.  (K)                                                                                                                                                                                                                                                                  1H71   3  O3OEXPA1H71E252                 
20071023000872007102300087CE  2007       10         23         2007FA0000892    120071010G27501434425         FLEX DRIVE                              CESSNA750   750         2076810CE  ALLSN AE3007AE3007C          GL                              RT TE FLAPS     BROKEN          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP2322NG                        7500204                                 THE RT FLAP FLEX DRIVE HOUSING FAILED AT THE SWAGED END OF THE HOUSING AT THE IB END.  ON SEPTEMBER 11, 2007 THIS AIRCRAFT HAD A SIMILAR EVENT WITH THE LT OB FLAP DRIVE WHICH ALLOWED THE FLEX DRIVE TO DISENGAGE FROM THE OB FLAP DRIVE CAUSING THE FLAPS TOP REMAIN AT 3 DEGREES POSITION AND PREVENTING FURTHER EXTENSION OR RETRACTION. WE OPERATE 2  AIRCRAFT AND THIS IS THE 4TH FAILURE OF THE FLEX DRIVE BETWEEN THE 2 AIRCRAFT.                                                                                                                                                                                                                                                                                                       2L72 4J4  FRTT00007WITE6CH                
20071023001272007102300127WP  2007       10         23         2007FA0000893    220070914G7230307516034       TURBINE WHEEL                           RAYTHNDH125 HAWKER800XP 7150012CE  GARRTTTFE731TFE7315BR        WP                              LP COMPRESSOR   FAILED          E      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      NM04800WY3172                   258556      107656                      CLIMBING THROUGH FL270, A LOUD BANG IN REAR OF ACFT.   LT ENGINE COMPUTER LIGHT ILLUMINATED. PF BROUGHT LT ENGINE TO IDLE, PNF PULLED CHECKLIST. AFTER SURVEY OF ENGINE PARAMETERS, PF TURNED LT ENGINE COMPUTER BACK ON TO CONTROL PARAMETERS.  ENGINE COMPUTER DID STAY ON & DID APPEAR TO CONTROLL ENGINE.  POWER ADVANCED SLOWLY ON LT ENGINE. AT APPROXIMATELY 70 % N1 ANOTHER LOUD BANG IN REAR & LT ENGINE COMPUTER LIGHT ILLUMINATED AGAIN. ENGINE PARAMETERS MOVED TO RED LINE. PF SHUTDOWN LT ENGINE.  PNF CONTACTED ATC, DECLARED AN EMERGENCY & REQUESTED & RECEIVED DIRECT CLOSEST AIRPORT.  SINGLE ENGINE APPROACH CHECKLIST & PROGRAMMED FMS FOR AN APPROACH.  ACFT CLEARED FOR VISUAL APPROACH.  AFTER A NON-EVENTFUL LANDING.  2L72 4F4  FRTA3EU    E6WE                 
20071023001092007102300109CE  2007       10         23         2007FA0000895    120071001G3150                UNKNOWN                                 BEECH MU300 400A        1155402CE                                                                               UNKNOWN         E      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      SO11418GJ                       RK418                                   AC EXPERIENCED A FLAP ASYMMETRIC LIGHT IN FLIGHT.  THE CREW DID NOT TRY TO PUT THE FLAPS DOWN AND DIVERTED FOR A NO FLAP LANDING.  CRITICAL CARE MAINTENANCE DROVE DOWN TO REPAIR THE AIRCRAFT.  MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AFTER SEVERAL ATTEMPTS.  MAINTENANCE INSPECTED AND CLEANED ALL CONNECTORS, INSPECTED HYDRAULIC SYSTEMS, AND FLAP RIGGING AND CABLES.  MAINTENANCE C/W ALL OPERATIONAL CHECK IAW THE MM.  THE PROBLEM WAS NEVER DUPLICATED.                                                                                                                                                                                                                                                                         2H72 4F    RTA16SW                        
20071023000032007102300003CE  2007       10         23         2007FA0000897    120071012G2730                CONTROL CABLE                           CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              ELEVATORS       WORN            D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP23379TA1560                   172S9379    L3083351A                   CONTROL CABLE, (P/N 0510105-308), FOUND WORN TO REPLACE LIMITS PER AC43.13-1A, CABLE INSPECTION.  CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7.  IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT.  MM DOES NOT CONTAIN ANY (CABLE WEAR) LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    1E10                 
20071023001352007102300135CE  2007       10         23         2007FA0000898    120071012G5712051179616       BULKHEAD                                CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              ZONE 100        MISALIGNED      D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP23373ES3780                   17280052    L2701351A                   CONTROL CABLE, (P/N 0510105-339), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION.  CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7.  IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT.  CESSNA MAINTENANCE MANUAL DOES NOT CONTAIN ANY (CABLE WEAR) LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                               1H71 3O3  ONT3A12    1E10                 
20071023001402007102300140CE  2007       10         23         2007FA0000900    120071012G2730                CONTROL CABLE                           CESSNA182   182S        2072701CE  LYC   O540  IO540AB1A5       EA                              ZONE 100        WORN            D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP237262Y1400                   18280812    L1241261E                   CONTROL CABLE, (P/N 0510105-189), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION.  CABLE WAS WORN DUE TO CONSTANT CONTACT WITH MICARDA GUARD PLATE OVER FUEL LINES AT FUEL SELECTOR AREA JUST FORWARD OF FRONT SEATS.  THE CABLES ARE IN CONSTANT CONTACT WITH PLATES EVEN WITH CABLE TENSION CORRECT.  MM DOES NOT CONTAIN ANY (CABLE WEAR) LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A13    1E4                  
20071023001342007102300134CE  2007       10         23         2007FA0000904    120071012G5712051179616       BULKHEAD                                CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              ZONE 100        MISALIGNED      D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP23625SP1560                   172S8616    L2922551A                   CONTROL CABLE, (P/N 0510105-339), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION.  CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7.  IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT.  MM DOES NOT CONTAIN ANY "CABLE WEAR" LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    1E10                 
20071023001372007102300137CE  2007       10         23         2007FA0000906    120071012G5712051179616       BULKHEAD                                CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              ZONE 100        MISALIGNED      D      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      WP23658SP4200                   172S8063    L2796451A                   CONTROL CABLE, (P/N 0510105-308), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION.  CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7.  IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT.  MM DOES NOT CONTAIN ANY "CABLE WEAR" LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    1E10                 
20071023001382007102300138CE  2007       10         23         2007FA0000907    120071012G5712051179616       BULKHEAD                                CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              ZONE 100        MISALIGNED      D      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      WP232630U1628                   17280568    L2761951A                   CONTROL CABLE, (P/N 0510105-308), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION.  CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7.  IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT.  MM DOES NOT CONTAIN ANY "CABLE WEAR" LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    1E10                 
20071023000042007102300004CE  2007       10         23         2007FA0000908    120070919G3230JE1             STOP                                    CESSNA310   310Q        2074242CE  CONT  O470  IO470*      17026SO                              MLG GEARBOX     BROKEN          B  OF1RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA1720SS 3235                   310Q0521                                PILOT HAD NO LT GEAR DOWN INDICATION.  HE CYCLED GEAR WITH NO SUBSEQUENT GEAR DOWN INDICATION.  HE ATTEMPTED MANUAL EXTENSION, CRANKED TO THE MECHANICAL STOP IN THE GEARBOX AND BROKE THE STOP.  BELLCRANK CONTINUED PAST DOWN AND THEN WENT PARTIALLY (UP).  GEAR COLLAPSED ON LANDING. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3O3  O  3A10    E1CE                 
20071023001652007102300165CE  2007       10         23         2007FA0000909    120070911G528045A3161521      DOOR                                    BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              NLG             CRACKED         B  ZKFRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA61262PA                       RK203                                   FOUND DURING INSPECTION.  NOSE GEAR FOLLOW UP DOOR PN 45A31615-21 ON BRACKETS, PN 45A31613-9 AND 45A31613-7 AT ATTACHING RIVET HAS CRACKS GOING FORWARD TO AFT THROUGH THE FIRST RIVET ALONG THE RIVET ROW.  RELATIVE WIND PUSHING AFT ON THE DOOR WHILE GEAR IS EXTENDED FOR TAKEOFF AND LANDING AND VIBRATION.  USING THICKER MATERIAL DURING MFG AND OR ADDING A DOUBLER.  (K)                                                                                                                                                                                                                                                                                                                                                               2H72 4F4  FRTA16SW   E25EA                
20071023001662007102300166CE  2007       10         23         2007FA0000910    120070920G528045A3161521      DOOR                                    BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              NLG             CRACKED         B  ZKFRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA61268PA                       RK323                                   FOUND DURING INSPECTION.  NOSE GEAR FOLLOW UP DOOR, P/N 45A31615-21 ON BRACKETS PN 45A31613-9, 45A31613-7 AND 45A31616-3 AT ATTACHING RIVET HAS CRACKS GOING FORWARD TO AFT THOUGH THE FIRST RIVET ALONG THE RIVET ROW. RELATIVE WIND PUSHING AFT ON THE DOOR WHILE GEAR IS EXTENDED FOR TAKEOFF AND LANDING AND VIBRATION.  USING THICKER MATERIAL DURING MFG AND OR ADDING A DOUBLER.  (K)                                                                                                                                                                                                                                                                                                                                                    2H72 4F4  FRTA16SW   E25EA                
20071101001722007110100172CE  2007       11         1          2007FA0000911    120070917G5280                STRUCTURE                               BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              NLG DOOR        CRACKED         B  ZKFRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA6126PA                        RK256                                   FOUND DURING INSPECTION.  NOSE GEAR FOLLOW UP DOOR PN 45A31615-21 ON BRACKETS PN 45A31613-9 AND 45A31613-7 AT ATTACHING RIVET HAS CRACKS GOING FORWARD TO AFT THROUGH THE FIRST RIVET ALONG THE RIVET ROW.  RELATIVE WIND PUSHING AFT ON THE DOOR WHILE GEAR IS EXTENDED FOR TAKEOFF AND LANDING AND VIBRATION.  USING THICKER MATERIAL DURING MFG AND OR ADDING A DOUBLER.  (K)                                                                                                                                                                                                                                                                                                                                                                2H72 4F4  FRTA16SW   E25EA                
20071101001732007110100173CE  2007       11         1          2007FA0000912    120071001G561045AS3101012     WINDOW                                  BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              COCKPIT         CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03480M                        RK6                                     WHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND NR 2 (COPILOT) SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD.  THE D-INSPECTION REQUIRES THAT BOTH WINDSHIELD RETAINERS OR USING OPTICAL PRISM INSPECTION METHOD.  THE IS NO STATEMENT IN THE AIRCRAFT MM OR IN THE A-D INSPECTION CHECKLIST THAT REQUIRES YOU TO INSPECT THE COCKPIT SIDE WINDOWS IN THE SAME MANNER AS THE WINDSHIELDS.  ALL OF THE WINDOWS IN THE COCKPIT AREA ARE INSTALLED OR FASTENED IN THE SAME MANNER AS THE WINDSHIELDS.  IT IS SUSPECTED THAT THE COPILOT WINDOW CRACKED FROM FATIGUE, OR TT INSTALLED. WOULD RECOMMEND THAT INSPECTIONS OF ALL COCKPIT WINDOWS WITH A PRISM AT SCHEDULED INTERVALS BE COMPLETED.  (K)                                     2H72 4F4  FRTA16SW   E25EA                
20071023000112007102300011CE  2007       10         23         2007FA0000914    120071003G5510                FITTING                                 BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              HORIZONTAL STAB LOOSE           C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03480M                        RK6                                     WHILE PERFORMING AN A-D INSPECTION FOUND 8 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A21183-11 ON THE BOTTOM OF THE HORIZONTAL STABILIZER.  IT IS SUSPECTED THAT THE LOOSE RIVETS WERE CAUSED BY FATIGUE AND AGE.  RECOMMEND INSPECTING AREA THOROUGHLY AT EACH INSPECTION.  RECOMMEND CONTACTING MFG FOR REPAIR OPTIONS.  THIS IS THE 3RD AIRCRAFT IN A ROW THAT THESE SAME RIVETS HAVE BEEN LOOSE OR MISSING.  (K)                                                                                                                                                                                                                                                                                          2H72 4F4  FRTA16SW   E25EA                
20071023000072007102300007CE  2007       10         23         2007FA0000915    120071001G5520                HINGE BRACKET                           CESSNA500   S550        2076607CE  PWA   JT15  JT15D4      52112NE                              LT ELEVATOR     CORRODED        B  SI6RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW1752FT                        S5500056                                LT OB HINGE BRACKET BROKE OFF DURING AILERON REMOVAL.  APPEARS TO HAVE FAILED DUE TO CORROSION. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 4F4  FRTA22CE   E1NE                 
20071023000102007102300010CE  2007       10         23         2007FA0000916    120070928G7830                STRUCTURE                               LEAR  35    35A         5170602CE  GARRTTTFE731TFE7312     01518WP                              THRUST REVERSER DAMAGED         C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA1710UF            0011        166         P74521C                     DURING THE PILOT PREFLIGHT, THE PILOT HAD NOTICED THAT THERE WAS A TEAR IN THE SHEET METAL OF THE LT ENGINE THRUST REVERSER INNER SKIN.  WE COULD NOT IDENTIFY WHAT HAS CAUSED THIS TEAR.  THE UNIT WILL BE REPAIRED BY THE MFG AND WILL INFORM YOU WITH ANY INFO THEY GIVE TO US ABOUT THIS INCIDENT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  F  A10CE   E6WE                 
20071023000172007102300017EA  2007       10         23         2007FA0000917    220070820G73223013460         ROD                                     EMB   110   EMB110P1    3260122SO  PWA   PT6   PT6A34      52043EA                              FUEL CONTROL    BROKEN          C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA65621KC                       110335                                  DURING A 150 HR INSPECTION THE LOWER FUEL CONTROL ROD WAS FOUND BROKEN ON THREADED SHAFT WHERE IT SCREWS INTO COUPLING.  IT LOOKS LIKE IT MAY HAVE BEEN BENT AND A MORE DETAILED INSPECTION OF THIS COMPONENT SHOULD OCCUR. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 4T4  T  A21SO   E4EA                 
20071101001752007110100175CE  2007       11         1          2007FA0000918    120070927G243523085001        STARTER GEN                             BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE                              LEFT            FAILED          B  E81RO   OTHER                                                                                           HJ ELECT. POWER LOSS-50 PC   WARNING INDICATION                                  NRNOT REPORTED   1                      GL03350TT     4822              FL413                                   PILOT REPORTED LT GENERATOR GOING OFF-LINE ON APPROACH.  FOUND STARTER/GENERATOR INOPERATIVE.  UPON REMOVAL NOTICED EVIDENCE OF COOLING FAN TIPS RUBBING ON HOUSING, BEARINGS WORN (ARMATURE ASSY LOOSE).(K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4T4  T  A24CE   E4EA                 
20071101001762007110100176GL  2007       11         1          2007FA0000919    120070913G7160                CONTROL ARM                             DIAMONDA40  DA40        2990002GL  LYC   O360  O360A4M     41514EA                              CARB HEAT       BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07423FP452                    40FC023                                 CARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  ONTA47CE   E286                 
20071101001772007110100177CE  2007       11         1          2007FA0000920    120071002G2420DOFF10300JR     ALTERNATOR                              CESSNA172   172M        2072418CE  LYC   O320  O320*       41508EA                              ENGINE          INOPERATIVE     D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM079531H40                     17266205                                ALTERNATOR, DEFECT UNKNOWN, FAILED INTERNALLY, GROUND POST LOOSE INTERNALY EXCESSIVE ARMATURE END PLAY.  RETURNED FOR WARRANTY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A12    E274                 
20071101001782007110100178CE  2007       11         1          2007FA0000921    120071002G2420DOFF10300JR     ALTERNATOR                              CESSNA172   172M        2072418CE  LYC   O320  O320*       41508EA                              ENGINE          INOPERATIVE     D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM079531H40                     17266205                                ALTERNATOR, DEFECT UNKNOWN, FAILED INTERNALLY.  RETURNED FOR WARRANTY. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    E274                 
20071023000152007102300015CE  2007       10         23         2007FA0000922    120071002G8011MHJ4003S        MOTOR                                   CESSNA340   340A        2076405CE  CONT  O520  TSIO520*    17040SO                              STARTER         NOISY           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07340RF46                     340A0212                                STARTER STARTED MAKING A LOUD SQUEALING NOISE WHEN OPERATING STARTER, AND SLOW ROTATION OF ENGINE.  REMOVED AND RETURNED FOR WARRANTY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  3A25    E8CE                 
20071026000862007102600086CE  2007       10         26         2007FA0000923    120071005G2797                CONNECTOR                               CESSNA750   750         2076810CE  ALLSN AE3007AE3007C          GL                                              MISINSTALLED    B  CNQRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE07964QS                       7500164                                 PRIMARY STAB TRIM FAILED CLIMBING THROUGH FL280 AT 300 KTS.  NO CAS MESSAGE WAS PRESENT.  CLACKER WAS STUCK ON. STAB WAS NOT MOVING WHEN CLACKER WAS GOING OFF.  AUTO PILOT DISENGAGED ON ITS OWN DUE TO HEAVY NOSE CONFIG.  AFTER TROUBLESHOOTING SHOULD THE ECM TO BE BAD.  REMOVED AND REPLACED (ECM NR 421400216J1) WITH NEW PART 4214-0021-11 (LATEST DASH NR)  COMPLETED PRIMARY CHANNEL A/B TRAVEL VERIFICATION CHECKS IAW 750 MM, TASK 27-40-00-721, NO FAULTS NOTED.  FOUND THE PRIMARY AND SECONDARY CONNECTORS SWAPPED.  WHICH HAD NO EFFECT IN THIS FAILURE.  (K)                                                                                                                                                                   2L72 4J4  FRTT00007WITE6CH                
20071023000122007102300012CE  2007       10         23         2007FA0000924    120070616G5712051179616       BULKHEAD                                CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              FUSELAGE        MISLOCATED      C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP232630U1628                   17280568    L2761951A                   CONTROL CABLE, ( P/N 0510105-308), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A.  THE CABLE CONSTANTLY RUBS THE S338-7 FAIRLEAD IN THE LANDING GEAR BULKHEAD HOLE.  IT IS BELIEVED THAT A HOLE MISLOCATION CAUSES THE MISALIGNMENT WHICH ALLOWS THE CABLE RUB.  MM DOES NOT CONTAIN ANY  (CABLE WEAR) LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                 1H71 3O3  ONT3A12    1E10                 
20071023000012007102300001CE  2007       10         23         2007FA0000925    120071018G7603632558A1        LINK ROD                                CESSNA185   A185F       2072821CE  CONT  O520  IO520D      17032SO                              THROTTLE        WORN            D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM074640E877                    18503824    832429R                     THROTTLE BUTTERFLY (P/N: 625601G) AND THROTTLE BODY (P/N: 639437)ARE WORN, ALLOWING BUTTERFLY SHAFT TO SLIDE SIDE TO SIDE CAUSING THE LINK ROD ASSEMBLY (P/N: 632558A1)TO WEAR CHAFING THE WAVE WASHER AND COTTER PIN. THE COTTER PIN AND WAVE WASHER AT THE THROTTLE BODY WERE MISSING AT THE TIME OF INSPECTION. IF THE LINK ROD FROM THE THROTTLE BODY ARM AND THE METERING BLOCK ARM DETACHES, PROPER FUEL METERING CEASES.                                                                                                                                                                                                                                                                                                                 1H71 3O3  O  3A24    E5CE                 
20071023000522007102300052CE  2007       10         23         2007FA0000926    120070812G5712051179616       BULKHEAD                                CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              ZONE 100        WORN            C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP23379TA1560                   172S9379    L3083351A                   CONTROL CABLE, ( P/N 0510105-308), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A.  THE CABLE CONSTANTLY RUBS THE S338-7 FAIRLEAD IN THE LANDING GEAR BULKHEAD HOLE.  IT IS BELIEVED THAT A HOLE MISLOCATION CAUSES THE MISALIGNMENT WHICH ALLOWS THE CABLE RUB.  MM DOES NOT CONTAIN ANY (CABLE WEAR) LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    1E10                 
20071023001602007102300160CE  2007       10         23         2007FA0000929    120070712G5712051179616       BULKHEAD                                CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA                              ZONE 100        MISALIGNED      C      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      WP23373ES3780                   17280052    L2701351A                   CONTROL CABLE, ( P/N 0510105-308), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A.  THE CABLE CONSTANTLY RUBS THE S338-7 FAIRLEAD IN THE LANDING GEAR BULKHEAD HOLE.  IT IS BELIEVED THAT A HOLE MISLOCATION CAUSES THE MISALIGNMENT WHICH ALLOWS THE CABLE RUB.  MM DOES NOT CONTAIN ANY (CABLE WEAR) LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    1E10                 
20071101001872007110100187CE  2007       11         1          2007FA0000930    120071018G7603632558A1        LINK ROD        CONT                    CESSNA185   A185F       2072821CE  CONT  O520  IO520D      17032SO                              THROTTLE        WORN            D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM074640E877                    18503824    832429R                     THROTTLE BUTTERFLY (P/N: 625601G) AND THROTTLE BODY (P/N: 639437) ARE WORN, ALLOWING BUTTERFLY SHAFT TO SLIDE SIDE TO SIDE CAUSING THE LINK ROD ASSEMBLY (P/N: 632558A1)TO WEAR CHAFING THE WAVE WASHER AND COTTER PIN. THE COTTER PIN AND WAVE WASHER AT THE THROTTLE BODY WERE MISSING AT THE TIME OF INSPECTION.  IF THE LINK ROD FROM THE THROTTLE BODY ARM AND THE METERING BLOCK ARM DETACHES, PROPER FUEL METERING CEASES.                                                                                                                                                                                                                                                                                                               1H71 3O3  O  3A24    E5CE                 
20071023001612007102300161CE  2007       10         23         2007FA0000931    120070912G5712051179616       BULKHEAD                                CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              ZONE 100        MISALIGNED      C      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      WP23658SP4200                   172S8063    L3083351A                   CONTROL CABLE, ( P/N 0510105-308), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A.  THE CABLE CONSTANTLY RUBS THE S338-7 FAIRLEAD IN THE LANDING GEAR BULKHEAD HOLE.  IT IS BELIEVED THAT A HOLE MISLOCATION CAUSES THE MISALIGNMENT WHICH ALLOWS THE CABLE RUB.  MM DOES NOT CONTAIN ANY (CABLE WEAR) LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    1E10                 
20071101001862007110100186EA  2007       11         1          2007FA0000932    220071018G8520AS18840         CAMSHAFT                                BEECH 23    A2324       1151226CE  LYC   O360  IO360A1A    41514EA                              ENGINE          SPALLED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA236956Q556  556               MA304       RL707851A                   556 HOURS SINCE MAJOR OVERHAUL, CAMSHAFT AND LIFTERS SPALLED AND CORROSION IS EVIDENT.  ENGINE HAS BEEN OPERATED ON PHILLIPS XC 20W50 OIL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  O  A1CE    1E10                 
20071101001932007110100193SO  2007       11         1          2007FA0000933    120071019G2432MS915861        SHUNT                                   PIPER PA32  PA32R301T   7103220SO  LYC   O540  TIO540*     41532EA                              MASTER BATTERY  BLOWN           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NE03788JG440                    3257369                                 COMPLETE ELECTRICAL FAILURE. WHEN BATTERY MASTER SWITCH WAS TURNED ON, NO POWER REACHED MAIN BUSS.  FOUND BATTERY AMMETER SHUNT BURNED THROUGH.  BATTERY AMMETER SHUNT INSTALLED WAS 30 AMP VALUE. (P/N MS91586-1)  BATTERY AMMETER SHUNT SHOULD BE 100 AMP VALUE.  NO RECORD OF BATTERY AMMETER SHUNT BEING REPLACED SINCE AIRCRAFT WAS MANUFACTURED.  INSTALLED CORRECT AMP VALUE SHUNT AND ELECTRICAL SYSTEM OPS CHECKED GOOD. PIPER P/N 486-684 (MS91586-6)  RECOMMEND THAT ALL SHUNTS BE CHECKED FOR ALL THIS MODEL AIRCRAFT. (ALTERNATOR AMMETER SHUNT IS SAME P/N)                                                                                                                                                                       1L71 3O3  O  A3SO    E14EA                
20071101001822007110100182EA  2007       11         1          2007FA0000935    220071018G7414                PIN                                     PIPER PA44  PA44180     7104402SO  LYC   O360  O360E1A6    41514EA                              MAGNETO         GROOVED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL092916W633        G03EA044    447995300   L45577T                     STOP PINS GROOVED BEYOND LIMITS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3O3  O  A19S0   E286                 
20071023001622007102300162CE  2007       10         23         2007FA0000937    120070912G2730                CONTROL CABLE                           CESSNA182   182S        2072701CE  LYC   IO360 IO360L2A         EA                              ZONE 100        WORN            C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP237262Y1400                   18280812    L3083351A                   LT AND RT ELEVATOR CONTROL CABLES, ( P/N 0510105-189), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A.  CABLE WAS WORN DUE TO CONSTANT CONTACT WITH THE MICARDA PLATES OVER THE FUEL LINES AT FUEL SELECTOR AREA JUST FORWARD OF THE FRONT SEATS.  THE CABLE TENSIONS ARE CORRECT BUT THE CABLES ARE IN CONSTANT CONTACT WITH PLATES.  MM DOES NOT CONTAIN ANY (CABLE WEAR) LIMITS OR COMMENTS, ONLY CABLE WIRE BREAKAGE AND CORROSION LIMITS.                                                                                                                                                                                                                                                             1H71 3O3  ONT3A13    1E10                 
20071026000952007102600095SO  2007       10         26         2007FA0000938    120071022G3297AN551           BOLT            PIPER                   PIPER PA44  PA44180     7104402SO  LYC   O360  O360*       41514EA                              DRAG LINK       SHEARED         B      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      WP07574ER3743       NA          4496150                                 FORWARD DRAG LINK BOLT ON NOSE GEAR FAILED DURING TOUCH AND GO PRACTICE.  A/C RETURNED TO DEPARTURE AND LANDED WITH THE NOSE GEAR STUCK IN THE NOSEWHEEL WELL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3O3  O  A19S0   E286                 
20071026000972007102600097CE  2007       10         26         2007FA0000939    120071021G3260                LAMP                                    BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              MLG INDICATOR   INOPERATIVE     D      O   OTHER                                                                                           P  NO WARNING INDICATION                                                         DEDESCENT        1                      SO11442GJ                       RK442                                   PILOT HAD NO GREEN DOWN AND LOCKED INDICATION FOR THE RT GEAR WHEN LANDING. PILOT CONFIRMED WITH THE TOWER THE GEAR WAS DOWN, ALSO THE PILOT CONFIRMED THAT THE LIGHT WOULD NOT ILLUMINATE WHEN TESTED. AFTER LANDING MAINTENANCE CHECKED OUT AIRCRAFT AND REPLACED LAMP IN GEAR INDICATION. SYSTEM OPERATIONAL CHECK GOOD.                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4F4  FRTA16SW   E25EA                
20071204000042007120400004SW  2007       12         4          2007FA0000941    120071009G2700KS178           ROLL SERVO                              MOONEYM20   M20K        5870220SW  CONT  O360  TSIO360*    17025SO                              INSIDE CASE     LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA13697SP160        5644        252002                                  MOTOR ASSY COMING LOOSE ON SERVO MOUNT. LOOSE HARDWARE, LOOSE MOTOR.  RECOMMEND SERVO TO BE INSPECTED FOR PROPER SERVO ASSY (THAT MOTOR AND HARDWARE ARE NOT LOOSE).   (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  O  2A3     E9CE                 
20071026001092007102600109SO  2007       10         26         2007FA0000942    120070921G3220                LANDING GEAR                            PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360KB   17025SO                              NOSE            COLLAPSED       C  AG3RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP1584643                       348233033                               AIRCRAFT TAXIED TO RUNWAY AFTER LOADING CARGO.  AFTER NORMAL RUNUP, THE PILOT TAXIED ONTO THE RUNWAY AND STOPPED.  THE PILOT ADVANCED THROTTLES AND RELEASED BRAKES, AFTER RELEASING BRAKE, THE NOSE GEAR COLLAPSED.  AIRCRAFT WAS RECOVERED AND TOWED OFF RUNWAY TO A SAFE TIE DOWN SPOT.  NO CAUSE IS YET KNOWN AS TO WHY THE NOSE GEAR COLLAPSED.  (K)                                                                                                                                                                                                                                                                                                                                                                                       1L72 3O3  O  A7SO    E9CE                 
20071026001102007102600110CE  2007       10         26         2007FA0000944    120071012G80116462751         STARTER                                 CESSNA421   421C        2076016CE  CONT  O520  GTSIO520N   17032SO                              RT ENGINE       SHORTED         C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA25421KD29                     421C1006    808319R                     OVERHAULED STARTER FAILED AFTER 30 HOURS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3O3  O  A7CE    E7CE                 
20071026001112007102600111CE  2007       10         26         2007FA0000945    120071012G2913                PUMP                                    RAYTHN390   390         7150030CE  WILINTFJ44  FJ442A           GL                              HYD SYSTEM      DAMAGED         D  JAS2O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP09408J                        RB193                                   HYDRAULIC PUMP ASSY, PN 390-389022-0003, INSPECTED AND FOUND NOT DEFECTIVE.  FOUND DEFECTIVE/ DAMAGED PART PN MS28778-6, PACKING.  FLIGHT CREW COMPLETED ABNORMAL CHECKLIST.  UPON INSPECTION FOUND THAT PACKING AT HYDRAULIC PUMP PRESSURE OUTLET FITTING HAD FAILED.  THIS COMPONENT WAS WORKED ON IAW MFG SAFETY COMMUNIQUE , CONTROL NR JAS-SDR-001.  (K)                                                                                                                                                                                                                                                                                                                                                                                   1L72 3F4  FRTA00010WIE3GL                 
20071026001132007102600113NM  2007       10         26         2007FA0000946    120071016G5313                STRINGER                                BOEING727   727200      138407ENM  PWA   JT8   JT8D217C    52053NE                              BS940-945       CRACKED         B  FY4YK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP03705AA                       22462                                   THE AIRCRAFT INPUT FOR 4C CHECK AND CPCP ON SEPT 3, 2007.  DURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND 5 INCH CRACK BOTH ON LT AND RT FUSELAGE STRINGER S18A BETWEEN BS940 AND BS945 ON SEPT 21, 2007.  A PROPOSAL WAS INITIALLY SUBMITTED ON SEPT 22.  AFTER REPAIR TO THE STRINGERS, FORM 337 WILL BE SUBMITTED TO FAA FOR FINAL RESULT OF CORRECTIVE ACTIONS DETAIL.  (K)                                                                                                                                                                                                                                                                                                                                               2L73 4F4  FRTA3WE    E9NE                 
20071102000022007110200002EU  2007       11         2          2007FA0000947    120071003G3233X110061         ACTUATOR                                DIAMONDA42  DA42        2990004EU                                                               MLG             INOPERATIVE     D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07240TS681                    42072                                   PILOTS WERE UNABLE TO EXTEND RT MLG WITH THE EMERGENCY EXTENSION HANDLE IN FLIGHT.  EMERGENCY SYSTEM OPERATED WITHIN LIMITS ON THE GROUND.  UPON REMOVAL, THE ACTUATOR WAS FOUND TO BE VERY DIFFICULT TO MOVE.  ( K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3I    RTA57CE                        
20071026001122007102600112SO  2007       10         26         2007FA0000948    120071024G3220                CENTERING MECH  PIPER                   PIPER PA46  PA46310P    7104605SO  CONT  O520  TSIO520*    17040SO                              NLG             FAILED          G      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      SO11383SA                       4608033                                 UPON TOUCHDOWN AIRCRAFT VEERED LT ABRUPTLY AND DEPARTED RUNWAY SURFACE. GEAR EXTENSION AND INDICATION WERE NORMAL. INVESTIGATION REVEALED THAT UPON TOUCHDOWN THE NOSE LANDING GEAR HAD FAILED TO CENTER CORRECTLY DURING EXTENSION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3O3  ORTA25SO   E8CE                 
20071026001062007102600106NM  2007       10         26         2007FA0000949    120071017G561058935578        WINDSCREEN                              BOEING737   7377H4      1384404NM  GE    CFM56 CFM567B24        NE                              COCKPIT         CRACKED         D      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      WP0166ZB 2985                   29233                                   IN CRUISE, 41,000FT (8.5PSID), -60C, ARCING AND SMOLDERING OBSERVED FROM MID BOTTOM OF WINDOW PROPAGATING UP TO TOP FWD EDGE OF RT NR 2 SLIDING WINDOW.  WINDOW HEAT, RT, SIDE SWITCH SELECTED OFF. WHILE QRH CONSULTED, AS WINDOW COOLED, CRACKING OBSERVED ON OUTER PANE ONLY THROUGHOUT THE WINDOW AREA.  QRH STATES NO FURTHER ACTION REQUIRED DUE OUTER PANE NOT PRIMARY STRUCTURAL SUPPORT.  FLIGHT CONTINUED AT 41,000 FT FOR NEXT 20 MINS TO TOP OF DESCENT.  LANDING CARRIED OUT NORMALLY.  WINDOW ASSY REPLACED..                                                                                                                                                                                                                     2L72 4F4  FRTA16WE   E00055EN             
20071026001072007102600107NM  2007       10         26         2007FA0000950    120071017G561058935578        WINDSCREEN                              BOEING737   7377H4      1384404NM  GE    CFM56 CFM567B24        NE                              COCKPIT         CRACKED         D      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      WP01     2985                   29233                                   IN CRUISE, 41,000FT (8.5PSID), -60C, ARCING AND SMOULDERING OBSERVED FROM MID BOTTOM OF WINDOW PROPAGATING UP TO TOP FWD EDGE OF RT NR 2 SLIDING WINDOW.  WINDOW HEAT, RT, SIDE SWITCH SELECTED OFF. WHILE QRH CONSULTED, AS WINDOW COOLED, CRACKING OBSERVED ON OUTER PANE ONLY THROUGHOUT THE WINDOW AREA.  QRH STATES NO FURTHER ACTION REQUIRED DUE OUTER PANE NOT PIMARY STRUCTURAL SUPPORT.  FLIGHT CONTINUED AT 41,000 FT FOR NEXT 20 MINS TO TOP OF DESCENT.  LANDING CARRIED OUT NORMALLY.  WINDOW ASSY REPLACED.                                                                                                                                                                                                                      2L72 4F4  FRTA16WE   E00055EN             
20071130001422007113000142EA  2007       11         30         2007FA0000951    220070713G726156G23399        BAFFLE                                  FOUND FBA   FBA2C1      3640103EA  LYC   O540  TIO540*     41532EA                              OIL SUMP        BROKEN          B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL03796  599                    50                                      OIL BAFFLE IN SUMP RUBBING ON BOTTOM OF SUMP.  4 OUT OF 6 HOLES CRACKED OUT AROUND MOUNTING AREA.  2 HOLES COMPLETELY WORN THROUGH AND STILL HAD PARTS OF BAFFLE UNDER WASHER AND MOUNTING SCREW.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3O3  ONCA7EA    E14EA                
20071105000082007110500008EA  2007       11         5          2007FA0000952    220071010G8530AEL85099        CYLINDER                                PIPER PA28  PA28161     7102803SO  LYC   O320  O320*       41508EA                              NR 4            FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO15602FT733                    2841196                                 CYLINDER HAD FAILURE, SEPARATION FROM BARREL AT 733 HRS, NOT INCORPORATED IN AD2006-12-7.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 3O3  O  2A13    E274                 
20071105000092007110500009    2007       11         5          2007FA0000953    420071011G2562                BATTERY         AMERIKING               PIPER PA28  PA28151     7102805SO  LYC   O320  O320*       41508EA                              ELT             DAMAGED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM0232276                       287515109                               FOUND ELT BATTERY CASE BULGED ON BOTTOM.  FOUND ALL CONTACTS WITHIN BATTERY COMPARTMENT LOOSE DUE TO HIGH TEMPERATURE (COULD SEE WHERE PLASTIC HAD MELTED) COULD NOT DETERMINE WHAT CAUSED THE SHORT.  REPLACED ELT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  O  2A13    E274                 
20071105000122007110500012    2007       11         5          2007FA0000954    420071011G2562                BATTERY         AMERIKING               CESSNA210   210C        2073412CE  CONT  O470  IO470*      17026SO                              ELT             DAMAGED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM0222GP                        58202                                   DURING ANNUAL INSPECTION FOUND DRIED ALKILINE BATTERY SUBSTANCE ON EXTERIOR OF CASE.  OPEND CASE AND FOUND THAT THE BATTERIES, ALKALINE BATTERIES WERE COMING APART AT THE SEAMS AND LEAKING.  CLEANED BATTERY COMPARTMENT AND INSTALLED FRESH SET OF BATTERIES.  FUNCTION TESTED OK.  THIS IS THE THIRD SUCH OCCURENCE THIS YEAR. OF ACID LEAK INTO THE TRANSMITTER.  UNIT HAD TO BE REPLACED.  (K)                                                                                                                                                                                                                                                                                                                                            1H71 3O3  O  3A21    E1CE                 
20071105000142007110500014SO  2007       11         5          2007FA0000955    220070921G8530                CYLINDER HEAD                           BEECH 33    F33A        1151425CE  CONT  O520  IO520*      17032SO                              NR 2            SEPARATED       D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA09711JA                       CE478                                   IN-FLIGHT NR 2 CYLINDER HEAD SEPARATED FROM CYLINDER BASE AT TOP OF SLEEVE. PUSHRODS AND TUBES BENT.  EXHAUST MANIFOLD BENT. NOZZLE ASSEMBLY DAMAGED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  O  3A15    E5CE                 
20071130001432007113000143CE  2007       11         30         2007FA0000956    120070919G574050270025        BRACKET                                 CESSNA310   310R        2074245CE  CONT  O520  IO520*      17032SO                              RT MLG WW       INOPERATIVE     E      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL135338C                       310R1544                                THE RT MAIN LANDING GEAR WOULD NOT RETRACT INTO WHEEL WELL.  PILOT REPORTED LOUD BANG HEARD AFTER RETRACTING OF GEAR.  WHEN EXTENDING THE GEAR FOR LANDING, THE RT GEAR WOULD NOT INDICATE GREEN BUT WAS VISUALLY CONFIRMED DOWN.  PILOT LANDED WITHOUT INCIDENT AND GREEN LIGHT ILLUMINATED UPON TOUCHDOWN.  INSPECTION OF THE RT GEAR FOUND THE TORQUE TUBE SUPPORT BRACKET ASSY, PN 50270025, BEARING PULLED LATERALLY FROM BRACKET AND ROD END FOR THE UPLOCK PUSH-PULL TUBE BROKEN OFF AT THE TORQUE TUBE ATTACH POINT PN HM4, AND FORWARD TORQUE TUBE ATTACH BOLT, PN NAS146-40, BENT SLIGHTLY.  FAILURE OF THE SUPPORT BRACKET PN 5027002-5 POSSIBLY DUE TO FATIGUE.  (K)                                                                1L72 3O3  O  3A10    E5CE                 
20071130001452007113000145SO  2007       11         30         2007FA0000957    220071004G741410500556101     MAGNETO                                 CIRRUSSR    SR22        2130001GL  CONT  O550  IO550N      17042SO                              ENGINE          MISOVERHAULED   B  YD5RO   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      GL15434SR20                     2557        690898                      AIRCRAFT ENGINE RUNNING ROUGH AND BACKFIRING ON FLIGHT TEST.  PILOT RETURNED AND GROUNDED AIRCRAFT FOR MAINTENANCE.  MAINTENANCE PERSONNEL PERFORMED INTERNAL INSPECTION OF CONVERTED MAGNETOS TO PRESSURIZATION.  MAGNETO CONVERTED TO PRESSURIZED, INSPECTION REVEALED CARBON BRUSHES MISSING ON BOTH MAGNETOS, INTERNAL TIMING WAS WRONG ON ONE OF THE MAGNETOS, WIRES WERE CHAFED, EXCESS GREASE WAS FOUND ON ROTOR BRUSH ASSEMBLY.  FURTHER INVESTIGATION OF AIRCRAFT WITH MAGNETO PN 10-550556-101 MODIFIED, INSTALLED ON AIRCRAFT FOR TURBO NORMALIZING. 6 ADDITIONAL MAGNETOS EXHIBITED THE SAME CONDITIONS LISTED ABOVE.  RECOMMENDATIONS FOR CORRECTION ARE TO CONVERT MAGNETOS IAW PUBLISHED SPECS AND PROCEDURES.  (K)              1L71 3O3  ONTA00009CHE3SO                 
20071105000132007110500013EU  2007       11         5          2007FA0000958    220070913G7310CASC216         REGULATOR                               GULSTMG1159 G1159A      3970109SO  RROYCESPEY  SPEY5118    54523EU                              FUEL FLOW       FAILED          D      O   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      EA07776MA891                    447         11298                       PILOTS REPORT FELT HEAVY VIBRATION FOR 3 TO 4 SECONDS, THEN HEARD A LOUD BANG FOLLOWED BY LT ENGINE SPOOLING DOWN.  AIRCRAFT SAFELY LANDED AT AIRPORT.  CONTACTED MFG, WHO DISPATCHED A RESPONSE CREW TO AIRPORT.  FOUND THAT THE FUEL FLOW REGULATOR HAD FAILED IN FLIGHT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  F  A12EA   E2EU                 
20071130001462007113000146WP  2007       11         30         2007FA0000959    220071002G731430708507        PUMP                                    LEAR  35    35LEAR      5170600CE  GARRTTTFE731TFE73122B   01518WP                              RT ENGINE FUEL  FAILED          B  X5ERK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW05354PM     4254              015         P74271                      RT ENGINE FAILED ON TAKEOFF ROLL JUST BEFORE 80 KNTS IAS.  AIRCRAFT WAS STILL ON GROUND.  FUEL PUMP, FAILED TO PUMP FUEL.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  F  A10CE   E6WE                 
20071130001472007113000147SO  2007       11         30         2007FA0000960    120070906G3240                BRAKE                                   MAULE MX7   MX7180A     5460186SO  LYC   O360  O360*       41514EA                              PARK SYS        INOPERATIVE     D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO0330822                       22003C                                  PARK BRAKE CABLE HANGING ON 90 DEGREE CABIN FITTING COMING THROUGH FIREWALL.  AIRCRAFT BRAKES LOCKED ON WHEN LANDING.  DISCONNECTED PARK BRAKE CABLE AND SAFETY WIRED BRAKE LOCK LEVERS ON MASTER CYLINDER IN NEUTRAL/OFF POSITION PLACARD PANEL MADE LOG BOOK ENTRY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONC3A23    E286                 
20071105000152007110500015SO  2007       11         5          2007FA0000961    120070718G21401386725         HEATER                                  PIPER PA31T PA31T       7103124SO  PWA   PT6   PT6A60A     52043NE                              COCKPIT         LEAKING         B      O   OTHER                                                                                           KBJFLUID LOSS                SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION        CRCRUISE         1                      GL25650RS     1                 31T8020071                              DURING OPERATION OF COMBUSTION HEATER, THE PILOT NOTED JET FUEL ODOR AND SMOKE IN CABIN.  HEATER OPERATION WAS TERMINATED, CABIN WAS VENTED.  EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT NEAREST AIRPORT WITHOUT INCIDENT.  UPON REMOVAL, A FUEL LEAK WAS NOTED AT COMBUSTION HEAD AND FUEL SOLENOID AREA.  HEATER WAS REPLACED WITH A SERVICEABLE UNIT.  (K)                                                                                                                                                                                                                                                                                                                                                                                1L72 3T4  T  A8EA    E4EA                 
20071130001552007113000155SO  2007       11         30         2007FA0000962    120071018G32503526202         BUNGEE                                  PIPER PA28  PA28140     7102802SO  LYC   O320  O320*       41508EA                              NLG STEERING    FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL0956978                       287425077                               SHORTLY AFTER TAKEOFF, AIRCRAFT WENT INTO SHARP RT TURN.  THE PILOT, BY USING FULL OPPOSITE RUDDER AND AVAILABLE RUDDER TRIM, WAS ABLE TO LAND AIRCRAFT SUCCESSFULLY.  INSPECTION DETERMINED THAT THE RT NOSE GEAR STEERING BUNGEE SPRING RETAINER HAD DEPARTED AND THE SPRING WAS EXTENDED FROM THE BARREL ASSY.  THE TURN WAS ALSO EXAGGERATED BY THE LARGE FIN USED ON THE NOSE WHEEL FAIRING.  AS IT IS DIFFICULT TO EXAMINE THE RETAINER DUE TO THE LOCATION OF THE BUNGEE ASSY UNDER THE EXHAUST SYSTEM, IT CAN NOT BE DETERMINED IF THE BACK SIDE OF THE RETAINER IS BEING WORN OR CORRODED.  THIS PART IS ONLY HELD IN PLACE BY A FEW TWISTS OF SAFETY WIRE.  IT IS SUGGESTED THAT THE MFG LOOK AT THIS AS A MAJOR SAFETY ISSUE AND EITH1L71 3O3  O  2A13    E274                 
20071130001572007113000157CE  2007       11         30         2007FA0000963    120071018G322207436062        FITTING                                 CESSNA182   182T        2072703CE  LYC   O540  IO540AB1A5       EA                              NLG STRUT       CHAFED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO036025D                       18281830                                LOWER STRUT SUPPORT FITTING CLAMPING RING CENTER BORE IS NOT CENTERED.  THIS CAUSES THE STEERING COLLAR AND LOWER STRUT SUPPORT TO CHAFE AND FOR METAL TO METAL CONTACT TO OCCUR.  HAVE TRIED TWO OTHER NEW LOWER STRUT SUPPORT FITTING RESULTING WITH METAL TO METAL CHAFING.  INITIALLY CONTACTED MFG AND REPORTED THE PROBLEM REVEALING NUMEROUS IDENTICAL PARTS HAVE THE SAME DEFECT.  RECOMMEND THAT CONTACT BE MADE WITH MFG AND TO MEASURE FOR PROPER THICKNESS OF THE RING ON THE LOWER STRUT SUPPORT FITTING.  (K)                                                                                                                                                                                                                     1H71 3O3  ONT3A13    1E4                  
20071204000052007120400005SO  2007       12         4          2007FA0000964    120071017G282235328803        PUMP                                    PIPER PA28  PA28161     7102803SO  LYC   O320  O320*       41508EA                              FUEL BOOST      MALFUNCTIONED   D      O   OTHER                                                                                           Y  ENGINE STOPPAGE                                                               CRCRUISE         1                      NM02515MS2750                   2842157                                 REPORTED ENGINE QUITTING DURING NORMAL CRUISE, PROBLEM ASSOCIATED WITH FUEL SYSTEM, ONCE ELECTRIC FUEL PUMP TURNED ON ENGINE WOULD RUN NORMAL, FUEL PRESS READINGS CONFIRMED FUEL STARVATION PROBLEM, INITIAL INSPECTIONS FAILED TO FIND A PROBLEM & COULD NOT BE DUPLICATED, REPLACED EDP WITH NEW & FLEW ACFT, PROBLEM REOCCURRED & APPEARED TO BE ISOLATED TO THE RT SIDE FUEL TANK SELECTION, REMOVED FUEL LINE AT CARB & PUMPED FUEL USING BOOST PUMP, MONITORED FLOW RATE FOR BOTH RT AND LT TANKS, INSTALLED VACUUM GAUGE IN SYSTEM AT GASCOLATOR AND MONITORED AMOUNT OF SUCTION CREATED FOR BOTH THE LT & RT, PROBLEM FINALLY DUPLICATED WHILE MONITORING & PUMPING FUEL, FOUND PROBLEM WAS NOT ISOLATED TO ONE SIDE BUT WOULD OCCUR ON1L71 3O3  O  2A13    E274                 
20071130001812007113000181EA  2007       11         30         2007FA0000966    220070810G8530LW15322         VALVE                                                                      LYC   O360  O360E1A6    41514EA                              CYLINDER        WRONG PART      D      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      GL03                                        RL15377T                    DURING ASSEMBLY OF THE ENGINE AFTER MAJOR OVERHAUL, ONE OF THE FACTORY NEW CYLINDERS (PN LW15322) HAD A DIFFERENT INTAKE VALVE INSTALLED (PN 73938), AND THE CORRECT VALVE PN LW15314 WAS INSTALLED BY THE CYLINDER SHOP. THIS CYLINDER WAS FACTORY NEW.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          3  O          E286                 
20071105000022007110500002GL  2007       11         5          2007FA0000967    120071031G3150M835366022M     RELAY                                   BOMBDRBD700 BD7001A10   1390006GL                                                               MASTER CAUTION  FAILED          D      K   NONE                                                                                            N  FALSE WARNING                                                                 ININSP/MAINT     1                      NM09     1690                   9114                                    MASTER CAUTION RELAY (WIRING DIAGRAM 31-52-00 SHEET 1 - K28, LOCATED ON CIRCUIT CARD DB5 OF JUNCTION BOX 4 FAILED CAUSING BOTH MASTER CAUTION WARNING ANNUNCIATORS TO STAY ILLUMINATED - NO RESET AVAILABLE. THIS IS A SINGLE POINT OF FAILURE FOR THE WARNING/CAUTION CONTROL SYSTEM. (3) INTEGRATED AVIONICS COMPUTERS FEED THIS MASTER CAUTION RELAY - SAME WITH THE MASTER WARNING.  AFTER DOING A LIMITED INDEPENDENT SURVEY, I DETERMINED THAT THIS HAS OCCURRED ON SEVERAL OTHER AIRCRAFT.                                                                                                                                                                                                                                               2L72 4F    RTT00003NY                     
20071204000502007120400050SO  2007       12         4          2007FA0000968    120071102G2510110744701       INERTIA REEL    PIPER                   PIPER PA28  PA28161     7102803SO  LYC   O320  O320D3G     41508EA  SNSNCH74D   74DM        EA  SEAT HARNESS    SEVERED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW998440M8718                   288216002   L1042639A   A61404          PILOTS SHOULDER HARNESS INERTIA REEL LOCKED UP, UPON EXAMINATION THE METAL GUIDE WHICH SURROUNDS THE FABRIC AND GUIDES IT ONTO THE REEL, HAD RUBBED AGAINST THE CENTER SHAFT OF THE REEL ITSELF.  THIS OVER TIME REDUCED THE DIAMETER OF THE SHAFT UNTIL IT FAILED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  O  2A13    E274    5  NP88614   
20071204000612007120400061    2007       12         4          2007FA0000969    120071029G6510538715          SHAFT                                                                                                                                   TAIL ROTOR      CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP23                                                                    FINE TRANSVERSE CRACK(S) LOCATED NEAR THE CENTER PORTION OF PART.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         
20071204000632007120400063    2007       12         4          2007FA0000970    120071029G6510538715          SHAFT                                                                                                                                   TAIL ROTOR      CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP23                                                                    FINE TRANSVERSE CRACK(S) LOCATED NEAR THE CENTER PORTION OF PART.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         
20071204000482007120400048CE  2007       12         4          2007FA0000971    120071031G326041EN16          SQUAT SWITCH                            BEECH MU300 400BEECH           CE  PWA   JT15  JT15D4      52112NE                              LEFT            FAILED          E      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      SO118HQ                         RJ50                                    PILOTS REPORTED THAT THE THRUST REVERSER ARM LIGHTS WERE ILLUMINATED IN FLIGHT. PILOTS LANDED AT LZU MAINTENANCE FOUND A FAULTY LT GROUND SAFE SWITCH. MAINTENANCE REPLACED SWITCH WITH NEW UNIT AIRCRAFT CHECKED GOOD.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4F4  FRTA16SW   E1NE                 
20071130001522007113000152EA  2007       11         30         2007FA0000974    220071031G7414K3975           COIL            SLICK                   CESSNA206   T206H       2073303CE  LYC   O540  TIO540AJ1A       EA                              RT MAGNETO      OPEN            D      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      NM072378X1168       98060921    T20608023   L1003761A                   PILOT REPORTED RT MAGNETO FAILED WHEN CHECKED DURING RUN UP. FOUND COIL HAD OPEN CIRCUIT WHEN CHECK IAW TABLE SEVEN IN UNISON'S 4300/6300 SERIES MM P/N L-1363C.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ORTA4CE    E14EA                
20071130001842007113000184GL  2007       11         30         2007FA0000975    120071031G3150M835366022M     RELAY                                   BOMBDRBD700 BD7001A10   1390006GL                                                                               FAILED          C      K   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      NM09999YY1690                   9114                                    MASTER CAUTION RELAY (WIRING DIAGRAM 31-52-00 SHEET 1 - K28), LOCATED ON CIRCUIT CARD DB5 OF JUNCTION BOX 4 FAILED CAUSING BOTH MASTER CAUTION WARNING ENUNCIATORS TO STAY ILLUMINATED - NO RESET AVAILABLE. THIS IS A SINGLE POINT OF FAILURE FOR THE WARNING/CAUTION CONTROL SYSTEM. THREE INTEGRATED AVIONICS COMPUTERS FEED THIS MASTER CAUTION RELAY - SAME WITH THE MASTER WARNING.  AFTER DOING A LIMITED INDEPENDENT SURVEY, I DETERMINED THAT THIS HAS OCCURRED ON SEVERAL OTHER AIRCRAFT.                                                                                                                                                                                                                                             2L72 4F    RTT00003NY                     
20071130001252007113000125WP  2007       11         30         2007FA0000976    220071029G725030606266        ROTOR                                   ISRAEL1125  ASTRASPX    4500205EU  ALIDSGTFE731TFE7313AR        WP                              LPT3            SEPARATED       B      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      WP07400CP                       131         113211                      IAW SERVICE BULLETIN TFE731-72-5175.  BLADE SEPARATION ON ONE LPT3 BLADE AS LISTED IN TABLE 1 OF S/B 72-5175.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA16NM   E6WE                 
20071204001362007120400136EA  2007       12         4          2007FA0000979    220071018G7322                CONTROL ARM                             DIAMONDA40  DA40        2990002GL  LYC   O360  O360A4M     41514EA                              CARB HEAT       BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW99423FP                       40FC023                                 CARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  ONTA47CE   E286                 
20071204001372007120400137SO  2007       12         4          2007FA0000980    120071019G7820E362000         MUFFLER                                 PIPER PA18  PA18150     7101828SO  LYC   O320  O320B2B     41508EA                              ENGINE          BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL1398SA 996                    187609088   L1333839A                   THE TAILPIPE CRACKED AWAY FROM THE SHELL.  THERE ARE NO STRAPS WELDED FROM THE PIPE TO THE SHELL LIKE SOME OTHER MUFFLERS.  THE METAL FAILED, NOT THE WELD.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  1A2     E274                 
20071204001392007120400139CE  2007       12         4          2007FA0000981    120071103G3710RV05268         RELIEF VALVE                            CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                              PNEUMATIC SYS   SEPARATED       D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL031232Y3                      208B0566                                RELIEF VALVE FOR BLEED AIR PNEUMATIC SYSTEM END WASHER AND CAP SEPARATED FROM VALVE AND LAYING IN BOTTOM OF COWLING.  SUSPECT RIVET HOLDING PARTS ON IS TOO SOFT.  THIS IS THE THIRD VALVE TO FAIL LIKE THIS ON DIFFERENT AIRCRAFT IN THE LAST MONTH. AND ALL WERE NEW WITH LESS THAN 70 HOURS TIME IN SERVICE. (K)                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3T3  T  A37CE   E4EA                 
20071204001422007120400142SO  2007       12         4          2007FA0000982    120071028G3233HM6             BEARING                                 PIPER PA24  PA24250     7102404SO  LYC   O540  O540*       41532EA                              RT MLG ACTUATOR BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL13108SG2160                   24149                                   RT OB HEIM BEARING BROKE AT THREADS NEXT TO JAM NUT ON ACTUATOR ROD DURING TAKEOFF ROLL W/RESULTANT GEAR COLLAPSE. INCREASE SIZE AND STRENGTH OF PART.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L71 3O3  O  1A15    E295                 
20071204001432007120400143CE  2007       12         4          2007FA0000983    120071022G301080713           CONTROLLER                              LEAR  60    60LEAR      5170707CE  PWA   305   PW305A      52128NE                              STAB DEICE      INOPERATIVE     C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM07415NP                       024                                     REPLACED HORIZONTAL STAB HEAT CONTROLLER.  AFTER CHANGING CONTROLLER AIRCRAFT STILL HAD FAULT IN SYSTEM. T/S FURTHER DETERMINED REPAIRED CONTROLLER WAS NO GOOD.  CONTROLLER SHOWED A FAULT IN T8.  INSTALLED ANOTHER CONTROLLER SYSTEM CHECKED GOOD.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA10CE   E35NE                
20071204001642007120400164CE  2007       12         4          2007FA0000986    120071008G2910165580001135    LINE                                    BEECH 23    C24R        1151254CE  LYC   O360  IO360A1A    41514EA                              HYD SYSTEM      CHAFED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO095246M6712                   MC564                                   PILOT REPORTED HAVING TO SERVICE BRAKE HYDRAULIC RESERVOIR AND/OR RT SIDE OF THE BRAKES VERY SOFT.  DURING INSPECTION, FOUND HYDRAULIC FLUID ON WIRE BUNDLE FORWARD OF COPILOTS RT RUDDER PEDAL.  CLEANED LINE AND LT LINE SIT FOR A COUPLE DAYS, WHILE DOING AN INSPECTION ON THE REST OF THE AIRCRAFT.  FOUND HYDRAULIC FLUID ON LINE.  REMOVAL OF THE LINE REVEALED A WORN/CHAFED SPOT APPROX 12 INCHES TO THE LT OF THE B-NUT WHERE IT ATTACHES TO THE BULKHEAD FITTING FROM THE RESERVOIR.  DID NOT SEE THE CAUSE OF THE CHAFED AREA ON THE TUBE.  SUSPECT AIRFRAME VIBRATION CAUSED THE LINE TO VIBRATE.  RECOMMEND THAT ALL LINES ARE CHECKED FOR CLEARANCE FROM AIRFRAME STRUCTURE OR OTHER LINES.  (K)                                 1L71 3O3  O  A1CE    1E10                 
20071204001652007120400165CE  2007       12         4          2007FA0000987    120071101G531245A3490111      BULKHEAD                                BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              BS 329          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL19940VA                       RK197                                   WHILE PERFORMING AN A-C INSPECTION FOUND RT AFT FUSELAGE BLEED AIR LINE ATTACH BRACKET PULLED FROM FUSELAGE BULKHEAD RESULTING IN A CRACK IN THE BULKHEAD AT FRAME STATION 329.92.  RECOMMEND CONTACTING MFG FOR REPAIR OPTIONS  CRACK HAS BEEN FOUND ON BOTH SIDES OF THE AIRCRAFT.(K)                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4F4  FRTA16SW   E25EA                
20071204001662007120400166CE  2007       12         4          2007FA0000988    120071031G555145A2100291      PIVOT                                   BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              HORIZONTAL STAB LOOSE           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL19940VA                       RK197                                   WHILE PERFORMING AN A-C INSPECTION FOUND 8 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A2118311 ON THE BOTTOM OF THE HORIZONTAL STABILIZER.  IT IS SUSPECTED THAT THE LOOSE RIVETS WERE CAUSED BY FATIGUE AND AGE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4F4  FRTA16SW   E25EA                
20071204001032007120400103SO  2007       12         4          2007FA0000989    120071106G3211                LANDING GEAR                            PIPER PA30  PA30        7103002SO  LYC   O320  IO320*      41508EA                              MAINS           WORN            G      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CE0722HW 5124 893               30791                                   PART (A) OF AD 77-13-21 REQUIRES INSPECTION OF LANDING GEAR EVERY 1000 HRS IAW SL 782.  AIRCRAFT EXPERIENCED A COLLAPSED RT MLG FOLLOWING A SCENARIO THAT IS IDENTIFIED IN SL 782.  THIS SCENARIO INCLUDES A POPPED LANDING GEAR MOTOR CIRCUIT BREAKER RESULTING IN A FAILED MLG EXTENSION, FOLLOWED BY A MANUAL GEAR EXTENSION.  INVESTIGATION FOUND MANY OF THE PARTS IDENTIFIED IN SL 782 WERE WORN AND REQUIRED REPLACEMENT.  PART (A) OF THE AD 77-13-21 HAD BEEN COMPLETED 893 HRS AND 12 YEARS AGO.  OWNERS AND OPERATORS SHOULD CONSIDER COMPLYING WITH AD 77-13-21 PART (A) MORE OFTEN THAN THE 1000 HRS AS REQUIRED.  AD 77-13-21 DOES NOT CONTAIN A CALENDAR REQUIREMENT.                                                            1L72 3O3  O  A1EA    1E12                 
20071204001302007120400130SO  2007       12         4          2007FA0000990    120070130G3230452729          BEARING                                 PIPER PA32  PA32R300    7103213SO  LYC   O540  IO540*      41532EA                              ROD END         BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CE01406RB6700                   32R7880009                              NOSE GEAR EXTENDED SUDDENLY AND UNCOMMANDED IN FLIGHT,  EXAMINED AND FOUND CYLINDER ROD END TO NOSE GEAR RETRACT ASSY WAS BROKEN.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O3  O  A3SO    1E4                  
20071204001672007120400167CE  2007       12         4          2007FA0000995    120071107G24206041H190        RELAY                                   BEECH 200   A200        1152921CE                                                               RT STARTER GEN  MELTED          D      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      SW99                            BC27                                    RT STARTER GENERATOR RELAY P/N: 6041H190 MELTED AT BUSS BAR CONNECTION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 4T      A24CE                        
20071204001102007120400110CE  2007       12         4          2007FA0000996    120071107G5753086210057       TUBE                                    CESSNA414   414A        2075907CE                                                               TE FLAPS        BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      GL27     7707                                                           DURING FLAP EXTENSION THE RT SIDE FLAPS RETRACTED SUDDENLY LEAVING THE LT FLAPS DOWN.  FOUND THE PUSHROD TUBE CONNECTING THE IB AND MIDDLE FLAP BELLCRANK TO HAVE FAILED AT THE OB END OF THE TUBE.  THE TUBE APPEARS TO HAVE BEEN ABOUT 60 PERCENT CRACKED THROUGH THE DIAMETER FOR SOME TIME, POSSIBLY SINCE NEW.  THIS FAILURE OCCURRED JUST BELOW THE LOCK NUT WHICH SECURES THE ROD END TO THE TUBE, AND THE FAILED AREA IS IN THE THREADED PORTION OF THE TUBE MAKING IT DIFFICULT OR IMPOSSIBLE TO SEE A DEVELOPING CRACK.                                                                                                                                                                                                               1L72 3O      A7CE                         
20071204000702007120400070SO  2007       12         4          2007FA0000997    120071105G3220452729          BEARING                                 PIPER PA32  PA32R301    7103218SO  LYC   O540  IO540*      41532EA                              NLG ROD END     FAILED          C      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CE01832136282                   32R8113035                              WHILE IN FLIGHT THE NOSE GEAR RETRACT CYLINDER PISTON ROD END FAILED, CAUSING IMMEDIATE EXTENSION OF THE NOSE GEAR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  O  A3SO    1E4                  
20071204001742007120400174GL  2007       12         4          2007FA0000999    120071108G2421                BRUSHES         CESSNA                  CIRRUSSR    SR20        05628AJGL  LYC   IO360 IO360L2A         EA                              ALTERNATOR      WORN            D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL091180 494        A180062     1576        L3328651E                   DURING FLIGHT, PILOT REPORTED LOW VOLTAGE INDICATION.  RESET ATTEMPTS WERE UNSUCESSFUL.  PILOT RETURNED TO STATION. ALTERNATOR BRUSHES FOUND TO BE WORN BEYOND USE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  ONTA00009CH1E10                 
20071204001732007120400173EU  2007       12         4          2007FA0001000    120071108G33206178A           POWER SUPPLY                            HAWKERBAE125BAE125700B  7450007EU  GARRTTTFE731TFE731*     01518WP                              CABIN LIGHTING  BURNED          B      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL15107LT                       257146                                  DISCREPANCY WAS CABIN INDIRECT LIGHTING IS INTERMITTENT. FOUND SHORTED WIRING AT AFT LT SIDE VALANCE, 2 BURNED POWER SUPPLIES AND SEVERAL CRACKED LAMP FIXTURES. CUSTOMER STATED THIS IS THE 3RD TIME THE POWER SUPPLIES WERE FOUND BURNED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA3EU    E6WE                 
20071109002452007110900245CE  2007       11         9          2007FA0001001    120071109G2750040010740       CONTROL CABLE                           CESSNA150   150E        2071812CE                                                               TE FLAP         FRAYED          B      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      WP0731ER 6487 98                15061072                                ASSYMETRIC DEPLOYMENT OF FLAPS ON FINAL APPROACH.  LOUD SNAP HEARD NOVING FLAPS FROM 30 TO 40 DEGREES. MAINTENANCE FOUND THE LEFT FLAP EXTEND CABLE BROKEN AT THE OUTBOARD PULLEY.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O      3A19                         
20071213002432007121300243SW  2007       12         13         2007FA0001002    120071106G5520                TORQUE TUBE                             SWRNGNSA227 SA227*             SW                                                               LT ELEVATOR     SHEARED         H      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW17     6734                   858                                     DURING A ROUTINE PHASE INSPECTION OF THE AIRCRAFT, IT WAS DISCOVERED THAT THE LT ELEVATOR PIVOT PIN ON THE TORQUE TUBE ASSEMBLY PN 27-44026-007 WAS SHEARED. INITIAL INSPECTION REVEALED CORROSION/RUST AND EXTENSIVE PITTING IN THE PIN. THIS PIN IS (1) OF (3) IN A LINEAR LINE ATTACHING THE ELEVATOR TO THE AIRCRAFT STABILIZER. THIS AIRCRAFT IS NORMALLY LOCATED OUTSIDE EXPOSED TO THE WEATHER ELEMENTS NEAR SALT AIR/RAIN. THIS PART ALSO REVEALED A CORRODED VTA BEARING PN VTA04270.  A VISUAL GVI IN THE SUSPECT AREA CAN EASILY INDICATE A PROBLEM FOR CORROSION.  RECOMMENDATION: (1) GVI OF TORQUE TUBE ASSEMBLY IF THE AIRCRAFT IS STORED EXPOSED TO SALT AIR OR RAIN ON A ROUTINE BASIS. (2) GVI OF THE VTA BEARING.   IPC 27-302L72 4T    RTA5SW                         
20071205000182007120500018EA  2007       12         5          2007FA0001007    120071031G3246269A3245919     SKID                                    SCWZER269   269D        8059501EA  ALLSN 250C  250C30      03013GL                              LT MLG          DAMAGED         D      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      EA63411HU122                    0040                                    UPON LANDING THE HELICOPTER IN A SLIGHT FWD AND LT MOTION IN FLAT GRASS AREA HEARD SLIGHT CLICK OR CLUNK, PIC DIDN`T SEE ANY DAMAGE, PICKED UP AIRCRAFT TO A HOVER AND GROUND CREW SAW FWD END OF LT SKID TUBE HANGING BELOW THE AIRCRAFT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3U3  U0 4H12    E1GL                 
20071205000192007120500019CE  2007       12         5          2007FA0001008    120071029G2612991203611       FIRE LOOP                               CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              NR 1 ENGINE     FAILED          D      F   ACTIVATE FIRE EXT.                                                                              N  FALSE WARNING                                                                 CRCRUISE         1                      GL09189WW                       5605069                                 NR 1 ENGINE FIRE LOOP FAILED, CAUSING THE NR 1 ENGINE FIRE INDICATOR IN COCKPIT TO ERRONEOUSLY INDICATE A FIRE.  CREW FIRED BOTH FIRE EXTINGUISHERS FOR THE ENGINE WHICH DID NOT EXTINGUISH THE FIRE INDICATOR.  THE CREW THEN DECLARED AN IN-FLIGHT EMERGENCY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA22CE   E00059EN             
20071205000202007120500020SO  2007       12         5          2007FA0001009    120071003G3230757496          PIN             WIEBEL                  PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540*     41532EA                              LOWER CLEVIS    BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO0531NW 5912                   318152139                               EMERGENCY GEAR EXTENSION PUMP LOWER CLEVIS PIN BROKEN, FAILURE FOUND ON 2 SIMILAR AIRCRAFT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3O3  O  A20SO   E14EA                
20071205000212007120500021SO  2007       12         5          2007FA0001010    120071101G7810PA18ESA         PIPE                                    PIPER PA18  PA18150     7101828SO  LYC   O360  O360A1A     41514EA  MCAULY1A200 1A200FA     GL  EXHAUST         FAILED          G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL157066B                       185140      L76336                      LEADING EDGE EXHAUST SYSTEM INSTALLED BY STC SA02200AK FAILED AT THE SAIL PIPE TO MUFFLER WELD.  SYSTEM HAS 36 HOURS SINCE NEW.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  O  1A2     E286    5  NP874     
20071205000222007120500022SO  2007       12         5          2007FA0001011    220071025G8550SA56250         DRAIN                                   BBAVIA7     7EC         2110120SW  CONT  O200  O200*       17020SO                              ENGINE OIL      LEAKING         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      GL13274AC                       101407                                  INSTALLED QUICK DRAIN VALVE (OIL) ON NEW AIRCRAFT/ ENGINE.  AIRCRAFT FLEW APPROX 1 HR , INITIAL FLIGHT TEST.  VERY MINUTE OIL LEAK WAS NOTED FROM OIL QUICK DRAIN VALVE.  REMOVED VALVE TO FIND VALVE SNAP RING IN OIL DRAINED FROM ENGINE, ALSO FOUND O-RING SPLIT.  NOTE:  NO DAMAGE TO ENGINE OCCURRED. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  O  A759    E252                 
20071205000242007120500024CE  2007       12         5          2007FA0001012    120071030G2140HYLZ50336001    TRANSISTOR      BARBERCOL               BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A60A     52043NE                              TEMP CONTROL    FAILED          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL13200CJ           377OK       BB143                                   PC BOARD IN ASSY PN HYLZ50336-001 HAD FAILURE, BURNED/ OVERHEATED TRANSISTOR.  NOTE: FAN IN ASSY WAS WORKING.  PC BOARD PN HYLZ 105-001.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A24CE   E4EA                 
20071205000262007120500026CE  2007       12         5          2007FA0001013    120071105G2612991203611       FIRE LOOP                               CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              NR 1 ENGINE     FAILED          D      F   ACTIVATE FIRE EXT.                                                                              N  FALSE WARNING                                                                 CRCRUISE         1                      EA09189WW                       5605069                                 NR 1 ENGINE FIRE LOOP FAILED CAUSING THE NR 1 ENGINE FIRE INDICATOR IN COCKPIT TO ERRONEOUSLY INDICATE A FIRE.  CREW FIRED BOTH FIRE EXTINGUISHERS FOR THE ENGINE WHICH DID NOT EXTINGUISH THE FIRE INDICATOR.  THE CREW THEN DECLARED AN IN-FLIGHT EMERGENCY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA22CE   E00059EN             
20071205000272007120500027SO  2007       12         5          2007FA0001015    120071105G2797061E1P1E1       CONNECTOR                               GULSTMGV    GULFSTREAMGV3980116SO  RROYCEBR700 BR700710A110     NE                              RT FLAP RESOLVERCRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA11507QS                       625                                     BACK SHELL IS BROKEN/CRACKED AND SEPARATED FROM CONNECTOR PLUG ASSY.  POSSIBLE CAUSE IS WIRE BUNDLE TO CONNECTOR PLUG STRESSES AND PULLING ON BACK SHELL.  BACK SHELL IS MADE ON PLASTIC NOT METAL. IF BACK SHELL WAS MADE OF METAL IT WOULD HOLD UP AS A STRAIN RELIEF FOR THE ATTACHING WIRE BUNDLE.  IF A PLASTIC BACK SHELL IS CONTINUED TO BE USED, WIRE BUNDLE SHOULD ALLOW SLACK ENOUGH NOT TO STRAIN THE STRAIN RELIEF.  A METAL BACKSHELL IS THE MORE POSITIVE FIX FOR THIS PROBLEM.  (K)                                                                                                                                                                                                                                              2L72 4F4  FRTA12EA   E00057EN             
20071205000282007120500028EU  2007       12         5          2007FA0001016    120071106G5330                SKIN                                    AEROSPAS355 AS355F2     8680812EU  ALLSN 250C  250C20      03013GL                              FUSELAGE        WORN            B  UOHRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL13942MS6444                   5498                                    RT AND LT FUSELAGE SKIN AT TAILBOOM ATTACH BULKHEAD.  FOUND WORKING RIVETS ON BOTH SIDES. (40) FOUND SKIN UNDER WORKING RIVETS WORN .018. ASB 05-00-42 AS FACTOR.  FUSELAGE SENT TO A REPAIR FACILITY FOR SKIN REPLACEMENT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G72 3U3  U  H11EU   E4CE                 
20071205000292007120500029SW  2007       12         5          2007FA0001017    120070830G8120635630          TURBOCHARGER                            MOONEYM20   M20K        5870220SW  CONT  O520  TSIO520NB   17040SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW05231GZ959                    250253      8223022R                    FOUND APPROX 1.25 INCH CRACK IN TURBO CHARGER HOUSING BELOW EXHAUST INLET AT WELD.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3O3  O  2A3     E8CE                 
20071205000302007120500030EU  2007       12         5          2007FA0001018    120071024G2820                CONTROL UNIT                            AMD   FALC90FALCON900EX 2730009EU  GARRTTTFE731TFE731*     01518WP                              CROSSFEED       LEAKING         C      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA2547EG 903        B72992      154                                     FUEL LEAKING FROM CENTRAL LB CROSSFEED UNIT AND DRAIN TUBE CAP BROKEN. REF MFG SERVICE ADVISORY FSA900EX-EASY-28-10-03-R1.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L73 4F4  FRTA46EU   E6WE                 
20071205000342007120500034SO  2007       12         5          2007FA0001019    220071113G8530TISN712ACA      CYLINDER HEAD                           BEECH 55    D55         1152730CE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW0569RP 937                    TE766       282253R                     CRACKED CYL HEAD BEHIND INJECTOR BETWEEN FIN NR 12, NR 3.  DEFECTIVE MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3O3  O  3A16    E8CE                 
20071205000352007120500035SO  2007       12         5          2007FA0001020    220071113G8530TISN712ACA      CYLINDER HEAD                           BEECH 55    D55         1152730CE  CONT  O520  TSIO520EB   17040SO                              NR 3            CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW0569RP 937                    TE766       282253R                     CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3O3  O  3A16    E8CE                 
20071205000362007120500036SO  2007       12         5          2007FA0001021    220071113G8530TISN712ACA      CYLINDER HEAD                           BEECH 55    D55         1152730CE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW0569RP 937                    TE766       282253R                     CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3.  DEFECTIVE MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  3A16    E8CE                 
20071205000372007120500037SO  2007       12         5          2007FA0001022    220071113G8530TISN712ACA      CYLINDER HEAD                           BEECH 55    D55         1152730CE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW0369RP 937                    TE766       2822253R                    CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3.  DEFECTIVE MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  3A16    E8CE                 
20071205000382007120500038SO  2007       12         5          2007FA0001023    220071113G8530TISN712ACA      CYLINDER HEAD                           BEECH 55    D55         1152730CE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         C      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW0569RP 937                    TE766       282253R                     CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3.  DEFECTIVE MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  3A16    E8CE                 
20071205000392007120500039SO  2007       12         5          2007FA0001024    220071108G8530TISN712BCA      CYLINDER HEAD                           CESSNA402   402B        207590PCE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW054165G677                    402B1212    510771                      CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR1, NR3.  DEFECT IN MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3O3  O  A7CE    E8CE                 
20071205000402007120500040SO  2007       12         5          2007FA0001025    220071108G8530TISN712BCA      CYLINDER HEAD                           CESSNA402   402B        207590PCE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW054165G677                    402B1212    510771                      CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3.  DEFECT IN MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A7CE    E8CE                 
20071205000412007120500041SO  2007       12         5          2007FA0001026    220071108G8530TISN712BCA      CYLINDER HEAD                           CESSNA402   402B        207590PCE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW054165G677                    402B1212    510771                      CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3.  DEFECT IN MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A7CE    E8CE                 
20071205000422007120500042SO  2007       12         5          2007FA0001027    220071108G8530TISN712BCA      CYLINDER HEAD                           CESSNA402   402B        207590PCE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW054165G677                    402B1212    510771                      CRACKED CYL HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3O3  O  A7CE    E8CE                 
20071205000432007120500043SO  2007       12         5          2007FA0001028    220071107G8530TISN712BCA      CYLINDER HEAD                           CESSNA402   402B        207590PCE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW054165G677                    402B1212    510771                      CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR1, NR3.  DEFECT IN MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3O3  O  A7CE    E8CE                 
20071205000442007120500044SO  2007       12         5          2007FA0001029    220071113G8530TISN712ACA      CYLINDER HEAD                           BEECH 55    D55         1152730CE  CONT  O520  TSIO520EB   17040SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW0569RP 937                    TE766       282253R                     CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3.  DEFECTIVE MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  3A16    E8CE                 
20071205000462007120500046CE  2007       12         5          2007FA0001030    120071106G57405012007716      SUPPORT BRACKET                         BEECH 90    C90         1152913CE  PWA   PT6   PT6*        52043EA                              MLGWW           CRACKED         B  HSRRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM0528KP 6171                   LJ845                                   DRAG LEG SUPPORT BRACKETS FOUND CRACKED ON BOTH LT AND RT SIDES DURING A ROUTINE INSPECTION.  MOST LIKELY FATIGUE CRACKS OR A ROUGH LANDING.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 3T3  T  3A20    E2NE                 
20071205000472007120500047CE  2007       12         5          2007FA0001031    120071106G57405012007717      SUPPORT BRACKET                         BEECH 90    C90         1152913CE  PWA   PT6   PT6*        52043EA                              MLG WW          CRACKED         B  HSRRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM0528KP 6171                   LJ845                                   DRAG LEG SUPPORT BRACKETS FOUND CRACKED ON BOTH LT AND RT SIDES DURING A ROUTINE INSPECTION.  MOST LIKELY FATIGUE CRACKS OR A ROUGH LANDING.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 3T3  T  3A20    E2NE                 
20071205000492007120500049CE  2007       12         5          2007FA0001032    120071022G2120354021          DUCT                                    RKWELLNA265 NA26560     7630106CE  PWA   JT12  JT12A8      52042NE                              CABIN PRESSURE  DEFORMED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL1559K                         30682       P672922NB                   ATTACHING SLEEVE SLID OFF OF DUCT CAUSING LOSS OF PRESSURIZATION.  EMERGENCY PRESSURIZATION FUNCTIONED NORMALLY.  CLAMPS TIGHTENED TOO TIGHT AND DEFORMED FIBERGLASS DUCT.  RECOMMEND METAL SLEEVE BE INSTALLED TO ALLEVIATE DEFORMATION. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4J4  JRTA2WE    1E9                  
20071205000502007120500050SO  2007       12         5          2007FA0001033    120071106G531249099           BULKHEAD                                LUSCOM8     8F          8190114SO  LYC   O320  O320*       41508EA                              FUSELAGE        CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL159937B2115                   S41                                     DURING AN ANNUAL INSPECTION, FOUND AFT FUSELAGE BULKHEAD CRACKED AT TOP OF CUTOUT FOR ELEVATOR HORN.  50 PERCENT.  THIS IS WHERE THE VERTICAL AND HORIZONTAL STABILIZERS ATTACH.  THIS AREA IS HIDDEN BEHIND THE WEB OF THE VERTICAL STAB AFT SPAR AND WAS FOUND WHEN COMPONENTS WERE REMOVED TO REPAIR FWD SPAR (FOUND CRACKED) OF THE HORIZONTAL STAB.  THE VERTICAL STAB IS NOT OF THE ROUNDED TIP TYPE, HAS AN ALUMINUM FWD ATTACHMENT AND STEEL AFT ATTACHMENT.  (K)                                                                                                                                                                                                                                                                       1H71 3O3  O  A694    E274                 
20071205000512007120500051CE  2007       12         5          2007FA0001034    120070913G52301211673323      DOOR                                    CESSNA206   T206H       2073303CE  LYC   O540  TIO540AJ1A       EA                              RT AFT CARGO    MISRIGGED       D      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CE07168JS154                    T20608735                               MM (52-30-00 PG 201), (THE AFT DOOR IS HINGED AT FUSELAGE STA 112 AND IS A STRUCTURAL, LOAD CARRYING MEMBER WHEN CLOSED AND LOCKED).  REMOVED AFT CARGO DOOR ROYALITE AND TRIM TO GAIN ACCESS TO  LWR AFT CABIN LOWER HOOK ADJUSTMENT ROD.  THIS WAS DUE TO A CLUB MEMBER IMPROPERLY CLOSING THE DOOR AND BENDING THE ROD.  THE PERSON FAILED TO PULL-DOWN RED HANDLE WHEN CLOSING DOOR AND JAMMED THE LOWER HOOK.  HOWEVER, FOUND THE ADJUSTMENT RODS LOOSE(UPPER AND LOWER) AND WOULD EASILY TURN, INCLUDING THE TURNBUCKLES, UPPER AND LWR.  THIS WAS DUE TO THE JAM NUTS FOR THE TURNBUCKLES LOOSE AND/OR BACKED OFF TO WHERE THERE WERE BOTTOM OF THREADS ON THE ADJUSTMENT RODS FOR THE HOOKS.  IF LEFT UNADDRESSED COULD CAUSE PREVENTING1H71 3O3  ORTA4CE    E14EA                
20071205000532007120500053CE  2007       12         5          2007FA0001035    120071114G28200500106326      LINE                                    CESSNA180   180J        2072622CE  CONT  O470  O470*       17026SO                              FUEL SYS        MISROUTED       D      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      GL196WH  2365                   18052492                                (2) AILERON CABLES, (1) FLAP CABLE AND THE FUEL LINE ARE ALL ROUTED THROUGH THE LT LOWER AFT DOOR POST AREA.  THE FUEL LINE IS PROTECTED BY A PLASTIC SLEEVE BUT THE CABLE WORE THROUGH THE SLEEVE AND WAS WEARING INTO THE FUEL LINE.  THE LINE IS APPROX 20 INCHES LONG WITH (4) BENDS.  SUGGEST A (1) TIME INSPECTION IN CASE OTHER AC MIGHT HAVE THIS PROBLEM.  (K)                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  5A6     E273                 
20071205000542007120500054CE  2007       12         5          2007FA0001036    120071108G5610                WINDSHIELD                              CESSNA750   750         2076810CE  ALLSN AE3007AE3007C          GL                              COCKPIT         FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CE0393TX                        7500099                                 AC IN FLIGHT AND AT CRUISE ALTITUDE THE LT WINDSHIELD HEAT FAILED, A VISABLE SHORT OR ARCING AREA WAS SEEN, CONDITION OF UNIT MATCHED WITH SWITCH (OFF) 30 SEC LATER WINDSHIELD CRACKED IN A SPIDER WEB FASHION.  AC LANDED IN STL.  WINDSHIELD REPLACED BY SERVICE CENTER WITH A NEW STYLE WINDSHIELD PN 139731-1 (9914380-13).                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4J4  FRTT00007WITE6CH                
20071205000552007120500055    2007       12         5          2007FA0001037    120071101G3246                BEARING                                                                                                                                 NLG WHEEL       WRONG PART      B  SCSZK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA33                1170                                                ON OCT 10, INFORMED BY TECH THAT THEY HAD AN INSTALLED NOSEWHEEL (PN 277A6000-851, SN 1170) ON AIRCRAFT, WITH A WRONG BEARING INSTALLED.  IAW STS, THE ERROR WAS ONLY DISCOVERED AFTER THE WHEEL HAD BEEN INSTALLED, BUT BEFORE THE AC WAS RELEASED TO SERVICE.  REPORTED ERROR WAS THAT THE INNER BEARING DIAMETER  WAS 11MM TOO WIDE. ONCE WHEEL WAS RETURNED TO SHOP, INVESTIGATION SHOWED THAT A WRONG BEARING HAD BEEN INSTALLED.  INSTEAD OF THE CORRECT BEARING, A MD80 BEARING HAD BEEN INSTALLED.  INVESTIGATION OF THE ASSY PROCESS REVEALED NO DISCREPANCIES IN THE PROCESS ITSELF.  IT HAS THEREFORE BEEN JUDGED AS A HUMAN ERROR.  IN ORDER TO RAISE AWARENESS AMONG THE TECHNICIANS AND ENSURE PREVENTIVE MEASURES, THE PRODUCTION                                          
20071205000562007120500056SO  2007       12         5          2007FA0001038    120070828G781076048           GASKET                                  PIPER PA31  PA31P       7103120SO  LYC   O541  TIGO541E1A  41539EA                              EXHAUST         WRONG PART      D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE077325L                       31P7400206                              VISUALLY INSPECTED RT ENG AFTER RECOVERING THE A/C FROM A FIELD.  FOUND MELTED WIRING AT NR 6 CYLINDER AND BEHIND IT.  THE P-LEAD FOR THE RT MAG WAS MELTED AND WHEN TESTED FOUND TO BE SHORTED OUT.  THIS SHUT-OFF RT MAG.  THE NR 6 BOTTOM PLUG WIRE WAS HANGING LOOSE AND THE NUT ATTACHING LEAD TO THE PLUG WAS MELTED OFF. SEVERAL OTHER PLUG WIRES WERE BURNED AS WELL. CAUSE OF THIS DAMAGE WAS A BLOWN OUT EXHAUST GASKET ON NR 6 CYLINDER. WHEN THE GASKET BLEW OUT, HOT EXHAUST WAS ALLOWED TO BURN UP THE PLUG WIRES AND MAG P-LEAD.  P-LEAD THEN SHUT OFF THE RT MAG PROTECTIVE COATING WAS BURNED OFF.  SO NOW AT BEST, HAVE 1 MAG WORKING AND ONLY FIRING ON 5 CYLINDERS, AND A LARGE EXHAUST LEAK WHICH WILL LOWER MANIFOLD PRESS1L72 3O3  O  A8EA    E19EA                
20071204003432007120400343SO  2007       12         4          2007FA0001039    120071118G272162829003        SHAFT           PIPER                   PIPER PA28  PA28161     7102803SO  LYC   O320  O320*       41508EA                              RUDDER TRIM     SHEARED         C      D   RETURN TO BLOCK                                                                                 F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      EA15149LH1697                   2842192                                 THE RUDDER TRIM SHAFT ASSEMBLY'S SPRING RETAINING PIN SHEARED AT WELD, CAUSING HIGH LT RUDDER STIFFNESS AND PREVENTING THE NOSE WHEEL FROM BEING TURNED WITH TOW BAR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L71 3O3  O  2A13    E274                 
20071205000162007120500016EU  2007       12         5          2007FA0001040    220071108G7320057610E000201   FADEC                                   DIAMONDA42  DA42        2990004EU  THIELTTAE125TAE1250299       EU                                              MALFUNCTIONED   D      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      SO15490TS6                      42AC090     020201763                   DURING FLIGHT TRAINING MANEUVERS, SIMULATED SINGLE ENGINE OPERATIONS AT 5000 FT ASL, THE LT ENGINE WAS THROTTLED BACK TO FLIGHT IDLE (5 PERCENT POWER, THROTTLE RETARDED). UPON RETURN TO NORMAL POWER OPERATIONS THE LT ENGINE BEGAN TO SURGE FROM 20-100 PERCENT POWER, REGARDLESS OF THROTTLE POSITION, ENGINE WAS UNCONTROLLABLE.  THE LT ENGINE FADEC WAS SELECTED FROM ECU A TO ECU B AND CONTROL OF LT ENGINE WAS REGAINED. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. DISCREPANCY COULD NOT BE DUPLICATED DURING GROUND TESTS. LT ENGINE OPERATED NORMALLY ON BOTH ECU A AND ECU B OF THE LT FADEC. LT FADEC REPLACED AND AIRCRAFT RELEASED FOR TEST FLIGHT. NO FURTHER ENGINE SURGING NOTED.              1L72 3I3  BRTA57CE   E00069EN             
20071204003272007120400327NE  2007       12         4          2007FA0001042    220071115G7320RSA10AD1        FUEL CONTROL                            RHNFLUEXT300EA300L      70218DGEU  LYC   O540  AEIO540L1B5 41532NE                              ENGINE          MALFUNCTIONED   G      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      WP0551E  1759                   015         L2570748A                   THE AIRCRAFT EXPERIENCED AN INFLIGHT ENGINE SHUTDOWN RESULTING IN A FORCED LANDING ON THE BEACH. THE CAUSE OF THE INFLIGHT ENGINE SHUTDOWN WAS THE INTERNAL FAILURE OF THE FUEL SERVO.  THE FUEL SERVO WAS EVALUATED . THE FAILED UNIT WAS SENT TO THE MANUFACTURER FOR FURTHER EVALUATION. AFTER FURTHER INVESTIGATION THEY DETERMINED THE CAUSE OF THE INTERNAL FAILURE WAS DUE TO FOD ENTERING THE FUEL SERVO AND WORE AWAY AT THE REGULATOR ASSEMBLY. THE DIFINITIVE CAUSE IS STILL UNDER INVESTIGATION AT MFG.                                                                                                                                                                                                                             1M71 3O3  ONCEA67U   1E4                  
20071213002602007121300260CE  2007       12         13         2007FA0001043    120071024G32223908204080001   STOP                                    RAYTHN390   390         7150030CE                                                               NLG STRUT       DISTORTED       B  E81RO   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      GL03112CM                       RB123                                   PILOT REPORTED LANDING GEAR UNLOCKED INDICATION AFTER GEAR RETRACTION AFTER TAKEOFF.  FOUND NLG STOPPER ASSY DAMAGED AND PREVENTING NLG ASSY FROM CENTERING AND ENGAGING UPLOCK ASSY.  REPLACED STOPPER ASSY AFTER NLG DISASSEMBLY AND INSPECTION, LANDING GEAR OPERATIONS NORMAL.  REPORTED THAT AIRCRAFT WAS PREVIOUSLY TOWED WITH NLG TORQUE LINKS CONNECTED.  FLIGHT CREW, GROUND OPERATIONS, PERSONNEL AND TECHS SHOULD BE AWARE OF CORRECT PREMIER TOWING PROCEDURES AS SPECIFIED IN THE 390 MM, SEC 9-10-01-201.  (K)                                                                                                                                                                                                                    1L72 3F    RTA00010WI                     
20071213002612007121300261CE  2007       12         13         2007FA0001044    120071114G321012116013        CASTING                                 CESSNA206   T206H       2073303CE                                                               LT MLG          CRACKED         B  RDDRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM11     1250                   T20608075                               AIRCRAFT OPERATED ON MOSTLY UNIMPROVED AIRSTRIPS.  PART IS SAME AS 206F AND G MODELS.  PART IN QUESTION WAS INSTALLED AT TIME OF MFG OF AIRPLANE.  CASTING IS CRACKED IN (3) DIFFERENT LOCATIONS.  WE OPERATE NUMEROUS OF THESE AC AND HAVE A LONG HISTORY WITH 206 AIRCRAFT.  WE HAVE SEEN CRACKS OF THIS NATURE BEFORE, BUT RARELY WITH SO LITTLE TIME IN SERVICE.  (K)                                                                                                                                                                                                                                                                                                                                                                       1H71 3O    RTA4CE                         
20071213002802007121300280CE  2007       12         13         2007FA0001045    120071113G2420E3FF10300AA     ALTERNATOR                              CESSNA210   P210N       2073454CE  CONT  O520  TSIO520P    17040SO                                              FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      WP274814K     10                P21000332   513626                      DURING NIGHT IMC APPROACH, LOW VOLTAGE LIGHT ILLUMINATED AND BUS VOLTAGE DROPPED BELOW 24 VOLTS.  PILOT RECYCLED ALTERNATOR SWITCH BUT WAS UNABLE TO KEEP ALTERNATOR ON LINE.  PILOT REDUCED LOADS AND SUCCESSFULLY EXECUTED APPROACH AND LANDED WITHOUT INCIDENT.  CHARGING SYSTEM TROUBLESHOOT BY MECHANIC.  FOUND LATERNATOR OUTPUT TO BE 26 VOLTS UNLOADED, AND WITH 50 PERCENT LOAD ON BUSS, LATERNATOR VOLTAGE WOULD DROP BELOW 24 VOLTS.  NOTE: SECOND ALTERNATOR FAILURE IN 50 HOURS.  (K)                                                                                                                                                                                                                                              1H71 3O3  O  3A21    E8CE                 
20071213002812007121300281CE  2007       12         13         2007FA0001046    120071110G2420E3FF10300AA     ALTERNATOR                              CESSNA210   P210N       2073454CE  CONT  O520  TSIO520P    17040SO                                              FAILED          D      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      WP274814K     50                P21000332   513626                      DURING DAY VMC FLIGHT, LOW VOLTAGE LIGHT ILLUMINATED AND BUS VOLTAGE DROPPED BELOW 24 VOLTS.  PILOT MINIMIZED LOADS, DID A MANUAL GEAR EXTENSION, AND LANDED WITHOUT INCIDENT.  CHARGING SYSTEM TROUBLESHOOT BY MECHANIC.  FOUND ALTERNATOR OUTPUT TO BE 26 VOLTS UNLOADED, AND WITH 50 PERCENT LOAD ON BUS, ALTERNATOR VOLTAGE WOULD DROP BELOW 24 VOLTS.  NOTE: ALTERNATOR OVERHAULED.  (K)                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  O  3A21    E8CE                 
20071213002822007121300282CE  2007       12         13         2007FA0001047    120071107G2910632701617       LINE                                    CESSNA525   525A        2076615CE  WILINTFJ44  FJ442A           GL                              HYDRAULIC SYS   SEPARATED       B  RO3RK   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CE03361JR                       525A0361                                FOUND FLAP RETRACT LINE SEPARATED FROM BACK OF B-NUT.  SYSTEM FLUID WAS LOST.  SUSPECT DEFECT WAS AT TIME OF MANUFACTURE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 4F4  FRTA1WI    E3GL                 
20071213002832007121300283CE  2007       12         13         2007FA0001048    120070911G321012116013        CASTING                                 CESSNA206   T206H       2073303CE                                                               MLG             CRACKED         B  RDDRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM11     1776                   T20608105                               AIRCRAFT OPERATED ON MOSTLY UNIMPROVED AIRSTRIPS.  PART IS SAME AS 206F AND G MODELS.  PART IN QUESTION WAS INSTALLED AT TIME OF MFG OF AIRPLANE.  CASTING CRACKED AND FAILED UPON LANDING.  AFT BOLT ALSO WAS CRACKED AND SHEARED.  LANDING WAS A NORMAL APPROACH AND LANDING.  GEAR LEG BROKE LOOSE FROM OB CASTING AND PUSHED BACKWARDS, PINCHING BRAKE LINE AND LOCKING UP LT BRAKE.  (K)                                                                                                                                                                                                                                                                                                                                                   1H71 3O    RTA4CE                         
20071213002732007121300273NE  2007       12         13         2007FA0001050    220071127G7261                ENGINE                                  BEECH MU300 400BEECH           CE  PWA   JT15  JT15D5      52112NE                              NR 1            LEAKING         E      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  DEDESCENT        1                      SO118HQ                         RJ50        100151                      ON THE DECENT, THE CREW HAD AN OIL PRESSURE LOW LIGHT AT THAT TIME THE CREW OBSERVED THE OIL PRESSURE GAUGE WAS INDICATING LOW PRESSURE. THE CREW SHUTDOWN THE NR 1 ENGINE DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. UPON INSPECTION BY MAINTENANCE IT WAS FOUND THAT THE OIL FILL CAP WAS NOT PROPERLY LATCHED DOWN AND THAT OIL HAD LEAKED OUT OVER THE COURSE OF THE FLIGHT. DO TO THE AMOUNT OF OIL MISSING FROM THE OIL TANK THE ENGINE IS BEING REMOVED FOR FURTHER INSPECTION.                                                                                                                                                                                                                                                      2H72 4F4  FRTA16SW   E25EA                
20071213003152007121300315SO  2007       12         13         2007FA0001051    120071130G3220                SPRING                                  LUSCOM8     8A          8190104SO  CONT  A65   A65*        17003SO                              TAIL WHEEL      BROKEN          G      D   RETURN TO BLOCK                                                                                 D  INFLIGHT SEPARATION                                                           TOTAKEOFF        1                      SO092099K2826                   4826        6153488                     ON TAKEOFF ROLL AND BEFORE ROTATION, THE TAILSKID SPRING ASSEMBLY BROKE AND THE TAIL WHEEL, CONNECTED TO THE FUSELAGE BY THE CONNECTOR SPRINGS, CAME TO REST ON TOP OF THE ELEVATOR AND WEDGED ITSELF AGAINST THE RUDDER, EFFECTIVELY JAMMING IT IN PLACE, CAUSING THE AIRCRAFT TO YAW 30 TO 40 DEGREES AND CREATED AN EXTREME SIDE SLIP NOT ALLOWING THE AIRCRAFT TO CLIMB.                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  O  A694    E205                 
20071213003202007121300320EU  2007       12         13         2007FA0001052    120071115G3250                STEERING SYS                            AMTR  EVKTORSPORTSTAR   0600012EU  ROTAX 912   ROTAX912ULS 55172EU                              NLG             SENSITIVITY     D      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      NM03617EV                       20071001                                AFTER A NORMAL LANDING, CFI (WITH 80 HOURS IN TYPE) AND STUDENT (WITH 1.2 HOURS IN TYPE) LOST CONTROL OF THE AIRCRAFT, EXITED THE RUNWAY, AND CAME TO REST IN A DRAINAGE DITCH.  THEY STATED THAT THE EXTREME SENSITIVITY OF THE NOSEWHEEL STEERING LED TO PILOT INDUCED OSCILLATIONS THAT GREW PROGRESSIVELY WORSE UNTIL THE AIRPLANE WAS COMPLETELY UNCONTROLLABLE.  THE SENSITIVITY OF THE NOSEWHEEL STEERING IS A COMMON COMPLAINT, AND HAS BEEN CITED IN SEVERAL OTHER INCIDENTS.                                                                                                                                                                                                                                                          1L71 3O3  ONTEXPA1L71EXPE3O               
20071213003172007121300317SO  2007       12         13         2007FA0001053    220071130G8510641909          LOCK PLATE                              CESSNA421   421B        2076014CE  CONT  O520  GTSIO520*   17032SO                              CRANKSHAFT      MISSING         D      H   DEACTIVATE SYST/CIRCUITS                                                                        JF WARNING INDICATION        FLT CONT AFFECTED                                   CRCRUISE         1                      SO15707DT65   65    HO13474     421B0468    218370R                     THIS ENGINE WAS REMOVED ON AUGUST 31, 2007, HOBBS TIME 1523.9 DUE TO CRACKED ENGINE CASE. THE ENGINE WAS SENT TO RAM AIRCRAFT FOR REPAIR. RAM REPAIRED THE ENGINE ON SEPT 20, 2007. THIS ENGINE WAS REINSTALLED BACK ON THE AIRCRAFT. DURING A NIGHT FLIGHT ON NOVEMBER 20, 2007 THE PILOT HAD AN ALTERNATOR FAILURE. HE REPORTED THE PROBLEM THE NEXT DAY. UPON INSPECTION OF THE ALTERNATOR, IT WAS FOUND IN PIECES, WITH THE MOUNT HOUSING STILL ATTACHED TO THE ENGINE. THE INSIDE OF THE ALTERNATOR INSTALLATION HOLE WAS INSPECTED.THE INSPECTION REVEALED THAT THE ATTACH BOLTS ON THE ALTERNATOR FACE GEAR HAD NO TAB LOCK PLATES INSTALLED. THE ATTACH BOLTS CAME LOOSE AND DAMAGED THE ENGINE AND ALTERNATOR. RAM AIRCRAFT WAS NOTIFIE1L72 3O3  O  A7CE    E7CE                 
20071213003412007121300341SO  2007       12         13         2007FA0001054    220071121G8530TISN712ACA      CYLINDER HEAD                           BEECH 36    36BEECH     1151602CE  CONT  O520  IO520BA     17032SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW051194A785                    E159        807201R                     CRACKED BEHIND INJECTOR BETWEEN FIRST AND THIRD FIN.  SAME AS ALL THE OTHERS.  THE (NEW) E-SERIES CYLINDER HEAD IS DEFECTIVE. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O3  O  3A15    E5CE                 
20071213003422007121300342SO  2007       12         13         2007FA0001055    220071121G8530TISN712ACA      CYLINDER HEAD                           BEECH 36    36BEECH     1151602CE  CONT  O520  IO520BA     17032SO                              ENGINE          CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW051194A901                    E159        807201R                     CYLINDER HEAD CRACKED BEHIND INJECTOR BETWEEN FIN NR 1 AND 3.  DEFECTIVE MFG PROCESS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  O  3A15    E5CE                 
20071213003432007121300343CE  2007       12         13         2007FA0001056    120071113G2450                CIRCUIT BREAKER                         CESSNA172   172R        2072401CE  LYC   O360  IO360A1A    41514EA                                              INOPERATIVE     D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM0224442251                    17280862                                PILOT SQUAWKED ON INTERMITTENT SWITCH.  THE SWITCH WAS DISASSEMBLED AND INSPECTED.  THE BONDED INTERNAL CONDUCTOR HAD SEPARATED FROM CONTACTOR.  A TOTAL OF 20 SWITCHES IN OUR FLEET, HAVE ALREADY BEEN REPLACED.  UPON INSPECTION, NUMEROUS SWITCHES HAD SIMILAR PROBLEMS INTERNALLY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  ONT3A12    1E10                 
20071213003462007121300346EA  2007       12         13         2007FA0001057    220071127G741406058002        BOOSTER                                 PIPER PA28  PA28R200    7102811SO  LYC   O360  IO360C1C    41514EA                              MAGNETO         SHORTED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP251473T                       28R7235300  RL1904551A                  PILOT REPORTED ROUGH ENGINE; IGNITION SYSTEM TROUBLESHOOT FOUND START MAGNETO STARTER BOOSTER INTERNALLY SHORTED, GROUNDING MAGNETO P-LEAD CAUSING MAGNETO FAILURE.  REMEDIED BY REMOVING START FROM AIRCRAFT AND MAGNETO OPERATING NORMALLY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  2A13    1E10                 
20071213003642007121300364CE  2007       12         13         2007FA0001058    120071204G2497                CONNECTOR                               BEECH 100   A100        1152915CE  PWA   PT6   PT6A60A     52043NE                              ELECTRICAL      ARCED           B      A   UNSCHED LANDING                                                                                 BH SMOKE/FUMES/ODORS/SPARKS  ELECT. POWER LOSS-50 PC                             CLCLIMB          1                      GL072340410027                  B234                                    PARTIAL ELECTRICAL POWER LOSS TO COMPONENTS FROM RT NR 1 AND NR 2 SUBPANEL CIRCUIT BREAKERS.  FOUND RT CIRCUIT PANEL CONNECTOR SOCKET MODULE AND SOCKET RT 1B BURNED.  REPLACED MODULE (NR 8 WIRE-4 SOCKET) AND 4 SOCKETS.  REPLACED PINS (4).  FUNCTION CHECK SATISFACTORY.  SUGGEST THESE HEAVY WIRE CONNECTIONS BE CHECKED MORE CLOSELY ON THE OLDER AIRCRAFT. THIS PARTICULAR AIRCRAFT IS 30 YEARS OLD.                                                                                                                                                                                                                                                                                                                                     1L72 3T4  T  A14CE   E4EA                 
20071213003272007121300327NM  2007       12         13         2007FA0001060    120071203G3060SMR6201         STRAP                                   COLUMBLC41  LC41550FG4005150011NM  CONT  O550  TSIO550C         SO  HARTZLHCC3Y HCC3YF1     GL  PROPELLER DEICE DEBONDED        D      K   NONE                                                                                            G  MULTIPLE FAILURE                                                              ININSP/MAINT     1                      SW07969GM266                    41616                   LX163B          PROPELLER DEICE BOOT RETAINER STRAP DEBONDED OVER HALF OF THE BLADE CIRCUMFERENCE.  OTHER (2) BLADES DEBONDED ABOUT .3.  THIS STRAP HOLDS THE IB END OF THE DEICE BOOT AND TRIES TO KEEP THE LONG DEICE LEADS FROM PULLING UP THE BOOT.  THE PROP DEICE BOOT BEGINS TO COME LOOSE AFTER THE STRAP DEBONDS.  THE RETAINER STRAPS NEED TY-RAPS TO HOLD THE LEADS, AS IS COMMON PRACTICE ON OTHER PROPELLERS.                                                                                                                                                                                                                                                                                                                                      1L71 3O3  ONTA00003SEE5SO    5  CP25EA    
20071214002902007121400290EU  2007       12         14         2007FA0001061    120071203G2435                COMMUTATOR      BFGOODRICH              PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE                              STARTER GEN     FAILED          B      BA  EMER. DESCENT           UNSCHED LANDING                                                         HE ELECT. POWER LOSS-50 PC   VIBRATION/BUFFET                                    CRCRUISE         1                      CE07462PC           97102       462         PCEPR0336                   DURING CRUISE FLIGHT, LOUD NOISE FROM ENGINE COMPARTMENT FOLLOWED BY VIBRATION AND LOSS OF PRIMARY ELECTRICAL POWER.  UPON INSPECTION, ONE SEGMENT FROM COMMUTATOR WAS MISSING AND AFT END OF GENERATOR AND BRUSHES HAD SUSTAINED HEAVY DAMAGE.  AFTER REPLACEMENT WITH OVERHAULED UNIT, NO ABNORMALITIES WERE NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                           1L71 3T4  TRTA78EU   E26NE                
20071214003352007121400335CE  2007       12         14         2007FA0001066    120071119G2751100TA1966N4     TRANSMITTER                             BEECH MU300 400A        1155402CE                                                               TE FLAPS        INOPERATIVE     B  E81RK   NONE                                                                                            N  FALSE WARNING                                                                 ININSP/MAINT     1                      GL03420CT                       RK517                                   TROUBLESHOT IN-FLIGHT (FLAP ASSYMETRY) ANNUNCIATOR INDICATION.  FOUND RT FLAP POSITION TRANSMITTER RESISTANCE TO GO ABOVE SERVICE LIMITS WHEN COLD SOAKED.  REPLACED RT FLAP POSITION TRANSMITTER AND ADJUSTED LT , RT FLAP FOLLOW-UP SWITCHES AND POSITION TRANSMITTER RIGGING AS REQUIRED.  VERIFIED FLAP SYSTEM RIGGING CABLE TENSIONS WITHIN SERVICE LIMITS.  FLAP SYS FUNCTIONAL TESTS OK.  SUGGEST MFG INVESTIGATE CURRENT PRODUCTION TRANSMITTER ASSY FOR QC OR MOISTURE INGRESS FAULTS.  HBC PN 45AS86805-031, MFG DATE 8/07/2006.  (K)                                                                                                                                                                                                 2H72 4F    RTA16SW                        
20071214003372007121400337CE  2007       12         14         2007FA0001067    120071119G783064760           CONTROL VALVE                           BEECH MU300 400A        1155402CE                                                               THRUST REVERSER MALFUNCTIONED   B  E81RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03420CT                       RK517                                   TROUBLESHOT INOPERATIVE THRUST REVERSER DEPLOYMENT.  FOUND LT, RT REVERSERS MECHANICALLY STIFF AND DIFFICULT TO OPERATE.  THRUST REVERSER LINKS AND PIVOTS FOUND DRY, INITIAL 400 HR LUBRICATION NOT DUE FOR 55 HRS.  LUBED REVERSERS IAW MM.  12-20-00, VERIFIED OPERATIONS OK.  FOUND LT REVERSER NOT DEPLOYING UNTIL AFTER RT DEPLOYED.  REPLACED LT CONTROL VALVE, OPERATIONAL CHECKS NORMAL.  SUGGEST ALL THRUST REVERSER LUBES BE COMPLIED WITH AT 200 HR INITIAL INSPECTION.  SUGGEST MFG INVESTIGATE CNTRL VALVE FOR POSSIBLE QUALITY CONTROL OR SYSTEM CONTAMINATION ISSUES.  (K)                                                                                                                                                      2H72 4F    RTA16SW                        
20071214003392007121400339CE  2007       12         14         2007FA0001068    120071111G2730MS250836BB5     BONDING JUMPER                          BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              ELEVATOR        FRAYED          B  E81RO   OTHER                                                                                           O  OTHER                                                                         ININSP/MAINT     1                      GL03400MV1596                   RK286                                   TROUBLESHOT REPORT OF HORIZONTAL STABILIZER ANTI-ICE SYSTEM FAIL INDICATION.  NOTED ELEVATOR HORN HEAT SYSTEM RESISTANCE READINGS ERRATIC WHEN ELEVATORS MOVED.  FOUND ELEVATOR BONDING JUMPERS FRAYED AND CORRODED.  REPLACED ELEVATOR BONDING JUMPERS, ELEVATOR HORN HEATER RESISTANCE READINGS NOW WITHIN SERVICE LIMITS.  HORIZONTAL STABILIZER ANTI-ICE SYSTEM TESTS IAW MM 30-12-00 NORMAL, NO FAULTS INDICATED.  RECOMMEND TECH/INSP NOTE CONDITION OF ELEVATOR BONDING JUMPERS CLOSELY DURING SCHEDULED INSPECTIONS AND REPLACE JUMPERS WHEN DETERIORATION EVIDENT.  (K)                                                                                                                                                                2H72 4F4  FRTA16SW   E25EA                
20071214003412007121400341NE  2007       12         14         2007FA0001069    220071111G7230                PIPE                                    BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              GAS GENERATOR   CRACKED         B  E81RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03400MV           A000*LNX    RK286                                   PERFORMED HOT SECTION INSPECTION PRIOR TO SCHEDULED 1800 HR INTERVAL TO INVESTIGATE COMPLAINT OF SLOW STARTING.  UPON DISASSEMBLY, FOUND DIFFUSER PIPES OF GAS GENERATOR CASE CRACKED AND PORTIONS MISSING AT APPROXIMATE 10:30, 11:00 POSITION.  SUSPECT CAUSED BY STREAKING FUEL NOZZLES WITH COKED-UP TIPS FROM LOW IDLE OPERATION WITH EFC OFF.  PILOTS AND TECH SHOULD BE AWARE OF MONITORING ENGINE RPM DURING TAXING OPERATIONS WITH EFC TURNED-OFF.  (K)                                                                                                                                                                                                                                                                                2H72 4F4  FRTA16SW   E25EA                
20071214003492007121400349CE  2007       12         14         2007FA0001070    120071201G2420AC2101          CONTROL UNIT                            CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  ALTERNATOR      FAILED          C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP252472J215                    172S10072   L3240751E   ZK23029         THE AIRCRAFT FACTORY INSTALLED ACU BEGAN FAILING AT 200 HOURS (INTERMITTENT ALTERNATOR DROPPING (OFF LINE) FOR A FEW SECONDS) (ON ONE OCCASION, THE FIELD CB DISENGAGED)  A NEW ACU WAS INSTALLED AT 215.9.  AT 246.1 THE SAME PROBLEM SURFACED, AND THE THIRD ACU WAS INSTALLED.  THE SERVICE CENTER HAS HAD THE SAME PROBLEM WITH OTHER AC.  (K)                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A12    1E10    5  NP857     
20080108003472008010800347CE  2008       1          8          2007FA0001072    120071208G2751                WARNING SYSTEM                          CESSNA310   310K        2074228CE                                                               T/E FLAP        MALFUNCTIONED   E      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CRCRUISE         1                      SO11418GJ                       310K0067                                AC EXPERIENCED FLAP ASYMMETRIC LIGHT IN CRUISE FLIGHT CREW DIVERTED TO ATL LIGHT WENT OUT AND FLAPS WORKED PROPERLY FOR AN UNEVENTFUL LANDING. PROBLEM COULD NOT BE DUPLICATED SO BOTH FLAP FOLLOW UPS WERE REPLACED IAW THE MM. AIRCRAFT OPS CHECK GOOD.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3O      3A10                         
20080108003502008010800350SO  2008       1          8          2007FA0001073    120071211G321167042013        TRUNNION                                PIPER PA44  PA44180     7104402SO                                                               RT MLG          CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP07570ER4145                   4496146                                 RT AFT MAIN TRUNNION CASTING, P/N 67042-013, FOUND TO BE CRACKED DURING INSPECTION.  THIS IS A NEARLY IDENTICAL CRACK TO ONE FOUND AUGUST 2006 ON A SISTER SHIP.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3O      A19S0                        
20071214003442007121400344SO  2007       12         14         2007FA0001074    120071130G2720                CONTROL SYSTEM                          PIPER PA34  PA34220T    7103420SO  CONT  O360  TSIO360*    17025SO                              RUDDER          SEIZED          C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO11557C                        3449247                                 WITH FULL RT RUDDER TRIM, RT RUDDER FOR HARD CLIMBING RT TURN, RUDDER FROZE WITH FULL RT DEFLECTION.  RUDDER CABLE TURNBUCKLE IN TAIL SECTION WAS (CAUGHT) UNDER BULKHEAD TOP EDGE CAUSING RUDDER TO FREEZE IN FULL RT DEFLECTION - DESPITE SIGNIFICANT LT RUDDER PRESSURE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A7SO    E9CE                 
20080108003562008010800356CE  2008       1          8          2007FA0001075    120071212G2730053200135       ADAPTER                                 CESSNA172   172E        2072412CE  CONT  O300  O300*       17022SO                              LT ELEVATOR     WORN            G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM073901S6491                   17251101                                LT ELEVATOR TORQUE TUBE ARM ADAPTER RIVET HOLES WERE WORN POSSIBLY DUE TO UNSECURED CONTROLS IN GUSTY WINDS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  ONT3A12    E253                 
20080108003712008010800371    2008       1          8          2007FA0001076    220071215G741410357586        DISTRIBUTOR GEARCONT                                                                                                                    MAGNETO         LOOSE           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15     500  500                                                       500-HOUR INSPECTION PERFORMED ON BOTH MAGNETOS REMOVED FROM. FOUND AXLE CRIMPED WASHER LOOSE ON SHAFT AND WORN TO THE POINT OF FALLING OFF GEAR. THIS IS THE SECOND TIME THIS CONDITION HAS BEEN FOUND ON MAGNETOS USING THIS GEAR. TTS NEW 500 AND 580.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  
20080108003722008010800372    2008       1          8          2007FA0001077    220071215G741410357586        DISTRIBUTOR GEARCONT                                                                                                                    MAGNETO         LOOSE           D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15     500  500                                                       500-HOUR INSPECTION PERFORMED ON BOTH MAGNETOS REMOVED. FOUND AXLE CRIMPED WASHER LOOSE ON SHAFT AND WORN TO THE POINT OF FALLING OFF GEAR. THIS IS THE SECOND TIME THIS CONDITION HAS BEEN FOUND ON MAGNETOS USING THIS GEAR. TTSNEW 500 AND 580.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        
20080108003672008010800367EU  2008       1          8          2007FA0001078    120071214G3230PNDIN47108VE    RETAINING CLIP  DIAMON                  DIAMONDA42  DA42        2990004EU                                                               LT MLG          MISSING         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15904ER100  2                 42281                                   DURING PREFLIGHT THE PILOT NOTICED THAT THE LMG DOWNLOCK PIN (P/N-D60-3237-11-34) HAD NO RETAINING CLIP(P/N-DIN471-08-VERZ) AND HAD SHIFTED AFT. THE FORWARD DOWNLOCK HOOK WAS COVERING ONE HALF OF THE HOLE SINCE THERE WAS NO PIN TO STOP ITS MOVEMENT. THE REMAINING CLIP BROKE IN HALF WHEN IT WAS REMOVED. IT APPEARED TO BE BRITTLE. A NEW PIN WAS INSTALLED WITH NEW CLIPS. THOSE CLIPS HAD MORE SPRING TO THEM. ALSO, THE GROOVES IN THE PIN ARE VERY SHALLOW.                                                                                                                                                                                                                                                                          1L72 3I    RTA57CE                        
20080108003682008010800368EU  2008       1          8          2007FA0001079    120071214G3230PNDIN47108VE    RETAINING CLIP  DIAMON                  DIAMONDA42  DA42        2990004EU                                                               LT MLG          MISSING         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15904ER100  2                 42281                                   DURING PREFLIGHT THE PILOT NOTICED THAT THE LMG DOWNLOCK PIN (P/N-D60-3237-11-34) HAD NO RETAINING CLIP(P/N-DIN471-08-VERZ) AND HAD SHIFTED AFT. THE FORWARD DOWNLOCK HOOK WAS COVERING ONE HALF OF THE HOLE SINCE THERE WAS NO PIN TO STOP ITS MOVEMENT. THE REMAINING CLIP BROKE IN HALF WHEN IT WAS REMOVED. IT APPEARED TO BE BRITTLE. A NEW PIN WAS INSTALLED WITH NEW CLIPS. THOSE CLIPS HAD MORE SPRING TO THEM. ALSO, THE GROOVES IN THE PIN ARE VERY SHALLOW.                                                                                                                                                                                                                                                                          1L72 3I    RTA57CE                        
20080108003852008010800385SO  2008       1          8          2007FA0001080    120071115G3213653319004       CYLINDER                                PIPER PA28  PA28181     7102807SO  LYC   O360  O360A4M     41514EA                              RT MLG          FAILED          D      K   NONE                                                                                            O  OTHER                                                                         TXTAXI/GRND HDL  1                      SW178218Z11743                  288090320                               RT M/G CYLINDER FAILED AT THE UPPER TORQUE LINK ATTACH LUGS WHILE TAXIING FROM THE ACTIVE RUNWAY: THE AIRCRAFT  (SINCE NEW) IS USED FOR FLIGHT TRAINING IN A 141 FLIGHT SCHOOL.  THE PREMATURE FAILURE OF THE CYLINDER WAS PROBABLY CAUSED BY A HARD LANDING.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  2A13    E286                 
20080108003872008010800387WP  2008       1          8          2007FA0001081    120070926G792120006A          OIL COOLER                              ROBSINR22   R22ALPHA    7640104WP  LYC   O320  O320B2C     41508EA                                              CRACKED         D      A   UNSCHED LANDING                                                                                 K  FLUID LOSS                                                                    NRNOT REPORTED   1                      EA1197CP                        0421        L1414339A                   AT A 100 HR INSPECTION ON HELICOPTER, INSTALLED A NEW OIL COOLER REPLACING THE ORIGINAL OIL COOLER.  (NOVEMBER 5, 2007, HOUR METER 1042) WHILE FLYING, NOTICED THE OIL TEMPERATURE RISING AND THE OIL PRESSURE DROPPING.  MADE AN UNSCHECULED LANDING AND DISCOVERED THE TAILBOOM COVER WITH ENGINE OIL.  TRACED THE OIL BACK TO THE OIL COOLER, REMOVED OIL COOLER AND PRESSURE TESTED IT AND FOUND A .7500 INCH CRACK IN THE COOLER CORE.  (TT 16.8 HOURS) (K)                                                                                                                                                                                                                                                                                1G71 3O3  O  H10WE   E274                 
20080108003882008010800388CE  2008       1          8          2007FA0001082    120070926G5320                BRACKET                                 CESSNA441   441         2076020CE  GARRTTTPE331TPE331*     01514WP                                              CRACKED         D  OF1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA17731BH                       4410360                                 FOUND BROKEN T-BRACKET DURING ROUTINE 2, 3, D INSPECTION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3T3  TRTA28CE   E2WE                 
20080108003892008010800389CE  2008       1          8          2007FA0001083    120070927G5350581201412       TAIL CONE                               CESSNA441   441         2076020CE  GARRTTTPE331TPE331*     01514WP                                              CRACKED         D  OF1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA17731BH7779                   4410360                                 FOUND CRACK DURING ROUTINE 2,3,D PHASE INSPECTION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3T3  TRTA28CE   E2WE                 
20080108003932008010800393CE  2008       1          8          2007FA0001084    120071109G57533516505084      NOSE RIB                                BEECH 95    B95         1153404CE  LYC   O360  O360A1A     41514EA                              T/E FLAP        CRACKED         B  OF1RK   NONE                                                                                            O  OTHER                                                                         CRCRUISE         1                      EA179349Y4288                   TD445       L421536                     IN-FLIGHT, PILOT LOWERED FLAPS AND AIRCRAFT STARTED TO ROLL TO THE RT.  PILOT NOTICED RT FLAP WAS RETRACTED, HE THEN RETRACTED FLAP HANDLE.  AIRCRAFT LANDED SAFELY, WITHOUT INCIDENT.  UPON INSPECTION, FOUND RT FLAP ROD ATTACH BRACKET BROKEN AND FLAP NOSE RIB NUTPLATE FLANGE TORN.  INSPECTED LT SIDE AND FOUND NOSE RIB FLANGE AND WEB CRACKED.  (K)                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  3A16    E286                 
20080109003872008010900387CE  2008       1          9          2007FA0001085    120071109G57533516505084      NOSE RIB                                BEECH 55    D55         1152730CE  CONT  O520  IO520C      17032SO                              T/E FLAP        CRACKED         B  OF1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA17810WA4552                   TE486       267930R                     AT ANNUAL INSPECTION, FOUND CRACKED FLAP ROD ATTACH POINT RIB.  RT FLAP ONLY.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 3O3  O  3A16    E5CE                 
20080109003882008010900388CE  2008       1          9          2007FA0001086    120071109G57533516505084      NOSE RIB                                BEECH 36    A36         1151604CE  CONT  O550  IO550B           SO                              T/E FLAP        CRACKED         B  OF1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA1720TC 3144                   E873        281740R                     AT ANNUAL INSPECTION FOUND BOTH LT AND RT FLAP ATTACH POINT RIBS CRACKED. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  O  3A15    E3SO                 
20080109003892008010900389CE  2008       1          9          2007FA0001087    120071109G57533516505084      RIB             BEECH                   BEECH 35    V35B        1151548CE  CONT  O520  IO520BA     17032SO                              T/E FLAP        CRACKED         B  OF1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA174475S4248                   D9775       280904R                     AT ANNUAL INSPECTION FOUND RT FLAP ROD ATTACH POINT RIB CRACKED. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3O3  O  3A15    E5CE                 
20080109003902008010900390CE  2008       1          9          2007FA0001088    120071109G57533516505084      RIB             BEECH                   BEECH 95    95B55       1152729CE  CONT  O520  IO520E      17032SO                              T/E FLAP        CRACKED         B  OF1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA17127RW4421                   TC1958      215825R                     AT ANNUAL INSPECTION FOUND CRACK ON FLAP RIB.  (FLAP ROD ATTACH POINT) BOTH LT AND RT FLAPS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 3O3  ORT3A16    E5CE                 
20080109003912008010900391CE  2008       1          9          2007FA0001089    120071109G57533516505084      RIB             BEECH                   BEECH 33    F33A        1151425CE  CONT  O550  IO550B           SO                              T/E FLAP        CRACKED         B  OF1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA1789AU 5255                   CE1129      675607                      AT ANNUAL INSPECTION, FOUND RT FLAP ROD ATTACH POINT RIB CRACKED.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3O3  O  3A15    E3SO                 
20080110000242008011000024GL  2008       1          10         2007FA0001090    120071126G7160                CONTROL ARM                             DIAMONDA40  DA40        2990002GL  LYC   O360  O360A4M     41514EA                              AIRBOX          BROKEN          C  GO3SK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM07423FP28                     40FC023                                 CARBURETOR HEAT CONTROL ARM BROKEN OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE.  RECOMMEND INSTALLED THICKER MATERIAL ON CARB HEAT CONTROL ARM LEVER.  DIFFERENT WELDING PROCESS, OR DIFFERENT ATTACHMENT PROVISION ALTOGETHER.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O3  ONTA47CE   E286                 
20080110001312008011000131NM  2008       1          10         2007FA0001091    120070525G2761252T13021       MANIFOLD                                BOEING767   767*               NM                                                               SPOILERS        FRACTURED       D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP01                                                                    MANIFOLD CRACKED IN THE FILTER BOWL AS DESCRIBED IN BETWEEN WHAT IS DESCRIBED IN THE SERVICE LETTER AND THIS UNIT FRACTURED COMPLETELY.  VISUAL INSPECTION APPEARS TO SHOW THAT THE CRACK ORIGINATED IN THE THREAD ROOT AT THE THINNEST AREA OF THE HOUSING.  THE CRACK PROPAGATED UNTIL THERE WAS DUCTILE OVERLOAD FAILURE OF THE HOUSING.  (K)                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RTA1NM                         
20080111000052008011100005SO  2008       1          11         2007FA0001092    120071130G2530243185502       OVEN                                    GULSTMGVSP  GVSPG550    3980203SO  RROYCEBR700 BR700710A110     NE                              GALLEY          FAILED          B      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      EA11607PM105                    5146                                    FLIGHT CREW REPORTED THE ODOR OF ELECTRICAL SMOKE IN THE GALLEY.  THE ODOR WAS COMING FROM THE OVEN, THEN THE OVEN CB OPENED (POP).  THE OVEN WAS REMOVED AND REPLACED WITH A NEW UNIT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA12EA   E00057EN             
20080111000082008011100008EA  2008       1          11         2007FA0001094    120071211G2520                SEAT BACK                               DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA                              SEAT            BROKEN          B  SCIRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM07252SA           1691        614         PCE50502                    BOTH LOWER SEAT BACK BRACES BROKE JUST ABOVE THE WELDS, ABOVE WHERE THE FLANGE BOLTS ON TO THE SEAT BOTTOM.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H72 3T4  TRTA9EA    E4EA                 
20080109003932008010900393    2008       1          9          2007FA0001095    420071218G316070000006003     DISPLAY                                 PIPER PA46  PA46500TP   7104622SO  GARRTTTPE331TPE33111U   01514WP                              COCKPIT         MISREPAIRED     B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE033110T318                    4697221                                 WE SENT IN BOTH AIRCRAFT PFD'S FOR REPAIR AND SB COMPLIANCE.  BOTH UNITS WERE REPAIRED AND REINSTALLED.  WE TRIED TO CALIBRATE THE ADHRS AND THE PILOT PFD CONTINUED TO GIVE AN ERROR.  WE SPOKE WITH ANOTHER SHOP AND WERE TOLD THEY HAVE HAD THE SAME PROBLEM.  IN FACT, WE WERE TOLD THEY NORMALLY HAVE PROBLEMS WITH REPAIRED UNITS (ABOUT 50 PERCENT OF THE TIME).                                                                                                                                                                                                                                                                                                                                                                         1L71 3O4  TRTA25SO   E4WE                 
20080111000102008011100010EU  2008       1          11         2007FA0001096    120071121G712080446101403     MOUNT                                   PIAGIOP180  P180        6960204EU  PWA   PT6   PT6*        52043EA                              ENGINE          CHAFED          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL23180AV6059                   1018                                    OIL COOLER RETURN LINE CHAFED AGAINST ENGINE MOUNT. DID NOT SHOW SIGNS OF CHAFING STATICALLY DURING ROUTINE INSPECTIONS, WAS CHAFING DURING FLIGHT. INSTALLED REDESIGNED OIL LINE THAT CANNOT COME IN CONTACT WITH MOUNT.  MFG DID NOT INFORM OPERATORS ABOUT REDESIGNED OIL LINE, P/N MS8000M300JF, SAID USE AS SPARE IN ILLUSTRATED PARTS CATALOG. ALSO INSTALLED NEW ENGINE MOUNT.                                                                                                                                                                                                                                                                                                                                                           1H72 3O3  TRTA59EU   E2NE                 
20080111000562008011100056CE  2008       1          11         2007FA0001097    120071212G5720509800913       BUMPER BLOCK                            BEECH 90    C90A        1152911CE  PWA   PT6   PT6*        52043EA                              RT MLG          UNBONDED        B  EHHRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA17266RD1628                   LJ1633                                  COMMUNIQUE NR 2000-04 ANNOUNCED THAT STARTING LJ-1088 AND AFTER THAT LANDING GEAR BUMPER BLOCK WILL BE BONDED TO THE MAIN SPAR WHERE IT CROSSES INSIDE THE LANDING GEAR WHEEL WELLS.  THIS AC FOUND THE RT LANDING GEAR BUMPER BLOCK ON THE FLOOR OF HIS HANGER.  NOT KNOWING WHAT THIS PART WAS THE OWNER ALMOST THREW IT IN THE TRASH.  LUCKILY HE KEPT IT FOR AT OUR NEXT PHASE INSPECTION, WE FOUND THAT IT WAS MISSING AND TOLD THE OWNER, WHO REMEMBER STORING THIS UNKNOWN PART IN A LOCKER AT THIS HANGER.  CLEANED THE AREA AND ATTACHED THE BUMPER BY APPLYING THE EC2216 EPOXY IAW THE COMMUNIQUE.  THIS BLOCK ON EARLIER AC WERE BOLTED ONTO THE SPAR.  THIS METHOD WAS MOST LIKELY DISCONTINUED BECAUSE ELIMINATION OF APPLYING EXT1L72 3T3  TRT3A20    E2NE                 
20080111000152008011100015SW  2008       1          11         2007FA0001098    120071219G6710                ATTACH FITTING                          BELL  412   412         1182202SW  PWA   PT6   PT6*        52043EA                              CYCLIC STICK    GOUGED          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO19107X 19997                  33113                                   DURING INSPECTION FOR BHT ASB-412-07-127 (CYCLIC STICK BEARING INSPECTION) IT WAS FOUND THAT THE LATERAL CONTROL TUBE PN 412-001-307-101 FIXED (OB) CLEVIS PN 212-001-059-001 OR -103 HAD GOUGED THE CYCLIC LEVER ASSEMBLY BEYOND REPAIRABLE LIMITS AND THE BEARING GREASE SEAL RETAINER WAS DISLODGED.  THIS DAMAGE WAS CAUSED BY ANGULAR MISSALIGNMENT OF THE FIXED CLEVIS WITH RELATION TO THE ADJUSTABLE (IB) CLEVIS.  IT WAS ALSO NOTED THAT BOTH CLEVIS'S WERE A DIFFERENT DESIGN THAN THE OTHER CLEVIS'S INSTALLED ON THE CYCLIC OF THIS AND OTHER 412 AIRCRAFT AVAILIABLE FOR INSPECTION.  THIS DESIGN WAS A STRAIGHT (TUNNING FORK) DESIGN AS APPOSED TO THE OTHER CLEVIS DESIGN WITH AN ELONGATED (C) SHAPE WHICH ALLOWED FOR MORE CLE1G72 4U3  T  H4SW    E2NE                 
20080111000522008011100052SO  2008       1          11         2007FA0001103    120071220G520099271000        BRACKET                                 PIPER PA32  PA32R301    7103218SO                                                               ACCONDENSOR DOORCORRODED        D      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      SO199087V3700                   32R8613005                              AIR CONDITIONING CONDENSOR DOOR P/N 99271-000 FAILED IN FLIGHT WHILE DEPLOYED. THE SMALL EXTRUDED ANGLE BRACKET ON THE RT SIDE OF DOOR WHERE THE BEARING ASSY P/N 99561-000 CONNECTS TO THE DOOR CORRODED WHERE THE TWO MEET. THIS CONDITION IS IMPOSSIBLE TO INSPECT UNLESS THE MECHANIC DROPS THE CONDENSOR DOOR DOWN. THE LT SIDE WAS IN PERFECT CONDITION. THE MAIN CAUSE OF THE CORROSION IS THE FACT THAT THAT THE ENGINE EXHAUST TRAVELS DOWN THE RT SIDE OF THE BOTTOM OF THE AIRCRAFT. THIS PORTION OF THESE LOW WING PIPERS ALWAYS SHOW MORE SURFACE CORROSION ON THE RT SIDE OF THE BELLY.                                                                                                                                           1L71 3O      A3SO                         
20080111000122008011100012NM  2008       1          11         2007FA0001104    120071219G5330                SKIN                                    UNIVAR415   415C        0420302NM                                                               FUSELAGE        CORRODED        D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE0331140                       3143                                    IAW AD2002-26-02,- CORROSION FROM WATER, DIRT AND ACID FROM BATTERY ATE THROUGH BOTTOM SKINS 415-13058-1,415-13047L AND R, RIBS 415-13016L AND R AND BOTTOMS OF SERVICE ASSEMBLY NR 5.  AIRCRAFT HAD SAT SINCE 1977.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3O      A718                         
20080111001012008011100101GL  2008       1          11         2007FA0001106    120071222G2497                WIRE HARNESS                            CIRRUSSR    SR22        2130001GL  CONT  O550  IO550*           SO                              ALTERNATOR      DAMAGED         D      A   UNSCHED LANDING                                                                                 P  NO WARNING INDICATION                                                         CRCRUISE         1                      SO151501C1                      0528                                    ALTERNATOR FAILED ON FIRST FLIGHT AFTER INSTALLATION FROM OVERHAUL. FOUND FIELD WIRE RIPPED OUT OF FIELD BRUSH AND BARE WIRE DEBRIS INSIDE ALTERNATOR CASE. SUSPECT WIRE EPOXY HOLD DOWN VIBRATED LOOSE ALLOWING ROTOR ASSEMBLY TO SNAG WIRE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  ONTA00009CHE3SO                 
20080111001452008011100145NE  2008       1          11         2007FA0001107    220071129G7250                TURBINE BLADES                                                             RROYCERB211 RB211TRENT89     NE                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA35                                        61160                       DURING INSPECTION, A CRACKED FIRTREE POST HAS BEEN HIGHLIGHTED.  THE DISC HAS BEEN SCRAPPED OFF AND THIS ISSUE HAS BEEN FORWARDED TO MFG.  THE DISC HAS BEEN SENT TO LAB FOR ANALYSIS.  REF NR: MEM5 D070133. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      4  F          E00050EN             
20080111001462008011100146NE  2008       1          11         2007FA0001108    220071029G7200                BEARING                                                                    RROYCERB211 RB211535E4  54555NE                              ENGINE          DAMAGED         W  DR5YK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA35                                        31141                       DAMAGE FOUND ON STRIP.  HP AND IP SHAFTS SEIZED, HP/IP BEARING DAMAGED, ALSO LP VISIBLE COUPLINGS AND SEAL ARM.  DESIGN ORGANIZATION AND UK CAA HAVE BEE NOTIFIED.  THE ENGINE WAS BEING OPERATED BY AA AT TIME OF IN-FLIGHT SHUTDOWN.  THE ENGINE WAS RECEIVED IN OCTOBER, 2007 FOR REPAIR.  (MEMS D070108) (K)                                                                                                                                                                                                                                                                                                                                                                                                                                       4  F          E12EU                
20080111001532008011100153NM  2008       1          11         2007FA0001109    120071224G5320SB727570112     BRACKET                                 BOEING727   727233      138408ANM                                                               BS 760          CRACKED         B  EB1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO11CGXFA                       20938                                   RT PREVENTATIVE MODIFICATION FWD IB ANGLE CRACKED AT BS 760.95.   REPAIRED CRACK AT RT BL 70.5, BS 760.95, UPPER AND LOWER MOST FORWARD HOLES.  OVERSIZED CRACKED HOLE IAW 57-112.  NDT PERFORMED TO CONFIRM CRACK TERMINATION. COMPLIED WITH TERMINATION REPAIR IAW SB 727-57-0112.   REMOVED RT PREVENTATIVE MODIFICATION FWD IB ANGLE BRACKET.    (K)                                                                                                                                                                                                                                                                                                                                                                                        2L73 4F    RTA3WE                         
20080111001432008011100143EA  2008       1          11         2007FA0001110    120071227G552216920           SKIN                                    FRCHLDFH227 FH227D      3373050EA                                                               ELEVATOR        CRACKED         M      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW17                                                                    A SMALL CRACK WAS FOUND UNDERNEATH ELEVATOR STATIC WICK BASES APPROX. BL 84.0 ON BOTH LTAND RT ELEVATOR CONTROL SURFACES. A SECOND AIRCRAFT IN THE FLEET REVEALED A SIMILIAR CRACK UNDERNEATH THE STATIC BASE ON THE RT ELEVATOR ONLY.  SUSPECT THE CRACK WAS CAUSED BY VIBRATION ON STATIC WICK IN THE SLIPSTREAM OF THE ENGINES. REPAIRED IAW SRM 51-90-04 REPAIR SCHEME NR 6.                                                                                                                                                                                                                                                                                                                                                                2H72 4T      7A1                          
20080111002012008011100201SO  2008       1          11         2007FA0001111    220071217G8520SA6419311075    THRU BOLT                                                                  CONT  O520  IO520C      17032SO                              CRANKCASE       BROKEN          B  VI4RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15                                        17256H                      INSTALLING ALL NEW SA641931-10.75 LOT NR K070059179, REV E THRU BOLTS IN ENGINE.  AFTER TORQUE, WITHIN A FEW HOURS THE THRU BOLT SNAPPED, AT THE OIL RING GROOVE.  THIS IS THE THIRD THRU BOLT THAT HAS SNAPPED AFTER TORQUE, AND SETTING.  PROBABLE CAUSE, IS IMPROPER HEAT TREATING DURING OR AFTER PLATING.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                    3  O          E5CE                 
20080111002022008011100202CE  2008       1          11         2007FA0001112    120071130G2400727755          CIRCUIT BREAKER                         CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                                              FAILED          B  D0FRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW05187281489                   172S9929                                CIRCUIT BREAKER WILL RESET AFTER BEING TRIPPED BY ROTATING THE KNOB.  THIS RESULTS IN A BREAKER THAT IS RESET WHILE BEING IN THE TRIPPED POSITION.  THIS BREAKER WILL PRODUCE THIS RESULT EVERY TIME THAT THIS PROCEDURE IS TRIED. THIS PARTICULAR BREAKER WAS INSTALLED IN THE AUTOPILOT SYSTEM.  THE CIRCUIT BREAKER IN QUESTION IS ATTACHED.  (K)                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A12    1E10                 
20080111002032008011100203SO  2008       1          11         2007FA0001113    120071214G1400EWD0420839      BOLT                                    EMB   145   EMB145LR    3260212SO  ALLSN AE300 AE3007A          GL                              BEARING CAP     BROKEN          D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW21673AE                       145797                                  NEW BOLT BROKEN DURING TORQUE.  TORQUE VALUE NEVER OBTAINED BEFORE THE BOLT BROKE.  THIS BOLT HOLDS THE BEARING CAP IN PLACE THAT HOLDS THE MAIN LANDING GEAR ON THE AIRCRAFT.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4T4  FRTT00011ATTE6CH                
20070326001452007032600145CE  2007       3          26         2007FA0313001    120070313G521055123515        HINGE           CESSNA                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              PAX DOOR        CRACKED         B      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      SW136763L6986                   5500673                                 DESCRIPTION AMENDED TO SAY THAT THE LOWER LUG WAS CRACKED INSTEAD OF THE UPPER LUG.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 4F4  F  A22CE   E1NE                 
20070322000662007032200066    2007       3          22         2007FA032201     420070308G22006226717104      SERVO                                   BEECH MU300 400A        1155402CE                                                               ELEVATOR CONTROLMALFUNCTIONED   E      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             DEDESCENT        1                      WP05188JF351                    RK446                                   DIFFICULTY OCCURRED UPON DESCENT.  PILOT DISENGAGED AUTO-PILOT AND FELT RESISTANCE IN THE ELEVATOR CONTROL SYSTEM.  ON INSPECTION OF THE SYSTEM THE AUTO-PILOT ACTUATOR WAS FOUND PARTIALLY ENGAGED. UNIT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.  THIS AIRCRAFT WAS LAST INSPECTED ON 11/28/2006 AT 218HR.                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4F    RTA16SW                        
20070411000012007041100001SO  2007       4          11         2007FA041101     120070407G7160                AIR BOX                                 PIPER PA18  PA18105SPEC 7101808SO  LYC   O360  O360*       41514EA                              CARBURETOR      FAILED          P      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO118326 96   7                 182341                                  CARBURATOR AIR BOX AIR FILTER RETAINING SHAFT SHEARED ADJACENT TO FISH MOUNTH WELD AT FORWARD EDGE OF HORIZONTAL PLATE (APPROXIMATELY 1/3 SHAFT LENGTH FROM BASE).  AIR FILTER DOME, SHAFT AND RETAINING NUT APPEARANTLY DEPARTED AIRPLANE IN FLIGHT. AIR FILTER WAS FOUND LOOSE IN COWL AIR SCOOP AFTER LANDING.  NO OPERATIONAL INDICATIONS AND NO DAMAGE TO PROPELLER, COWL, FUSELAGE OR LANDING GEAR.  AIRPLANE COMPLETELY REBUILT 2004. NEW K & N AIR FILTER INSTALLED AT ANNUAL INSPECTION NOVEMBER 2006. PHOTOS AVAILABLE.                                                                                                                                                                                                               1H71 3O3  O  1A2     E286                 
20070323000012007032300001SW  2007       3          23         2007FA0703221    120070322G32345059            HANDLE                                  MOONEYM20   M20A        5870204SW  LYC   O360  O360*       41514EA                              MLG             BROKEN          G      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      SW171068B                       1295                                    GEAR HANDLE (MECHANICAL RETRACTION HANDLE) BROKE OFF IN THE PILOT'S HAND DURING GEAR EXTENSION ON LANDING APPROACH. THE LANDING GEAR DISENGAGED BUT IT DID NOT EXTEND FULLY.   THE BREAK WAS JUST BELOW THE WELD.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O3  O  2A3     E286                 
20071023001532007102300153CE  2007       10         23         2007FA1015001    120071015G2435MHB6016         STARTER GEN                             CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA                              ENGINE          MAKING METAL    D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM0352298376                    17274489    L1342739A                   STARTER BENDIX DRIVE HAS NOT BEEN FULLY RETRACTING AFTER ENGINE START AND HAS BEEN SCRAPING THE ENGINE STARTER RING GEAR, CAUSING WEAR ON STARTER RING GEAR AND BENDIX ENGAGEMENT GEAR.  WHEN THE BENDIX DRIVE DOES NOT DISENGAGE FROM STARTER RING GEAR COMPLETELY, THE BENDIX DRIVE DISENTIGRATES ALSO DAMAGING THE ENGINE STARTER RING GEAR.  THIS IS A REOCCURING   PROBLEM. WITH SILVER BENDIX DRIVES, P/N EBB-75A.                                                                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A12    E274                 
20070309000612007030900061CE  2007       3          9          2007H0002        120070305G2730556545092       ACTUATOR                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              ELEVATOR        MISOVERHAULED   B  R3R2K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      SW012663Y                       550602                                  ACTUATOR RODS PROVIDED WITH UNIT WERE TOO SHORT TO MOVE ELEVATOR TABS THE REQUIRED AMOUNT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 4F4  F  A22CE   E1NE                 
20080111002292008011100229    2008       1          11         2008FA0000005    420071220G2565                CABLE                                                                                                                                   ESCAPE SLIDE    WRONG PART      B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA35                                                                    INCORRECT PULL HANDLE CABLE (FIRING CABLE) DEPLOYMENT CABLE WAS SECURED WITH TAPE WHICH HINDERED DEPLOYMENT OF SLIDE.  INCORRECT HANDLE AND CABLE ASSEMBLY FITTED.  CABLE NOT THREADED TROUGH GROMMET DUE TO INCORRECT FIRING CABLE ASSEMBLY.  CMM 25-61-10, STEPS 26 PAGE 50 WAS NOT FOLLOWED. 8130-3 TRACKING NR SBP-5473, SO NR 287413, PO NR R9246, DATED 10/23/2007, MO 0598171.                                                                                                                                                                                                                                                                                                                                                                                                     
20080114000272008011400027NE  2008       1          14         2008FA0000020    220071015G7200                ENGINE                                  UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                                              MAKING METAL    D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      WP07179CB     26                1412        34435                       ON GROUND RUN, ENGINE CHIP DETECTOR ILLUMINATED. BOTH DETECTORS HAD METAL SLIVERS. SAMPLES TAKEN, AND MFG CONDEMNED ENGINE.  ENGINE REMOVED FROM SERVICE, AND RETURNED TO MFG FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G72 3U3  UNCR0001RD E34NE                
20080114000262008011400026NE  2008       1          14         2008FA0000022    220071221G7261                OIL JET                                 UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIUS2F    60010NE                              ENGINE          LEAKING         D      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      WP07183CB618  18                1421        34428                       ENGINE EXPERIENCING INTERNAL OIL LEAKAGE.  MFG CONDEMNED ENGINE. ENGINE REMOVED SERVICE, AND RETURNED TO MFG FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G72 3U3  UNCR0001RD E34NE                
20080114000252008011400025NE  2008       1          14         2008FA0000024    220071019G7200                ENGINE                                  UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIUS2F    60010NE                                              MAKING METAL    D      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      WP07197CB249  49                1448        34506                       ENGINE CHIP DETECTOR ILLUMINATED. BOTH CHIP DETECTORS HAD METAL CONTAMINATION. SAMPLES TAKEN, AND MFG CONDEMNED ENGINE. ENGINE REMOVED FROM SERVICE, AND RETURNED TO MFG FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G72 3U3  UNCR0001RD E34NE                
20080122001052008012200105    2008       1          22         2008FA0000026    220071227G732210603511        CARBURETOR                                                                                                                              ENGINE          FAILED          B  FCPRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM09                                                                    CARBURETOR FAILED THE STUMBLE TEST, FOUND TO BE ACCELERATOR CIRCUIT.  PART RETURNED TO PRECISION FOR FURTHER EVALUATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             
20080122001072008012200107CE  2008       1          22         2008FA0000027    120071212G5320109033          BRACKET                                 CESSNA185   185A        2072804CE  CONT  O470  IO470F      17026SO                              ALTERNATOR      CRACKED         D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SO131004445                     1850419                                 INSTALLED PLANE POWER ALTERNATOR CONVERSION KIT, STC SA 10682SC ON AC.  DURING OIL CHANGE FOUND ALTERNATOR BRACKET CRACKED TOTOALLY IN HALF.  ALTERNATOR HAD ONLY BEEN IN USE 3 WEEKS AND APPROX 45 HRS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  O  3A24    3E1                  
20080122001122008012200112SO  2008       1          22         2008FA0000028    120071226G7312MS21919DG3      CLAMP                                   PIPER PA22  PA22150     7102210SO  LYC   O320  O320*       41508EA                              HEAT BOX        LOOSE           D      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      AL017637D                       225346                                  ENGINE DID NOT RESPOND WHEN POWER APPLIED ON A LOW FLY BY AND CAUSED THE PLANE TO LAND NEXT TO RUNWAY IN SNOW,  DAMAGING ACFT.  FOLLOWING PROBLEMS WERE FOUND ON POST INCIDENT INSPECTION OF ENGINE AND EITHER ONE CAN CONTRIBUTE TO LOSS OF LITTLE ALONE BOTH TOGETHER.  FOUND CARBURETOR HEAT CABLE CLAMP LOOSE ON CABLE HOUSING.    WRONG CLAMP INSTALLED ON CARBURETOR HEAT CABLE HSG AT REAR OF AIR BOX. AND MUFFLER END WITH THE CARB HEAT SHROUD HAS A SUBSTANTIAL EXHAUST LEAK INTO THE CARB HEAT SHROUD.  THE INSIDE OF THE CARB HEAT SHROUD, SCAT HOSE AND AIR BOX ARE VERY SOOTY FROM EXHAUST GASSES.  THE EXHAUST MUFFLER CLAMP LEAKING.  THIS WILL CAUSE A POWER LOSS DUE TO THE HOT INDUCTION AIR,   (K)                          1H71 3O3  O  1A6     E274                 
20080122000502008012200050NE  2008       1          22         2008FA0000029    220071230G7261                WARNING LIGHT                           UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              CHIP DETECTOR   FALSE ACTIVATIOND      O   OTHER                                                                                           N  FALSE WARNING                                                                 CRCRUISE         1                      GL21372HS                       1460        34517                       ENGINE CHIP LIGHT IN CRUISE FLIGHT.  INSPECTED BOTH MAGNETIC PLUGS FOR FOREIGN MATERIAL, NONE WAS NOTED.  INSPECTED AND TESTED MAGNETIC PLUG HEADS IAW 79-38-00-750-801, INSPECTION AND OPS CHECKS WERE GOOD.  REMOVED AND REPLACED ENGINE OIL AND RETURN FILTER IAW 79-24-05-901-801-A01.  OPS AND LEAK CHECKS GOOD.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                      1G72 3U3  UNCR0001RD E34NE                
20080122001282008012200128NE  2008       1          22         2008FA0000030    320071211G61116607132886      BLADE           ROTOL                                                                                       ROTOL R389  R389*       NE  PROPELLER       CRACKED         B  MS1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA27     34226                                                          BLADE RECEIVED FROM CUSTOMER WITH A CRACKED ROOT END OUTERSLEEVE.  NO REPAIR AVAILABLE.  PART HAS BEEN REMOVED FROM FURTHER SERVICE. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     6  CP30NE    
20080122001482008012200148SW  2008       1          22         2008FA0000031    120071205G67102040012741      LINER                                   BELL  204   UH1B        1181410SW                                                               COLLECTIVE      WORN            D  H50LK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM0546969                       638548                                  PILOT EXPERIENCED COLLECTIVE BOUNCE ON TAKEOFF.  INSPECTION OF COLLECTIVE LINERS SHOWED A SUFFICIENT AMOUNT OF LINER REMAINING IN THE WEAR AREA.  WITH FURTHER INSPECTION, THE MINIMUM COLLECTIVE FRICTION WAS TOO LOW.  INSPECTION ON NR 3 AND NR 6 PHASE IAW TM 55-1520-219-PMS, PAGE 6, ITEM NR 2.14 REQUIRES TO INSPECT COLLECTIVE FRICTION LINERS FOR WEAR.  ADJUSTMENT OF MINIMUM COLLECTIVE FRICTION SHOULD ALSO BE INCLUDED IN THE PHASE INSPECTION CHECKLIST ALONG WITH VISUAL INSPECTION OF THE LINERS.  (K)                                                                                                                                                                                                                          1G71 4U      EXPA1G71                     
20080122001492008012200149SO  2008       1          22         2008FA0000032    120071212G8011MHB4016         STARTER                                 PIPER PA28  PA28181     7102807SO  LYC   O360  O360A4M     41514EA                              ENGINE          INOPERATIVE     B  UC2RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL19          326                                                       OPERATOR COMPLAINED THAT THE ENGINE STARTER WOULD NOT ENGAGE.  AFTER INSPECTION, FOUND THAT THE STARTER FIELD CASE HAD SEPARATED FROM GEAR HOUSING.  A DETAILED INSPECTION OF THE FIELD CASE SCREW HOLES REVEALED THAT MOST OF THE THREADS WERE STRIPPED OUT AND HOLES WERE ELONGATED.  WOULD RECOMMEND THAT AT EACH 100 HR/ANNUAL INSPECTION, PERFORM TORQUE CHECK OF GEAR HOUSING TO CASE ATTACH SCREWS AND REPAIR AS REQUIRED.  (K)                                                                                                                                                                                                                                                                                                          1L71 3O3  O  2A13    E286                 
20080122000662008012200066EA  2008       1          22         2008FA0000033    120071015G274021207008        ACTUATOR                                CNDAIRCL600 CL6002B16   1900305EA                                                               PITCH TRIM      FAILED          B  UO2RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      GL19BMAI 6552                   5049                                    PITCH TRIM ACTUATOR, PN 21207-008, SN 344:  CONNECTOR P5CD- PINS A, B AND D ARE SHORTED TO PIN E.  THE SHORT IS LESS THAN 1.  PIN C HAS A 25 SHORT TO PIN E.  FLEXING THE CONNECTOR CAUSES THE SHORT TO COME AND GO.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F    RTA21EA                        
20080122000512008012200051SO  2008       1          22         2008FA0000034    120071012G554063451000        SUPPORT                                 PIPER PA28  PA28181     7102807SO  LYC   O360  O360*       41514EA                              RUDDER BAR      CRACKED         B  UC2RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL194146R5820                   2843160                                 FOUND CRACKED AFT ZEE ASSY PN 62664-000.  THE ZEE ASSY IS RIVETED TO THE TOP FWD END OF TUNNEL PLATE PN 62601-003 AND AS AN ATTACHMENT POINT FOR THE RUDDER BAR SUPPORT ASSY PN 63451-000 USING 4 STANDARD AN3-4A BOLTS, WHICH ARE SECURED THROUGH NUTPLATES THAT ARE RIVETED ON BOTH FORE AND AFT ZEE ASSEMBLIES.  CRACKING POSSIBLY CAUSED BY LOOSENESS IN TOE BRAKE SUPPORT BRACKETS PN 63468-000 ON BOTH PILOT AND CO-PILOTS SIDE.  THE STANDARD AN3-13A BOLTS USED TO ATTACH THESE TOE BRAKE SUPPORT BRACKETS LOOSEN OVER TIME AND CAUSE LOSS OF SUPPORT TO THE RUDDER PEDAL BAR ASSY PN 63420-000.  EXCESS MOVEMENT IN RUDDER BAR SUPPORT ASSY.  THIS FLEXING TRANSFERS DOWN TO THE ZEE ASSEMBLIES CAUSING METAL FATIGUE AND SUBSEQUENT CR1L71 3O3  O  2A13    E286                 
20080122000432008012200043GL  2008       1          22         2008FA0000035    120071218G7312                CONTROL ARM                             DIAMONDA40  DA40        2990002GL  LYC   O360  O360*       41514EA                              CARB HEAT       BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM07418FP                       40FC018                                 CARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE.  RECOMMEND INSTALLED THINKER MATERIAL ON CARB HEAT CONTROL ARM LEVER, DIFFERENT WELDING PROCESS, OR DIFFERENT ATTACHMENT PROVISION ALTOGETHER.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  ONTA47CE   E286                 
20080122001262008012200126NE  2008       1          22         2008FA0000042    220071212G8530                CYLINDER HEAD                           DHAV  DHC2  DHC2*       2800108EA  PWA   R985  R985AN14B   52008NE                              ENGINE          CRACKED         E      O   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      AL05777DH     1434              47          42222299                    CYLINDER CRACKED IN THE AREA OF EXHAUST VALVE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3R3  R  A806    5E1                  
20080212002382008021200238NE  2008       2          12         2008FA0000045    320070823G61116607132886      BLADE           ROTOL                                                                                       ROTOL R389  R389*       NE  NR 1            CRACKED         B  MS1RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA27     398824932  DR6828288                           DR6828288       PROP REMOVED DUE TO NR 1 BLADE LOOSE IN HUB.  NR 1 BLADE SN 689 WAS FOUND TO HAVE A CRACKED OUTER SLEEVE ON BLADE ROOT END.  BLADE WAS REJECTED AND REMOVED FROM FURTHER SERVICE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       6  CP30NE    
20080131003042008013100304CE  2008       1          31         2008FA0000064    120071119G243523085001        STARTER GEN                             BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE                                              FAILED          D      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      SO0380BZ                        FA117       PCE95242                    THE NR 1 BEARING FAILED RESULTING IN A CATASTROPHIC FAILURE AND AN IN FLIGHT SHUTDOWN.  THE ENGINE WAS REMOVED AND SENT FOR REPAIR.  DURING THE FAILURE INVESTIGATION, ELECTRICAL ARCING WAS FOUND ON THE NR 1 BEARING, INPUT SHAFT, AND STARTER/GENERATOR DRIVE GEAR.  SD ADVISORY NR AV-2007-05 ISSUED THAT STATES ACCUMULATION OF BRUSH DUST CAN CAUSE STARTER GENERATOR ARMATURE LEAKAGE.  OUR RESEARCH DOES NOT SHOW ANY PREVENTATIVE MAINTENANCE ACTIONS THAT MAY BE PERFORMED TO THE STARTER GENERATOR TO CHECK FOR ELECTRICAL DISCHARGE.  (K)                                                                                                                                                                                           2L72 4T4  T  A24CE   E4EA                 
20080129002942008012900294CE  2008       1          29         2008FA0000065    120070824G3246                WHEEL HALF                              CESSNA310   310L        2074230CE                                                               LANDING GEAR    CRACKED         C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO0163EL 2200                   310L0088                                UPON CHANGING A TIRE ON A CLEVELAND WHEEL ASSEMBLY ON ABOVE AIRCRAFT IT WAS DISCOVERED THAT THE PORTION OF THE WHEEL HALF THAT HOLDS THE BEARING RACE WAS CRACKING. IT HAD CRACKED OVER 180 DEGREES AROUND THE AXLE OPENING, WHICH COULD HAVE EVENTUALLY HAD A SERIOUS ACCIDENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3O      3A10                         
20080204001052008020400105SO  2008       2          4          2008FA0000067    220071219G7414                GEAR                                    DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO                              RT MAGNETO      MAKING METAL    B  XGKRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP25293DC                       C0193       806439                      PRIOR TO PERFORMING SB 03-7 INSPECTION, 2 NEW GEARS WERE ORDERED FROM MFG IN EVENT WOULD NEED THEM DURING INSPECTION.  AT 372.9 TACH TIME, THE RT MAGNETO GEAR BROKE A TOOTH DURING START AND WAS IDENTIFIED DURING  PRE-TAKEOFF RUNUP.  THE ENGINE WAS INSPECTED AND FOUND TO HAVE METAL PARTICLES DISTRIBUTED THROUGHOUT THE ENGINE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                     1L71 3O3  ONTTA4CH   E7SO                 
20080220000622008022000062GL  2008       2          20         2008FA0000076    120071221G3233                ACTUATOR                                AMTR  QUTAIRQUESTAIRVENT0561898GL  CONT  O550  IO550N      17042SO  MCAULY2A34C B2A34C205   GL  MLG             MALFUNCTIONED   H      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      SO19203V 35                     22                                      NOSE GEAR LINEAR ACTUATOR TRIPPED CIRCUIT BREAKER INFLIGHT AND WAS NOT DETECTED PRIOR TO LANDING.  THE AIRCRAFT WAS INADVERTENTLY LANDED WITH THE NOSE GEAR NOT EXTENDED.  WHEN THE AIRCRAFT WAS RECOVERED, THE AIRCRAFT WAS LIFTED SO THE GEAR COULD BE EXTENDED.  WHEN POWER WAS APPLIED TO THE AIRCRAFT AND THE CIRCUIT BREAKER WAS RESET THE NOSE GEAR EXTENDED NORMALLY AND LOCKED IN THE DOWN POSITION, THE CIRCUIT BREAKER DID NOT TRIP.  OTHER AIRCRAFT IN THE FLEET HAVE HAD PROBLEMS WITH THE GEAR ACTUATOR BREAKERS BEING TO LOW OF A RATING BUT THIS AIRCRAFT HAS THE HIGHER RATED BREAKER INSTALLED.                                                                                                                               1L71 3O3  ORTEXPA1L71E3SO    5  CP3EA     
20080310003312008031000331CE  2008       3          10         2008FA0000090    120071112G2797C352B20         WIRE                                    BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              PITCH TRIM      CHAFED          B  AKGRO   OTHER                                                                                           F  FLT CONT AFFECTED                                                             NRNOT REPORTED   1                      CE05213BK3287                   RK216                                   PITCH TRIM INOPERATIVE REMOVED RT FWD GALLEY AND RT FWD PARTITION.  FOUND WIRE BUNDLE CHAFED BEHIND PARTITION.  REPAIRED (3) WIRES THAT WERE CHAFED THROUGH TO THE CONDUCTORS.  PROVIDED CLEARANCE BETWEEN WIRE BUNDLE AND PARTITION.  INSTALLED ANTI-CHAFE MATERIAL ON PARTITION.  AT THE TIME OF THE REPAIR NO OTHER COMPONENTS HAD MALFUNCTIONED FRO THE OTHER (2) CHAFED WIRES.  (K)                                                                                                                                                                                                                                                                                                                                                        2H72 4F4  FRTA16SW   E25EA                
20080310003422008031000342SO  2008       3          10         2008FA0000097    220071226G8520649900          CRANKSHAFT                              PIPER PA46  PA46310P    7104605SO  CONT  O550  TSIO550C         SO                              ENGINE          BROKEN          D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM0347BC                        4608129     814584                      CRANKSHAFT BROKE JUST AFT OF PROPELLER MOUNTNG FLANGE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L71 3O3  ORTA25SO   E5SO                 
20080310003452008031000345SO  2008       3          10         2008FA0000098    120071226G32211303400         MOUNT                                   PIPER PA22  PA22150     7102210SO  LYC   O320  O320*       41508EA                              NLG             CRACKED         D      K   NONE                                                                                            O  OTHER                                                                         LDLANDING        1                      AL017637D                       225346                                  FOUND NOSE GEAR MOUNT CORRODED THIN IN SPOTS ON THE LOWER TUBES FROM THE INSIDE.  ORIGINAL THICKNESS .049 INCH AND IN THE THIN SPOTS THE THICKNESS WAS LESS THAN .020 INCH.  THE MOUNT HAD BEEN REPAIRED BY WELDING AND ONE WELD WAS A COLD WELD THAT CRACKED AND ALLOWED MOISTURE INTO THE INSIDE OF THE TUBING.  ANNUAL INSP 35 HOURS BEFORE FAILURE.  THE MOUNT FAILED ON A SOFT FIELD LANDING AND CAUSED SUBSTANTIAL DAMAGE AFTER AN ENGINE FAILURE.  IN MY OPINION THE THIN WALL FROM THE CORROSION IS WHY THE MOUNT FAILED.  RECOMMENDATIONS TO PREVENT SUCH RECURRENCES ARE TO INSPECT ALL WELDS FOR CRACKS, ESPECIALLY FIELD REPAIRS.  THESE FIELD REPAIR WELDS NEED TO BE EXAMINED FOR THE QUALITY OF THE WELD, CRACKS AND PIN HOLES EA1H71 3O3  O  1A6     E274                 
20080319003662008031900366EA  2008       3          19         2008FA0000103    220071030G74146393            MAGNETO                                                                    LYC   O540  IO540E1B5   41532EA                              ENGINE          WORN            B      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TXTAXI/GRND HDL  1                      GL1551RF 58                                                             ENGINE WAS GETTING HARD TO START, CHECKED MAG TIMING AND FOUND LT MAG TIMING, OUT OF LIMITS.  DISASSEMBLED MAG AND FOUND THE CAM WORN OUT . 58.7 HRS SINCE NEW.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        3  O          1E4                  
20080324004352008032400435SO  2008       3          24         2008FA0000105    120071204G321331661STCSA4618NMFITTING                                 PIPER PA18  PA18        7101802SO  LYC   O360  O360A1A     41514EA                              RT MLG          BROKEN          G      K   NONE                                                                                            O  OTHER                                                                         LDLANDING        1                      AL03723C                        181150                                  PILOT STATED THAT HE PERFORMED AN OFF AIRPORT LANDING ALONG A BEACH WHILE HUNTING.  UPON LANDING, THE UPPER RT MLG CABANE FITTING BROKE.  THE LANDING GEAR SAFETY CABLES PREVENTED A TOTAL GEAR COLLAPSE.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  O  1A2     E286                 
20080331000462008033100046SO  2008       3          31         2008FA0000109    120071221G32106569100         TORQUE LINK                             PIPER PA28  PA28140     7102802SO  LYC   O320  O320*       41508EA                              MLG             SEPARATED       D      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      EA239855W6910                   2823369                                 TORQUE LINK SEPARATED ON ABORTED LANDING ALLOWING WHEEL AND AXLE ASSY TO SEPARATED FROM AC.  SAFE LANDING ON UPPER CASTING ASSY WAS MADE WITH DAMAGE TO CASTING AND FLAP.  AD 72-08-06 OR THIS LINK CALLED FOR 500 HR INSP.  INTERVAL PAR 203.8 HR PRIOR.  WOULD SUGGEST THAT AD SHOULD BE CHARGED TO RETIRE THESE PARTS AT 5000 HR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  O  2A13    E274                 
20080331001442008033100144GL  2008       3          31         2008FA0000134    120070727G282251000020        PUMP                                    DIAMONDA40  DA40        2990002GL  LYC   O360  O360A4M     41514EA                              FUEL SYS        INOPERATIVE     C  GO3SK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM07423FP156                    40FC023                                 AFTER A PREVIOUS FLIGHT AND BEFORE THE NEXT STUDENTS FLIGHT, THE ELECTRIC FUEL PUMP WAS FOUND TO BE INOPERATIVE.  INADEQUATE COOLING IS WHAT WE BELIEVE TO BE THE SOURCE OF THE MALFUNCTIONS.  PROVIDE RAM AIR PROPER COOLING OF THE FUEL PUMP AND MOTOR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 3O3  ONTA47CE   E286                 
20080331001452008033100145GL  2008       3          31         2008FA0000136    120070221G282251000020        PUMP                                    DIAMONDA40  DA40        2990002GL  LYC   O360  O360A4M     41514EA                              FUEL SYSTEM     INOPERATIVE     D  GO3SK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM07424FP232                    40FC024                                 AFTER A PREVIOUS FLIGHT, AND BEFORE THE NEXT STUDENTS FLIGHT, THE ELECTRIC FUEL PUMP WAS FOUND TO BE INOPERATIVE.  INADEQUATE COOLING IS WHAT WE BELIEVE TO BE THE SOURCE OF THE MALFUNCTIONS.  PROVIDE RAM AIR FOR PROPER COOLING OF FUEL PUMP AND MOTOR.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  ONTA47CE   E286                 
20080331001742008033100174EU  2008       3          31         2008FA0000147    120070615G6710                COVER                                   SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL1D1   60053NE                              COLLECTIVE STICKLOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA114048L2732                   3020        9245                        COLLECTIVE MOUNTED HOIST EMERGENCY RELEASE (JETT) SWITCH COVER SECURITY.  IF THE BASE OF THE COVER IS LOOSE AND TURNED 180 DEGREES, AS WAS THE CASE HERE, THE COVER OPENS FORWARD AND EXTENDS OFF OF THE END OF THE COLLECTIVE.  IN THIS CONDITION WHEN THE COLLECTIVE IS FULLY LOWERED, THE PUSHBUTTON COVER JAMS AGAINST THE GENEVA MODIFIED CENTER CONSOLE UNTIL THE PILOT PUSHES THE COLLECTIVE THROUGH THE BINDING, AND THE HINGED COVER POPS UP AND OUT OF THE WAY.  IN THIS CONDITION, WITH THE COLLECTIVE JETT SWITCH OPEN COVER WEDGED AGAINST THE CENTER CONSOLE, A PILOT MAY FEEL THAT THE COLLECTIVE IS FULLY DOWN WHEN IT IS NOT.                                                                                                  1G71 3U3  U  H9EU    E19EU                
20080410002612008041000261CE  2008       4          10         2008FA0000222    120071116G3260513771          DOWNLOCK SWITCH                         CESSNA210   210L        2073448CE                                                               MLG             BROKEN          G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP01987M 3344                   21061093                                EXAMINATION OF THE LANDING GEAR SYSTEM REVEALED THAT THE LT LDG DOWN LIMIT SWITCH PLUNGER WAS DAMAGED AND STUCK IN THE DEPRESSED POSITION WITH APPROX .012 INCH AIRGAP BETWEEN PLUNGER TIP AND STRIKER PLATE.  WITH SIMULATED AIR LOADS APPLIED TO THE LT MAIN GEAR THE LANDING GEAR PUMP WOULD SHUT OFF PRIOR TO THE LT MAIN GEAR LOCKING IN THE DOWN LOCK.  THE GEAR POSITION INDICATOR IN THE COCKPIT INDICATED GREEN AND THE UNSAFE HORN DID NOT SOUND WHEN THE THROTTLE WAS RETARDED.  (K)                                                                                                                                                                                                                                                 1H71 3O      3A21                         
20080410002332008041000233EA  2008       4          10         2008FA0000228    220071016G8530                INTAKE VALVE                            CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA                              CYLINDER        WORN            D      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP1549811           23C064444   15281332                                FOLLOWING ACCIDENT THAT RESULTED IN ENGINE FAILURE, INVESTIGATION FOUND NO COMPRESSION ON THE NR 1 CYL AND REPORTED VALVE CLEARANCE WAS 0.002 INCH. THE CYL WAS NOT REMOVED AND THE AC WAS RELEASED INTO CUSTODY.  REMOVED THE NR 1 CYLINDER AND VALVES.  BOTH VALVES HAD ACCELERATED WEAR TO THE VALVE SEATS WITH EVIDENCE OF LEAKAGE.  LAST VALVE GUIDE CHECK WAS PERFORMED 46 HOURS EARLIER WITHIN LIMITS.  (K)                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A19    E223                 
20080425001112008042500111SO  2008       4          25         2008FA0000251    120071114G534395555000        FITTING                                 PIPER PA34  PA34200T    7103406SO  CONT  O360  TSIO360*    17025SO                              NLG MOUNT       SEPARATED       C      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15467TC                       347870006                               SB 1123B TABLE 1, ITEM 14 STATES TO INSPECT TUNNEL BRACKET 95554-000 AND FITTING 95555-000 FOR CONDITION AND ATTACHMENT.  ACCORDING TO FIGURE 1A, THE CONDITION INDICATED NO PROBLEMS, HOWEVER FITTING 95555-000 WAS SEPARATED FROM BRACKET 95554-000.  ALL 4 AN426 RIVETS HAD SHEARED, ALLOWING FITTING TO SHIFT POSITIONS, ALLOWING NOSE GEAR OVERCENTER GEOMETRY TO CHANGE, RESULTING IN GEAR COLLAPSE.  ITEM 14 DESCRIBES INSPECTION THROUGH AND ACCESS OPENING IN BOTTOM SKIN AT BL 0.0 JUST AFT OF STATION 49.5.  IT IS UNCLEAR WHETHER THIS  ACCESS OPENING IS TO BE CUT IN THE SKIN AND A DOUBLER AND INSPECTION PLATE INSTALLED OR IF THIS HOLE IS ALREADY PRESENT.  NO PA-34 AC IN OUR FLEET HAS THIS OPENING.  THIS DEFECT WAS NOTED 1L72 3O3  O  A7SO    E9CE                 
20080428002992008042800299NM  2008       4          28         2008FA0000255    120071202G2497                CIRCUIT BREAKER                         AMD   FALC50FALCON2000  2730170NM  PWC   PW308 PW308C      52182NE                                              MISINSTALLED    W  BO5YK   NONE                                                                                            WB INADEQUATE Q C            SMOKE/FUMES/ODORS/SPARKS                            ININSP/MAINT     1                      EA334QG                         028                                     MAU 1B AND AGM 2 FAIL IN FLIGHT AND RECOVERED AFTER 3 SECONDS.  SHUNT (IPC 24-05-10, ITEM 210) INSECURED ON BREAKER, ELECTRIC ARC.  ONE SCREW ON BREAKER L501X, TOO THREAD LENGTH OVERSIZED.  RESULTS: EXCHANGE SHUNT AND BREAKERS.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA50NM   E00065EN             
             20080603     CE  2008       6          3          2008FA0000319    120071225G5100                UNKNOWN                                 CESSNA182   R182        2072734CE  LYC   O540  O540J3C5    41532EA                                              UNKNOWN         D      O   OTHER                                                                                           G  MULTIPLE FAILURE                                                              CRCRUISE         1                      WP056079C                       R18200371   RL1970540A                  INFLIGHT FAILURE OF PART OR PARTS UNKNOWN WITH NO SYMPTOMS FROM WITHIN COCKPIT, IE: OIL PRESSURE, OIL TEMPERATURE, AND CYLINDER HEAD TEMPERATURES WERE ALL INDICATING WITHIN NORMAL RANGES.  OUTWARD MANIFESTATIONS WERE EXCESSIVE BLOW-BY OIL ON BELLY OF THE AIRPLANE.  OTHER MANIFESTATIONS WERE: AN INTERRUPTION IN THE SMOOTH MOVEMENT OF THE PROP (WHEN ROTATING BY HAND) AT THE SAME LOCATION IN THE ROTATION ON EVERY OTHER COMPLETE ENGINE ROTATION, IE: RELATED TO THE CAMSHAFT (720 DEGREES OF ROTATION).  A CRACK IN THE LT SIDE OF THE ENGINE CASE OVER THE BASE OF THE NR 5 CYLINDER WHERE THE ENGINE CASE FARES INTO THE INTAKE VALVE PUSHROD TUBE.  A CRACK IN THE RT SIDE OF THE ENGINE CASE OVER THE BASE OF THE NR 6 CYLINDER1H71 3O3  ORT3A13    E295                 
             20080715     GL  2008       7          15         2008FA0000342    120070910G5210DA4522100002    DOOR                                    DIAMONDA40  DA40        2990002GL  LYC   O360  IO360LYC*   41514EA  HARTZLHCC2Y HCC2YR1     GL  PAX DOOR        DEPARTED        G      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           TOTAKEOFF        1                      WP07686US615                    40640       L3262751A   CH39554B        ON TAKEOFF ROLL AT VR, AFT PASSENGER DOOR DEPARTED AIRFRAME. (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  ONTA47CE   1E10    5  CP920     
             20080715     GL  2008       7          15         2008FA0000344    120071106G5210DA4522100002    DOOR                                    DIAMONDA40  DA40        2990002GL  LYC   O360  IO360LYC*   41514EA  HARTZLHCC2Y HCC2YR1     GL  PAX DOOR        DEPARTED        G      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           TOTAKEOFF        1                      WP07605US225                    40675       L3276151A   CH399768        WHILE TAXIING INTO TAKEOFF POSITION ON RUNWAY, AFT PASSENGER DOOR DEPARTED AIRFRAME.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  ONTA47CE   1E10    5  CP920     
             20080715     EA  2008       7          15         2008FA0000375    220071226G7322MS21919DG3      CLAMP           PIPER                   PIPER PA22  PA22150     7102210SO  LYC   O320  O320*       41508EA                              CARB HEAT       WORN            D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL017637D                       225346                                  ENGINE DID NOT RESPOND WHEN POWER WAS APPLIED ON A LOW FLY BY OF THE RUNWAY AND CAUSED THE PLANE TO LAND NEXT TO THE RUNWAY IN THE SNOW DAMAGING THE AIRCRAFT. THE FOLLOWING TWO PROBLEMS WERE FOUND ON POST INCIDENT INSPECTION OF THE ENGINE AND EITHER ONE CAN CONTRIBUTE TO LOSS.  THE FIRST PROBLEM FOUND WAS THE CARBURETOR HEAT CABLE CLAMP WAS LOOSE ON THE CABLE HOUSING. THIS WOULD ALLOW THE HOUSING TO SLIP IN THE CLAMP AND SOMETIME NOT MAKE STOP TO STOP TRAVEL. THE WRONG CLAMP WAS INSTALLED ON THE CARBURETOR HEAT CABLE HOUSING AT REAR OF AIR BOX. THE CLAMP INSTALLED  WAS PN MS21919GD3 (3/16) INCH DIAMETER ADEL CLAMP. THE ADEL CLAMP USED HAS AN CHLOROPRENE RUBBER CUSHION WITH A MAXIMUM TEMP OF 212 DEGREES (F). THE1H71 3O3  O  1A6     E274                 
             20080715     SO  2008       7          15         2008FA0000376    120071226G78101423500         CLAMP                                   PIPER PA22  PA22150     7102210SO  LYC   O320  O320*       41508EA                              EXHAUST PIPE    LOOSE           D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      AL017637                        225346                                  ENGINE DID NOT RESPOND WHEN POWER WAS APPLIED ON A LOW FLY BY OF THE RUNWAY AND CAUSED THE PLANE TO LAND NEXT TO THE RUNWAY IN THE SNOW DAMAGING THE AIRCRAFT.  THE FOLLOWING PROBLEM WAS FOUND ON POST INCIDENT INSPECTION OF ENGINE AND EITHER ONE CAN CONTRIBUTE TO LOSS. THE PROBLEM FOUND WAS THE MUFFLER END WITH THE CARB HEAT SHROUD HAS A SUBSTANTIAL EXHAUST LEAK INTO THE CARB HEAT SHROUD. THE INSIDE OF THE CARB HEAT SHROUD, SCAT HOSE AND AIR BOX ARE VERY SOOTY FROM EXHAUST GASSES.  THE EXHAUST MUFFLER PN 10308-03 END THAT EXHAUST PIPE PN 12043-23 END SLIDES INTO AND HAS PN 14235-00 EXHAUST CLAMP AROUND IT IS LEAKING.  THE PIPE END THAT SLIPS INTO THE MUFFLER IS VERY LOOSE, NOT A TIGHT SEAL LIKE NORMAL. THE CLAMP1H71 3O3  O  1A6     E274                 
             20080715     EU  2008       7          15         2008FA0000386    120071101G3250                STEERING SYS                            PIAGIOP180  P180        6960204EU                                                               NLG             CONTAMINATED    D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW07                                                                    STEERING SYSTEM DISENGAGEMENT DURING TAXI.  STEERING DRIFT DURING ENGAGEMENT. STEERING HART TO TURN (NO INPUT). STEERING RELIABILITY VERY LOW.  STEERING CONTAMINATION DURING MFG BENCH TESTING.  AIRCRAFT RUNWAY EXCURRSION DURING LANDING AND TAXI DUE TO STEERING CONTROL LOSS.  AIRCRAFT DAMAGED FROM STEERING DRIFT DURING LANDING.  (K)                                                                                                                                                                                                                                                                                                                                                                                                   1H72 3O    RTA59EU                        
             20080715     EA  2008       7          15         2008FA0000417    220071221G8500IGSO480         ENGINE                                  BEECH 65    A65         1152803CE  LYC   O480  GSO480*     41529EA                              LEFT            SEIZED          G      E   ENGINE SHUTDOWN                                                                                 O  OTHER                                                                         NRNOT REPORTED   1                      CE078108R                       LC329       L119933C                    AIRCRAFT LANDED WITH LT ENGINE SHUTDOWN (IN-FLIGHT SHUTDOWN). INITIAL INVESTIGATION REVEALED THAT THE ENGINE WAS SEIZED. OIL SCREEN WAS REMOVED AND FOUND HEAVILY CONTAMINATED WITH METAL PARTICLES.  ENGINE OIL SUMP DRAIN PLUG WAS REMOVED.  LARGE METAL PARTICLES, SOME APPROXIMATELY .25 IN DIAMETER WERE REMOVED FROM IMMEDIATELY INSIDE THE SUMP DRAIN HOLE.  OTHER PARTICLES APEAR TO BE GEAR TEETH, AS SHEARED FROM THE GEAR.  ENGINE WAS REMOVED FROM THE AIRCRAFT(12-18-2007) AND SENT TO CUSTOMER DESIGNATED REPAIR FACILITY.  (K)                                                                                                                                                                                                   1L72 3O3  O  3A20    E284                 
             20080715     GL  2008       7          15         2008FA0000423    120071106G5210DA4522100002    DOOR                                    DIAMONDA40  DA40        2990002GL                                                               REAR PASSENGER  DEPARTED        G      D   RETURN TO BLOCK                                                                                 D  INFLIGHT SEPARATION                                                           TXTAXI/GRND HDL  1                      WP28605US                       40675                                   WHILE TAXIING INTO TAKEOFF POSITION ON RUNWAY, AFT PASSENGER DOOR DEPARTED AIRFRAME.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O    NTA47CE                        
             20080715     GL  2008       7          15         2008FA0000425    120070910G5210DA4522100002    DOOR                                    DIAMONDA40  DA40        2990002GL                                                               REAR PAX DOOR   DEPARTED        G      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                TOTAKEOFF        1                      WP28686US                       40640                                   ON TAKEOFF ROLL AT VR, AFT PASSENGER DOOR DEPARTED AIRFRAME.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O    NTA47CE                        
20070322000482007032200048CE  2007       3          22         20582007TJ001    120070313G5344551123515       HINGE           CESSNA                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              PAX DOOR        CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW136763L6986                   5500673                                 DURING A DAILY INSPECTION OF THE AIRCRAFT A CRACK WAS FOUND ON THE UPPER LUG OF THE DOOR HINGE. DURING REPLACEMENT OF THE HINGE THE LUG COMPLETELY BROKE IN (2) PEICES.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 4F4  F  A22CE   E1NE                 
20071214002922007121400292NM  2007       12         14         220757           120071205G291365446747        HOUSING         BOEING                  BOEING737   737         UTILSYSNM                                                               MODULE          CRACKED         B  IU6RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM01                0728                                                HOUSING WAS FOUND CRACKED DURING TEARDOWN IN SHOP.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F    RTA16WE                        
20071205000452007120500045    2007       12         5          243DR1           420071121G22161C7921888       SERVO                                   CESSNA206   TU206G      2073357CE  CONT  O520  TSIO520*    17040SO                              ELEVATOR TRIM   MISINSTALLED    B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      SW17243DR4056                   U20604747                               WHILE UNDERGOING A SCHEDULED INSPECTION, MECHANIC FOUND ELEVATOR TRIM SYS WAS MISRIGGED. TRAVEL LIMITS WERE NOT CORRECT AND WERE ACTUALLY RIGGED OPPOSITE WITH REGARDS TO MAX TRAVEL UP/DOWN. TRAVEL LIMITS IN MM NR D2070-3-13 FIGURE 1-1 WERE MISINTERPRETED, MFG SHOULD REVISE THIS MANUAL SECTION TO BE MORE SPECIFIC SINCE WE HAVE SEEN THIS BEFORE. ADDITIONALLY IT WAS FOUND THAT ELEVATOR TRIM SYS COULD NOT BE RIGGED BECAUSE CENTURY 2000 AUTOPILOT ELEVATOR TRIM SERVO WAS NOT INSTALLED CORRECTLY WHEN SYS WAS INSTALLED ON 10/9/2001 UNDER STC SA3479SW-D.  FOUND SERVO MISMOUNTED, IT DID NOT MATCH CENTURY DRAWING 69D1754.  REINSTALLED THE TRIM SERVO IAW THE STC DRAWINGS.                                                    1H71 3O3  O  A4CE    E8CE                 
20070515001832007051500183GL  2007       5          15         26519A           320070502G6111A4564           BUSHING         MCAULY                  CESSNA208   208B        2073701CE  PWA   PT6   PT6*        52043EA  MCAULY3AF34C3GFR34C703  GL  BLADE LINK      CRACKED         B  WIWAK   NONE                                                                                            E  VIBRATION/BUFFET                                                              ININSP/MAINT     1                      WP07122JB1850                   208B1025                020657          VIBRATION REPORTED BY PILOT.  OPERATOR WAS UNABLE TO DYNAMIC BALANCE.  OPERATOR NOTICED ONE BLADE HAS ROTATIONAL PLAY.  UPON DISASSEMBLY NR 2 BLADE LINK BUSHING P/N A4564 WAS FOUND CRACKED WITH PIECES MISSING.  THE LINK P/N B4743 AND BLADE ACTUATING PIN P/N B5072-1 WERE DAMAGED FROM METAL TO METAL CONTACT.                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3T3  T  A37CE   E2NE    5  CP60GL    
20070511001512007051100151SW  2007       5          11         31038042507      120070425G56103G5630F00111A2  WINDOW                                  AGUSTAAB139 AB139       0260110SW  PWA   PT6   PT6*        52043EA                              CREW DOOR       DEPARTED        B      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           CRCRUISE         1                      EA17139BK                       31038                                   DURING CRUISE FLIGHT AT AN ALTITUDE OF 2000FT, IAS 152KTS,THE CO-PILOT DOOR WINDOW SEPARATED FROM AIRCRAFT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2G72 6U3  T  R00002RDE2NE                 
20070402001512007040200151CE  2007       4          2          40675            120070320G274145AS610023139   ACTUATOR                                BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              PITCH TRIM      INOPERATIVE     C  R71AO   OTHER                                                                                           F  FLT CONT AFFECTED                                                             DEDESCENT        1                      WP05790SS1550                   RK363                                   DIFFICULTY OCCURED UPON DESCENT.   PILOT RECIEVED A WARNING PITCH TRIM WAS NOT SYNCRONIZED WITH AUTOPILOT SYSTEM AND TO PREPARE FOR RESISTANCE WHEN AUTOPILOT IS DISCONNECTED. PITCH TRIM ACTUATOR WAS FOUND INOPERATIVE IN THE EMERGENCY MODE/AUTOPILOT MODE.  REPLACED PITCH TRIM UNIT AND RETURNED AIRCRAFT TO SERVICE. THIS AIRCRAFT WAS LAST INSPECTED ON 11-9-06 AT 1408.6 TT.                                                                                                                                                                                                                                                                                                                                                            2H72 4F4  FRTA16SW   E25EA                
20071204001072007120400107CE  2007       12         4          470884           120071105G4940CH3459          IGNITER         HONEYWELL   RE100       LEAR  45    45LEAR      5170805CE                                                               APU             BROKEN          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL09762EL549        P205        107                                     TIP OF IGNITER BROKE OFF AND WAS FOUND DURING COMPLIANCE WITH SB45-28-12.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F    RTT00008WI                     
20071003000052007100300005SO  2007       10         3          4757             220070925G8530AEC631397       CYLINDER        CONT                    CESSNA414   414A        2075907CE  CONT  O520  TSIO520NB   17040SO                              RT ENGINE       CRACKED         B  FCPRO   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      NM09919FA1120       276632R     414A0628    276632R                     PILOT WAS INFORMED BY LINE PERSONNEL DURING TAXI TO TIE DOWN, THAT ENGINE WAS MAKING A LOUD (AIR PULSING) SOUND. PILOT COULD ONLY HEAR THE SOUND AFTER REMOVING NOISE CANCELLING HEAD SET. PILOT THEN SHUTDOWN ENGINE. INSPECTION REVEALED THE NR 4 CYLINDER TO BE CRACKED AT THE PARTING SURFACE. EXHAUST WAS ESCAPING FROM THE CRACK CAUSING THE (AIR PULSING) SOUND.                                                                                                                                                                                                                                                                                                                                                                         1L72 3O3  O  A7CE    E8CE                 
20071214003462007121400346CE  2007       12         14         68DA             120070213G5512                SKIN                                    BEECH 100   B100        1152919CE  GARRTTTPE331TPE331*     01514WP                              HORIZONTAL STAB WRINKLED        B  ODARO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA2168DA                        BE14                                    DURING ROUTINE MAINTENANCE, MECHANIC DISCOVERED THAT THE HORIZONTAL STABILIZER SKIN WAS WRINKLED AT THE AFT RT ATTACH PIVOT POINT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 4T3  T  A14CE   E2WE                 
20070625000082007062500008GL  2007       6          25         A101913          220070612G726023038229        GEAR            ALLSN       T63A720                                        ALLSN 250C  T63A720     03002GL                              GEARBOX ASSY    FRACTURED       B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA25                NA                      AE405995                    ENGINE WAS SENT FOR REPAIR DUE TO GENERATING METAL.  UPON DISASSEMBLY FOUND THAT THE SHAFT ON THE FORWARD SIDE OF THE CENTRIFUGAL BREATHER GEAR WAS FRACTURED IN THE AREA OF THE RADIUS WHERE THE SHAFT JOINS THE GEAR.  THE RELATIVE MOTION BETWEEN THE SHAFT AND THE GEAR WAS THE CAUSE OF METAL GENERATION.                                                                                                                                                                                                                                                                                                                                                                                                                                         3  U          E4CE                 
20070625000092007062500009GL  2007       6          25         A1019131         220070612G726023038229        GEAR SHAFT      ALLSN       T63A720                                        ALLSN 250C  T63A720     03002GL                              GEARBOX ASSY    FRACTURED       B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA25                NA                      AE405995                    ENGINE WAS SENT FOR REPAIR DUE TO GENERATING METAL.  UPON DISASSEMBLY FOUND THAT THE SHAFT ON THE FORWARD SIDE OF THE CENTRIFUGAL BREATHER GEAR WAS FRACTURED IN THE AREA OF THE RADIUS WHERE THE SHAFT JOINS THE GEAR.  THE RELATIVE MOTION BETWEEN THE SHAFT AND THE GEAR WAS THE CAUSE OF METAL GENERATION.                                                                                                                                                                                                                                                                                                                                                                                                                                         3  U          E4CE                 
20071204002932007120400293CE  2007       12         4          AFASVRA3181      120071114G2432G25             BATTERY                                 CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA                              MASTER          OVERHEATED      D      K   NONE                                                                                            MJ OVER TEMP                 WARNING INDICATION                                  CRCRUISE         1                      NM039582V556                    17264384    L4623627A                   AIRCRAFT 12 VOLT BATTERY OVERHEATED CAUSING: ELECTROLYTE BOILING OVER, CORRODING OF ALUMINUM BATTERY BOX, LANDING LIGHT PLASTIC SWITCH MELTING, LANDING LIGHT PLASTIC CONNECTOR IN COWLING MELTING, LANDING LIGHT INOP AND ALTERNATOR FAILURE WITHOUT THE LANDING LIGHT CB TRIPPING.  PILOTS COMPLYING WITH FAA RECOMMENDATIONS OF LEAVING LANDING LIGHTS ON WITHIN 5 NM OF AIRPORT ARE THE CAUSE OF THIS PROBLEM DURING TRAINING SORTIES OF 1 TO 2 HOURS WITH THE LANDING LIGHTS ON FOR THE DU RATION OF FLIGHT. THESE AIRCRAFT ARE FLOWN IN A PILOT TRAINING OPERATION WHERE SORTIES ARE 1 TO 2 HOURS ENDURANCE AND 8 TO 10 TAKEOFFS AND LANDINGS WITH THE LANDING LIGHT/LIGHTS ON FOR THE DURATION OF THE FLIGHT.                            1H71 3O3  ONT3A12    E274                 
20070409000332007040900033SO  2007       4          9          AMCR200700001    120070329G2822B12520          PRESSURE SWITCH                         GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6118          EU                              BOOST PUMP      FAILED          B  AMCRO   OTHER                                                                                           J  WARNING INDICATION                                                            DEDESCENT        1                      GL09706VA1267                   1528                                    DURING DESCENT, THE RT MAIN FUEL PUMP FAILED. MAINTENANCE FOUND THAT THE FUEL PRESSURE SWITCH ON THE RT MAIN FUEL PUMP HAD FAILED. THIS IS THE SECOND FAILURE OF A PUMP PRESSURE SWITCH WE KNOW OF WITHIN THE LAST 4 MONTHS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA12EA   E25NE                
20070625000122007062500012NE  2007       6          25         AMCR200700002    120070612G261261423473205     FIRE DETECTOR                           SKRSKYS76   S76B        8143007NE                                                               NR 1 ENGINE     FAULTY          B  AMCRO   OTHER                                                                                           N  FALSE WARNING                                                                 TXTAXI/GRND HDL  1                      GL09520AC2282                   760380                                  UPON STARTER ENGAGEMENT FOR FIRST ENGINE START (EITHER ENGINE), THE NR 1 ENGINE FIRE ANNUNCIATOR WOULD ILLUMINATE ALONG WITH A FIRE TONE, BUT NO T-HANDLE ILLUMINATION. ILLUMINATION AND TONE WOULD CEASE AROUND 35-45% RPM. ALL FIRE DETECTION TESTS WOULD CHECK OK. REPLACEMENT OF NR 1 BOTTOM FLAME DETECTOR FIXED PROBLEM.                                                                                                                                                                                                                                                                                                                                                                                                                  1G72 4U      H1NE                         
20070718002202007071800220NE  2007       7          18         AMCR200700003    120070709G3240C20497000       BRAKE ASSY                              SKRSKYS92   S92A               NE                                                               MLG             BINDING         B  AMCRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL09252DV572                    920009                                  DURING WHEEL CHANGE (LT OB) COULD NOT REMOVE THE WHEEL OFF OF AXLE. FOUND ONE OF THE CENTER STATORS (A35579) OF THE BRAKE ASSY TO BE PROTRUDING OUT OF THE PACK. THE STATOR CUT INTO THE WHEEL PREVENTING THE REMOVAL. WE DID NOT TEARDOWN THE BRAKE BUT SUSPECT EITHER THE STATOR IS OUT OF ROUND OR HAS ID DAMAGE, OR THE TORQUE TUBE IS DAMAGED ALLOWING STATOR TO SHIFT BEYOND THE PACK CIRCUMFERENCE. P/N 78286/92250-00801-102.                                                                                                                                                                                                                                                                                                           2G72 4U      R00024BO                     
20071214003512007121400351CE  2007       12         14         AMCR200700004    120071207G5753NAS509L6        JAM-NUT                                 CESSNA525   525         2076601CE  WILINTFJ44  FJ44        66000GL                              TE FLAPS        WRONG PART      B  AMCRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL09279DV536                    0070                                    DURING COMPLIANCE WITH SL525B-27-01 WHICH IS CHECKING FLAP PUSH ROD FOR IMPROPER SAFETY WIRING, FOUND THAT THE AFT JAM NUT (NAS509L6) WAS UP AGAINST THE CENTER STUD (6365028-10) RATHER THAN TIGHT AGAINST THE ROD END TUBE (6365028-9). EVERYTHING WAS SAFETIED IN THIS POSITION.                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 4F4  FRTA1WI    E3GL                 
20070313000182007031300018GL  2007       3          13         AMTR02022007     120070202G5314                KEELBEAM                                AMTR  AIRCARSPENCERAIRCR       GL                                                               FUSLEAGE        CORRODED        G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE0141RH 2437                                                           DURING AN ACCIDENT INVESTIGATION OF A S12D, THE AIRFRAME REAR KEEL SUPPORT WAS FOUND TO HAVE EXCESSIVE CORROSION AND THE WOODEN STRUCTURE ATTACHED TO THE KEEL WAS DRY ROTTED. ALTHOUGH THE CORROSION IS EVIDENT, WE BELIEVE IT WAS NOT A CAUSE OF THE ACCIDENT. THE AIRCRAFT WAS BUILT IN 1975 AND WAS OPERATED IN A SALT WATER ENVIRONMENT. THE AIRCRAFT HAD JUST RECEIVED A CONDITION INSPECTION. THERE WAS NO ACCESS TO INSPECT THE KEEL SUPPORT WHICH IS LOCATED AFT OF THE PASSENGER COMPARTMENT. IT IS RECOMMENDED THAT AN ACCESS PANEL BE MADE TO INSPECT THE KEEL ASSEMBLY AND THAT IT BE INSPECTED AT LEAST EVERY CONDITION INSPECTION.                                                                                               1H71 3O      EXPA1H71                     
20070824002422007082400242SW  2007       8          24         AOC0701          120070816G6210                BEARING                                 BELL  412   412         1182202SW  PWA   PT6T  PT6T3B      52045NE                              PITCH LINK      DAMAGED         B  R29RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW1931893                       33110                                   DURING A PREFLIGHT INSPECTION OF THE SUBJECT AIRCRAFT, A PITCH CHANGE LINK BEARING (ATTACHED TO THE DRIVER END) APPEARED TO BE WORN. THE PILOT ATTEMPTED TO MOVE THE DRIVER TO CHECK FOR WEAR BUT THE BEARING, BOLT AND DRIVER WERE TIGHT. THE PILOT THEN OBSERVED THE BEARING WHILE THE OTHER PILOT PULLED SLIGHTLY UP ON THE COLLECTIVE CONTROL. AS THIS OCCURRED, THE PILOT FOUND THAT THE BOLT AND BEARING WERE MOVING APPROXIMATELY .1875 INCH. FURTHER INSPECTION REVEALED THAT THE STEEL BUSHING ON THE DRIVER, TRAILING (NUT) SIDE, WAS WORN DOWN CONSIDERABLY (.0001 - .0002 INCH OF STEEL REMAINING). HAD THIS BEEN ALLOWED TO CONTINUE, THE BOLT WOULD HAVE STARTED TO WEAR INTO THE SOFTER METAL OF THE DRIVER, EVENTUALLY CAUSING L1G72 4U4  U  H4SW    E22EA                
20070711001392007071100139EU  2007       7          11         AS350B3          120070628G6320350A32031002    GEARBOX                                 SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B1   60056NE                                              WARNING LIGHT   B      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      EA17808CP161                    4151        23335                       MGB CHIP LIGHT CAME ON IN FLIGHT. REMOVED CHIP PLUGS FROM THE MGB AND THE MAST FOUND PARTICLES ON THE MGB PLUG LESS THAN LIMITS CALLED OUT IN AEC AS350B3 SPM 20.08.01.601 NOTHING ON THE MAST PLUG.  PERFORMED 10 MIN. HOVER AND RECHECKED CHIP PLUGS IAW AEC AS350B3 MWC 05.53.00.608 NO MORE PARTICLES FOUND AND NO RE-OCCURRENCE OF THE CHIP LIGHT.                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  U  H9EU    E00054EN             
20071213002852007121300285CE  2007       12         13         ATL07LA057       120070319G2810                FUEL CELL                               BEECH 95    95B55       1152729CE  CONT  O470  IO470*      17026SO                              RT WING         LEAKING         G  E7TAED  ENGINE SHUTDOWN         RETURN TO BLOCK                                                         KA FLUID LOSS                FLAME/FIRE                                          TXTAXI/GRND HDL  1                      SO11500JP                       2396                                    DURING START OF RT ENGINE, PILOT REPORTED HEARING A LOUD THUMP, NOTED FIRE COMING FROM THE BOTTOM OF THE RT COWLING.  SHUTDOWN ENGINES, EVACUATED AIRCRAFT, AND NOTED APPARENT EXPLOSION HAD OCCURRED IN RT WING.    VISUAL INSPECTION DID NOT REVEAL CAUSE OF EVENT.  WING STILL HELD APPROXIMATELY 40 GALLONS OF FUEL AND WAS NOT LEAKING ALTHOUGH BOX CELL LINER HAD BEEN CRACKED OPEN FROM FORCE OF EXPLOSION.  FUEL TRUCK WAS DISPATCHED AND WING WAS FULLY TOPPED OFF TO INSPECT FOR LEAKS; NONE WERE NOTED.   AIR IN RT FUEL SYSTEM WAS DISPLACED AND AFTER APPROXIMATELY 10 MINUTES A LEAK WAS DETECTED IN THE RT WHEEL WELL.  FURTHER INVESTIGATION REVEALED THIS LEAK WAS ORIGINATING FROM A B-NUT ON THE OUTPUT SIDE OF THE AUXILIARY1L72 3O3  ORT3A16    E1CE                 
20070615002202007061500220CE  2007       6          15         B3OR2007131      120070511G2731556545092       ACTUATOR                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              ZONE 300        BINDING         B  B3ORK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW0326621                       5500593                                 A NEWLY OVERHAULED ELEVATOR TRIM TAB ACTUATOR WAS BINDING AND WOULD NOT PROVIDE ADEQUATE DEFLECTION AT THE TRIM TAB ONCE INSTALLED.  FURTHER INVESTIGATION REVEALED THAT THIS ACTUATOR HAD EXCESSIVE PLAY AT THE END BEARINGS AND THAT THE PRIMARY SPROCKET PN WAS INCORRECT RELATIVE TO THE ASSEMBLY PN. THIS ASSEMBLY WAS OVERHAULED UNDER WORK ORDER NR 15356 ON 4/2/2002.  THE ITEM WAS RETURNED TO THE OVERHAULING AGENCY FOR WARRANTY REPAIR.                                                                                                                                                                                                                                                                                             1L72 4F4  F  A22CE   E1NE                 
20070615002192007061500219CE  2007       6          15         B3OR2007138      120070518G2731556545098       ACTUATOR                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              ELEVATOR TRIM   BINDING         B  B3ORK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW0326621                       5500593                                 FOLLOWING INSTALLATION OF A NEWLY OVERHAULED ELEVATOR TRIM TAB ACTUATOR, PARTIAL BINDING OF THE ACTUATOR OCCURRED.  FURTHER INVESTIGATION REVEALED THAT THIS ACTUATOR HAD EXCESSIVELY WORN END BEARINGS ALLOWING LATERAL PLAY IN INTERNAL JACKSCREWS SUFFICIENT TO CAUSE BINDING ONCE INSTALLED.  ALSO DISCOVERED THAT THE LUBRICANT IN THIS ASSEMBLY WAS GREY IN COLOR, WHICH IS CONTRARY TO THE LOW MOISTURE CONTENT GREASE (PINK OR WHITE IN COLOR) STRICTLY SPECIFIED IN THE COMPONENT MM. THIS ASSEMBLY WAS RECENTLY OVERHAULED UNDER WO NR 1059 ON 3/20/2007.                                                                                                                                                                             1L72 4F4  F  A22CE   E1NE                 
20070808000282007080800028NM  2007       8          8          BAI71007         120070710G6300A1902           BELT                                    ROBSINR22   R22BETAII   7640110NM  LYC   O360  O360A1D     41514EA                              M/R DRIVE       BROKEN          B      B   EMER. DESCENT                                                                                   RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      SO157109C1085                   2952                                    MAIN ROTOR DRIVE BELTS SEPARATED IN FLIGHT CAUSING THE CLUTCH ACTUATOR TO RUN EXCESSIVELY. THE OVER-TRAVEL LIMIT-SWITCH LANYARD WAS SEVERED BY A PORTION OF THE BROKEN BELTS AND DID NOT PERFORM IT'S INTENDED FUNCTION. THE PIC HAD TO DISABLED THE CLUTCH ACTUATOR SYSTEM BY PULLING THE CLUTCH CIRCUIT BREAKER AND THEN AUTO ROTATED TO THE GROUND. THERE WAS NO ADDITIONAL DAMAGE TO THE AIRCRAFT OR INJURY TO OCCUPANTS AS A RESULT OF THE AUTOROTATION.                                                                                                                                                                                                                                                                                   1G71 3O3  O  H10WE   E286                 
20070129001952007012900195EA  2007       1          29         CA070103011      220070104G7250                TURBINE BLADES                          DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE          FRACTURED       W      O   OTHER                                                                                           RX PARTIAL RPM/PWR LOSS      ENGINE FLAMEOUT                                     CRCRUISE         1                      CA                                          41266                       (CAN) ENGINE OIL PRESSURE AND TORQUE WERE SEEN TO FLUCTUATE IN FLIGHT FOLLOWED BY A LOUD NOISE AND AN ENGINE FLAMEOUT.  SUBSEQUENT INSPECTION REVEALED METAL IN THE ENGINE OIL AND FRACTURED POWER TURBINE BLADES.  MFG WILL MONITOR THE INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070103011)                                                                                                                                                                                                                                                                                                                                                                                                              1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070129002012007012900201GL  2007       1          29         CA070105004      220070105G72406899237         COMBUSTION CASE ALLSN       250C28B     BELL  206   206L1       1182107SW  ALLSN 250C  250C28B     03013GL                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  CAE860657               CAE860657                   (CAN) DURING A 200 HR INSPECTION A CRACK WAS FOUND IN THE ARM PIT AREA OF THE OUTER COMBUSTION CASE.  CASE REPLACED. (TC NR 20070105004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3U3  U  H2SW    E1GL                 
20070507002402007050700240SW  2007       5          7          CA070105005      120070105G7921206061432031    IMPELLER        BELL                    BELL  206   206L1       1182107SW  ALLSN 250C  250C28B     03013GL                              OIL COOLER      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  VN7184                                              (CAN) 300 HR NDT FOUND CRACKS IN THE WEB AREA.  PART REPLACED. (TC NR 20070105005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1G71 3U3  U  H2SW    E1GL                 
20070507002412007050700241CE  2007       5          7          CA070105006      120070104G561010138402523     WINDSHIELD                              BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  COCKPIT         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         DEDESCENT        1                      CA                                                                      (CAN) DURING PRESSURIZED FLIGHT THE LT WINDSHIELD CRACKED IN SEVERAL PLACES ALL ALONG THE IB SECTION OF THE WINDOW. THE WINDOW WAS ORIGINALLY A REPAIRED WINDOW AND WAS INSTALLED FOR 1512.9HRS/1450CYCLES BEFORE FAILING. (TC NR 20070105006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070129002022007012900202CE  2007       1          29         CA070105007      120070103G243566082019        SHAFT                                   LEAR  35    35A         5170602CE  GARRTTTFE731TFE73122B   01518WP                              GENERATOR       SHEARED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA            616                                                       (CAN) LT GENERATOR CAME OFF LINE .5 HR BEFORE LANDING . THE INDICATOR SHOWED 0 AMPS, A RESET WAS ATTEMPED BUT DID NOT COME ONLINE. WHEN MAINTENANCE REMOVED THE GENERATOR FOR INSPECTION, THE GENERATOR SHAFT WAS FOUND SHEARED. THE GENERATOR WAS INSPECTED FURTHER AND ROTATED FREELY. CAUSE OF SHEARED SHAFT IS UNKNOWN. (TC NR 20070105007)                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  F  A10CE   E6WE                 
20070508001902007050800190CE  2007       5          8          CA070108001      120070103G3220                LANDING GEAR                            BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  NOSE            INOPERATIVE     W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) AIRCRAFT EXPERIENCED NO NOSE GEAR. (TC NR 20070108001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070508001912007050800191CE  2007       5          8          CA070108002      120070103G3260404EN16         DOWNLOCK SWITCH                         BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  MLG             MALFUNCTIONED   W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                      CVBCBNM7CXZZ    (CAN) THE AIRCRAFT ORIGINALLY EXPERIENCED A GEAR WARNING SYSTEM FAILURE ON APPROACH.  SUBSEQUENTLY, THE DOWNLOCK SWITCHES WERE CLEANED AND LUBRICATED AND THE SYSTEM TESTED SERVICEABLE. THE NEXT FLIGHT HAD A LT MAIN GEAR INDICATION FAILURE, EMERGENCY PROCEDURES WERE FOLLOWED AND THE LT GEAR INDICATION WORKED PRIOR TO TOUCH DOWN. THE AIRCRAFT WAS RETURNED TO MAINTENANCE AND THE LANDING GEAR SYSTEM WAS TROUBLESHOT EXTENSIVELY AND TEST FLOWN EACH TIME WORK WAS CARRIED OUT  UNSUCCESSFULLY.  THE SNAG ONLY OCCURRED AT HIGHER ALTITUDES OR COLDER TEMPERATURES. THE LT MAIN GEAR SWITCH WAS REPLACED DUE TO SUSPECT WATER PROPAGATION AND FREEZING. THE AIRCRAFT WAS TEST FLOWN AT THE SAME ALTITUDES AND WAS SUCCESSFUL. THE AIRC2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070129002042007012900204EA  2007       1          29         CA070108003      120070108G2910TA3050052403    FAIRLEAD                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              HYDRAULIC SYS   WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1471714717                                                     (CAN) DURING MAINTENANCE INSPECTION, FOUND FAIRLEAD (CLAMP) ON NR 1 HYDRAULIC SYSTEM LINES FAIRLEAD IN AFT FUSELAGE (APU COMPARTMENT) WORN. [IPC 29-11-00 FIG 15 (H) ITEM 395. BLOCK HAS 3 HOLES FOR CLAMPING HYDRAULIC LINES AND CENTER HOLE (PRESSURE LINE) MATERIAL WORN THROUGH TO CASE DRAIN LINE HOLE, ALLOWING PRESSURE LINE AND CASE DRAIN LINE TO START CHAFFING. SEVERAL SIMILAR CLAMPS IN THIS AREA ALSO EXHIBITING SIMILAR SIGNS OF WEAR. FAIRLEAD (CLAMP BLOCK) ASSEMBLY REPLACED. AIRCRAFT RETURNED TO SERVICE. (TC NR 20070108003)                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20070129002132007012900213WP  2007       1          29         CA070108009      220070105G7200TPE33111U6      ENGINE                                  FRCHLDSA227 SA227CC     3377522SW  GARRTTTPE331TPE33112UA  01514WP  MCAULY4HFR344HFR34C652  NE  LEFT            DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  APAPPROACH       1                      CA            366                                                       (CAN) UPON SHORT FINAL A "POP" WAS HEARD SIMILAR TO THE SOUND OF A DOOR SEAL.  THE AIRCRAFT YAWED A BIT YET NOT ENOEGH TO ALERT THE FLIGHT CREW THAT IT WAS ANYTHING MORE THAN TURBULENCE.  OIL PRESSURE WAS NOTED TO BE DROPPING. AN ENGINE FAILURE OCCURED ON THE LH SIDE.  ENGINE WAS SHUT DOWN ON THE RUNWAY AND NOT IN THE AIR.  UPON MAINTENANCE INITIAL REVIEW MOST OF THE DAMAGE WAS AT THE BACK OF THE ENGINE.  THERE WAS NO NOTED DAMAGE AT THE FRONT, GEARBOX, OF THE ENGINE.  FURTHER INVESTIGATION WIL BE CARRIED WHEN ENGINE ARRIVES AT THE OEM.  MORE DETAILS THEN.   (TC# 20070108009)                                                                                                                                          2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20070509000632007050900063CE  2007       5          9          CA070108010      120070105G5700817861018       BOLT                                    BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  WING            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1437                                                           (CAN) SCHEDULED WING BOLT INSPECTION, NOTED RT UPPER AFT WING BOLT CRACKED ON BOLT  HEAD TO SHANK RADIUS. BOLT REPLACED WITH NEW. (TC NR 20070108010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070129002192007012900219NM  2007       1          29         CA070109002      120070108G3040                INSULATION      SIERRACIN   80260007    DHAV  DHC8  DHC8*              NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  WINDSHIELD HEAT OUT OF POSITION W      H   DEACTIVATE SYST/CIRCUITS                                                                        WB INADEQUATE Q C            SMOKE/FUMES/ODORS/SPARKS                            CRCRUISE         1                      CA       30         729                                                 (CAN) INVESTIGATING SMELL OF SMOKE IN COCKPIT AFTER CREW TURNED ON WINDSHIELD HEAT.  FOUND THE LUG ON 3041-TB1 POSITION L2 HAD INSULATION BETWEEN THE SCREW HEAD AND THE LUG.  REMOVED THE INSULATION FROM UNDER THE HEAD OF THE SCREW. (TC NR 20070109002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070129002222007012900222SO  2007       1          29         CA070109006      220070109G8530AEC648005PL     PISTON RING                             CESSNA206   206CESSNA   2073302CE  CONT  O520  IO520F      17032SO                              ENGINE          SEPARATED       W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       1344 1344                                                      (CAN) MATERIAL FROM THE FACE OF THE TOP COMPRESSION RING HAD FLAKED AWAY ON PISTONS NR1, NR2, NR4, AND NR6 (TC NR 20070109006).                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3O3  O  A4CE    E5CE                 
20070129002242007012900224EA  2007       1          29         CA070110001      220070110G7200                ENGINE                                                                     PWA   PT6   PT6A34      52043EA                                              FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA       316127695                                                      (CAN) (IFSD WITH MAJOR INTERNAL DAMAGE). THE ENGINE SUFFERED SEVERE DISTRESS WITH COMPLETE LOSS OF ALL TURBINE BLADES AND ASSOCIATED STATIC COMPONENTS. THE GG CASE AND EXHAUST DUCT WERE SUBJECTED TO SEVERE TORQUE LOADS AND WERE FOUND DISTORTED.  ENGINE WAS CONVERTED STC SE96-02.  DURING FLIGHT AND FOLLOWING A LOUD BANG FROM THE ENGINE, AN ENGINE SHUTDOWN WAS CARRIED OUT.  CSN: 48301, CSO 10087 TSHSI: 64, CSHSI 25.  THIS ENGINE CONVERTED VIA STC SE96-02 (TC NR 20070110001).                                                                                                                                                                                                                                                          4  T          E4EA                 
20070312000482007031200048NM  2007       3          12         CA070110004      120070109G3240                BRAKE DISC      BFGOODRICH              DHAV  DHC5  DHC5A       2803018NM                                                               NR 1 BRAKES     DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            2492  411                                                 (CAN) DURING B4 CHECK ON THE AIRCRAFT, THE NR 1 TIRE WAS REMOVED TO SERVICE THE WHEEL BEARINGS, AT THIS TIME, A PIECE OF THE BRAKE DISC FELL FROM THE BRAKE UNIT. THE BRAKE UNIT WAS REMOVED AND A SERVICEABLE ONE WAS INSTALLED. UPON INVESTIGATION OF THE UNIT IT HAS BEEN DETERMINED THAT A BRAKE ADJUSTER HAD SEIZED RESULTING IN THE BRAKE DISC SITTING AT AN ANGLE INSTEAD OF AT 90 DEGREES TO THE AXLE LINE, THIS RESULTING FORCE CAUSED STRESS TO BE PLACED ON THE DISC RESULTING IN ITS FRACTURE, THIS ALSO CAUSED THE BRAKE PUCKS TO SCORE AND DAMAGE DISC FACE. IAW THE INSPECTION SCHEDULE, THE MAIN WHEELS ARE REMOVED EVERY 200 HOURS (B CHECK) TO INSPECT THE BRAKES AND WHEEL BEARINGS. THERE WAS NO FAULTS NOTED ON THE LAST B32H72 4T    RT                             
20070129002292007012900229EA  2007       1          29         CA070111003      120070109G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              WING            JAMMED          W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) FLAPS FAILED ON APPROACH WHEN SELECTED TO 8 DEGREES, FLAPS DID NOT MOVE AND FLAP FAIL EICAS MESSAGE, OAT WAS -30 DEGREES ON APPROACH, DURING CRUISE -58 DEGREES C, FAULTS CODES BEING RETRIEVED AND AIRCRAFT BEING PREPARED FOR FERRY FOR FOLLOW UP. (801573 1/9/2007 19:04) RESET FLAP SYSTEM AND SELECT FLAPS TO 8 DEGREES FOR FERRY FLIGHT, REFERENCE RJ-SL-27-077 (801573 1/9/2007 20:14).  FLAPS RESET. AIRCRAFT FERRIED (803789 1/10/2007 07:29) (TC NR 20070111003).                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20070129002302007012900230EA  2007       1          29         CA070111004      120070110G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              WING            JAMMED          W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) CREW REPORTED ON SHORT FINAL, WHEN SELECTING FLAPS TO 8 DEGREE THE FLAP FAIL MESSAGE APPEARED AND THE FLAPS DID NOT MOVE OUT OF 0 DEGREE. MAINTENANCE UNABLE TO GET CODES.  A/C FERRIED FOR FURTHER INVESTIGATION AND TROUBLESHOOTING. (TC NR 20070111004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20070129002312007012900231EA  2007       1          29         CA070111005      120070110G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              WING            JAMMED          W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) FLAPS SELECTED TO 8 DEGREES, NO ISSUES, THEN SELECTED TO 20 DEGREES, NO ISSUES, FLAPS 30 SELECTED NO ISSUES, UPON SELECTION TO 45 DEGREES, FLAP FAIL AND THE FLAPS LOCKED AT 30 DEGREES, OAT -30 IN FLIGHT, - 15 DEGREES OPN APPROACH, TEMP WAS -15. HAS OBTAINED FAULT CODES AND THEY HAVE BEEN FORWARDED TO TECH OPS (803789 1/10/2007 17:14). A/C GROUNDED FOR FURTHER INVESTIGATION AND TROUBLESHOOTING. (TC NR 20070111005)                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20070129002322007012900232EA  2007       1          29         CA070111006      120070110G2750                FLAP                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              WING            FROZEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             NRNOT REPORTED   1                      CA                                                                      (CAN) FLAP FAIL AT 20. ON APPROACH, ON FLAP EXTENSION, THEY FROZE AT 20 DEGREES.   OAT WAS ABOUT -25 DEGREES C AT THE TIME, ALTHOUGH THEY WERE ABOUT 1 HOUR AND 10 MINUTES IN FLIGHT AT ABOUT -50 DEGREES FOR MOST OF THE FLIGHT. AIRSPEED WAS 170 KNOTS AT THE TIME OF THE FAILURE.   (TC NR 20070111006)                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA21EA   E15NE                
20070129002332007012900233GL  2007       1          29         CA070111010      320070108G6110HCB4MP3A        PROPELLER                                                                                                   HARTZLHCB4M HCB4MP3     GL                  DAMAGED         W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       1678732                                                        (CAN) PROPELLER WAS RECEIVED FOR COMPLIANCE WITH AD 2006-24-07. PROPELLER PREVIOUSLY OVERHAULED ON SEPTEMBER 20, 2000. THE PROPELLER WAS DISSASSEMBLED AND THE FOLLOWING FINDINGS  WERE CORRECTED. (4) LOW STOP RODS WERE CORRODED BEYOND REPAIR. (4) BLADE CLAMP ASSEMBLIES WERE REPLACED DUE TO CORROSION AND LACK OF PLATING. PISTON HAD A CORROSION PIT IN FELT RING GROOVE. HUB WAS REPLACED DUE TO CORROSION/RUST IN PILOT TUBES. NR 4 BLADE HAD WATER IN BLADE BORE BEHIND GREASE BUT NO EVIDENCE OF CORROSION. COUNTERWEIGHT BOLTS WERE ALL RUSTED AND WATER WAS FOUND IN BLADE CLAMP COUNTERWEIGHT BOLT HOLES. (TC NR 20070111010)                                                                                                                                  6  CP56GL    
20070129002342007012900234EA  2007       1          29         CA070111011      120070110G2750                FLAP                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              WING            OBSTRUCTED      W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             NRNOT REPORTED   1                      CA                                                                      (CAN) FLAPS FAILED ON RETRACTION AFTER LANDING L 5 DEG, R 6 DEG. AFTER LANDING, FOUND SNOW COMPACTED, ALL SNOW REMOVED, FLAPS CYCLED.  (TC NR 20070111011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA21EA   E15NE                
20070129002352007012900235EU  2007       1          29         CA070111012      120070111G5610                WINDOW                                  BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 M  OVER TEMP                                                                     CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB THE FIRST OFFICERS MAIN WINDOW CRACKED. THE AIRCRAFT RETURNED TO POINT OF DEPARATURE WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE WINDOW AND THE AIRCRAFT WAS RETURNED TO SERVICE.  (TC NR 20070111012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 3T4  T  A24EU   A196    6  CP899     
20070129002362007012900236EA  2007       1          29         CA070111013      220070108G7310                FUEL LINE                               BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA                              ENGINE          CHAFED          W      K   NONE                                                                                            K  FLUID LOSS                                                                    NRNOT REPORTED   1                      CA                                                                      (CAN) THE FLIGHT CREW REPORTED FUEL LEAKAGE FROM THE RT ENGINE AREA AFTER SHUTDOWN. THE ENGINE COWLING WAS REMOVED AND INVESTIGATION HAD SHOWN THAT THE ENGINE DRIVEN FUEL PUMP TO FCU LINE HAD CHAFED AN THE BACK EDGE OF THE FCU.  THE LINE IS ON CONDITION AND NOT A TIMED UNIT.  A FLEET CAMPAIGN AND TECHNICAL INFORMATION BULLETIN WAS RELEASED TO ENSURE CORRECT ROUTING OF THE LINE AND ADEQUATE PROTECTION. ANY SUSPECT LINES REPLACED. (TC NR 20070111013)                                                                                                                                                                                                                                                                            2L72 4T4  TRTA24CE   E4EA                 
20070129002382007012900238NE  2007       1          29         CA070111015      220070111G73103035987         FUEL LINE                               DHAV  DHC8  DHC8202     2809007NM  PWA   120   PW123D      52152NE  HAMSTD14SF  14SF23      NE  ENGINE          CHAFED          W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) FUEL LEAK AT ENGINE FIREWALL PRESSURE LINE. THE LINE WAS DAMAGED BY CHAFFING ON COLLAR (P/N 3043536-01A) AND RETAINING PLATE (P/N 3043535-01). POST SB21460.  2 OTHER LINES COVERED BY THE SAME SB (INCORPORATED IN DEC.2001) SHOWED SAME DAMAGE AND NEEDS REPLACEMENT. (TC NR 20070111015)                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070129002392007012900239    2007       1          29         CA070111017      420070104G2360                STRUCTURE                               BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33112UHR      WP  ROTOL R333  R333482F12  GL  FUSELAGE        UNBONDED        W      O   OTHER                                                                                           G  MULTIPLE FAILURE                                                              CRCRUISE         1                      CA                                                                      (CAN) CREW REPORTED THAT WHEN THE AIRCRAFT ENTERED INTO A CLOUD, THE RADIOS BECAME UNREADABLE. ALL RADIO NAVIGATION EQUIPMENT BECAME UNRELIABLE AS WELL AS THE GPS SYSTEM. AIRCRAFT ARRIVED AT MTC. BASE AND AVIONICS STATIC SPECIALIST CONTRACTED. P-STATIC TEST CARRIED OUT AND FOUND BONDING ISSUES ON MULTIPLE AIRFRAME COMPONENTS. REPAIRS CARRIED OUT AND P-STATIC TEST CARRIED OUT AGAIN. NO FURTHER FAULTS. (TC NR 20070111017)                                                                                                                                                                                                                                                                                                         2L72 4T4  TRTBA15CAA E4WE    6  CP61GL    
20070509000642007050900064CE  2007       5          9          CA070111018      120070109G32335082021811      SHAFT                                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  NLG             CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN)  THE NOSE GEAR ACTUATOR WAS REMOVED TO PERFORM AN END PLAY CHECK. THE NOSE GEAR RETRACT DRIVE SPROCKET AND SHAFT (PN 50-820218-11) ASSEMBLY WAS REMOVED FOR CLEANING. INSPECTION OF THE DRIVE SPROCKET AND SHAFT FOUND THAT A CRACK HAD FORMED ON THE END DIAMETER (.745) THAT ENGAGES THE SUPPORT BEARING. THE CRACK STARTS AT THE END OF THE SHAFT, EXTENDS AXIALLY FOR .350 AND THEN EXTENDS RADIALLY FOR ANOTHER .400. THE CRACK HAS THE APPEARANCE OF STRESS CORROSION. THE TOTAL TIME AND TOTAL CYCLES OF THIS PART IS UNKNOWN. (TC NR 20070111018)                                                                                                                                                                                 1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070509000662007050900066EU  2007       5          9          CA070112002      120070106G55409408328506      BEARING                                 PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  RUDDER          WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION OF TAIL TOP ATTACH BOLT FOUND TO HAVE EXCESSIVE WEAR. RUDDER REMOVED AND NEW BOLT P/N 932.35.71.166 AND BEARING REPLACED. MFG AIRCRAFT NOTIFIED OF DEFECT.  (TC NR 20070112002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070820000322007082000032SW  2007       8          20         CA070112003      120070111G56102719442003      WINDSHIELD                              SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  COCKPIT         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3016                                                           (CAN) UPON LANDING THE FLIGHT CREW WITNESSED THE LT HEATED WINDSHIELD CRACK FROM THE LOWER RT CORNER TO THE UPPER CENTER PORTION OF THE WINDOW. THE LANDING WAS REPORTED AS NORMAL AND NO ABNORMAL INDICATIONS WERE NOTICED PRIOR TO FAILURE OF THE WINDOW.  UPON INSPECTION BY MAINTENANCE, THE WINDOW WAS FOUND CORRECTLY INSTALLED AND TRIMMED TO FIT CORRECTLY. THE ATTACHING SCREWS WERE TORQUE CHECKED AND A FEW WERE FOUND SLIGHTLY UNDERTORQUED. IT IS UNLIKELY THIS CAUSED THE FAILURE AS THIS OPERATOR HAS HAD SEVERAL IN FLIGHT HEATED WINDSHIELD FAILURES WITHIN THE LAST 24 MONTHS. ANOTHER OPERATOR OPERATING SIMILAR AIRCRAFT IN THE PNR HAS REPORTED INCREASED FAILURES AS WELL OF THESE HEATED WINDSHIELDS. THE WINDSHIELD IS B2L72 4T4  TRTA8SW    E4WE    5  CP10NE    
20070129002422007012900242NE  2007       1          29         CA070112004      320070110G6112                RELAY                                   DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  PROPELLER DE-ICEFAULTY          W      O   OTHER                                                                                           M  OVER TEMP                                                                     TXTAXI/GRND HDL  1                      CA                                                                      (CAN) WHEN AIRCRAFT POWER APPLIED, BLADES NR 2 AND NR 4 ON LT PROP HEATED AND BURNED OUT THE HEATER ELEMENTS.  FOR PRECAUTION RELAYS P/N KC-D4N AND E-387-C1 WERE REPLACED AND AIRCRAFT WAS TESTED WITH NO FAULTS FOUND. AIRFRAME HOURS=44789:11. CYCLES=48426. (TC NR 20070112004)                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070820000332007082000033EU  2007       8          20         CA070113001      120070102G53445531412027      HINGE                                   PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  PAX DOOR        CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7953 7953                                                      (CAN) AFTER A HEADS UP CONDITION FROM ANOTHER RCMP AIR SECTION.  AN INSPECTION OF CONDITION WAS CARRIED OUT ON MPI. THE PART INSPECTED WAS FOUND SEVERELY CORRODED AND IF LT UNCHECKED COULD AFFECT THE INTEGRITY OF THE CABIN DOOR FRAME.  THE HINGE PLATE MOUNTED AT THE BASE OF THE AIRSTAIR DOOR OPENING AND IS RIVETED TO THE DOOR SILL ASSY.  APPROXIMATELY 50 PERCENT OF THE HINGE WAS AFFECTED BY CORROSION.  THE CAUSE IS THOUGHT TO BE FROM SALT ON PASSENGER BOOTS IN WINTER OPERATIONS.  THE HINGE IS DIFFICULT TO INSPECT UNTIL DERIVATE FROM THE DOOR SILL ASSY.THE MFG HAD SEALED BETWEEN THE HINGE ASSY AND THE DOOR SILL WITH PRC AND THIS PREVENTED DOOR SILL DAMAGE. (TC NR 20070113001)                                     1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070129002452007012900245SO  2007       1          29         CA070114001      220070109G8530                EXHAUST VALVE                           CESSNA150   150M        2071830CE  CONT  O200  O200A       17020SO  MCAULY1A102 1A102OCM    GL  ENGINE          LEAKING         W      K   NONE                                                                                            R  PARTIAL RPM/PWR LOSS                                                          ININSP/MAINT     1                      CA            327                                                       (CAN) DURING ENGINE PERFORMANCE GROUND RUN AFTER INSPECTION, ENGINE WAS RUNNING ROUGH. ENGINE COMPRESSION CHECK CARRIED OUT AND CYLINDER NR 3 FAILED COMPRESSION CHECK AND AIR WAS LEAKING FROM THE EXHAUST.  ROUGH RUNNING DURING TAKEOFF WAS ALSO REPORTED BY PILOT PREVIOUSLY WHICH COULD NOT BE CONFIRMED DURING GROUND-RUN AT THAT TIME AND AIRCRAFT WAS TEST FLOWN SATISFACTORY. (TC NR 20070114001)                                                                                                                                                                                                                                                                                                                                      1H71 3O3  O  3A19    E252    5  NP918     
20070129002462007012900246EU  2007       1          29         CA070114002      220070112G7230GEJ818P060A     BOLT            CFMINT      CFM563                                         CFMINTCFM56 CFM563B2    13802EU                              FAN DISK        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  722356                                              (CAN) ENGINE WAS INDUCTED INTO SHOP FOR SCHEDULED MAINTENANCE. DURING THE SHOP VISIT THE FAN DISK WAS REMOVED FROM THE FAN ASSEMBLY AND ROUTED FOR OVERHAUL. THE DISK ATTACH BOLTS (QTY 30) WERE ROUTED FOR NDT INSPECTION.  FPI DETECTED ONE FAN DISK ATTACH BOLT WAS CRACKED FROM THE HEAD AND EXTENDING AXIALLY INTO THE SHANK.  FURTHER INSPECTION WITH A 10X MAGNIFYING GLASS REVEALED THAT THE CRACK HAD PROPAGATED FROM A FAINT AXIAL LINE ON THE SIDE OF THE HEAD THAT INITIALLY APPEARS TO BE A MFG DEFECT.  A SECOND BOLT (NOT CRACKED) WAS FOUND WITH THE IDENTICAL AXIAL LINE (SAME DIMENSION AND ANGLE) IN THE BOLT HEAD. REMAINING 28 BOLTS HAD NO DEFECTS NOTED.  ALL BOLTS INITIALLY APPEARED IN GOOD CONDITION WITH NO EVIDENCE       4  F          E21EU                
20070509000672007050900067    2007       5          9          CA070114003      420070104G3442066311400       INDICATOR                               BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  WEATHER RADAR   MALFUNCTIONED   W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA                              BB1343                                  (CAN) CREW REPORTS THAT IN CRUISE NOTED THE WEATHER RADAR FAILED AND IMMEDIATELY BOTH MAIN GENERATOR BUSES FAILED. CREWS RESET GENERATORS AND MONITORED BUS VOLTAGES AND LOADS, NORMAL. CREW THEN NOTED THE 28VDC CIRCUIT BREAKER POPPED ON THE AVIONICS BUS FOR THE WEATHER RADAR. BREAKER RESET BUT INDICATOR UNSERVICEABLE. AFTER AIRCRAFT RETURNED TO MTC BASE, MAINTENANCE CREW INSPECTED ELECTRICAL SYSTEM WITH NO FAULTS FOUND. RADAR INDICTOR REPLACED AND F/C NORMAL. UNSERVICEABLE WEATHER RADAR SENT TO REPAIR FACILITY WITH DETAILS OF INCIDENT AND REQUEST FOR WORK / STRIP REPORT. (TC 20070114003)                                                                                                                               1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070820000342007082000034EU  2007       8          20         CA070115001      120070109G2500                INSULATION                              PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  FUSELAGE        DETERIORATED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7963 7962                                                      (CAN) DURING AN INTERIOR REFURBISHMENT IT WAS NOTED THE FUSELAGE INSULATION FROM THE CABIN FLOOR AND UP HAD BADLY DEGRADED INSULATION BAGS.  THE THERMAL ACOUSTIC FOAM IS SURROUNDED BY BAGS WITH A VAPOR FOIL ON THE INNER SURFACE AND SEALED TO A THIN LATEX TYPE BARRIER ON THE OB SURFACE.  THE OUTER SURFACE HAD RUPTURED AND DEGRADED ON  ALL OUTER SURFACES OF THE INSULATION BAGS. ALL CABIN INSULATION HAD TO BE REMOVED AND REPAIRED WITH THE APPROVED TAPE.   IF LEFT UNCHECKED THIS COULD ADD  A CORROSION PROBLEM WITHIN THE FUSELAGE AS MOISTURE HAD WICKED INTO THE INSULATION IN SOME AREAS.  IF THE A/C WAS NOT HANGARED EACH NIGHT FOR DRYING IT COULD POSE A WEIGHT PROBLEM THAT WOULD BE UNKNOWN TO FLIGHT AND MAINTENANCE C1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070509000692007050900069SO  2007       5          9          CA070115002      120070109G2140D405065D793     HEATER                                  PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  CABIN           FAILED          W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA            649                                                       (CAN) PILOT REPORTED EXHAUST ODOR WHEN FRONT COMBUSTION HEATER WAS OPERATING. SOOT COLLECTED ON THE PILOT AND CO-PILOT WINDSHIELDS ABOVE THE DEFROST VENTS.  COMPLETED A HEATER DECAY TEST WHICH CONFIRMED THE BURNER CAN WAS DEFECTIVE. REMOVED THE HEATER FROM THE AIRCRAFT AND DISCOVERED 2 HOLES IN THE BURNER CAN APPROXIMATELY .5 INCH WIDE AND OPEN ABOUT .2500 INCH. HEATER WAS REPLACED WITH OVERHAULED UNIT AND AIRCRAFT RETURNED TO SERVICES. (TC NR 20070115002)                                                                                                                                                                                                                                                                    1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070129002552007012900255EA  2007       1          29         CA070115003      120070113G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              WING            JAMMED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) FLAPS FAILED UPON SELECTION TO 8 DEGREES, THEY DID NOT MOVE FROM 0 DEGREES, OAT -46 AT ALTITUDE, - 15 DEGREES ON APPROACH. AIRCRAFT LANDED FLAPS ZERO. (TC NR 20070115003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20070509000702007050900070NE  2007       5          9          CA070115004      220070115G7200                ENGINE                                  AIRBUS320   A320214     3930316EU  CFMINTCFM56 CFM565B4P        NE                              NR 1            FAILED          W      C   ABORTED TAKEOFF                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  TOTAKEOFF        1                      CA                                          757267                      (CAN) AFTER POWER SET FOR TAKEOFF, AND TAKEOFF ROLL COMMENCED, ENG NR 1 FAILED.  AIRCRAFT TAXIED BACK TO THE GATE. (TC NR 20070115004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA28NM   E38NE                
20070129002572007012900257    2007       1          29         CA070115005      420070115G2562E01G1           ELT                                                                                                                                     CABIN           FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) OVER THE LAST YEAR, HAVE HAD SEVERAL ACK ELTS E-01 WITH FAULTY (G) SWITCHES. FAULTS INCLUDE:  INTERMITTENT ACTIVATION, LIGHT ACTIVATION, NO ACTIVATION ACK HAS NO PUBLISHED DATA ON ACTIVATION BUT USES SIMILAR (G) SWITCH TO THE ELT WHICH HAS A PUBLISHED ACTIVATION OF 2 (GS).  HAVE ALSO SEEN SIMILAR FAULTS WITH ELTS.  (TC NR 20070115005)                                                                                                                                                                                                                                                                                                                                                                                                                                    
20070129002612007012900261EA  2007       1          29         CA070115007      220070112G8530                CYLINDER        LYC         LTIO540J2BD PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          SEPARATED       W      BA  EMER. DESCENT           UNSCHED LANDING                                                         R  PARTIAL RPM/PWR LOSS                                                          CLCLIMB          1                      CA            2175  L787161A                                            (CAN) ON THE CLIMB OUT A LOSS OF POWER OCCURED ON THE RT ENGINE.  THE MANIFOLD PRESSURE DROPPED FROM TAKEOFF POWER TO 30 INCHES. (TC NR 20070115007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070509000762007050900076SW  2007       5          9          CA070115014      120070102G5730204382          SKIN                                    AIRTRCAT802 AT802       0390305SW  PWA   PT6   PT6A67A     52043NE  HARTZLHCB5M HCB5MA3     GL  WING            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       452                                                            (CAN) DURING ANNUAL INSPECTION SEVERAL CRACKS WERE DETECTED AT THE RIVET HOLES WHERE THE FLAP BAY SKIN (PN 20438-2) ATTACH TO THE RIB FLANGES.  CRACKS WERE STOP DRILLED AND PLATE INSTALLED OVER THE RIB FLANGE AREA IAW AIR TRACTOR INSTRUCTIONS (ATTACHED).  THIS PROBLEM HAS BEEN FOUND ON EARLY SN AIRCRAFT (802-001 - 802A-0014), SUBSEQUENT S/N HAD EXTRA RIVETS INSTALLED BY MFG.  THIS AIRCRAFT S/N IS 802-0121.  (TC NR 20070115014)                                                                                                                                                                                                                                                                                                  1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20070820000372007082000037CE  2007       8          20         CA070115015      120070112G534050110131        MOUNT                                   CESSNA401   401         207590CCE  CONT  O520  TSIO520E    17040SO  MCAULY3AF32C3AF32C*     GL  MLG GEARBOX     LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING SCHEDULED LANDING GEAR ROUTINE INSPECTION, LANDING GEAR ACTUATOR GEARBOX MOUNTING BOLTS (3) FOUND MISSING AND REMAINING (1) BOLT FOUND SHEARED.  EMERGENCY GEAR OPERATION ATTEMPTED TO RELOCATE GEAR. EMERGENCY OPERATION INHIBITED DUE TO IMPROPER GEARBOX ALIGNMENT.  GEAR REPOSITIONED AND GEARBOX AND LANDING GEAR SYSTEM INSPECTED FOR CONDITION.  NEW MOUNTING BOLTS INSTALLED AND GEAR SYSTEM NORMAL AND EMERGENCY TESTED SERVICEABLE. (TC NR 20070115015)                                                                                                                                                                                                                                                                  1L72 3O3  O  A7CE    E8CE    5  CP22EA    
20070129003042007012900304EA  2007       1          29         CA070115016      120070112G2731C6CF14053       CONTROL CABLE                           DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  ELEVATOR TRIM   BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) TRIM CABLE WAS FOUND BROKEN AND WAS REPLACED. THE BROKEN CABLE IS BEING ANALYZED AT THEIR LOCAL AIRWORTHINESS AUTHORITY AND WE AWAIT THE RESULTS.  (TC NR 20070115016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20080306002812008030600281CE  2008       3          6          CA070115017      120070112G531297440019101     STIFFENER                               BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  BULKHEAD        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       16398                  BB84                                    (CAN)   SPECIAL INSP NR53 WAS COMPLETED IAW MM 5-20-05, WHICH INVOLVES THE FOLLOWING: AFT FUSELAGE AREA AND REAR PRESSURE BULKHEAD.  INSPECT THE ENTIRE FWD AND AFT SIDE OF THE REAR PRESSURE BULKHEAD FOR CRACKS AND LOOSE OR MISSING RIVETS. CHECKED OXYGEN BOTTLE MOUNTING BRACKETS FOR CRACKS AND LOOSE OR MISSING RIVETS. CHECKED OUTFLOW AND SAFETY VALVE BOX FOR CRACKS AND LOOSE OR MISSING RIVETS. THE INSP INTERVAL IS INITIALLY 10,000 CYCLES AND AT 500 CYCLES THERE AFTER.  DURING THIS INSP OF THE REAR PRESSURE BULKHEAD (F.S. 347.75) THE AFT ZEE STIFFENER (P/N:97-440019-101) WAS FOUND CRACKED. THE CRACK WAS LOCATED AT THE LOWER ATTACH POINT OF THE OXYGEN BOTTLE SUPPORT (P/N: 50-560019-13) WHICH ATTACHES TO THE ZEE ST1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070509000772007050900077SW  2007       5          9          CA070117003      120070115G56102719442004      WINDSHIELD                              SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  COCKPIT         DELAMINATED     W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       2751                                                           (CAN) DURING FLIGHT THE FLIGHT CREW HEARD A LOUD CRACK FROM THE RT HEATED WINDSHIELD. THEY IMMEDIATELY NOTICED THE WINDOW PANES BEGIN TO DELAMINATE. NO OBJECT WAS WITNESSED HITTING THE AIRCRAFT OR WINDSHIELD. THE AIRCRAFT LANDED SAFELY AND THEN RETURNED TO BASE ON A FLIGHT PERMIT FOR REPAIRS. NO CRACKING IN THE WINDOW WAS EVIDENT. THE WINDOW WAS REPLACED BY MAINTENANCE. (TC NR 20070117003)                                                                                                                                                                                                                                                                                                                                        2L72 4T4  TRTA8SW    E4WE    5  CP10NE    
20070129003072007012900307EA  2007       1          29         CA070117005      220070117G7320C6CF14043       CABLE                                   DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA                                              DAMAGED         W      O   OTHER                                                                                           W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) NEW CABLE, THE BALL END OF THE TRIM CABLE IS OUT OF ROUND AND WILL NOT FIT INTO THE TRIM JACK ASSEMBLY. WHERE THE CABLE MEETS THE BALL END IT HAS BEEN BRAZED AND THE CABLE HAS NOW FRAYED AFTER ATTEMPTING TO INSTALL IT INTO HTE TRIM JACK ASSEMBLY. (TC NR 20070117005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H72 3T4  TRTA9EA    E4EA                 
20070509000782007050900078WP  2007       5          9          CA070117006      120070117G6310C1883           SPRAG CLUTCH                            ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              MAIN ROTOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       933                                                            (CAN) DURING AN AES 1000HR INSPECTION, A CRACK WAS FOUND ON THE CAGE IN THE MIDDLE OF (1) CROSSBAR. (TC NR 20070117006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3O3  O  H11NM   1E4                  
20070509001862007050900186EA  2007       5          9          CA070117007      120070115G5610601R3303311     WINDOW                                  CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C1          NE                              COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       9980                                                           (CAN) PILOT SIDE WINDOW INNER LAYER CRACKED.  SIDE WINDOW ACC AMM 56-12-01 REPLACED. OPERATIONAL TEST OF WINDOW TEMP CONTR.  DO A LEAK TEST OF LT SIDE WINDOW AFTER REPLACEMENT ACC AMM 56-12-400-801 A01 PERFORMED SATISFIED (TC NR 20070117007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   EOOO63EN             
20070509001872007050900187EA  2007       5          9          CA070117008      120070115G32137339FT160T      SEAL            BFGOODRICH              CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C1          NE                              NLG STRUT       LEAKING         W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA                  SPP510096                                           (CAN) FLIGHT 5663 DEPARTED WITH 65 PASSENGERS ON BOARD WITH NO ISSUES NOTED.  ON APPROACH, AFTER GEAR DOWN SELECTION CREW NOTED A NWS INOP CAUTION MESSAGE.  TO GIVE THEMSELVES TIME TO GO THROUGH THE NWS INOP MESSAGE, THEY CARRIED OUT A GO AROUND.  AS THEY FLEW BY THE RUNWAY, THE TOWER INFORMED THEM THAT THE NOSEWHEELS APPEARED TO BE TURNED 90 DEGREES.  AN AC FLYING NEARBY OFFERED TO FLY BY THE AIRCRAFT AND INSPECT THE NOSE GEAR.  THE PILOT REPORTED THAT THE NOSE GEAR WHEELS WERE OFF CENTER BY 20 DEGREES.  AT THE GATE MAINTENANCE INSPECTED THE NOSE GEAR AND FOUND THAT THE STRUT WAS FLAT.  MAINTENANCE SERVICED THE STRUT AND NOTED THAT THE STRUT WAS LEAKING.  STL MAINTENANCE IS DISPATCHING MAINTENANCE AND SEALS TO2L72 4F4  FRTA21EA   EOOO63EN             
20070509001882007050900188CE  2007       5          9          CA070118001      120070115G554204330106        SKIN            CESSNA                  CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  RUDDER          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE DOING 100 HR INSPECTION ON AIRCRAFT, MECHANIC NOTICED THAT THERE WAS A CRACK BY THE LIGHTING HOLE BELOW THE TOP HINGE ATTACH BRACKET. NEW SKIN ORDERED AND WHEN RECEIVED NOTICED THAT MFG HAS REMOVED THIS LIGHTING HOLE.  REST OF AIRCRAFT OF THIS TYPE IN FLEET WILL BE INSPECTED FOR THIS SAME DAMAGE. (TC NR 20070118001)                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  ONT3A19    E223    5  NP50GL    
20070509001892007050900189EA  2007       5          9          CA070118002      120070117G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              TE FLAPS        MALFUNCTIONED   W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA                                                                      (CAN) THE CREW REPORTED A FLAP FAIL MESSAGE ON APPROACH. THE CREW SELECTED FLAP 8 AND FLAP FAIL MESSAGE CAME ON IMMEDIATELY AND THE FLAPS FROZE AT 0 DEGREES INDICATED. ON THE GROUND A CB RESET WAS CARRIED OUT AND THE CODES WERE OBTAINED . THE AIRCRAFT WAS FERRIED WHERE AN INVESTIGATION IS STILL ONGOING BY LINE MAINTENANCE (TC NR 20070118002)                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA21EA   E15NE                
20070129003082007012900308SO  2007       1          29         CA070118003      220070110G73146467582         PUMP                                    PIPER PA28  PA28R201T   7102813SO  CONT  O360  TSIO360F    17025SO  HARTZLHCC2Y BHCC2YF1    GL  ENGINE          FAULTY          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA            1056                                                      (CAN) ENGINE DRIVEN FUEL PUMP OUTPUT IS LOW AT RATED RPM 2600. (TC NR 20070118003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  2A13    E9CE    5  CP920     
20070129003092007012900309GL  2007       1          29         CA070118004      320070112G6110B2222           PLATE                                   PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2B   41532EA  HARTZLHCE2Y HCE2YR2     GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3850 2009                                                      (CAN) PROPELLER RECEIVED FROM CUSTOMER FOR ROUTINE OVERHAUL. PROPELLER DISMANTLED, PARTS NDT INSPECTED AND CRACK FOUND. NO AD`S OR BULLETIN`S ON THAT PART.  (TC NR 20070118004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3O3  O  A20SO   E14EA   5  CP9EA     
20070129003102007012900310EA  2007       1          29         CA070118005      220070103G73203027791         SENSE LINE                              BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE          BROKEN          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA       5597                               PCE85142                    (CAN) P3 TUBE SUDDENLY BROKEN WHILE AIRCRAFT WAS IN CLIMB. ENGINE FAIL TO IDLE, ENGINE WAS SHUTDOWN BY THE CREW.  AIRCRAFT RETURN TO DEPARTURE AIRPORT WITHOUT OTHER DIFFICULTY. (TC NR 20070118005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070509001902007050900190WP  2007       5          9          CA070118006      120070117G6210369D21100516A   BLADE                                   HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              MAIN ROTOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2813                                                           (CAN) THE UPPER BLADE SURFACE IS CRACKED CHORDWISE FROM LEADING EDGE TO TRAILING EDGE BETWEEN BLADE STATION 120 AND 124. THE LOWER BLADE SURFACE IS ALSO CRACKED IN THE MID CORD AREA BETWEEN STATION 120 AND 124 BUT DOES NOT EXTENT TO THE LEADING EDGE OR TRAILING EDGE. (TC NR 20070118006)                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3U3  U  H3WE    E4CE                 
20070511000052007051100005EA  2007       5          11         CA070118008      120070117G2752852D10019       ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        CONTAMINATED    W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       6959 6959                                                      (CAN) ON APPROACH CREW REPORTED A FLAPS FAIL MESSAGE AFTER SELECTION TO 8 DEGREES. FLIGHT COMPLETED A FLAPLESS LANDING WITHOUT INCIDENT. AIRCRAFT THEN COMPLETED A FERRY FLIGHT. TROUBLESHOOTING OF FAULT CODES AND REPAIRS CURRENTLY ONGOING BY MAINTENANCE. THE RT IB FLAP ACTUATOR WAS REPLACED DUE TO NOT ACCEPTING GREASE. SUSPECT MOISTURE INGRESS HAD FROZEN INSIDE ACTUATOR. AS PART OF REPAIRS MOD IS601R227530052 REV B: FLAP DRIVE SYSTEM-ALTERNATE METALLIC SEAL FOR FLEXIBLE DRIVE SHAFT WAS INCORPORATED. (TC NR 20070118008)                                                                                                                                                                                                     2L72 4F4  FRTA21EA   E15NE                
20070511000062007051100006EA  2007       5          11         CA070118009      120070116G2910AE7090072       LINE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              NR 2 EDP        LOOSE           W      O   OTHER                                                                                           EKJVIBRATION/BUFFET          FLUID LOSS                WARNING INDICATION        CRCRUISE         1                      CA                  MX598642                                            (CAN) ENROUTE CREW ADVISED THAT THEY HAD LOST NR 2 HYDRAULIC  SYSTEM AND WERE  DIVERTING.  CREW DECLARED AN EMERGENCY AND ADVISED PASSENGERS OF REASON. WHEN THE INCIDENT HAPPENED THE CREW HAD A HYD 2 LOW PRESSURE MESSAGE, WHEN THEY TURNED ON NR 2 PUMP (HYD PUMP 2A) MESSAGE WAS CONTINUOUSLY ON. A FEW MINUTES LATER ALL NR 2 HYD QUANTITY WAS LOST.  MAINTENANCE INSPECTION REVEALED THAT THE QUICK DISCONNECT FITTING ON THE CASE DRAIN LINE TO THE NR 2 PUMP WAS LEAKING AROUND THE BASE OF THE COUPLER.  ONCE ALL THE FLUID LEAKED OUT IT STARVED THE PUMP CAUSING IT TO MAKE METAL CAUSING ENGINE VIBRATION AND EVENTUALLY SEIZE.  THE CASE DRAIN LINE, NR2 EDP, PRESS AND CASE DRAIN FILTERS WERE REPLACED AND AIRCRAFT WAS FUNCTION2L72 4F4  FRTA21EA   E15NE                
20070511000072007051100007EU  2007       5          11         CA070118010      120070118G5302350A13111620    BOLT                                    SNIAS 350   AS350B1     8680811EU  TMECA ARRIELARRIEL1D         NE                              TAILBOOM        DAMAGED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) THIS IS (1) OF (2) BOLTS USED TO RETAIN THE HORIZONTAL STAB. TO THE TAIL BOOM OF THE HELICOPTER.  THE THREADED SECTION OF THE BOLT AND THE NUT WERE FOUND MISSING.  IT APPEARS THAT THE THREADED SECTION OF THE BOLT HAD BEEN CRACKED FOR SOME TIME BEFORE DEPARTING. (TC NR 20070118010)                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3U3  U  H9EU    E19EU                
20070511000082007051100008EU  2007       5          11         CA070118011      120070104G6730AC67244         SERVO                                   SNIAS 350   AS350B      8680801EU  TMECA ARRIELARRIEL1B    6OO30NE                              ROTOR           UNSERVICEABLE   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1263                                                      (CAN) DURING HYDRAULIC PRE-FLIGHT CHECK CAUSED CYCLIC TO MOVE 4-5 INCHES TOWARDS 8 OCLOCK POSITION.  SERVO REMOVED SERVICEABLE UNIT INSTALLED.  SERVO SENT OUT FOR REPAIR AWAITING TEARDOWN REPORT. (TC NR 20070118011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3U3  U  H9EU    E19EU                
20070511000092007051100009EA  2007       5          11         CA070119001      120070117G5610NP1393229       WINDOW                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              COCKPIT         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6269                                                           (CAN) SEVERAL CRACKS IN LT SIDEWINDOW INNER AND CENTER. A/C AOG LT SIDEWINDOW CHANGED ACC AMM. ALL TESTS SATISFIED (TC NR 20070119001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20070129003112007012900311EU  2007       1          29         CA070119003      120070109G2930AIR45428        INDICATOR                               BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  HYDRAULIC SYS   LEAKING         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) ENROUTE, THE CREW OBSERVED BOTH HYD SYSTEMS INDICATING APPROXIMATELY 1200 PSI WITH LOW FLOW LIGHTS ON. THE CREW CONTINUED WHERE ON APPROACH THE HYDRAULIC PRESSURE RECOVERED AND THE FLOW LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE HYDRAULIC FLOW INDICATION VALVE LEAKING WHICH WAS REPLACED PRIOR TO THE AIRCRAFT RETURNING TO SERVICE. (TC NR 20070119003)                                                                                                                                                                                                                                                                                                                              2L72 3T4  T  A24EU   A196    6  CP899     
20070129003122007012900312EA  2007       1          29         CA070119004      120070118G5343                FASTENER                                DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF15      NE  NLG TRUNNION    LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) NLG TRUNNION FITTING FASTENERS FOUND LOOSE. REFERENCE IPC 53-20-00; FIGURE 25; ITEM 190. BOTH SIDES (LT AND RT) AFT ROW OF BOLTS.  RE-TORQUED NUTS IAW SB8-53-49. (TC NR 20070119004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070511000112007051100011EU  2007       5          11         CA070119005      120070118G30972840A           SWITCH                                  BOLKMS105   BO105S      5626006EU  ALLSN 250C  250C20B     03013GL                              ANTI ICE        SHORTED         W      H   DEACTIVATE SYST/CIRCUITS                                                                        H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA       851                                                            (CAN) AIRCRAFT IS IN CRUISE FLIGHT WHEN PILOT SELECTED NR 1 AND NR 2 ANTI-ICE (ON) DUE TO THE OAT AND VISIBLE MOISTURE.  ON SHORT FINAL TO THE BASE THE PILOT SELECTED BOTH ANTI-ICE SWITCHES TO THE (OFF) POSITION. IMMEDIATELY UPON ACTIVATING NR 1 SWITCH TO (OFF) THE PILOT HEARD AN AUDIBLE (CLICK).  LOOKING DOWN HE NOTICED THAT THE NR1 ANTI-ICE 3AMP BREAKER HAD POPPED.  ONE UNSUCCESSFUL ATTEMPT WAS MADE TO RESET THE BREAKER.  AFTER THE AIRCRAFT HAD SHUTDOWN THE MAINTENANCE STAFF TROUBLESHOT THE SYSTEM AND FOUND THAT THERE WAS A (DEAD SHORT) IN THE ANTI ICE SWITCH P/N 2840A.  THE SWITCH WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070119005)                                                           1G72 3U3  U  H3EU    E4CE                 
20070511000162007051100016CE  2007       5          11         CA070119009      120070116G5711122210614       SPAR                                    CESSNA206   TU206G      2073357CE  CONT  O520  TSIO520M    17040SO  MCAULYD3A34 D3A34C402   GL  RT WING         FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) EDGE DISTANCE OF RIVETS ON LOWER FLANGE LESS THAN MINIMUM ALLOWED.  REPLACEMENT OF PART REQUIRED TO REPAIR PROBLEM. (TC NR 20070119009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  O  A4CE    E8CE    5  CP47GL    
20070808001252007080800125CE  2007       8          8          CA070119010      120070116G571112220052        SPAR                                    CESSNA206   TU206G      2073357CE  CONT  O520  TSIO520M    17040SO  MCAULYD3A34 D3A34C402   GL  RT WING         FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING REPLACEMENT OF LOWER OB SKIN, EDGE DISTANCE OF RIVETS THROUGH LOWER FLANGE LESS THAN MINIMUM ALLOWED IN 32 PLACES FROM STAT. 100.0 TO STAT. 154.00  REPLACEMENT OF PARTS REQUIRED TO REPAIR PROBLEM. (TC NR 20070119010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O3  O  A4CE    E8CE    5  CP47GL    
20070511000182007051100018NM  2007       5          11         CA070119011      120070116G534369634801        BOLT                                    BOEING727   727227      1384078NM  PWA   JT8   JT8D9A      52048NE                              TRUNION         SHEARED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       63218                                                          (CAN) DURING A ROUTINE (C) CHECK INSPECTION, IT WAS NOTICED THAT THE LT MAIN LANDING GEAR TRUNION BOLT P/N 69-63480-1 APPEARED TO BE SHEARED. UPON REMOVAL OF THE GEAR, IT WAS CONFIRME4D THAT THE BOLT WAS SHEARED AND ALSO THE BEARING P/N 10-61849-10 WAS CRACKED. THE ABOVE PN ARE WITH REFERENCE TO MFG IPC 32-10-00-01 P.4 ITEM 317.  (TC NR 20070119011)                                                                                                                                                                                                                                                                                                                                                                                 2L73 4F4  F  A3WE    E2EA                 
20070511000192007051100019SO  2007       5          11         CA070119012      120070113G81204091709001      TURBOCHARGER                            PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2     GL  ENGINE          LEAKING         W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      APAPPROACH       1                      CA            1362                          L430261A                    (CAN) EXCESSIVE SMOKE FROM THE LT ENGINE WAS REPORTED BY PASSENGER AND GROUND CONTROL DURING APPROACH TO AIRPORT. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED AND PASSENGERS IMMEDIATELY DISEMBARKED. AIRPORT EMERGENCY RESPONSE VEHICLES ATTENDED. NO VISIBLE FLAMES OR FIRE WAS EVIDENT PRIOR TO OR AFTER LANDING. AIRCRAFT WAS TOWED FROM THE RUNWAY TO MAINTENANCE FACILITY. MAINTENANCE INVESTIGATION REVEALED EXCESSIVE OIL IN THE TURBOCHARGER EXHAUST. TURBOCHARGER REPLACED WITH O`HAULED UNIT AND AIRCRAFT/ENGINE OPERATION CHECKED NORMAL. (TC NR 20070119012)                                                                                                                                                             1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070511000212007051100021SO  2007       5          11         CA070120001      120070118G8120                BEARING                                 PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  TURBOCHARGER    FAILED          W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       13433121                           L206368A                    (CAN)  RT ENGINE OIL CONSUMPTION HAD INCREASED, OIL RESIDUE FOUND ON EXHAUST STACK. INSPECTION FOUND THAT THE EXHAUST SIDE OF THE RT TURBOCHARGER WAS COVER IN OIL. FOUND THAT THE INNNER SUPPORT BEARING AND SEAL HAD FAILED ALLOWING OIL TO BE INTRODUCED TO THE HOT SIDE OF THE TURBO. REPLACED TURBOCHARGER, CHANGED ENGINE OIL,  INSPECTED RT ENGINE OIL FILTER FOR METAL, NO FAULT FOUND.   (TC NR 20070120001)                                                                                                                                                                                                                                                                                                                           1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070511000232007051100023EA  2007       5          11         CA070122001      120070119G3213C6UM117227      RETAINING NUT                           DHAV  DHC6  DHC6        2802606EA                                                               AXLE            MISMANUFACTURED W      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      CA                                                                      (CAN) NEW AXLE NUTS FOR THE SERIES AIRCRAFT NOT FULLY ASSEMBLED. THE HOLES FOR THE (2) PINS HAVE BEEN DRILLED BUT NO PINS HAVE BEEN INSTALLED, INCOMPLETE PARTS. MARKING ON NUT WO-04403/1, DEC 07 2006 C6UM1172-27. (TC NR 20070122001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H72 3T    RTA9EA                         
20070511000252007051100025WP  2007       5          11         CA070122002      120070122G7800D3171           HEAT SHIELD                             ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                                              CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       152                                                            (CAN) DURING A ROUTINE 100 HR ENGINE/AIRFRAME INSPECTION, IT WAS NOTED THAT THE SUBJECT HEAT SHIELD, THAT IS INSTALLED ON THE ENGINE EXHAUST TAILPIPE, WAS FOUND CRACKED. THE CRACK ORIGINATED IN THE DOUBLER AREA WHERE THE FORWARD CLAMP IS ATTACHED. THE CRACK LOOKS LIKE IT HAS ORIGINATED FROM A RIVET THAT ATTACHES THE DOUBLER AND BRACKET, WHICH PROVIDES A MEANS TO ATTACH THE CLAMP TO THE EXHAUST TAILPIPE. THE PART IN QUESTION HAS 151.3 HOURS SINCE NEW ON IT. THE AIRCRAFT IN QUESTION HAS 495.0 HOURS SINCE NEW. THE PART WILL BE SUBMITTED TO MFG FOR WARRANTY. THIS IS THE 3RD HEAT SHIELD TO BE REPLACED ON THIS AIRCRAFT SINCE IT WAS NEW. THE PRIOR HEAT SHIELDS WHERE REPLACED AT 343.5 AIRCRAFT HOURS, AND 203.2 AIRCRAFT1G71 3O3  O  H11NM   1E4                  
20070511000262007051100026WP  2007       5          11         CA070122003      120070122G5310D3807           SHROUD                                  ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE BAY      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       202                                                            (CAN) DURING A ROUTINE 100 HR ENGINE/AIRFRAME INSP, IT WAS NOTED THAT THE SUBJECT SHROUD WAS CRACKED JUST AFT OF THE UPPER/AFT MOUNTING SCREW LOCATION. THE SHROUD IS PART OF A SERIES OF SHROUD COVERS THAT SURROUND THE ENGINE FOR COOLING PURPOSES. THE SHROUD HAS 201.8 HOURS SINCE NEW ON IT. THE AIRCRAFT HAS ACCUMULATED 495.0 HOURS SINCE NEW. THIS IS THE SECOND TIME THAT THIS PARTICULAR SHROUD HAS BEEN REPLACED. THE ORIGINAL SHROUD THAT CAME NEW WITH THE AIRCRAFT WAS FOUND CRACKED IN THE SAME LOCATION, AND REPLACED AT 293.2 AIRCRAFT HOURS. THIS SEEMS TO BE A WEAK AREA THAT IS SUBJECTED TO ENGINE VIBRATION. HAVE TAKEN NOTE OF THIS WEAK AREA AND HAVE STEPPED UP OUR VISUAL INSPECTIONS TO SPOT CRACKS IN THEIR EARLY D1G71 3O3  O  H11NM   1E4                  
20070511000282007051100028WP  2007       5          11         CA070122004      120070122G5311C2617C2618      RIB                                     ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       495                                                            (CAN) DURING A ROUTINE 100 HOUR ENGINE/AIRFRAME INSPECTION, IT WAS NOTED THAT THE SUBJECT PARTS WHERE CRACKED. THE CRACKS WHERE FOUND AT THE FORWARD ANCHOR NUT LOCTIONS. THE RIBS ARE PART OF THE STRUCTURE THAT ENCLOSES THAT MAST AREA. THE RIBS WHERE REPLACED WITH NEW ASSEMBLIES. THE AIRCRAFT IN QUESTION HAS 495.0 HRS SINCE NEW. (TC NR 20070122004)                                                                                                                                                                                                                                                                                                                                                                                   1G71 3O3  O  H11NM   1E4                  
20070511000292007051100029EA  2007       5          11         CA070122005      120070119G5551600210713       BUSHING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              HORIZONTAL STAB LACK OF LUBE    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5433                                                           (CAN) CREAKING NOISE HEARD WHEN HORIZONTAL STABLIZER WAS CYCLED THROUGH FULL RANGE. HORIZONTAL STAB HINGE BUSHINGS.THEY WERE FOUND DRY.  IPC REF:27-43-01-01, ITEM NR 60. PARTS HAND LUBED AND RE-ASSEMBLED IAW MM TASK NR 000-13-320-121.  CURRENT INTERVAL FOR THIS  TASK IS 10,000 FLT.HRS (TC NR 20070122005)                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20070511000422007051100042EA  2007       5          11         CA070122006      120070121G5551600210713       BUSHING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              HORZONTAL STAB  LACK OF LUBE    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5406                                                           (CAN) CREAKING NOISE HEARD WHEN THE HORIZONTAL STABILIZER WAS CYCLED THROUGH FULL RANGE.  AFT FITTING ON THE HORIZONTAL STABILIZER DISASSEMBLED.  BUSHING WAS FOUND DRY ( NO LUBRICATION ).  PARTS CLEANED, INSPECTED, HAND LUBED AND RE-ASSEMBLED IAW MM TASK NR 000-12-320-121.  CURRENT INTERVAL FOR THIS TASK IN THE MANUAL IS 10,000 FLIGHT HOURS. (TC NR 20070122006)                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA21EA   E15NE                
20070511000432007051100043NM  2007       5          11         CA070122007      120070105G291082970009235     LINE                                    DHAV  DHC8  DHC8101     2809002NM  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF7       NE  RT MLG          RUPTURED        W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA       27198                                                          (CAN) DURING TAKEOFF, AFTER SELECTING LANDING GEAR UP, NR 2 ENGINE HYD PUMP FAILED AND AFTER SEVERAL MIN, A/C LOST ALL OF THE NR 2 HYD QUANTITY. SYSTEM NR 2 PRESSURE LOW AND QUANTITY DEPLETED, ALTERNATE LANDING GEAR EXTENSION.  AFTER INVESTIGATION HYD TUBE, P/N 82970009-235 AT RT HYD SYSTEM (L/G BAY), WAS FOUND RUPTURED (IN THE FLARED AREA). TUBE WAS REPLACED; BLEEDING AND LEAK CHECK C/OUT OF RT HYD SYSTEM AND NO LEAKS OBSERVED.  (TC NR 20070122007)                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070511000652007051100065CE  2007       5          11         CA070122008      120070120G3230508103385       DRAG LINK                               BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  RT MLG          FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFTER SCHEDULED MAINTENANCE THE AIRCRAFT WAS REMOVED FROM THE HANGER AND WAS TOWED TO THE FUEL PUMPS TO BE LEAK CHECKED. AFTER TOWING THE AIRCRAFT ABOUT 500 FEET THE RT MLG COLLAPSED CAUSING DAMAGE TO THE RT MAIN LANDING GEAR AND DOORS, WING TIP, CARGO POD AND ONE BLADE OF THE RT PROP. THE AIRCRAFT WAS THEN LIFTED AND JACKED TO ALLOW INSPECTION OF THE LANDING GEAR AREA AND ALLOWED FOR A TEMPORARY DOWNLOCK TO BE MADE AND THE AIRCRAFT WAS RETURNED TO THE HANGER. THE AIRCRAFT IS STILL BEING INSPECTED FOR OTHER UNSEEN DAMAGE. THE PRELIMINARY FINDINGS SHOW THAT THE PRIMARY FAILURE WAS OF THE DRAG LINK LOCK. THIS IS ONLY A PRELIMINARY REPORT A MORE CONCLUSIVE REPORT WILL BE ADDED TO THIS SDR WHEN THE FINDINGS A1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070511000442007051100044SO  2007       5          11         CA070122009      220070117G8530EC649358CN      CYLINDER                                CESSNA206   U206F       2073333CE  CONT  O520  IO520F      17032SO  HARTZLHCC3Y HCC3YF1     GL  NR 4            FAILED          W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA       755                                                            (CAN) NR 4 CYILINDER FAILED, BURNING VARIOUS ENGINE COMPARTMENT WIRING AND DUCTING. (TC NR 20070122009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  A4CE    E5CE    5  CP25EA    
20070511000452007051100045CE  2007       5          11         CA070122010      120070106G24971003641621      CONTROL PANEL                           BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCD4N3HCD4N3A     GL  COCKPIT LIGHTS  SHORTED         W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                                                      (CAN) CREW REPORTED COCKPIT OVERHEAD PANEL LIGHTS CIRCUIT BREAKER POPPED AND ABOUT THE SAME TIME REPORTED SMELLING SMOKE. PCB PANEL REMOVED AND FOUND TO OF SHORTED OUT CAUSING SMALL BURN HOLE THROUGH PANEL SCORCHING METAL BEHIND PANEL. CAUSE OF SHORT BELIVED TO BE MOISTURE FROM EXCESSIVE CONDENSATION. (TC NR 20070122010)                                                                                                                                                                                                                                                                                                                                                                                                              1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070511000462007051100046SW  2007       5          11         CA070122011      120070122G67102040011841      COLLECTIVE STICK                        BELL  204   204B        1181404SW  LYC   T53   T5311B      41549NE                              MAIN ROTOR      RATCHETING      W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) PILOT COMPLAINED OF RATCHETING FEEL TO COLLECTIVE CONTROL STICK.  AIRCRAFT RETURNED TO BASE.  INSPECTION REVEALED THAT THE COLLECTIVE FRICTION SURFACE ROLL PIN WAS WORKING INTERNALLY AND CAUSING THE RATCHETING FEEL.  ELBOW WAS REPLACED. (TC NR 20070122011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 4U4  U  H1SW    E1EA                 
20070511000472007051100047CE  2007       5          11         CA070123001      120070119G76039938000521      CONTROL CABLE                           BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  HARTZLHCB4T HCB4TN3     GL  LT ENGINE       SEPARATED       W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             NRNOT REPORTED   1                      CA                                                                      (CAN) THE LT ENGINE COULD NOT BE SHUTDOWN ON THE GROUND USING THE CONDITION LEVER, THE PILOT HAD TO USE THE FIREWALL SHUT-OFF IN ORDER TO SHUT THE ENGINE DOWN. INVESTIGATION BY MAINTENANCE FOUND THAT THE LT IDLE CONTROL CABLE ASSY FAILED AT THE MALE TERMINAL END AT THE ENGINE. THE MALE THREADED END PORTION SLIPPED OFF THE CABLE SLIDE AT THE POINT WHERE IT IS SWAGED/PRESSED ON. (TC NR 20070123001)                                                                                                                                                                                                                                                                                                                                 1L72 3T4  T  A14CE   E4EA    6  CP40EA    
20070511000492007051100049EA  2007       5          11         CA070123002      120070122G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        JAMMED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) AIRCRAFT HAD A FLAPLESS LANDING, AFTER FLAP SELECTION 8, LT FLAP INDICATED ZERO, RT UNKNOWN, CREW THEN SELECTED TO 20 AND FLAPS TRAVELED TO APROX 5 DEGREES INDICATION WAS GREEN TRAVELED TO 5 DEGREES AND THEN TURNED WHITE. CREW THEN RETRACTED FLAPS BACK TO FLAP ZERO AND LANDED FLAPLESS, FLAP FAIL CAUTION WAS NOT ILLUMINATED.  FERRY FLIGHT FOR TROUBLESHOOTING.  T/S C/O AND ALL DCU`S ARE DISPLAYING THE SAME INFO, APPEARS TO BE POTENTIOMETER FAIL.  WAITING FOR PART TO BE INSTALLED. (TC NR 20070123002)                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20070808001262007080800126CE  2007       8          8          CA070123004      120070121G304099180021        FAN                                     CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              WINDSHIELD      ODOR            W      GH  O2 MASK DEPLOYED        DEACTIVATE SYST/CIRCUITS                                                B  SMOKE/FUMES/ODORS/SPARKS                                                      APAPPROACH       1                      CA       6004                                                           (CAN) ON APPROACH WHEN THE CREW SMELLED SOMETHING BURNING IN THE CABIN.  THE CABIN FILLED UP WITH SMOKE AND THE CREW PUT ON THEIR MASKS AND DROPPED THE PASSENGERS MASKS.  THEY LANDED WITHOUT DECLARING AN EMERGENCY.  AN AME WAS SENT TO AND DETERMINED THAT THE DEFOG FAN WAS AT FAULT.  THE FAN WAS DEFERRED AND WILL BE REPLACED ON ITS RETURN. (TC NR 20070123004)                                                                                                                                                                                                                                                                                                                                                                        1L72 4F4  F  A22CE   E1NE                 
20070511000502007051100050EA  2007       5          11         CA070123005      120070118G2752852D10019       ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        WORN            W      L   ABORTED APPROACH                                                                                F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       5457 5321                                                      (CAN) ON FINAL APPROACH CREW SELECTED FLAPS 20 DEGREES. FLAPS STUCK AT 8 DEGREES AND CREW RECEIVED A FLAP FAIL MESSAGE. CREW BROKE OFF APPROACH AND CONTACTED DISPATCH. AIRCRAFT SUBSEQUENTLY LANDED WITHOUT INCIDENT WITH FLAPS AT 8 DEGREES. MAINTENANCE TROUBLESHOOTING FOUND EXCESSIVE LINEAR PLAY IN THE LT AND RT IB FLAP ACTUATORS. ACTUATORS REPLACED (RT IB ACTUATOR PN CL600-2B19, S/N 5051. TSN 5321:44 HOURS, TSO 5321:44, CYCLES 4332) MOD SUM IS601R27530052 REV B: FLAP DRIVE SYSTEM, ALTERNATE METALLIC SEAL FOR FLEXIBLE DRIVE SHAFT COMPLETED. SYSTEM RE-GREASED. FLAP SYSTEM RIGGED IAW AMM 27-51-10. SUCCESSFUL TEST FLIGHT COMPLETED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070123005)                                 2L72 4F4  FRTA21EA   E15NE                
20070511000512007051100051EA  2007       5          11         CA070123006      120070122G3230574205A         VALVE                                   DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF15      NE  MLG             MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA       366499188                                                      (CAN) DURING APPROACH WHEN LANDING GEAR SELECTED DOWN, NO GEAR MOVEMENT. CIRCUIT BREAKERS, HYDRAULIC PX AND QUANTITY AND DOORS ALL NORMAL. AFTER APPROXIMATELY 10 MINUETS, LANDING GEAR DEPLOYED NORMALLY TO EXTENDED POSITION. AIRCRAFT FERRIED GEAR DOWN TO MAINTENANCE BASE. LANDING GEAR SELECTOR VALVE REPLACED, GEAR SWINGS CARRIED OUT. SERVICEABLE. AIRCRAFT RETURNED TO SERVICE.  (TC NR 20070123006)                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070511000662007051100066NE  2007       5          11         CA070123007      120070106G64209235806343101   CONE            SKRSKY                  SKRSKYS92   S92A               NE                                                               TAILROTOR G/B   SPLIT           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       596        A13200020                                           (CAN) ON 06 JAN 07, THE TAIL ROTOR HEAD WAS IN PROCESS OF BEING REPLACED WHEN IT WAS NOTICED THAT THE IB SET OF SPLIT CONES WHICH CENTER AND SUPPORT THE TAIL ROTOR HUB LOADS WERE MISSING. FURTHER INVESTIGATION FOUND THAT WHEN THIS TAIL GEARBOX WAS INSTALLED 596 HOURS PREVIOUS ON 18 JUNE 06 THE MFG MM DID NOT HAVE ANY REFERENCE TO THE INNER SPLIT CONES.  NO MENTION OF THEM IN THE REMOVAL/INSTALLATION INSTRUCTION, OR THE REQUIRED PARTS LISTING OR ON ANY ILLUSTRATION.( NOTE: MFG MM HAVE SINCE BEEN UPDATED AS OF SEPT  06 TO INCLUDE THE IB SPLIT CONES)  FIELDS FOR P/N NOT LONG ENOUGH TGB P/N 92358-06100-043 (TC NR 20070123007)                                                                                           2G72 4U      R00024BO                     
20070511000522007051100052EA  2007       5          11         CA070123008      120070123G5415TA305002403     FAIRLEAD                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              HYD LINE        WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       102208646                                                      (CAN) DURING MAINTENANCE INSPECTION , FOUND AFT FUSELAGE EQUIPMENT BAY HYDRAULIC LINE CLAMPS (FAIRLEAD), WITH CENTER (PRESSURE LINE) HOLES WORN THROUGH RUBBER/SILICON COMPOUND AND ALLOWING TUBING TO CHAFE ON METAL PORTION OF BLOCK.  BLOCK PN TA3050024-03 CONSISTS OF (2) HALVES (INK STAMP P/N B0305103-002 OR 601R75126-3). CLAMP HALVES REPLACED. (TC NR 20070123008)                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA21EA   E15NE                
             20080520     CE  2008       5          20         CA070123009      120070123G532051220465        BRACKET                                 CESSNA402   402C        207590RCE  CONT  O520  TSIO520VB   17040SO  MCAULY3AF32C3AF32C505   GL                  CORRODED        W      O   OTHER                                                                                           O  OTHER                                                                         DEDESCENT        1                      CA                                                                      (CAN) WHEN FLAPS LOWERED AC SEEMED TO ROTATE SLIGHTLY. PILOT RETURNED TO BASE. FLAP SYS INSPECTED AND FAULT FOUND WITH LT FLAP BELLCRANK LOWER MOUNTING BRACKET. BELLCRANK MOUNTING HOLE WAS SEVERELY CORRODED ALLOWING LARGE BOLT MOVEMENT WHEN FLAPS OPERATED. BRACKET REMOVED AND NEW PART ON ORDER. (TC NR 20070123009)                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A7CE    E8CE    5  CP22EA    
20070511000682007051100068NE  2007       5          11         CA070123010      220070123G7261311145101       SEAL                                    BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                              NR 2 ENGINE     LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       158524083                                                      (CAN) CREW LANDED AND REPORTED ENGINE NR 2 LEAKING OIL. MAINTENANCE INSPECTED AND FOUND THE OIL LEVEL DOWN CONSIDERABLY, THEY INSPECTED THE FWD CHIP DETECTOR, OIL FILTER, FUEL OIL HEATER AND FOUND NO DEFECTS. THE ENGINE WAS GROUND RUN WITH A LITTLE OIL LEAKAGE FOUND. THE OIL BREATHER LINE WAS REMOVED AND THE A/C SENT ON A TEST FLIGHT. WHEN IT RETURNED THE BAG WAS FULL (.5 LTR) WITH SOME SPILLAGE FROM THE BAG .THE A/C WAS GROUNDED AND WITH THE AID OF A MFG ENGINEER, THE REDUCTION GEAR BOX ASSY WAS REMOVED FROM THE ENGINE. CLOSE INSPECTION FOUND THE INTERNAL CARBON SEAL ASSY WITH SLIGHT DAMAGE AND STUCK IN THE OPEN POSITION. AS SOON AS THE SEAL WAS TOUCHED THE SPRING IN THE ASSY CLOSED THE OPENING IN THE SEAL ASS2L72 4T4  TRTA24CE   E26NE                
20070808001272007080800127NM  2007       8          8          CA070123012      120070119G3520RVA7101         CONTROL UNIT                            AMD   FALC50FALCON2000  2730170NM                                                               OXYGEN SYSTEM   FAILED          W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA            1564                                                      (CAN) UPON A NON-ROUTINE DEPLOYMENT OF THE OXYGEN MASKS ON THE GROUND BY MAINTENANCE.  OXYGEN CONTROL UNIT (10WJ) WAS PLACED INTO (OVERRIDE) TO MANUALLY DEPLOY THE PAX OXYGEN MASKS.  THEY DID NOT DEPLOY ON COMMAND.  MULTIPLE ATTEMPTS WERE MADE TO MANUALLY DEPLOY THE PAX OXYGEN MASKS IN (OVERRIDE).  THEY STILL DID NOT DEPLOY.  OXYGEN CONTROL UNIT (10WJ) WAS REPLACED IAW MP35-203, OPS TESTED SERVICEABLE.  PN OFF: RVA71-01  SN OFF: 0640 ATSO: 1563.8 ACSO: 711.  FAULTY OXYGEN CONTROL UNIT FORWARDED TO MFG FOR EXCHANGE. (TC NR 20070123012)                                                                                                                                                                                    2K72 4F    RTA50NM                        
20070511000552007051100055EA  2007       5          11         CA070123013      120070117G2910AE2460260G0074  HOSE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              HYD SYSTEM      LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  LDLANDING        1                      CA                                                                      (CAN) ON FINAL APPROACH WITH GEAR DOWN AND AT 2000FT THE MESSAGE HYD NR3 LOW PRESS CAME ON EICAS WITH THE HYDRAULIC NR3 RESERVOIR LEVEL AT 0 PERCENT.  CREW COMPLIED WITH QRH.   THE AIRCRAFT LANDED NORMALLY AND DEPLOYED THE THRUST REVERSER , THE GROUND SPOILERS DEPLOYED AND OPERATED BRAKES .  THE AIRCRAFT AT A SPEED AROUND 70 KTS SUDDENLY DIVERTED ON THE RT END SIDE . THE AIRCRAFT LEFT THE SIDE OF THE RUNWAY BY 13 METER AND ENDED UP ON THE GRASS AFTER THE A/C COVERED 50/55 METERS  (TC NR 20070123013)                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20070511000562007051100056EA  2007       5          11         CA070123014      120070121G5610NP13932114      WINDSHIELD                              CNDAIRCL600 CL6002D24   1390016EA  GE    CF34  CF348C1          NE                              COCKPIT         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA       565                                                            (CAN) RT WINDSHIELD CRACKED, FL240.IAS250 DIFF PRESS 7.4  RT WINDSHIELD REPLACED ACC AMM 56-11-01-400. CURE TIME OF SEALANT TIL 21-01-2007, 20:00 LOC TIME. PLS PERFORM ADJUSTMENT OF WIPER ARM TENSION ACC AMM 30-42-09-400-801-A01 AND OPS TEST OF WIPER AND PERFORM A LEAK TEST OF WINDSHIELD ACC AMM 56-11-01-400-801-A01 (E).  CONDITION OF SEALANT CHECKED OK.  ADJUSTMENT OF WIPER ARM IAW.AMM. CHECKED OK. OPS TEST OF WIPER OK.  CABIN PRESSURE TEST UP TO DELTA P 6.0 PERFORMED FOUND SATISFIED. (TC NR 20070123014)                                                                                                                                                                                                                  2L72 4F4  FRTA21EA   EOOO63EN             
20070511000582007051100058EA  2007       5          11         CA070123015      120070118G5610NP13932113      WINDSHIELD                              CNDAIRCL600 CL6002D24   1390016EA  GE    CF34  CF348C1          NE                              COCKPIT         CRACKED         W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       564                                                            (CAN) LT WINDSHIELD CRACKED.  LT WINDSHIELD REPLACED IAW AMM 56-11-01-000-801 (TC NR 20070123015)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   EOOO63EN             
20070511001262007051100126EA  2007       5          11         CA070124001      120070122G284073664310        COMPUTER                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              FUEL QUANTITY   MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA       1022010220                                                     (CAN) JUST PRIOR TO TOP OF CLIMB, LEFT FUEL QUANTITY AND TOTAL FUEL QUANTITY STARTED TO REDUCE, FOLLOWED BY FUEL IMBALANCE MESSAGE. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. ON FINAL APPROACH FUEL INDICATIONS RETURNED TO NORMAL. FUEL SYSTEM INSPECTED, WITH NO LEAKAGE FOUND. AIRCRAFT DISPATCHED UNDER MEL. ON NEXT MAINTENANCE VISIT FUEL COMPUTER REPLACED. (TC# 20070124001)                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20070808001282007080800128CE  2007       8          8          CA070124002      120070122G3020991240216       SOLENOID VALVE                          CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              ANTI-ICE SYS    FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) STILL IN CRUISE CONFIG PILOTS DECIDED TO SELECT ANTI-ICE IN PREPARATION FOR DECENT TO AIRPORT. AT THIS TIME, A LT ANTI-ICE FAIL LIGHT ILLUMINATED.  TROUBLESHOOTING LATER CONFIRMED THAT THE LT ENGINE ANTI-ICE VALVE HAD FAILED.  THE VALVE IS POWERED 28VDC CLOSED UNTIL THE PILOT SELECTS ANTI-ICE ON, THEN POWER IS REMOVED AND THE VALVE IS OPENED BY ENGINE BLEED AIR PRESSURE. THE SYSTEM IS INTENDED TO BE A FAILSAFE SYSTEM, WHERE A NO POWER SITUATION WILL ALWAYS ALLOW BLEED AIR TO THE ENGINE INTAKE.  THIS PARTICULAR VALVE FAILED TO PROVIDE THE FAILSAFE CONDITION. NO ENGINE BLEED AIR WAS AVAILABLE TO THE ENGINE INLET ALLOWING AN EXCESSIVE BUILD UP OF ICE. THIS CONDITION COULD HAVE LED TO ICE INGESTION CAUSING EN1L72 4F4  F  A22CE   E1NE                 
20070511000692007051100069CE  2007       5          11         CA070124003      120070119G575399160011        ROLLER                                  BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  TE FLAPS        WORN            W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) PILOT REPORTED INTERFERENCE WITH AILERON CONTROL UPON APPROACH WHEN FLAPS WERE APPROXIMATELY 30 PERCENT.  AIRCRAFT LANDED WITHOUT INCIDENT.  INVESTIGATION REVEALED RT OB FLAP IB HINGE ATTACH BRACKET, PN 35-165050-31, FAILED AT THE AFT ROLLER ASSY ATTACH AREA.  THIS IN TURN CAUSED THE OPPOSITE ATTACH BRACKET TO FAIL.  THIS CAUSED THE IB AFT AREA OF THE FLAP TO MOVE FREELY AND CHANGE THE NORMAL ATTITUDE OF THE FLAP CAUSING INTERFERENCE WITH THE IB RT AILERON SKIN.  THE HINGE ATTACH BRACKET FAILED FROM THE AFT ROLLER ASSY, P/N 99-160011, WEARING INTO THE HINGE ATTACH BRACKET.  INSPECTED ALL OTHER HINGE ATTACH AREAS AND FOUND SIMILAR WEAR IN OTHER AFT ROLLER ATTACH LOCATIONS.  THE ROLLER ASSEMBLY, PN 99-160011L72 3T4  T  A14CE   E4EA    5  CSTC      
20070511000592007051100059EA  2007       5          11         CA070125001      120070125G32336008500185      ACTUATOR                                CNDAIRCL601 CL6012A12   1900303EA  GE    CF34  CF343A      30015NE                              MLG             INOPERATIVE     W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA       251896776                                                      (CAN) RT MAIN LANDING GEAR UNLOCK INDICATION APPROX. 15 - 20 MIN. AFTER ARRIVAL, NO PUMP, NO GEAR COMMAND, LOCK PARTIALLY MOVED TO UNLOCK POSITION. RETRACTING ACTUATOR REPLACED AND AC RETURNED TO SERVICE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21AE   E15NE                
20070808001292007080800129CE  2007       8          8          CA070125002      120070124G323108411131        SCREW                                   CESSNA401   401B        207590ECE  CONT  O520  TSIO520EB   17040SO  MCAULY3AF32C3AF32C505   GL  RT MLG ADJ      BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) UPON LANDING RT MLG INADVETENTLY RETRACTED. AIRCRAFT VEERED OFF RUNWAY. AIRCRAFT INSPECTED AND CAUSE DEEMED FAILURE OF RT MLG ADJUSTING SCREW CAUSING SIDE BRACE ASSY TO UNLOCK. (TC NR 20070125002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A7CE    E8CE    5  CP22EA    
20070511001272007051100127NM  2007       5          11         CA070125003      120070123G26123023143         SMOKE DETECTOR                          DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  CARGO BAY       FALSE INDICATIONW      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA       2853028530                                                     (CAN) ON DEPARTURE THROUGH 4000 FT, FLT CREW RECEIVED A MASTER WARNING BAGGAGE SMOKE INDICATION. FLIGHT CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DEPARTURE AIRPORT. THERE WAS A COMPANY LINE CHECK CAPTAIN ON BOARD WHO WITH THE FLIGHT ATTENDANT WENT TO CHECK THE CARGO HOLD. THERE WAS NO INDICATION OF SMOKE. FLIGHT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 BAGGAGE SMOKE DETECTOR , THE LAMPS IN THE NR 2 DETECTOR (P/N 376), CLEANED THE CONNECTORS OF BOTH DETECTORS AND GROUND TESTED THEM SERVICEABLE. ENGINE RUNS WERE CARRIED OUT WITH NO DUPLICATION OF THE ORIGINAL DEFECT. TIME SINCE LAST REPAIR OF THE NR 1 DETECTOR WAS 1883:46 HOURS. (TC 20070125003)                              2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070511000702007051100070EU  2007       5          11         CA070125004      120070123G6220601741          BEARING                                 BOLKMS105   BO105S      5626006EU  ALLSN 250C  250C20B     03013GL                              PENDULUM ABSORB FRACTURED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) UPON LANDING AT THE MAINTENANCE BASE AND FOLLOWING HELICOPTER BEING SHUTDOWN, THE PILOT WAS EXITING AND LEAVING THE AIRCRAFT HE NOTICED THAT THE M/R PENDULUM ABSORBER ON THE YELLOW MAIN ROTOR BLADE WAS IN THE HORIZONTAL POSITION. CLOSER INSPECTION REVEALED THAT WHEN AN ATTEMPT TO ROTATE THE PENDULUM ABSORBER IT WAS EXTREMELY ROUGH AND DIFFICULT TO ROTATE.  PENDULUM ABSORBER WAS REMOVED AND DISASSEMBLED, WHERE IT WAS FOUND THAT ONE OF THE BEARINGS HAD A FRACTURED OUTER CASE.  THE BEARING APPEARED TO BE DRY, AS NO EVIDENCE OF LUBRICATION WAS FOUND.  NEW BEARINGS, SEALS, AND O-RINGS WERE INSTALLED.  PENDULUM ABSORBER WAS RE-INSTALLED AND AIRCRAFT NOW RETURNED TO SERVICE. (TC NR 20070125004)                  1G72 3U3  U  H3EU    E4CE                 
20070511000712007051100071EA  2007       5          11         CA070125005      220070125G7250312111101       BLADE                                                                      PWA   PT6   PT6A65B     52043EA                              TURBINE SECTION FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THE ENGINE PT6A-65B S/N: PCE-32399 WAS RECEIVED FOR OVERHAUL.  DURING THE ENGINE DISASSEMBLING IT WAS FOUND THAT THE COMPRESSOR TURBINE BLADES WERE SEVERELY RUBBED AND ONE BLADE FAILED AT FIRTREE.  ALSO THE INSPECTION REVEALED THAT THE COMPRESSOR TURBINE VANE TRAILING EDGE, SHROUD SEGMENTS AND SHROUD HOUSING ARE DAMAGED. THE POWER TURBINE COMPONENTS: 1ST AND 2ND STAGES BLADES AND VANES FOUND IMPACT DAMAGED.    THE BLADE WHICH FAILED AT THE FIRTREE SHOWED EVIDENCE OF FATIGUE WITH AN ANOMALY AT THE ORIGIN.  NOTE: CODES DETERMINED FROM PILOT REPORT.  (TC NR 20070125005)                                                                                                                                                    4  T          E4EA                 
20070511000602007051100060NE  2007       5          11         CA070125006      220070123G7261                ENGINE                                  BOEING727   727243      138408DNM  PWA   JT8   JT8D9A      52048NE                              NR 3            LEAKING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA       674678505                          666071                      (CAN) ENROUTE, NR 3 ENGINE OIL LOSS, AIRCRAFT DIVERTED.  INSPECTED AND FERRIED AIRCRAFT.  ENGINE REPLACED (TC NR 20070125006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L73 4F4  FRTA3WE    E2EA                 
20070511000612007051100061GL  2007       5          11         CA070126001      220070121G7200                ENGINE                                  EMB   135   EMB135LR    3260305SO  ALLSN AE300 AE3007A          GL                                              MALFUNCTIONED   W      EBA ENGINE SHUTDOWN         EMER. DESCENT           UNSCHED LANDING                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CLCLIMB          1                      CA       9808                               CAE312136                   (CAN) DURING CLIMB (280 KNOTS) AT FL350 , CREW HEARD A LOUD POP FOLLOWED BY MULTIPLE UNSPECIFIED EICAS MESSAGES AND ITT WAS IN THE AMBER RANGE.  ENGINE SHUTDOWN UNCOMMANDED.  F/A REPORTED WHITE SMOKE IN THE CABIN.  CREW CONSIDERED ATTEMPTING A RE-START BUT OIL QUANTITY WAS ONLY 3 QUARTS. CREW DIVERTED AND A CMC DOWNLOAD REVEALED THAT AN OIL DEBRIS MESSAGE HAD BEEN SET ON JANUARY 19. ENGINE ENROUTE TO MFG FOR INVESTIGATION, FURTHER REPORT WILL BE SUBMITTED ON ENGINE TEARDOWN. (TC NR 20070126001)                                                                                                                                                                                                                             2L72 4F4  FRTT00011ATTE6CH                
20070808001302007080800130CE  2007       8          8          CA070126002      120070125G3260426EN98         SQUAT SWITCH                            LEAR  35    35LEAR      5170600CE  GARRTTTFE731TFE73122B   01518WP                              LT MAIN GEAR    SHORTED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) PRELIMINARY REPORT, SUSPECT THAT THE SHUTTLE VALVE THAT DIRECTS HYDRAULICS TO THE UP- OR DOWN-SIDE OF THE LANDING GEAR WAS STUCK OR BROKEN IN THE UP DIRECTION.  WHEN THE L/G WAS SELECTED DOWN ON THE ARRIVAL, NOTHING HAPPENED EXCEPT THE L/G DOORS OPENED THE FIRST TIME, NOTHING AT ALL ON THE SECOND ATTEMPT.  THE CREW WENT AROUND AND PUT THE L/G DOWN WITH EMERGENCY SYSTEM.  IT WORKED AND THEY HAD THREE GREEN, BUT THE EMERGENCY GEAR EXTENSION LEVER DID NOT LOCK AS IT SHOULD, AND THE L/G RETRACTED ON ITS OWN SHORTLY THEREAFTER!  THE EMERGENCY SYSTEM WAS RE-ACTIVATED, THE L/G WENT DOWN AS IT SHOULD AND THE LEVER WAS HELD IN THE DOWN POSITION.  THREE GREEN, NORMAL LANDING, AND THE A/C TURNED ONTO A TAXIWAY AND W2L72 4F4  F  A10CE   E6WE                 
20070511001282007051100128NM  2007       5          11         CA070126005      120070126G534385310340015     FITTING                                 DHAV  DHC8  DHC8106     2809020NM                                                               NLG WHEEL WELL  LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING "C-CHECK", WE FOUND THE NLG ACTUATOR FUSELAGE FITTING WITH A FASTENER BROKEN AND ALL THE OTHER ONE LOOSE. WE EMBODIED THE SB 8-53-50. THIS SB WAS NOT ATTACH TO ANY AD. (TC# 20070126005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T    RTA13NM                        
20070511000752007051100075SW  2007       5          11         CA070126006      120070121G5302206020113207    TAIL BOOM                               BELL  206   206L4       1182110SW  ALLSN 250C  250C30P     03013GL                              VERTICAL FIN    DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3368                   52054                                   (CAN) UPON CHANGING FORMER P/N 206-020-113-093 ON VERTICAL FIN, DAMAGE/GOUGING DETECTED ON THE IB FIN SKIN WITHIN CLOSE PROXIMITY TO VERTICAL FIN MOUNTING HOLE. IT IS SUSPECTED THAT WHEN ORIGINALLY FITTING THE COWLS THAT THE FORMER WAS TRIMMED AND THAT AT THIS TIME THE DAMAGE OCCURRED.   MFG WAS CONTACTED AND AN APPROVED REPAIR WAS PROVIDED AND CARRIED OUT. (TC NR 20070126006)                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  UNCH2SW    E1GL                 
20070511001292007051100129SW  2007       5          11         CA070126007      120070121G5302205030767005    FITTING                                 BELL  205   205A1       1181414SW                                                               TAIL BOOM       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING AIRFRAME INSPECTION, A CRACK WAS FOUND ON LONGERON P/N 205-030-207-005 UNDER FITTING P/N 205-030-767-005. FITTING REMOVED, INSPECTED FOUND TO BE CRACKED AT AFT SIDE OF BOLT LOCATION. CRACKS IN FITTING P/N 205-030-767-005 NOT FOUND UNTIL REMOVAL OF PART. THIS FITTING IS KNOWN TO CRACK AT THE RIVET HOLE LOCATIONS, BUT IN THIS INSTANCE, IT WAS CRACKED ON THE AFT SIDE OF THE BOLT HOLE LOCATION. LONGERON AND FITTING WERE REPLACED WITH NEW PARTS.  (TC# 20070126007)                                                                                                                                                                                                                                                    1G71 4U      H1SW                         
20070530000062007053000006NM  2007       5          30         CA070126008      120070117G2611                SMOKE DETECTOR                          DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  LAVATORY        MALFUNCTIONED   W      D   RETURN TO BLOCK                                                                                 N  FALSE WARNING                                                                 TXTAXI/GRND HDL  1                      CA                                                                      (CAN) ON GOING REPORTS OF LAVATORY SMOKE DETECTOR ACTIVATION. PROBLEM APPEARS TO HAVE BEGUN ON JANUARY 17, 2007 WITH A PILOT REPORT OF THE NR 2 ENGINE WILL NOT START AFTER (3) ATTEMPTS AND THEN AN OIL LEAK. MAINTENANCE REPLACED THE ENGINE IGNITERS AND CLEANED THE RESIDUAL OIL. ENGINE WAS THEN STARTED SUCCESSFULLY AND RUN TO TROUBLESHOOT THE OIL LEAK. NO OIL LEAK COULD BE FOUND AND IT WAS SUSPECTED TO BE AS A RESULT OF THE NO START CONDITION. ON JANUARY 18, 2007 LAVATORY SMOKE DETECTOR ACTIVATED ON FINAL APPROACH. FLIGHT ATTENDANT DETECTED ODOR ON GROUND. MAINTENANCE REPLACED DETECTOR (P/N 46-0083-4) AND SYSTEM CHECKED SERVICEABLE. ON NEXT FLIGHT, DETECTOR ACTIVATED AGAIN WITH NO SMOKE OR ODOR. LOW BATTERY (TC N2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070511001742007051100174SO  2007       5          11         CA070126009      120070118G3246402377          BOLT                                    PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2B   41532EA  HARTZLHCE3Y HCE3YR2A    GL  LT MLG          BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) WHILE TAXIING, THE UPPER TORQUE LINK BOLT BROKE WHICH ALLOWED THE LT MAIN WHEEL TO TURN SIDEWAYS. (TC NR 20070126009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070511001752007051100175CE  2007       5          11         CA070126010      120070123G2110206SZZC         BEARING         BEECH       115555024   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  COMPRESSOR      DISINTEGRATED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) BEARING WITHIN RT ENGINE AIR CONDITIONING COMPRESSOR DRIVE PULLEY DISINTEGRATED WHICH GREATLY CAUSED FURTHER HARM TO ITS ASSOCIATED PARTS.  THE QUILL SHAFT, COMPRESSOR DRIVE PULLEY, COMPRESSOR MOUNT ASSEMBLY, DRIVE SUPPORT, BEARING SHIMS AND SPACER, AND DUAL BELT (COMPRESSOR DRIVE BELT) HAVE HAD IRREVOCABLE DAMAGE. QUILL SHAFT DID NOT SHEAR. (TC NR 20070126010)                                                                                                                                                                                                                                                                                                                                                               1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070808001312007080800131CE  2007       8          8          CA070126011      120070118G321350411148        TORQUE LINK                             CESSNA401   401         207590CCE                                                               RT MLG          FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AIRCRAFT WAS DOING TOUCH AND GO`S ON THE 2ND LANDING PILOT REPORTED ABNORMAL LANDING AND NO GEAR UP INDICATION.  GEAR CYCLED AND ONLY 2 OUT OF 3 INDICATOR LIGHTS ILUMINATED. RT MAIN, NO INDICATION. GEAR CYCLED AGAIN NO UP INDICATION AND NO RT GREEN DOWN INDICATION. AIRCRAFT COMPLETED FLY BY CONTROL TOWER WHEN PILOT WAS INFORMED OF HIS RT MAIN WHEEL AT A 45 DEGREE ANGLE. AIRCRAFT CARRIED OUT A FLY OVER OF MORGAN AIR`S FACILITY WHERE WITH BINOCULARS, I COULD SEE THE RT MAIN GEAR OVER CENTER DOWN AND LOCK WAS OVER CENTERED. PILOT CARRIED OUT SUCCESSFUL LANDING AND AIRCRAFT WAS REMOVED FROM RUNWAY WITHIN 10 MINUTES. (TC NR 20070126011)                                                                           1L72 3O      A7CE                         
20070511001782007051100178    2007       5          11         CA070126012      420070124G2300                FEEDER CABLE                            BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33112UHR      WP  ROTOL R333  R333482F12  GL  RADIO           LOOSE           W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       APAPPROACH       1                      CA                                                                      (CAN) TOTAL LOSS OF CAPT`S RADIO COMMUNICATIONS. TROUBLESHOOTING FOUND MAIN POWER FEED CONNECTION NOT TIGHTEN ON TERMINAL BLOCK T5GA CAUSING CONNECTOR TERMINAL RING TO FLOAT AND REMOVE POWER SUPPLY TO CAPT`S AUDIO STATION BOX (TC NR 20070126012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4T4  TRTBA15CAA E4WE    6  CP61GL    
20070511001792007051100179NE  2007       5          11         CA070126013      220070126G7220                FAN                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              ENGINE          DISLODGED       W      BA  EMER. DESCENT           UNSCHED LANDING                                                         DTYINFLIGHT SEPARATION       ENGINE CASE PENETRATION   ENGINE STOPPAGE           CLCLIMB          1                      CA                                                                      (CAN) THE NR 1 ENGINE FAN DISLODGED ITSELF FROM THE ENGINE AND TORE OFF THE INLET AND FAN CASING.  IT ALSO DID EXTENSIVE DAMAGE TO THE PYLON AND THE FUSELAGE. NTSB IS ON SITE FOR THE INVESTIGATION. MORE INFORMATIOON TO FOLLOW ONCE AVAILABLE. (TC NR 20070126013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA21EA   E15NE                
20070511001802007051100180SO  2007       5          11         CA070127002      120070123G6120454254          CONTROL CABLE                           PIPER PA31  PA31325     7103105SO  LYC   O540  TIO540F2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  PROPELLER       FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                              317512033                               (CAN) LT PROPELLER CONTROL CABLE FAILURE. THE PILOT NOTED THAT THE LT PROPELLER CONTROL WAS STIFF ON APPROACH. THE LT ENGINE AND PROPELLER CONTROLS WERE INSPECTED, MAINTENANCE DETERMINED THE LT PROPELLER CONTROL CABLE IN THE CABIN PEDESTAL HAD FAILED. THE PROPELLER CONTROL CABLE WIRES HAD TWISTED AND SEVERED APPROXIMATELY .2500 FROM THE SWAGED PORTION OF THE ROD END.  THE LT PROPELLER CONTROL CABLE PN: 454-254 (ALT P/N: 24894-08) WAS REPLACED. THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070127002)                                                                                                                                                                                                                           1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070516001332007051600133NE  2007       5          16         CA070128001      220070125G7250                BEARING SEAL                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              NR 2 ENGINE     LEAKING         W      A   UNSCHED LANDING                                                                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CLCLIMB          1                      CA       1181111811                         872974                      (CAN) REPORTS OF LAV SMOKE CAUTION MSG COMING ON. PROBLEM APPEARS TO HAVE BEGUN ON DEC 5,2006 FLT. 8620, ON CLIMB-OUT, CREW RECEIVED A LAV SMOKE DETECT CAUTION LIGHT, FA CHECKED LAV NO SMOKE WAS EVIDENT, FLIGHT RETURNED TO DEPARTURE. A/C WAS DE-ICED PRIOR TO DEPARTURE AND DE-ICE FLUID WAS THE SUSPECTED CAUSE.  BOTH COALESER BAGS WERE REPLACED AND GROUND RUNS WERE CARRIED OUT.  A 2ND EVENT OCCURRED ON THE GROUND , DEC 5,2006, LAV SMOKE MSG CAME ON FOR 30 SECS THEN DID NOT COME ON AGAIN, C/BS WERE RESET AND A/C WAS POWERED DOWN AND RESET, FUNCTION CHECKED SERVICEABLE.  3RD EVENT, JANUARY 17, 2007, FLT. 7690,  SHORTLY AFTER ROTATION, FLIGHT CREW RECEIVED A SMOKE IN THE LAV INDICATION AND FA CONFIRMED LAV SMOKE D2L72 4F4  FRTA21EA   E15NE                
20070511001832007051100183EA  2007       5          11         CA070128002      120070126G4900                APU                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                                              CONTAMINATED    W      O   OTHER                                                                                           BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) SHORTLY AFTER DEPARTURE, THE CREW NOTICED A LAV SMOKE WARNING AND SMOKE WAS VISIBLE IN THE CABIN FOR 3-4 MINUTES  THEN IT DISSIPATED. SMOKE WAS BLUISH IN COLOR AND OILY SMELLING. (2) MAINTENANCE PERSONNEL WERE ON BOARD, INITIALLY THEY THOUGHT SINCE THE AIRCRAFT HAD JUST BEEN DE-ICED WITH ENGINES AND APU RUNNING THAT DE-ICE FLUID WAS THE CAUSE SO A DECISION WAS MADE TO CONTINUE. THE COALESER BAGS WERE INSPECTED AND REPLACED. AFTER ENGINE RUNS AND FURTHER TROUBLESHOOTING IT WAS NOTICED THAT NR 2 PRSOV IS RUNNING AT 38 TO 41 PSI AND MAY HAVE CAUSED DAMAGE TO NR 2 ACM.  FURTHER TROUBLESHOOTING ON GOING. (TC NR 20070128002)                                                                                        2L72 4F4  FRTA21EA   E15NE                
20070511001842007051100184EU  2007       5          11         CA070129001      120070127G3800                LINE                                    EMB   ERJ190ERJ190100IGW3260408EU                                                               WATER           LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    CRCRUISE         1                      CA       2865                                                           (CAN) REPORTED STIFF AILERONS IN FLIGHT AND IT APPEARS THE ROOT CAUSE WAS A WATER LEAK RESULTING IN WATER POOLING IN THE BILGE AND BINDING THE AILERON CABLES. AN INVESTIGATION IS STILL TAKING PLACE. (TC NR 20070129001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F    RTA57NM                        
20070511001852007051100185EU  2007       5          11         CA070129002      120070125G3244                TIRE                                    EMB   ERJ190ERJ190100IGW3260408EU                                                               MLG             FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) ON LANDING, RT OB MAIN WHEEL TIRE FAILED, DUE TO BRAKE SEIZING. INVESTIGATION STILL UNDERWAY ON CAUSE. (TC NR 20070129002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RTA57NM                        
20070530000072007053000007GL  2007       5          30         CA070129003      120070122G38104E32612         VALVE           BFGOODRICH              BOMBDRBD700 BD7001A10   1390006GL                                                               WATER SYSTEM    OPEN            W      H   DEACTIVATE SYST/CIRCUITS                                                                        KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) OVER AN HOUR INTO THE FLIGHT, A SPOILER MOMENTARY DEPLOYMENT WITH WING ROLL AFTER SPOILER FAULT CAS OCCURRED.  FLIGHT SPOILER FAIL CAS POSTED SHORTLY AFTERWARDS.  SEVERAL CABIN SYSTEM MALFUNCTIONS OCCURRING NEXT FOLLOWED BY HAVING NO WATER FROM ANY FAUCET AVAILABLE. A/C LANDED AT FINAL DESTINATION AND SPOILER/STAB IN BIT CAS POSTED. WATER NOTED TO BE DRAINING FROM FORWARD FUSELAGE BELLY SKIN DRAINS WITH WATER TANK QUANTITY SHOWING EMPTY.  GALLEY CARPET FOUND WET WITH GALLEY UNDER SINK AREA WET AS WELL. VISUAL INSPECTION OF AVIONICS BAY CARRIED OUT WITH FCU RESET PROCEDURE CARRIED OUT. SPOILER FAIL CAS CLEARED WITH SPOILER/STAB IN BIT ONLY THAT WAS MMEL`D . WATER SYSTEM LEFT EMPTY AND TURNED OFF FOR UNEVEN2L72 4F    RTT00003NY                     
20070511001862007051100186EA  2007       5          11         CA070129004      120070115G256011011200        BUCKLE                                  DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  CREW SEATBELT   DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) SPECIAL INSPECTION OF CREW SEAT BELT ROTORY LATCH SYSTEM PERFORMED. BOTH LT AND RT CREW SEATBELT BUCKLE ASSEMBLIES WERE CAPABLE OF BEING UNLATCHED WHEN CONTACTED BY THE CONTROL YOKE WHEN ROTATED LT OR RT WITH THE YOKE FULL AFT AND THE SEAT IN THE MOST FORWARD POSITION. THIS SPECIAL INSPECTION WAS MANDATED BY A COMPANY CAMPAIGN NOTICE TO INSPECT AIRCRAFT IAW FAA SPECIAL AIRWORTHINESS INFORMATION BULLETIN (NM-06-39)TO DATE, NO RECTIFICATION FOR THIS PROBLEM HAS BEEN PUBLISHED. (TC NR20070129004)                                                                                                                                                                                                                        1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070511001882007051100188NM  2007       5          11         CA070129005      120070128G323083221002003     LOCK                                    DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  NLG             DAMAGED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF THE NOSE LANDING GEAR FAILED TO RETRACT.  FLIGHT CONTINUED AND LANDED TO THE DESTINATION AIRPORT WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AFTER ARRIVAL AND FOUND THE NOSE GEAR GROUND LOCK OUT, AND IN LOCK POSITION.  (TC NR 20070129005)                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070511001912007051100191SW  2007       5          11         CA070129007      120070125G6510                DRIVE SHAFT                             BELL  407   407         1182206SW                                                               TAIL ROTOR      BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) THE A/C WAS BEING LANDED TO DROP OFF SKIERS AND REPORTEDLY HAD A T/R DRIVE SHAFT BREAK BETWEEN THE ENGINE AND THE OIL COOLER. THE A/C WAS LANDED WITHOUT DAMAGE. THERE WAS NO INDICATION OF A T/R STRIKE. (TC NR 20070129007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U    O H2SW                         
20070515001882007051500188NM  2007       5          15         CA070129008      120070126G3230483023          VALVE                                   BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  LT NACELLE      FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       215                                                            (CAN) CREW REPORTED THAT THE GEAR WENT UP BUT THE LT MAIN LANDING GEAR DOORS REMAINED OPEN.  JACKED AIRCRAFT AND PERFORMED A GEAR SWING. GEAR WENT UP BUT THE LT DOORS REMAINED OPEN AFTER SYSTEM WENT TO BYPASS MODE.  ON SELECTION OF GEAR DOWN THE LT MAIN GEAR DOORS CLOSED AND THE GEAR CAME DOWN WITH THE LT UPLOCK RELEASING.  RETRACTED THE GEAR AND TURNED OFF THE HYDRAULICS.  PERFORMED AN ALTERNATE GEAR EXTENSION TO GET THE GEAR DOWN. (TC NR 20070129008)                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070511001942007051100194EA  2007       5          11         CA070130001      120070129G2820                LINE                                    DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  FUEL VACUUM     LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) FLIGHT CREWS REPORTED THAT FUEL FLOW FLUCTUATES WHEN BOOST PUMPS ARE SELECTED OFF. SEVERAL VACUUM LEAKS WHERE FOUND IN THE FUEL LINES IN THE NACELLE AREA. SYSTEM SEALED AS REQUIRED, ENGINE GROUND RUNS CARRIED OUT AND NO FLUCTUATIONS NOTED AT TAKEOFF POWER WITH BOOST PUMPS OFF. (TC NR 20070130001)                                                                                                                                                                                                                                                                                                                                                                                                                                 1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070516001342007051600134    2007       5          16         CA070130002      420070123G3414                INDICATOR                               BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  AIRSPEED        INOPERATIVE     W      C   ABORTED TAKEOFF                                                                                 P  NO WARNING INDICATION                                                         TOTAKEOFF        1                      CA                                                                      (CAN) ON TAKEOFF ROLL THE CREW REJECTED THE TAKEOFF AT 85 KTS WITH NO INDICATION ON FIRST OFFICERS SIDE. MAINTENANCE CONDUCTED A PURGE OF THE SYSTEM AND CARRIED OUT A PITOT/STATIC SYSTEM TEST.THE SYSTEM WAS VERIFIED SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070130002)                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 3T4  T  A24EU   A196    6  CP899     
20070511001952007051100195CE  2007       5          11         CA070130003      120070129G76005052456849      CONDITION LEVER                         BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  CONTROL PEDESTALCRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) PILOTS REPORTED LT FUEL CONDITION LEVER CRACKED HALF WAY DOWN LEVER.  AIRCRAFT REMOVED FROM SERVICE.  RT CONDITION LEVER INSPECTED AND SHOWED SIGNS OF WEAR.  LT AND RT CONDITION LEVERS ON ORDER. (TC NR 20070130003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070511001962007051100196NM  2007       5          11         CA070130004      120070126G2820                O-RING                                  BOEING767   767306      1385148NM  GE    CF6   CF680C2B6F  30025NE                              FUEL SYSTEM     LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  LDLANDING        1                      CA                                                                      (CAN) AC LANDED WITH LOW HYD FLUID IN CENTER SYS FOUND ACMP NR 2 CENTER FILTER MODULE PRESSURE DELTA P POP-UP LEAKING DUE TO A FAILED O-RING.  O-RING REPLACED AND HYD SYSTEM SERVICED (37 QTS). (TC NR 20070130004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA1NM    E13NE                
20070511001982007051100198EA  2007       5          11         CA070131001      220070129G7397                CONNECTOR       BENDIX                  DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  NR 1 TRANSMITTERSEPARATED       W      O   OTHER                                                                                           N  FALSE WARNING                                                                 NRNOT REPORTED   1                      CA            4801  812141                                              (CAN) AIRCREW REPORTED THAT THE NR 1 FUEL FLOW WAS FLUCTUATING WITH NO OTHER ENGINE PARAMETERS BEING AFFECTED. MAINTENANCE TROUBLESHOT THE SYSTEM, SWAPPED GAUGES FROM SIDE TO SIDE, PERFORMED ENGINE RUNS AND COULD NOT FAULT THE SYSTEM.  AIRCRAFT WAS RELEASED FOR FLIGHT. WHEN AIRCRAFT RETURNED TO BASE THE AIRCREW REPORTED THAT THE SNAG WAS STILL PRESENT. MAINTENANCE BEGAN INVESTIGATING DEEPER INTO SYSTEM. WHEN THE NR 1 FUEL FLOW TRANSMITTER WAS LOOKED AT, IT WAS FOUND THAT THE CONNECTOR PLUG BOSS HAD SEPARATED FROM THE MAIN BODY, THIS ALLOWED THE WIRES TO STRIKE THE HOUSING SIDES DURING FLIGHT DUE TO NORMAL VIBRATIONS, SHORTING OUT THE TRANSMITTER. THIS COMPONENT HAS BEEN INSTALLED ON THE AIRCRAFT SINCE WE TOOK P1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070808001322007080800132EA  2007       8          8          CA070131002      120070131G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA                                                                      (CAN) THE CREW REPORTED THAT ON APPROACH THAT THEY RECEIVED AN INITIAL FLAP HALFSPEED MESSAGE FOLLOWED BY A (FLAP FAIL) MESSAGE WHEN FLAPS SELECTED ON APPROACH.  ZERO FLAP LANDING WAS COMPLETED. THE AIRCRAFT IS CURRENTLY WITH LINE MAINTENANCE TROUBELSHOOTING THE INCIDENT. (TC NR 20070131002)                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA21EA   E15NE                
20070511002002007051100200EA  2007       5          11         CA070131003      120070130G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        FAILED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) THE CREW REPORTED THAT UPON APPROACH FLAPS 8 DEGREES WERE SELECTED OKAY. UPON FLAP 20 DEGREE SELECTION, THE FLAPS DID NOT MOVE AND THE FLAP FAIL CAUTION LIGHT ILLUMINATED. THE FLAPS LOCKED AT 8 DEGREES. THE AIRCRAFT IS CURRENTLY IN LINE, MAINTENANCE IS TROUBLESHOOTING.(TC NR 20070131003)                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20070511002022007051100202SW  2007       5          11         CA070131004      120070122G6210206010200133    BLADES                                  BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              MAIN ROTOR      OUT OF BALANCE  W      K   NONE                                                                                            E  VIBRATION/BUFFET                                                              ININSP/MAINT     1                      CA                                                                      (CAN) COULD NOT ACHEIVE DYNAMIC BALANCE OF A/C. (TC NR 20070131004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U3  U  H2SW    E4CE                 
20070808001332007080800133EA  2007       8          8          CA070131005      120070124G3230                LANDING GEAR                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              MAINS           INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) THE AIRCRAFT LANDED WITH ALL LANDING GEAR UP. BA FSR ON SITE. FSR REPORTED THAT THE ADG WAS DEPLOYED, AND FLAPS RETRACTED. AIRPORT AUTHORITIES ARE PRESENTLY IN THE PROCESS OF LIFTING THE A/C IAW THE AIRCRAFT RECOVERY MANUAL USING CRANES. AIRCRAFT CONDITION APPEARS TO BE GOOD.   CONFIRMATION OF A WHEELS UP LANDING HAS BEEN RECEIVED. BA AIR SAFETY IS IN CONTACT WITH THE TSBC TO ESTABLISH WHAT ACTUALLY OCCURRED. IT IS NOT KNOWN IF THERE WERE ANY INJURIES. AN UPDATE WILL BE ISSUED SHORTLY. THE TSBC HAS CONTACTED THE CIAIC (SAFETY BOARD) OF SPAIN. THE BA RESPONSE WILL BE BASED ON THE NEXT UPDATE FROM BARCELONA.   THE FOLLOWING COULD BE OBSERVED IN THE COCKPIT (VERY LIMITED TIME ALLOWED): LANDING GEAR CONTROL H2L72 4F4  FRTA21EA   E15NE                
20070511002032007051100203EU  2007       5          11         CA070131007      120070128G56101379628C401     WINDSHIELD                              BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33110UG  01514WP  MCAULY4HFR344HFR34C652  NE  COCKPIT         DELAMINATED     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING MAINTENANCE INSPECTION, WINDOW WAS FOUND TO BE DELAMINATING AT THE CENTER OF THE BOTTOM EDGE. WINDOW WAS REPLACED. (TC NR 20070131007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4T4  TRTBA15CAA E4WE    6  C3PNE     
20070511002042007051100204EU  2007       5          11         CA070131008      120070131G2910373Q2277        LINE                                    BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  HYDRAULIC SYS   LEAKING         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE FLIGHT (30 MINUTES AFTER DEPARTURE THE FLIGHT CREW OBSERVED NR 1 AND NR 2 LOW HYDRAULIC PRESSURE LIGHTS ILLUMINATED. THE FLIGHT CREW RETURNED TO DEPARTURE, USED ALTERNATE MEANS FOR EXTENDING THE LANDING GEAR AND LANDED UNEVENTFUL.  MAINTENANCE FOUND INSUFFICENT FLUID IN THE HYDRAULIC SYSTEM. A LEAK IN HYDRAULIC LINE P/N 373Q2277, CAUSED BY CHAFING WAS FOUND IN THE LT MAIN LANDING GEAR WHEEL WELL.   THE LINE WAS REPLACED, SYSTEM BLEED AND FUNCTION CHECKED OK.   (TC NR 20070131008)                                                                                                                                                                                                                            2L72 3T4  T  A24EU   A196    6  CP899     
20070514000042007051400004NM  2007       5          14         CA070201003      120070201G324631573           WHEEL                                   BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NR 3            FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) AN AIRCRAFT EXPERIENCED NR 3 WHEEL AND TIRE SEPARATION UPON LANDING DUE TO WHEEL BEARING FAILURE. DETERIORATION OF THE MAIN LANDING GEAR WHEEL BEARINGS, RESULTING IN DAMAGE TO THE WHEEL, AXLE, AND BRAKE UNITS.    (TC NR 20070201003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070514000052007051400005EA  2007       5          14         CA070201004      120070201G2797                WIRE            CNDAIR                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              FLAP SYSTEM     BROKEN          W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) APPROX 1 MILE OUTSIDE THE OUTER MARKER AT 3000 AGL, THE AMBER FLAP CAUTION LIGHT ILLUMINATED.  THE CREW SELECTED FLAP 20 AND THE FLAPS WENT TO 20. WHEN THE LIGHT ILLUMINATED THE CREW WENT THROUGH THEIR EMERGENCY CHECKLIST AND CARRIED OUT AN UNEVENTFUL LANDING.  THE AIRCRAFT WAS THEN FERRIED FOR MAINTENANCE.  ALL FLAP ACTUATORS WERE PURGED AND SERVICED WITH FRESH GREASE IAW MM TASK 12-20-29-640-805.  BOTH BPSUS WERE REPLACED IAW MM TASK 27-51-10-000-80.  FLAP OPERATIONAL TESTS AND A TEST FLIGHT WERE CARRIED OUT WITH NO FAULTS FOUND. JANUARY 29/2007 IN HOUSE TASK RJ2-275002 FLAP MOISTURE PREVENTION PROGRAM WAS CARRIED OUT.  JANUARY 30/2007 THE AIRCRAFT FLEW FOUR LEGS AND ON THE FORTH LEG, THE FLAPS FAILED 2L72 4F4  FRTA21EA   E15NE                
20070514000062007051400006EU  2007       5          14         CA070201005      120070130G2710S27010022120100 WASHER                                  AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  AILERON         SPLIT           W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) THE CREW OBSERVED BINDING IN THE AILERON SYSTEM WHILE EXECUTING A RT TURN DURING DEPARTURE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER PROBLEM. POST FLIGHT INSPECTION DETECTED A LOCATION IN THE SYSTEM WHICH EXHIBITED AN INCREASED RESISTANCE TO TRAVEL WHEN CYCLING THE SYSTEM BUT THERE WAS NO RESTRICTION TO FULL MOVEMENT. MAINTENANCE FOUND A SPLIT TEFLON WASHER FOULING THE BEARING AT THE SWING LINK BETWEEN RIBS 8 AND 9. THE WASHER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE WITHOUT FURTHER PROBLEM. (TC NR 20070201005)                                                                                                                                                                      2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080320000012008032000001CE  2008       3          20         CA070201007      120070123G32440283353         TIRE                                    BEECH 200   B200        1152922CE                                                               SIDEWALL        SCORED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       18                                                             (CAN) DURING MAINT WALK AROUND INSP, IT WAS NOTED THAT ALL (4) MLG LOCATIONS RECEIVED SIDE WALL DAMAGE ON FIRST 20 HRS OF FLIGHT ON A FACTORY NEW AC DUE TO INTERFERENCE FIT.  AC HAS (2) STCS INCLUDED IN THE MLG. THEY ARE AS FOLLOWS:  AC EQUIPPED WITH  (P/N:028-335-3) (WILDERNESS TIRES):  STC SA00184LA.   AC ALSO EQUIPPED WITH WHEEL AND BRAKE CONVERSION KIT:  STC SA757GL BY STC HOLDER - MFG WAS CONTACTED AND STATED THAT THEY WERE AWARE OF THE PROBLEM SOME SIX MONTHS AGO. IM TOLD THE PROBLEM HAS ARISEN WITH THE (19.5X6.75-8/10/190 P/N:028335-3) WHEN MFG OUTSOURCED ITS MANUFACTURE TO FROM THE EXISTING USA FACILITY. THE OUT OF COUNTRY MFG TIRES ARE BUILT TO A WIDER TOLERANCE FOR SOME REASON. NOTE: ALL AFFECTED TI1L72 4T      A24CE                        
20070514000072007051400007GL  2007       5          14         CA070201008      220070127G732123034702        FCU                                     HUGHES369   369HS       4470728WP  ALLSN 250C  250C20      03013GL                              THROTTLE LEVER  FAILED          W      E   ENGINE SHUTDOWN                                                                                 K  FLUID LOSS                                                                    NRNOT REPORTED   1                      CA            2719                          CAE820727                   (CAN) AFTER THE AIRCRAFT WAS STARTED, THE PILOT DECIDED TO DO A WALK AROUND THE AIRCRAFT. FUEL WAS NOTICED FLOWING FROM THE ENGINE BAY TO THE GROUND. FURTHER INVESTIGATION REVEALED A MASSIVE FUEL LEAK AT THE FUEL CONTROL THROTTLE LEVER SHAFT SEAL. FUEL WAS FLOWING FROM THE FUEL CONTROL AND SATURATING THE STARTER GENERATOR WITH FUEL. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT EVACUATED. FCU REPLACED WITH SERVICABLE UNIT, STARTER VISUALLY INSPECTED AIRCRAFT GROUND RUN, LEAK CHECKED AND TEST FLOWN. AIRCRAFT RELEASED. THIS COULD HAVE BEEN A DIFFERENT STORY.  NORMALLY THE PILOT WOULD HAVE JUST TAKEN OFF AFTER STARTING THE AIRCRAFT. HIS DECISION TO PERFORM A WALK AROUND MAY HAVE SAVED LIVES AS THE AMOUNT OF FUEL LEAKIN1G71 3U3  U  H3WE    E4CE                 
20070514000112007051400011SW  2007       5          14         CA070201009      120070201G2410                BRACKET         LYC         LW11147     GULSTM500   500S        0141107SW  LYC   O540  IO540E1B5   41532EA  HARTZLHCC3Y HCC3YR2     NE  ALTERNATOR      WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THE ALTERNATOR ADJUSTING BRACKET BOLT HOLE THAT ATTACHES THE BRACKET TO THE ENGINE WAS FOUND CRACKED ALL THE WAY THROUGH. THE BRACKET WAS ONLY BEING HELD IN PLACE BY THE TENSION OF THE BELT. THERE IS SEVERAL OTHER REPORTS OF CRACKS IN THE BOLT HOLE OF THIS BRACKET ON OUR ENGINES. (TC NR 20070201009)                                                                                                                                                                                                                                                                                                                                                                                                                              1H72 3O3  O  6A1     1E4     5  CP25EA    
20070808001352007080800135EU  2007       8          8          CA070202001      120070130G71105711012091      COWLING                                 PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL                  DAMAGED         W      A   UNSCHED LANDING                                                                                 D  INFLIGHT SEPARATION                                                           CLCLIMB          1                      CA       14281                                                          (CAN) AFTER TAKEOFF THE PILOTS NOTICED THAT THE TOP FRONT COWLING WAS LIFTING OFF AT THE REAR. THEY RETURNED TO THE FIELD AND DURING THE FLARE THE COWLING DEPARTED THE AIRCRAFT, STRIKING AND DAMAGING THE PROP REQUIRING ITS DISASSEMBLY AND RT WING DAMAGING THE OB DEICE BOOT. THE POWER SECTION WAS REMOVED FOR A PROP STRIKE INSPECTION. MAINTENANCE HAD BEEN ACCOMPLISHED THE PREVIOUS EVENING WHERE THAT COWLING HAD BEEN REMOVED AND REINSTALLED. THE (4) LATCHES APPEARED SECURE TO THE AME AND THE PILOTS ON THEIR WALK AROUND. THERE IS NO VISUAL AID ON THIS COWLING DESIGN OTHER THEN THE LATCH BEING (FLUSH) TO INDICATE TO THE PILOT OR TECHNICIAN THAT THE LATCH IS SECURED. PREVIOUS EXPERIENCE HAS SHOWN THAT THE DIFFERENCE 1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070514000132007051400013EA  2007       5          14         CA070202002      120070126G493038834491        LINE            HONEYWELL   38004883    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              APU FUEL        CHAFED          W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      NRNOT REPORTED   1                      CA                  P160                                                (CAN) JANUARY 296/2007 DEFECT 591259,  THERE WAS A FUEL SMELL COMING FROM THE APU BLEED. THE APU WAS DEFERRED AND INHIBITED IAW MEL 49-10-01-1.  JANUARY 29/2007 MAINTENANCE REPLACED THE ECU FOR TROUBLESHOOTING, BUT THERE WAS NO FIX. FEBRUARY 01/2007 FURTHER TROUBLESHOOTING CARRIED OUT BY MAINTENANCE AND APU FUEL LINE FOUND TO BE LEAKING ABOVE THE EXCITER BOX.  THE ADEL CLAMP HAD CHAFED THROUGH THE LINE.  FUEL LINE PN 3883449-1  WAS REPLACED, NEW CLAMPS INSTALLED AND APU LEAK AND FUNCTION CHECKED SERVICEABLE.  APU HOUR SINCE OVERHAUL ARE 3254 AND CYCLES 2660. (TC NR 20070202002)                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20070514000152007051400015NM  2007       5          14         CA070202003      120070116G5210                SEAL                                    BOEING727   727225      1384077NM  PWA   JT8   JT8D15A     52051NE                                              FAILED          W      G   O2 MASK DEPLOYED                                                                                O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE AT FL320, CABIN RATE STARTED TO CLIMB AT 1500 FPM. CREW (CARGO FIT) DONED O2 MASKS. PRESSURIZATION CONTROLLER SELECTED TO (MANUAL) AND (STBY), NO CHANGE. CARGO HEAT OUTFLOW VALVE CLOSED, RECOVERED PRESSURE. O2 REMOVED, FLIGHT CONTINUED WITHOUT FURTHER INCIDENT.  MAINTENANCE CLEANED DOOR SEALS OF DEBRIS AND CARRIED OUT PRESSURIZATION CONTROL TEST IAW MM 21-31-00 AND FOUND SERVICEABLE. (TC NR 20070202003)                                                                                                                                                                                                                                                                                                      2L73 4F4  F  A3WE    E2EA                 
20070514000162007051400016NM  2007       5          14         CA070202004      120070117G2697W27260718       WIRE                                    BOEING727   727225      1384077NM  PWA   JT8   JT8D15A     52051NE                              FIRE DETECTION  SHORTED         W      F   ACTIVATE FIRE EXT.                                                                              N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB AT FL120, APU FIRE LIGHT AND BELL ILLUMINATED. APU FIRE DRILL CARRIED OUT, REMAINED (ON). DECLARED EMERGENCY, RETURNED TO AIRPORT WITHOUT INCIDENT.  UPON INSPECTION NO FIRE DETECTED.  MAINTENANCE FOUND (FIRE WARNING) WIRE  NR W272-607-18 SHORTED TO GROUND. WIRE REPLACED, FUNCTIONED CHECKED SERVICEABLE IAW MM 26-15-01.  (TC NR 20070202004)                                                                                                                                                                                                                                                                                                                                                                         2L73 4F4  F  A3WE    E2EA                 
20070514000172007051400017NM  2007       5          14         CA070202005      120070130G7110                DUCT                                    BOEING727   727225      1384077NM  PWA   JT8   JT8D15A     52051NE                              ENGINE COWLING  MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) UPON ARRIVAL, MAINTENANCE NOTICED AN APPROXIMATELY 6 INCH HOLE IN NR 1 ENGINE COWL. FURTHER INVESTIGATION DETERMINED THE CAP ON THE 6TH STAGE SADDLE DUCT MISSING, LOCATED IN COWL. CAP INSTALLED AND SECURED IAW MM AND COWL REPAIRED. (TC NR 20070202005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L73 4F4  F  A3WE    E2EA                 
20070514000182007051400018SW  2007       5          14         CA070202006      120070124G2432301265AA        DIODE           BELL                    BELL  206   206L1       1182107SW  ALLSN 250C  250C30P     03013GL                              BATTERY RELAY   FAILED          W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      APAPPROACH       1                      CA                  81640                                               (CAN) SINCE THE DIODE FAILED, A DIRECT SHORT TO GROUND OCCURED.  CAUSING THE BATTERY CIRCUIT WIRING TO BURN OFF ITS SHIELDING AND THE DIODE PIG TAIL FROM X1 TO X2 ON THE RELAY HEATED UP TO THE POINT OF BREAKING, FLAME WAS PRESENT.  THE BATTERY SWITCH WAS NOT DAMAGED, NOR WAS THE RELAY. (TC NR 20070202006)                                                                                                                                                                                                                                                                                                                                                                                                                              1G71 3U3  U  H2SW    E1GL                 
20070516001352007051600135NM  2007       5          16         CA070202007      120070201G7500311269001       ADAPTER                                 DHAV  DHC8  DHC8202     2809007NM  PWA   120   PW123D      52152NE  HAMSTD14SF  14SF23      NE  P3 BLEED AIR    CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9051 9051                          PCE123291                   (CAN) DURING ENGINE OIL SERVICING, TECHNICIAN NOTICED HEAT BLANKET WAS DAMAGED ON HP DUCT, BLANKET WAS REMOVED AND CRACK WAS FOUND ON DUCT. (TC NR 20070202007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070808001362007080800136EU  2007       8          8          CA070202008      120070130G3251NB046547R       COLLAR                                  BNORM BN2   BN2A26      1520226EU  LYC   O540  O540E4C5    41532EA  HARTZLHCC2Y HCC2YK2     GL  NLG STEERING    BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) NOSE LANDING GEAR STEERING COLLAR, BROKE IN TWO PIECES DURING GROUND HANDLING. COLLAR CRACKED AFT GREASE FITTING HOLE ANF FWD RT RELEASE DOG SLOT. (TC NR 20070202008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H72 3O3  O  A17EU   E295    5  CP920     
20070514000792007051400079NE  2007       5          14         CA070202009      220070114G7313311992001       FUEL NOZZLE                             BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING ROUTINE FUEL NOZZLE CLEANING AND FLOW TEST IT WAS NOTICED THAT ONE FUEL NOZZLE SHEATH WAS CRACKED FROM THE AIR BLEED SLOT AT A 45 DEGREE ANGLE TOWARDS THE NOZZLE HOLE. THE SHEATH HAD 400 HOURS TIME IN SERVICE SINCE LAST INSPECTION. (TC NR 20070202009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070808001372007080800137CE  2007       8          8          CA070202010      120070202G554012310231920     HINGE BRACKET   CESSNA                  CESSNA206   U206G       2073356CE  CONT  O520  IO520F      17032SO  HARTZLHCJ3Y PHCJ3YF1    GL  RUDDER          WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       *                                                              (CAN) DURING A 200 HR INSPECTION THE RUDDER WAS REMOVED FROM THE AIRCRAFT TO REPLACE THE RUDDER HINGE BEARINGS. INSPECTION OF THE RUDDER HINGE PIONT BRACKETS FOUND THE UPPER BRACKET P/N 1231023-19 OF THE LOWER HINGE POINT WORN COMPLETLY THROUGH BY THE BEARING, AND UPPER BRACKET P/N 1231023-20 HAD GROVES WORN INTO IT BY THE BEARING. THE BRACKETS WERE REPLACED WITH NEW PARTS AND THE RUDDER WAS REINSTALLED ON THE AIRCRAFT. (TC NR 20070202010)                                                                                                                                                                                                                                                                                     1H71 3O3  O  A4CE    E5CE    5  CP36EA    
20070808001382007080800138EU  2007       8          8          CA070202011      120070201G32225322012165      BARREL NUT      PILATS      532201203   PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  NLG             CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5232       IL192                                               (CAN) PILOT REPORTED THAT ON OCCASION DURING EXTENSION OF LANDING GEAR THAT A LOUD CLUNK WAS HEARD IN NOSE GEAR AREA.DURING A TEARDOWN OF NOSE LANDING GEAR TO REPLACE INTERNAL SEALS ,IT WAS NOTED THAT ON THE INNER GROOVE OF BARREL NUT ,THAT SUPPORTS A PHENOLIC GUIDE RING THAT CORROSION WAS OCCURING IN THE ALUMINIUM BARRLE NUT.THIS CORROSION PUT SO MUCH PRESSURE ON BACKSIDE OF GUIDE RING THAT THE RING WAS CLAMPING TO OLEO STRUT NOT ALLOWING THE STRUT TO FULLY EXTEND PRIOR TO RETRACTION OF GEAR. WHEN GEAR WAS LOWERED IN COLD FLIGHT CONDITIONS THE NOSE FORK WOULD CONTACT GEAR RETRACT MECHANISM ON EXITING GEAR WELL CAUSING CLUNK.  REMOVAL AND TREATMENT OF CORROSION, CLEANING OF GUIDE RING ALLOWED FREE MOVEMENT OF O1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070613001542007061300154NM  2007       6          13         CA070202012      120070131G2410                BEARING         LUCAS                   DHAV  DHC5  DHC5A       2803018NM                                                               DC GENERATOR    FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       1850 102   1093                                                (CAN) AIRCRAFT WAS RETURNING TO BASE WHEN THE NR 1 GENERATOR FAILED. FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEMS. WHEN MAINTENANCE REMOVED THE GENERATOR FOR REPLACEMENT THE QUILL SHAFT WAS FOUND SHEARED AND THE FORWARD BEARING ON THE GENERATOR SUFFERED A CATASTROPHIC FAILURE AND WAS COMPLETELY DESTROYED. THE GENERATOR HAD JUST BEEN INSTALLED 102 HOURS PREVIOUSLY FRESH FROM OVERHAUL FACILITY. ANOTHER GENERATOR WAS INSTALLED AND CHECKED SERVICEABLE. (TC  20070202012)                                                                                                                                                                                                                                                         2H72 4T    RT                             
20070514000812007051400081EA  2007       5          14         CA070202013      120070202G291365WE01042       PUMP                                    CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  HYDRAULIC SYS   WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            763                                                       (CAN) PUMP INSIDES COUPLING SPLINES BADLY WORN, OUT OF LIMITS.  (TC NR 20070202013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20070514000822007051400082NM  2007       5          14         CA070202014      120070118G5610NP15790114      WINDSHIELD                              DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA       11448                                                          (CAN) DURING FLIGHT, SMOKE AND FLAMES STARTING COMING FROM THE TOP OF FO`S WINDSCREEN.  SECONDS LATER WINDSCREEN SHOWED SEVERAL CRACKS. FOUND TERMINAL END L2 BURNED, REMOVED AND REPLACED TERMINAL END AND F/O`S WINDSHIELD.   (TC NR 20070202014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070514000832007051400083CE  2007       5          14         CA070202015      120070202G2612473275          FIRE DETECTOR                           BEECH 90    C90A        1152911CE  PWA   PT6   PT6A21      52043EA  HARTZLHCE4N HCE4N3      NE  RT NACELLE      MALFUNCTIONED   W      EFA ENGINE SHUTDOWN         ACTIVATE FIRE EXT.      UNSCHED LANDING                                 N  FALSE WARNING                                                                 CRCRUISE         1                      CA       289                                                            (CAN) DURING A ROUTINE MISSION, THE RT FIRE WARNING ANNUNCIATOR LIGHTS ILLUMINATED. THERE WAS NO VISUAL INDICATION OF FIRE. THE PILOT`S SECURED THE ENGINE IAW PUBLISHED PROCEDURES, ACTIVATED THE FIRE SUPPRESSION SYSTEM AND RETURNED TO THE BASE. MAINTENANCE WAS ABLE TO FAULT THE FIRE DETECTION SYSTEM FWD OF THE RT ENGINE FIREWALL, BUT WERE UNABLE TO PINPOINT THE EXACT CAUSE TO EITHER OF THE UPPER FIRE DETECTORS OR THE CONNECTING HARNESS. BOTH DETECTORS AND THE HARNESS WERE REPLACED.  THE ENGINE WAS INSPECTED FOR DAMAGE FROM THE RELEASE OF FIRE SUPPRESSION AGENT. NO DAMAGE WAS EVIDENT. THE FIRE BOTTLE AND SQUIB WERE REPLACED. AIRCRAFT WAS RELEASED INTO SERVICE. (TC NR 20070202015)                                 1L72 3T4  TRT3A20    E4EA    5  CP10NE    
20070514000842007051400084CE  2007       5          14         CA070202016      120070202G2810509215873       GASKET                                  BEECH 90    C90A        1152911CE  PWA   PT6   PT6A21      52043EA  HARTZLHCE4N HCE4N3      NE  RT ENGINE       DAMAGED         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA       166                                                            (CAN) PILOTS NOTICED FUEL (STREAMING) FROM THE RT NACELLE TOP COVER SHORTLY AFTER TAKEOFF. THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. THIS HAPPENED (3) TIMES BEFORE THE PROBLEM WAS CORRECTED. 1ST NOTICE, AFT 86.9 HRS. MAINTENANCE ATTRIBUTED THE EXCESS FUEL FOUND UNDER THE NACELLE COVER TO A PROBABLE FAULTY FUEL VENT CHECK VALVE ATTACHED TO THE FUEL FILLER NECK IN THIS AREA. THIS AREA OF THE AIRCRAFT WAS REINSPECTED DURING SCHEDULED MAINTENANCE AND MINIMAL FUEL WAS NOTICED.  2ND NOTICE - AFT 157.6 HRS. MAINTENANCE CHECKED THE AREA, PLUGGED THE VENT LINES AND FILLED THE FUEL CELL COMPLETELY. NO FAULTS WERE NOTED, SO ANOTHER CHECK VALVE WAS INSTALLED. 3RD NOTICE -- AFT 165.9 HRS. MAINTENANCE REMOVED THE RT NA1L72 3T4  TRT3A20    E4EA    5  CP10NE    
20070514000862007051400086CE  2007       5          14         CA070202017      120070201G2497                CONNECTOR                               CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA  MCAULY1C235 1C235LFA    GL  POWER JUNCTION  CORRODED        W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       NRNOT REPORTED   1                      CA       3758                                                           (CAN) DURING A PREFLIGHT INSPECTION WHEN THE FLAPS WERE SELECTED TO LOWER A COMPLETE POWER FAILURE RESULTED. UPON INSPECTION BY THE AMO THE POWER JUNCTION BOX PLUG WAS FOUND CORRODED RESULTING IN PINS BREAKING WHEN PLUG WAS PULLED APART FOR INSPECTION. THIS PLUG FAILURE RESULTED IN A POOR CONTINUITY FROM THE MASTER SOLENOID AND THE MASTER SWITCH RESULTING IN A 12+ VOLTAGE LOSS AND THE HOMINOID FAILING TO ENGAGE. (TC NR 20070202017)                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A12    1E10    5  NP12EA    
20070514000882007051400088EA  2007       5          14         CA070202018      120070201G324650105711        WHEEL                                   CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              MLG             DAMAGED         W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      CA       6836                                                           (CAN) DURING ROTATION THE A/C PULLED TO THE LT ON CLIMB OUT , ASSOCIATED WITH SEVERE VIBRATION. THE FLIGHT CREW DECIDED TO DIVERT THE A/C. UPON LANDING THE ROB TIRE DEFLATED.  UPON INVESTIGATION, THE FOLLOWING WAS FOUND . THE INNER RT MAIN WHEEL CORD WAS DAMAGED AND DEFLATED. ( FROM ORIGINAL REPORT ON T/O. BOTH MAIN WHEEL`S WERE REPLACED . THE OUTER RT MAIN WHEEL WAS DAMAGED ON LANDING.  THE RT INNER FLAP WAS DAMAGED BY THE TIRE SEPARATION NR REPLACED . THE AFT FUSELAGE BODY FAIRING WAS SLIGHTLY DAMAGED AND REPAIRED UNDER REO 601R-53-82-267( 500 FT/HRS )  (TC NR 20070202018)                                                                                                                                           2L72 4F4  FRTA21EA   E15NE                
20070514000902007051400090EA  2007       5          14         CA070202019      120070131G5610601R3303031     WINDOW                                  CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C1          NE                              COCKPIT         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         DEDESCENT        1                      CA       8520                                                           (CAN) CREW NOTED ON DESCENT, CAPT SIDE WINDOW CRACKED HOWEVER CABIN PRESS REMAINED NORMAL AND A.C LANDED SAFELY.  C/A---REMOVED AND REPLACED CAPT SIDE WINDOW IAW CRJ AMM 56-10-05 AND OPS CK GOOD   MX REPORT CAPT SIDE WINDOW SHATTERED (TC NR 20070202019)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA21EA   EOOO63EN             
20070514001002007051400100EU  2007       5          14         CA070204001      120070201G5320                CHANNEL                                 SNIAS 350   AS350D      8680803EU  LYC   LTS101LTS101600A2 41560NE                              FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING AN UNSCHEDULED MAINTENANCE PROCEDURE OF THE VIBRATION DAMPER ASSEMBLIES UNDER THE CABIN FLOOR, IT WAS FOUND THROUGH THE USE OF A BOROSCOPE THAT THE IB CHANNELS OF THE LATERAL SUPPORT STRUCTURE WERE CRACKED AT THE UPPER ENDS.  SUBSEQUENT INSPECTION OF ALL OUR AIRCRAFT REVEALED SIMILAR DISCREPANCIES. (TC NR 20070204001)                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3U3  U  H9EU    E5NE                 
20070514001012007051400101EU  2007       5          14         CA070205001      120070202G6220704A33341003    SPRING                                  SNIAS 350   AS350*             EU  TMECA ARRIELARRIEL1B    6OO30NE                              ANTI VIBRATION  BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       113591460                                                      (CAN) WE ARE DOING A 12 YEAR INSPECTION ON AIRCRAFT, AS WELL AS SEND IT OUT FOR PAINT. THE MAIN ROTOR ANTI-VIBRATOR WAS REMOVED FOR CHECK AND MODIFICATION. WHEN SPRINGS WERE REMOVED, ONE WAS FOUND TO BE BROKEN 40 MM FROM OB END. THIS AREA IS HIDDEN BEHIND SIDE COVERS. (TC NR 20070205001)                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3U3  U  H9EU    E19EU                
20070514001032007051400103    2007       5          14         CA070205002      420070203G34180861HB          VANE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              AOA             FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA       1428 1428                                                      (CAN) DURING CLIMB OUT STALL FAIL CAUTION MESSAGE ILLUMINATED. CREW UNABLE TO RESET DURING FLIGHT. CREW ELECTED TO LAND AT ENROUTE MAINTENANCE BASE. MAINTENANCE REPLACED RT AOA VANE, FUNCTION CHECKED AND AIRCRAFT RETURNED TO SERVICE (TC NR 20070205002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20070514001052007051400105EA  2007       5          14         CA070205003      120070203G2752                ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              TE FLAP         FAILED          W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH, CREW SELECTED FLAP 8 AND RECEIVED A (FLAP FAIL) MESSAGE. FLAP FAILED AT 0. CREW ADVISED ATC AND DECLARED EMERGENCY. LANDING WAS UNEVENTFUL. (TC NR 20070205003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA21EA   E15NE                
20070516001362007051600136NM  2007       5          16         CA070205004      120070121G323183232013003     BELLCRANK                               DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  NLG DOOR        BROKEN          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       3000                                                           (CAN) AN OPERATOR MADE AIR TURN BACK DUE TO NOSE GEAR DOOR MALFUNCTION. THE NLG DOORS WONT CLOSE WHEN SELECTED. THE AMBER NOSE GEAR DOOR LIGHT SHOWED ON LANDING GEAR CONTROL PANEL. MAINTENANCE FOUND THE NOSE GEAR BELLCRANK BROKEN AT ONE OF THE LUGS. (TC NR 20070205004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070514001072007051400107CE  2007       5          14         CA070205005      120070205G2560497900312       BUCKLE                                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              ROTARY SEAT BELTFAILED          W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) REF FAA SPECIAL AIRWORTHINESS INFORMATION BULLETIN NM-06-29 AND MFG CAMPAIGN NOTICE 010-25-10-011 REV 1 FIXED WING AIRCRAFT EQUIPPED WITH ROTARY CREW SEAT BELT BUCKLES.  WHEN THE CONTROL COLUMN IS PULLED FULLY AFT THE SEAT BELT BUCKLE CAN BE RELEASED BY ROTATING THE CONTROL WHEEL IN BOTH THE PILOT AND CO-PILOT POSITIONS. (TC NR 20070205005)                                                                                                                                                                                                                                                                                                                                                                                    1L72 4F4  F  A22CE   E1NE                 
20070514001102007051400110NM  2007       5          14         CA070205007      120070130G2741651948218       GEARBOX                                 BOEING727   727227      1384078NM  PWA   JT8   JT8D9A      52048NE                              HORIZONTAL STAB FAILED          W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) AFTER DEPARTURE, CREW EXPERIENCED STAB TRIM FAILURE.  A/C RETURNED TO AIRPORT WITHOUT INCIDENT.  MAINTENANCE CREWS FOUND THE STAB TRIM GEARBOX TO BE QUITE STIFF TO OPERATE AND REPLACED IT.  A/C RETURNED TO SERVICE.  THE STAB TRIM GEARBOX AND JACKSCREW WERE INSPECTED AND LUBED ON A 2A CHECK NOV 19/2006. (TC NR 20070205007)                                                                                                                                                                                                                                                                                                                                                                                                       2L73 4F4  F  A3WE    E2EA                 
20070514001122007051400112CE  2007       5          14         CA070206002      120070205G3260                LANDING GEAR                            BEECH 100   B100        1152919CE  GARRTTTPE331TPE3316252B 01514WP  HARTZLHCB4T HCB4TN5     GL  MAINS           UNKNOWN         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) LANDING GEAR (IN TRANSIT) LIGHT STAYED ON AFTER GEAR UP SELECTION AFTER TAKEOFF. GEAR DOWN SELECTED AND GEAR WENT DOWN AND LOCKED NORMALLY (3 GREEN LIGHTS) FOR LANDING BACK TO DEPARTURE AIRPORT.  AIRCRAFT JACKED, RETRACTIONS DONE, LANDING GEARS INSPECTED, CLEANED AND LUBED, NO DEFAULT FOUND, SYSTEM FOUND SERVICEABLE. (TC NR 20070206002)                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A14CE   E2WE    6  CP40EA    
20070514001152007051400115    2007       5          14         CA070206003      420070204G8300                COVER                                   CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              AGB             DISLODGED       W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) APPROX 10 MINS INTO THEIR DESCENT, THE NR 1 OIL PRESSURE WARNING LIGHT ILLUMINATED. THE NR 1 OIL PRESSURE READ 0.  THE CREW REFERENCED THEIR CHECKLIST AND SHUTDOWN THE ENGINE. THE CREW ANNOUNCED TO THE PAX THAT DUE TO LOW OIL PRESSURE THEY WERE GOING TO SHUT DOWN AN ENGINE. MAINTENANCE CHECKED AND CLEANED TRANSDUCER CONNECTOR PLUGS, OIL TANK AND ASSOCIATED PLUMBING. THE ONLY ANOMALY NOTED WAS THE PLUG ON THE ACCESSORY GEAR BOX WAS NOT PROPERLY SECURED. THE CIRCLIP WAS OFF AND THE PLUG DISLODGED SOMEWHAT. THERE WAS NO EVIDENCE OF MASSIVE OIL LOSS, BUT SUSPECT WITH CAP OFF ENGINE WAS PROBABLY SUCKING AIR, AND NOT PRESSURIZING ACCESSORY GEAR BOX PROPERLY. CIRCLIP SECURED. IDLE AND HIGH POWER RUNS COMPLETED S2L72 4F4  FRTA21EA   E15NE                
20070514001172007051400117CE  2007       5          14         CA070207001      120070203G3230MC815A51        RELAY                                   BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  MLG             INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA            484                                                       (CAN) LANDING GEAR IN TRANSIT LIGHT STAYED ON AFTER GEAR WAS SELECTED UP AND AN ALTERNATE GEAR EXTENSION WAS DONE AND THE A/C RETURNED TO BASE. THE LANDING GEAR CONTROL RELAY BOX WAS REPLACED AND LANDING GEAR SYSTEM FUNCTION CHECKED SERVICEABLE. (TC NR 20070207001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070514001192007051400119EA  2007       5          14         CA070207002      120070131G5210600315351001    STRIKER                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              DOOR SEAL       DAMAGED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) DURING A TYPE III REPAIR (MFG REO 601R-53-22-033) DUE TO A CRACK FOUND ON THE OUTER FLANGE OF THE PASSENGER DOOR FWD SEAL STRIKER, THE FORWARD SEAL STRIKER FLANGE WAS FOUND CRACKED IN THE RADIUS  (OVER 3INCHES IN LENGTH) UNDER AN EXISTING REPAIR (REPAIR TYPE I, REO 601R-53-22-033). AFTER A VISUAL CHECK, THE AFT PASSENGER DOOR SEAL STRIKER (ALSO PREVIOUSLY REPAIRED TYPE I) WAS FOUND CRACKED IN THE RADIUS. (TC NR 20070207002)                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20070514001212007051400121CE  2007       5          14         CA070207003      120070206G25601101983         BUCKLE                                  BEECH 90    C90A        1152911CE  PWA   PT6   PT6A21      52043EA  HARTZLHCB3T HCB3TN3     GL  CREW SEATBELTS  DAMAGED         W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) CAMPAIGN NOTICE 010-25-10-011 / FAA SAIB NM-06-29.  CREW SEAT BELT ROTARY LATCH IS CONTACED BY THE CONTROL YOKE AND THE POSSIBLITY EXISTS TO RELEASE THE BELT WITH ROTATION OF THE CONTROL YOKE WHEN FUNCTIONAL TEST WAS CARRIED OUT IAW SAIB. (TC NR 20070207003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T4  TRT3A20    E4EA    6  CP15EA    
20070514001312007051400131CE  2007       5          14         CA070207007      120070206G3310                LIGHT                                   BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCD4N3HCD4N3A     GL  CABIN           INOPERATIVE     W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      APAPPROACH       1                      CA       8862 8862                                                      (CAN) WHILE ON FINAL APPROACH, SMOKE WAS OBSERVED IN COCKPIT COMING FROM THE LOWER LT C/B PANEL. SIDE LIGHT C/B POPPED AND SMOKE STOPPED. LANDING COMPLETED WITHOUT FURTHER INCIDENT.  MAINTENANCE WAS CONTACTED AND IN CONVERSATION WITH FLIGHT CREW SMOKE PROBLEM WAS ISOLATED TO EDGE OF PANEL LIGHTING, C/B WAS PULLED AND POWER FUNCTION TEST REVEALED NO FURTHER SMOKE ISSUES. RETURN FLIGHT WITH ESSENTIAL CREW WAS CARRIED OUT. MAINTENANCE STAFF CONFIRMED PROBLEM AND SHORTED PANEL WAS REPAIRED. (TC NR 20070207007)                                                                                                                                                                                                                 1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070514001332007051400133WP  2007       5          14         CA070207008      120070202G6710A9182           BUNGEE                                  ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FLT CONTROLS    DISCONNECTED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       87                                                             (CAN) UPON INSPECTION, BUNGEE FOUND HANGING DOWN AND DISCONNECTED FROM THE FLIGHT CONTROL. THERE WERE NO FLIGHT PERFORMANCE ISSUES REPORTED. MINOR SCRAPES FOUND IN CONTROL TUBE PAINT. CORDS WERE CHECKED FOR DAMAGE AND RECONNECTED. (TC NR 20070207008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 3O3  O  H11NM   1E4                  
20070514001362007051400136EA  2007       5          14         CA070208001      120070207G27507805013         CONTROL LEVER                           CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              TE FLAP CONTROL DAMAGED         W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  LDLANDING        1                      CA                                                                      (CAN) AFTER LANDING WITH FLAPS SELECTED TO 45 DEGREES, THE CREW SELECTED FLAPS FROM 45 TO 20 DEGREES AND THE FLAPS DID NOT MOVE. CAPTAIN PUT THE FLAPS BACK TO 45 DEGREES. FECU (FLAPS ELECTRONIC CONTROL UNIT) CODES RETRIEVED BY MAINTENANCE POINTED OUT TO THE FLAP CONTROL LEVER WHICH WAS REPLACED. (TC NR 20070208001)                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20070514001392007051400139CE  2007       5          14         CA070208002      120070128G561050420066137     WINDOW                                  BEECH 100   B100        1152919CE  GARRTTTPE331TPE3316252B 01514WP  HARTZLHCB4T HCB4TN5     GL  COCKPIT         DEPARTED        W      B   EMER. DESCENT                                                                                   D  INFLIGHT SEPARATION                                                           CLCLIMB          1                      CA       10639                                                          (CAN) AFTER TAKEOFF AND CLIMB TO APPROXIMATELY 10,000 FEET, THE LT.   (TC NR 20070208002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 4T4  T  A14CE   E2WE    6  CP40EA    
20070514001572007051400157SO  2007       5          14         CA070208003      120070117G760330205002        THROTTLE CABLE                          PIPER PA23  PA23250     7102308SO  LYC   O540  IO540C4B5   41532EA  HARTZLHCE2Y HCE2YR2     GL                  FAILED          W      E   ENGINE SHUTDOWN                                                                                 RF PARTIAL RPM/PWR LOSS      FLT CONT AFFECTED                                   DEDESCENT        1                      CA                                                                      (CAN) DURING DESCENT THE RT THROTTLE DID NOT RESPOND. THE ENGINE WAS SHUTDOWN AND PROPELLER FEATHERED. UPON RETURN TO THE HANGAR, CABLE 30205-002 WAS REPLACED AND DUAL INSPECTION CARRIED OUT. (TC NR 20070208003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 3O3  O  1A10    1E4     5  CP9EA     
20070514001602007051400160CE  2007       5          14         CA070208004      120070207G2497S21351          WIRE                                    CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160DTM    GL  CONNECTOR       BURNED          W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                                                                      (CAN) DURING A ROUTINE INSPECTION IT WAS DISCOVERED THAT ONE WIRE GOING TO THE OVER VOLTAGE WARNING LIGHT WAS FOUND BURNED.  CAUSE OF THE BURNED WIRE WAS DUE TO FAILURE OF A BUTT SPLICE IN THE WIRE WHICH HAD EXPOSED THE BARE WIRE CAUSING IT TO SHORT OUT. THE BURNED SECTION OF WIRE WAS REPLACED. THE AIRCRAFT WAS GROUND CHECKED SERVICEABLE AND RETURNED TO SERVICE. (TC NR 20070208004)                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A12    E274    5  NP910     
20070514001642007051400164SW  2007       5          14         CA070208005      120070205G56102719442004      WINDSHIELD                              SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  COCKPIT         CRACKED         W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA            2415                                                      (CAN) DURING TAXI WITH THE WINDSHEILD HEAT SELECTED ON THE RT COCKPIT HEATED WINDSHEILD CRACKED. THE FLIGHTCREW RETURNED TO THE TERMINAL AND THE AIRCRAFT WINDOW HAS BEEN REPALCED BY MAINTENANCE. NO CAUSE OF THE CRACKED GLASS COULD BE DETERMINED. THIS IS THE THIRD FAILURE OF A HEATED WINDSHEID THIS COMPANY HAS INCURRED SINCE JAN 1, 2007. 12 WERE REPORTED IN 2006. OTHER AIRCRAFT OPERATORS OF THIS TYPE OF AIRCRAFT HAVE BEEN CONTACTED AND ARE INCURRING SIMILAR FAILURE RATES. (TC NR 20070208005)                                                                                                                                                                                                                                 2L72 4T4  TRTA8SW    E4WE    5  CP10NE    
20070514001612007051400161CE  2007       5          14         CA070209001      120070207G2560110198301       BUCKLE                                  BEECH 90    C90A        1152911CE  PWA   PT6   PT6A21      52043EA  HARTZLHCB3T HCB3TN3     GL  SEAT BELT ASSY  DAMAGED         W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) WITH A COCKPIT CREW MEMBER STRAPPED INTO THEIR SEAT WITH THE SEAT FULLY FORWARD, INTERFERENCE BETWEEN THE CONTROL COLUMN YOKE AND THE ROTARY SEAT BELT BUCKLE FINS OCCURS WHEN THE CONTROL YOKE IS PULLED FULLY AFT AND ROTATED. THE POSSIBILITY EXISTS THAT THE SEAT BELT ROTARY BUCKLE COULD BE INADVERTENTLY RELEASED DURING EXTREME FLIGHT CONTROL MOVEMENTS. THIS CONDITION WAS VERIFIED WHILE PERFORMING THE PROCEDURE AS DESCIBED IN FAA SAIB NM-06-29. A GUARDED BUCKLE WOULD NEGATE THE POSSIBILITY OF ACCIDENTAL RELEASE (TC NR 20070209001)                                                                                                                                                                                    1L72 3T4  TRT3A20    E4EA    6  CP15EA    
20070514001582007051400158CE  2007       5          14         CA070209002      120070207G2560110193201       BUCKLE                                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              SEAT BELT       MALFUNCTIONED   W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) WITH A COCKPIT CREW MEMBER STRAPPED INTO THEIR SEAT WITH THE SEAT FULLY FORWARD, INTERFERENCE BETWEEN THE CONTROL COLUMN YOKE AND THE ROTARY SEAT BELT BUCKLE FINS OCCURS WHEN THE CONTROL YOKE IS PULLED FULLY AFT AND ROTATED. THE POSSIBILITY EXISTS THAT THE SEAT BELT ROTARY BUCKLE COULD BE INADVERTENTLY RELEASED DURING EXTREME FLIGHT CONTROL MOVEMENTS. THIS CONDITION WAS VERIFIED WHILE PERFORMING THE PROCEDURE AS DESCIBED IN FAA SAIB NM-06-29. A GUARDED BUCKLE WOULD NEGATE THE POSSIBILITY OF ACCIDENTAL RELEASE (TC NR 20070209002)                                                                                                                                                                                    1L72 4F4  F  A22CE   E1NE                 
20070514001592007051400159CE  2007       5          14         CA070209003      120070207G2560110193201       BUCKLE                                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              CREW SEATS      INTERFERENCE    W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) WITH A COCKPIT CREW MEMBER STRAPPED INTO THEIR SEAT WITH THE SEAT FULLY FORWARD, INTERFERENCE BETWEEN THE CONTROL COLUMN YOKE AND THE ROTARY SEAT BELT BUCKLE FINS OCCURS WHEN THE CONTROL YOKE IS PULLED FULLY AFT AND ROTATED. THE POSSIBILITY EXISTS THAT THE SEAT BELT ROTARY BUCKLE COULD BE INADVERTENTLY RELEASED DURING EXTREME FLIGHT CONTROL MOVEMENTS. THIS CONDITION WAS VERIFIED WHILE PERFORMING THE PROCEDURE AS DESCIBED IN FAA SAIB NM-06-29. A GUARDED BUCKLE WOULD NEGATE THE POSSIBILITY OF ACCIDENTAL RELEASE.  (TC NR 20070209003)                                                                                                                                                                                  1L72 4F4  F  A22CE   E1NE                 
20070514001622007051400162GL  2007       5          14         CA070209004      320070203G6110HCE4A3D         PROPELLER                               PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL                  LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      CA       3188 3188                                      HJ1517          (CAN) DURING FLIGHT OIL WAS NOTICED ON THE WINDSCREEN WHILE ON ROUTE. UPON INSPECTION AFTER LANDING, MAINTENANCE FOUND EXCESSIVE OIL ON ENGINE COWLING. PROP WAS REMOVED AND SENT FOR REPAIRS. REPAIR SHOP CHANGED ALL THE INTERNAL SEALS AND RETURNED THE PROP. REPAIRED PROP WAS RE-INSTALLED. AFTER 6 HRS IN OPERATION FLUID WAS NOTICED LEAKING FROM PROP AGAIN ALTHOUGH NOT TO THE DEGREE THAT OCCURRED ON THE FIRST OCCASION. AFTER CLEANING AND GROUND RUNS IT WAS DETERMINED THAT THE PROP WAS LEAKING OIL AGAIN.  PROP WAS REMOVED AND SENT FOR REPAIR AGAIN. REPAIR SHOP FINDINGS HAVE YET TO BE DETERMINED. (TC NR 20070209004)                                                                                                      1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070514001632007051400163GL  2007       5          14         CA070209005      120070209G2720C2TR445         BELLCRANK                               DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  RUDDER          CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       23428                                                          (CAN) ON REMOVAL OF RUDDER FOR BEARING REPLACEMENT CORROSION WAS PRESENT ON THE OB ATTACH POINTS OF THE RUDDER BELLCRANK NR C2TR445 (PICTURE ATTACHED) CORROSION WAS NOT EVIDENT BEFORE THE REMOVAL OF THE RUDDER AS THE DAMAGED AREA WAS COVERED BY THE RUDDER CONNECTING RODS NR C2UT233. THE AIRCRAFT NOTED ABOVE HAS BEEN OPERATED EXTENSIVELY FROM SALT WATER. (TC NR 20070209005)                                                                                                                                                                                                                                                                                                                                                         1H71 3R3  RRCA806    5E1     5  CP206     
20070514001732007051400173NE  2007       5          14         CA070209008      220070111G7200                ENGINE                                  BELL  427   427         1182207SW  PWC   PW207 PW207D           NE                                              OVERSPEED       W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                          BF0116                      (CAN) THE ENGINE WENT TO AN OVERSPEED CONDITION ON TAKE-OFF AND THE TAKE-OFF WAS ABORTED.  MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070209008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  R00001RCE42NE                
20070515001892007051500189NE  2007       5          15         CA070209009      220070112G753231J285704       MOTOR                                   CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              BLEED VALVE     UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY VIBRATION, AN EEC REVERSION AND A LACK OF THROTTLE RESPONSE.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED A UNSERVICEABLE BLEED VALVE TORQUE MOTOR. (TC NR 20070209009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA22CE   E00059EN             
20070515001902007051500190EA  2007       5          15         CA070209010      220070103G73213027791         TUBE                                    BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  FCU P3          FRACTURED       W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA       5581                                                           (CAN) ON CLIMB, ENGINE POWER REDUCED TO IDLE UNCOMMANDED.  THE ENGINE WAS SHUTDOWN IN FLIGHT. INSPECTION REVEALED A FRACTURED FCU P3 DELIVERY TUBE. (TC NR 20070209010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070515001912007051500191NE  2007       5          15         CA070209011      220070118G73103026779         LINE                                    BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE                              FUEL SYSTEM     FRACTURED       W      K   NONE                                                                                            KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            ININSP/MAINT     1                      CA                                                                      (CAN) ON INSPECTION FOLLOWING A REPORT OF FUEL ODOR IN THE CABIN, THE ENGINE HIGH PRESSURE FUEL DELIVERY TUBE WAS FOUND CRACKED. (TC NR 20070209011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 4T4  T  A24CE   E4EA                 
20070515001922007051500192NE  2007       5          15         CA070209012      220070116G7260                DRIVE GEAR                              FOKKERF27   F27MK50            EU  PWA   PW120 PW127            NE                              GEARBOX         DAMAGED         W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  DEDESCENT        1                      CA                                                                      (CAN) THE ENGINE FLAMED OUT ON DESCENT.  SUBSQUENT INSPECTION REVEALED DAMAGE TO THE ANGLE DRIVE GEARBOX GEARING. (TC NR 20070209012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA817    E20NE                
20070515001932007051500193NE  2007       5          15         CA070209013      220070118G7260                GEAR                                    AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              GEARBOX         DAMAGED         W      O   OTHER                                                                                           X  ENGINE FLAMEOUT                                                               CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE FLAMED OUT IN CRUISE.  SUBSEQUENT INVESTIGATION REVEALED DAMAGED TOWERSHAFT DRIVE BEVEL GEARS. (TC NR 20070209013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRT        E20NE                
20070515001942007051500194NE  2007       5          15         CA070209014      220070119G73218237007         HMU                                     CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              ENGINE          UNSERVICEABLE   W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  NRNOT REPORTED   1                      CA                  F51037                                              (CAN) THE ENGINE FLAMED OUT IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED AN UNSERVICEABLE HYDROMECHANICAL FCU. (TC NR 20070209014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA22CE   E00059EN             
20070515001952007051500195NE  2007       5          15         CA070209015      220070121G7261                TUBE                                    EMB   120   EMB120      3260201SO  PWA   118   PW118            NE                              ENGINE OIL      FRACTURED       W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE ENGINE OIL PRESSURE REDUCED AND THE PILOT SHUT THE ENGINE DOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED A FRACTURED NR 6 AND 7 BEARING OIL TRANSFER TUBE. (TC NR 20070209015)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4T4  TRTA31SO   E20NE                
20070515001962007051500196NE  2007       5          15         CA070209016      220070123G7200                ENGINE                                  DORNERDO32  DO328100    2996000NM  PWA   119   PW119B           NE                                              FAILED          W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                          116011                      (CAN) DURING CRUISE THE ENGINE CHIP DETECTOR AND LOW OIL PRESSURE WARNINGS ACTIVATED AND THE ENGINE FLAMED OUT IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070209016)                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA45NM   E20NE                
20070515001982007051500198CE  2007       5          15         CA070209019      120070131G57115016000355      SPAR                                    BEECH 100   100BEECH    1152916CE                                                               RT WING         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       17018                                                          (CAN) RT IB FLAP P/N 50-160003-97 REMOVED FOR HINGE BRACKET REPLACEMENT.  UPON TEARDOWN OF FLAP FOR HINGE BRACKET REMOVAL, AN 8 INCH CRACK WAS NOTED ON THE SPAR UPPER RADIUS.  THE CRACK EXTENDED 4 INCHES EITHER SIDE OF THE FLAP ACTUATOR BRACKET ATTACH AREA. PROBABLY CRACKED DUE TO CYCLING OF THE FLAP OVER TIME AND THE LOCALIZED STRESSES IN THAT AREA OF THE FLAP, AROUND THE ACTUATOR BRACKET. CRACK IN SPAR CANNOT BE SEEN WITHOUT DISASSEMBLY OF FLAP. (TC NR 20070209019)                                                                                                                                                                                                                                                         1L72 3T      A14CE                        
20070515001992007051500199SO  2007       5          15         CA070209020      120070207G2424B002861         VOLT REGULATOR                          PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  LT ALTERNATOR   FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE FLIGHT, THE LT ALTERNATOR FAIL LIGHT CAME ON, AIRCRAFT RETURNED TO BASE FOR REPAIRS. VOLTAGE REGULATORS REPLACED WITH NEW, RT ALTERNATOR P/N ALU8521 REPLACED WITH OVERHAULED UNIT. GROUND RUNS CARRIED OUT TO CHECK FUNCTION, CHECKED OK.  TEST FLIGHT CARRIED OUT AND SYSTEM CHECKED NORMAL. (TC NR 20070209020)                                                                                                                                                                                                                                                                                                                                                                                                              1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070515002002007051500200NE  2007       5          15         CA070209021      220070207G7250                BLADE                                   SAAB  SF340 340B        7860101EU  GE    CT7TP CT79B       30030NE  ROTOL R390  R3904123F27 NE  TURBINE DISK    SEPARATED       W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA       1245812458                         785590                      (CAN) AFTER REACHING CRUISING ALTITUDE OF 23000 FT THE LT ENGINE SURGED AND THE LOW OIL PRESSURE LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE FLIGHT CONTINUED TO WHERE AN UNEVENTFULL LANDING WAS MADE. THE ENGINE STRIP SHOWED THAT THE COMPRESSOR STAGE ONE TURBINE DISK HAD LOST A BLADE. THE REMAINING BLADES HAD SUFFERED EXTENSIVE DAMAGE, AS TOO HAD THE STATOR ASSY. THE ENGINE AND COMPONENTS HAVE BEEN RETURNED TO GE (ENGINE OEM) FOR INVESTIGATION. (TC NR 20070209021)                                                                                                                                                                                                                                                      2L72 4T4  TRTA52EU   E8NE    6  CP31NE    
20070515002012007051500201EU  2007       5          15         CA070209022      120070209G2750                FLAP SYSTEM                             GROB  120   G120A       1660208EU  LYC   O540  AEIO540D4D5      EA                                              FROZEN          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       261                                                            (CAN) THE COLD WEATHER HAS AFFECTED SEVERAL AIRCRAFT IN THE FLEET OF 9. IN -25 C OR COLDER TEMPERATURES, THE CIRCUIT BREAKERS POP AFTER LANDING WHEN THE FLAPS ARE SELECTED (TC NR 20070209022)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  ORTA49CE   1E4                  
20070516001372007051600137EA  2007       5          16         CA070209023      120070207G56106003303026      WINDSHIELD                              CNDAIRCL601 CL6013A     8070802EA                                                               COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 Z  SIGNIFICANT FAILURE REPORT                                                    CRCRUISE         1                      CA       1167                                                           (CAN) RT WINDSHIELD OUTER LAYER CRACKED DURING FLIGHT, A SINGLE CRACK LOCATED IN THE CENTER OF THE WINDSHIELD AND IS VERTICAL FROM TOP TO BOTTOM. AIRCRAFT PRESSURIZATION WAS NOT AFFECTED AND AIRCRAFT RETURNED TO BASE. (TC NR  20070209023)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F    RTA21EA                        
20070516001382007051600138EU  2007       5          16         CA070212001      120070201G2711978731813       ACTUATOR                                PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  AILERON TRIM TABINTERMITTENT    W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) AILERON TRIM INTERMITTENT. TRIM TAB ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERVICE (TC NR 20070212001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070516001392007051600139EU  2007       5          16         CA070212002      120070208G7600941941141       CONDITION LEVER                         PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  COCKPIT         STIFF           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6263                                                           (CAN) DURING INSPECTION, IT WAS FOUND THAT THE CONDITION LEVER WAS EXTREMELY HARD TO MOVE.  THE CONDITION LEVER CABLE WAS REPLACED. (TC NR 20070212002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070516001402007051600140EU  2007       5          16         CA070212003      120070207G3250                STEERING SYS                            BAG   JETSTMJETSTM3212  1500217EU                                                               NLG             UNSERVICEABLE   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA            4808                                                      (CAN) INTERNAL STEERING MECHANISM SLOPPY. A/C HARD TO CONTROL DURING TAXI. NOSE LANDING GEAR REMOVED AND REPLACED WITH OVERHAULED UNIT, GROUND TEST CARRIED OUT AND FOUND SERVICEABLE. DEFECTIVE LANDING GEAR HAS NOT BEEN SHIPPED FOR OVERHAUL AT THIS TIME. (TC NR 20070212003)                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4T    RTBA15CAA                      
20070516001412007051600141GL  2007       5          16         CA070212004      120070208G5340C2FS5487A       FITTING                                 DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HARTZLHCB3R HCB3R304    GL  FUSELAGE        CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AT SCHEDULED INSPECTION THE PORK CHOP FITTINGS WERE FOUND CORRODED. THESE C2FS5487A LT AND RT WERE BOTH REPLACED. DEPTH OF CORROSION WAS APPROX 20 PERCENT OF OVERALL PART THICKNESS. THE MANUFACTURE WAS CONTACTED AND REPORTED SEVERAL SERVICE DIFFICULTY REPORTS HAVE BEEN FILED BY OEM. (TC NR 20070212004)                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3R3  RRCA806    5E1     5  CP28EA    
20070516001422007051600142WP  2007       5          16         CA070212005      220070207G7200TPE33110UG      ENGINE                                  BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33110UG  01514WP                                              UNSERVICEABLE   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       172444760                                                      (CAN) DURING PRE FLIGHT INSPECTION FLIGHT CREW HEARD ABNORMAL NOISE COMING FROM ENGINE WHILE THEY TURNED THE PROPELLER. MAINTENANCE WAS NOTIFIED AND ENGINE WAS INSPECTED, SUSPECT REAR BEARING FAILURE, OIL SYSTEM INSPECTED AND FOUND TO HAVE NO METAL CONTAMINATION. ENGINE REMOVED AND HAS NOT YET BEEN SENT FOR REPAIR. (TC NR 20070212005)                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T4  TRTBA15CAA E4WE                 
20070516001432007051600143EU  2007       5          16         CA070212006      120070211G5210                MECHANISM                               EMB   ERJ190ERJ190100IGW3260408EU                                                               L2 DOOR         FROZEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1243                                                           (CAN) F/A ADVISED L2 DOOR FROZEN UNABLE TO OPEN VENT FLAP.  L2 DOOR THAWED OUT IN HANGAR, GVI CARRIED OUT ON DOOR, CHECKED SERVICEABLE. NOTE:  SINCE NOV 1 2006, HAVE FOUND 8 OTHER SNAGS RELATED TO E190 FROZEN DOORS.  COULD BE A CONCERN IN THE EVENT OF AN EMERGENCY SITUATION. (TC NR 20070212006)                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F    RTA57NM                        
20070516001442007051600144CE  2007       5          16         CA070212007      120070129G27301155240465      TORQUE TUBE                             BEECH 99    B99         1154004CE  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  ELEVATOR        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THE TAIL CONE WAS REMOVED FOR OTHER SCHEDULED MAINTENANCE.  IT WAS NOTICED THAT THE ELEVATOR BELLCRANK TORQUE TUBE WAS CRACKED. THE CRACK STARTED AT THE HORN ATTACH TAPER PIN AND SPIRALED AROUND THE TORQUE TUBE APPROX 270 DEGREES. THE ASSEMBLY WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE (TC 20070212007)                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20070516001452007051600145EU  2007       5          16         CA070212008      120070127G3800                LINE                                    EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF34*            NE                              WATER SYS       RUPTURED        W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) WHILE ENROUTE TO DESTINATION CREW REPORTED TO MAINTENANCE THAT AILERON CONTROL COLUMN FREEZES AND TAKES EXCESSIVE FORCE TO FREE UP, UPON INSPECTION AT DESTINATION MAINTENANCE FOUND AILERON CONTROLS COVERED IN ICE CAUSED BY A BROKEN WATER LINE.  A MAINTENANCE INVESTIGATION FOUND THAT A CLAMP HAD COME OFF FROM THE FORWARD WATER SYSTEM DRAIN PLUMBING.  (TC NR 20070212008)                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA57NM   E15NE                
20070516001462007051600146CE  2007       5          16         CA070212010      120070201G3246                BEARING                                 BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3A     NE  MAIN WHEEL      DESTROYED       W      K   NONE                                                                                            O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) WHEN THE AIRCRAFT LANDED ALL OF PASSENGERS WERE UNLOADED FOR REFUELING.  THE CAPTAIN OF THE AIRCRAFT WALKED AROUND THE RT SIDE OF THE AIRCRAFT TO TALK TO THE FUELER AND NOTICED THAT THE RT MAIN GEAR ONLY HAD ONE MAIN WHEEL ASSEMBLY ATTACHED.  HE IMMEDIATELY CONTACTED MAINTENANCE AND GROUNDED THE AIRCRAFT. UPON INSPECTION OF THE AXLE STUB IT WAS FOUND THAT THE INNER RACES OF THE BEARINGS, NUT AND SAFETY HARDWARE WAS STILL ATTACHED.  THE OTHER 3 WHEEL ASSEMBLIES WERE REMOVED AND INSPECTED FOR CONDITION AND SECURITY.  ONE OF THE 3 HAD BEEN CHANGED BY US ALREADY AND WAS FINE.  THE LAST TWO WERE FOUND TO HAVE GREASE COATED ON THE OUTSIDE OF THE BEARINGS BUT NOT (PACKED) INSIDE.   NOTE:  THE AIRCRAFT IS NEW TO 2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070516001472007051600147EA  2007       5          16         CA070213001      120070212G2750                FCU                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              TE FLAPS        MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) FLAP FAIL MESSAGE RECEIVED IN-FLIGHT. AIRCRAFT LANDED UNEVENTFUL WITH FLAPS ZERO (FLAPS WOULD NOT MOVE). (TC NR 20070213001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA21EA   E15NE                
20070516001482007051600148CE  2007       5          16         CA070213002      120070131G2910991242339       VALVE                                   CESSNA525   525         2076601CE  WILINTFJ44  FJ44        66000GL                              HYD SYSTEM      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1409                                                           (CAN) POST INSPECTION RUN REVEALED HYDRAULIC PRESSURE ON ANNUNCIATOR LIGHT DID NOT EXTINGUISH WHEN SYSTEM SHOULD HAVE BEEN AT REST. HYDAULIC LOADING VALVE FOUND FAILED.  BLEED ORIFICE RECOVERED FROM HYDRAULIC MANIFOLD UNDER RELIEF VALVE (3RD FROM LOADING VALVE). LOADING VALVE MAY HAVE FALLEN APART DURING EMERGENCY GEAR EXTENSION TEST.  LOADING VALVE REPLACED. ALL TESTS NORMAL. FAILED VALVE SENT TO MFG FOR ANALYSIS.  (TC NR 20070213002)                                                                                                                                                                                                                                                                                         1L72 4F4  FRTA1WI    E3GL                 
20070516001492007051600149NM  2007       5          16         CA070213003      120070206G249750086003        CONTACT                                 BOEING727   727223      1384074NM  PWA   JT8   JT8D15      52051NE                              GENERATOR       BURNED          W      O   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB OUT ALL 4 CB`S POPPED FOR TANK 2 FUEL BOOST PUMPS, AIRCRAFT RETURNED TO AIRPORT. DETERMINED NR 3 GENERATOR VOLTAGE FLUCTUATING, (THE PUMP FAULT WAS ATTRIBUTED TO THE POWER FLUCTUATION WHICH WAS POWERING THE (ESSENTIAL POWER) AND THE (SYNC BUSS POWERING THESE PUMPS).  INSPECTION OF NR 3 GENERATOR CB FOUND BURNED CONTACTS. CB REPLACED, CONTACTS CLEANED NO FURTHER REPORTS. (TC NR 20070213003)                                                                                                                                                                                                                                                                                                                     2L73 4F4  F  A3WE    E2EA                 
20070516001502007051600150CE  2007       5          16         CA070213005      120070213G3510510010951       LINE                                    CESSNA425   425         2076018CE  PWA   PT6   PT6A112     52043NE  MCAULY4HFR344HFR34C762  NE  CREW O2 SYS     CORRODED        W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) FOUND LT SIDE CABIN OXYGEN LINE P/N 5100109-51 CORRODED WHERE IT CROSSES THE OVERHEAD CABIN AIR DUCT P/N CM3212-2 (WL 103.10) AT FS 160.0. (TC NR 20070213005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3T3  TRTA7CE    E4EA    6  C3PNE     
20070516001512007051600151    2007       5          16         CA070213006      420070206G3444401020101       PROXIMITY SENSOR                        BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  RT MLG WOW 1    MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA       369                                                            (CAN) ON TAKEOFF CREW GOT (WT ON WHEELS) CAUTION LIGHT MOMENTARILY.  LIGHT CAME ON AGAIN IN FLIGHT, QRH ACTIONED AND RETURN TO BASE.  PSEU SHOWED THAT RT MLG WOW 1 SENSOR PROXIMITY SHOWED  (UNREASONABLY NEAR). COULD ADJUST OUT SO THAT MILLIHENERYS WERE IN SPEC BUT THE GAP WAS OUT.  REPLACED SENSOR PROXIMITY. (TC NR 20070213006)                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070613001552007061300155NM  2007       6          13         CA070213007      120070206G3230483023          SEQUENCE VALVE                          BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA                              NLG             FAILED          W      A   UNSCHED LANDING                                                                                 DJ INFLIGHT SEPARATION       WARNING INDICATION                                  CLCLIMB          1                      CA       654                                                            (CAN) NOSE LANDING GEAR DOORS WOULD NOT CLOSE ON GEAR RETRACTION. GEAR WOULD NOT EXTEND NORMALLY SO CREW DID AN ALTERNATE GEAR EXTENSION.  REPLACED VALVE,SOLENOID SEQUENCE AS WE HAD DEALT WITH THIS ISSUE A WEEK EARLIER ON ANOTHER AIRCRAFT (TC# 20070213007).                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4T4  TRTA13NM   E00062EN             
20070516001522007051600152WP  2007       5          16         CA070213008      120070204G6730D2121           SERVO                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              MAIN ROTOR      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) RT LATERAL SERVO FOUND LEAKING BY ENGINEER DURING DI.  SERVO REMOVED FOR REPAIR AND SERVICABLE UNIT INSTALLED. (TC NR 20070213008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3O3  O  H11NM   1E4                  
20070516001532007051600153EU  2007       5          16         CA070213009      120070113G6730704A44831142    SERVO                                   SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B         NE                              TAIL ROTOR      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       6258 2996                                                      (CAN) SERVO FOUND LEAKING BY ENGINEER ON POST FLIGHT INSP.  SERVO REPLACED WITH SERVICABLE UNIT.  SERVO WAS SENT OUT FOR REPAIR.  THE SERVO WAS OVERHAULED AND IS BEING SHIPPED BACK TO US FOR INSTALLATION. (TC NR 20070213009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3U3  U  H9EU    E00054EN             
20070516001542007051600154EA  2007       5          16         CA070214001      120070214G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              TE FLAPS        JAMMED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH, WHEN THE CREW SELECTED FLAP 8, THE FLAPS DID NOT MOVE AND THEY STAYED AT 0. CREW LANDED FLAPLESS WITHOUT INCIDENT. NO MORE DETAILS. INFORMATION WILL BE UPDATED AS SOON AS IS AVAILABLE.  (TC NR 20070214001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20070516001552007051600155EU  2007       5          16         CA070214002      120070207G760355CF8891        CABLE                                   UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              THROTTLE        FAILED          W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA       4461 4461                                                      (CAN) THROTTLE FROZEN IN THE FULL OPEN POSITION. FUEL FIRE WALL SHUT OFF USED TO CONTAIN ENGINE.  (TC NR 20070214002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G72 3U3  UNCR0001RD E34NE                
20070516001562007051600156SO  2007       5          16         CA070214004      220070203G85305A10204         EXHAUST VALVE                           CESSNA150   150L        2071826CE  CONT  O200  O200A       17020SO  MCAULY1A102 1A102OCM    GL  CYLINDER HEAD   BROKEN          W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      CA       1541                                                           (CAN) DURING TAKEOFF, AN ENGINE VIBRATION WAS FELT. A PRIORITY LANDING WAS REQUESTED. CYLINDER EXHAUST VALVE NR 3 FOUND BROKEN AT THE VALVE HEAD. CYLINDER SA10200, S/N AM1376 INSTALLED. OTHER VALVES INSPECTED AND REPLACED VALVES SA10204 ON CYLINDER NR 4 AND NR 2.  (TC NR 20070214004)                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  O  3A19    E252    5  NP918     
20070516001572007051600157EA  2007       5          16         CA070214005      120070212G36103035279         LINE                                    DHAV  DHC7  DHC7102     2802708EA  PWA   PT6   PT6A50      52043EA  HAMSTD24PF  24PF305     GL  PNEUMATIC SYS   BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) AFTER LANDING THE NR 1 PROP RPM WAS LOWER THAN NORMAL. MAINTENANCE FOUND THAT THE P3 LINE FROM THE P3 FILTER BOWL TO THE ENGINE WAS BROKEN PN 3035279. THE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.   (TC NR 20070214005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H74 4T4  T  A20EA   E4EA    6  CP1NE     
20070808001402007080800140CE  2007       8          8          CA070215001      120070213G3340CM358910        SWITCH                                  CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  LANDING LIGHT   SMOKE           W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA       2364                                                           (CAN) LANDING LIGHT SWITCH GAVE OFF ODOR OF SMOKE, WHEN PILOT WENT TO TURN OFF, THE SWITCH WAS HOT AND THE SHUTOFF THE SWITCH WAS REPLACED WITH A NEW UNIT (TC NR 20070215001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    1E10    5  NP857     
20070516001582007051600158WP  2007       5          16         CA070215002      220070213G7260                HOUSING         ALIDSG                  BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33110UG  01514WP  MCAULY4HFR344HFR34C652  NE  ACCESSORY DRIVE BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  P63269C                                             (CAN) ACCESSORY DRIVE HOUSING BOTTOM CASE DRAIN THREADED MOUNTING BOSS DISCOVERED BROKEN. ENGINE REMOVED AND LOANER ENGINE INSTALLED. (TC NR 20070215002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4T4  TRTBA15CAA E4WE    6  C3PNE     
20070516001592007051600159CE  2007       5          16         CA070215003      120070215G2435                SPLINE                                  BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  STARTER GEN     WORN            W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA            624   19360                                               (CAN) START ATTEMPTED ON ENGINE. STARTER/GENERATOR ROTATED BUT ENGINE DID NOT. S/G REMOVED AND INSPECTED. S/G SHAFT SPLINE NOTED AS EXTREMELY WORN. ENGINE ACCESSORY HOUSING INTERNAL SPLINE CHECKED FOR WEAR WITH WEAR CHECK TOOL. DIMENSIONS WITHIN ACCEPTABLE LIMITS. S/G REPLACED WITH NEW UNIT. (TC NR 20070215003)                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20070808001412007080800141CE  2007       8          8          CA070215004      120070210G243410300B          ALTERNATOR                              CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA  MCAULY1C160 1C160DTM    GL  ENGINE          MALFUNCTIONED   W      O   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) ON CLIMB OUT A LOW VOLTAGE LIGHT INDICATION. PILOT RECYCLED ALTERNATOR, LOW VOLTAGE INDICATION WAS NOT CORRECTED AND PILOT RETURNED FOR LANDING (TC NR 20070215004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  ONT3A12    E274    5  NP910     
20070808001422007080800142CE  2007       8          8          CA070215007      120070214G3221NAS464P4A10     BOLT                                    CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              NLG             BROKEN          W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      CA       7092                                                           (CAN) AFTER GEAR WERE RETRACTED A VIBRATION IN THE NOSE OF THE AIRCRAFT WAS NOTICED.  THE AIRCRAFT RETURNED TO BASE WITH NO INCIDENT. AN INSPECTION WAS CONDUCTED AND THE NOSE GEAR DOOR TORQUE TUBE ATTACH BOLT WAS FOUND BROKEN.  THIS BOLT ATTACHES THE TORQUE TUBE TO THE WHEEL WELL STRUCTURE AND THE TORQUE TUBE ROTATES AROUND THIS BOLT. THE TORQUE TUBE WAS INSPECTED AND REINSTALLED. (TC NR 20070215007)                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA22CE   E25EA                
20070516001602007051600160SW  2007       5          16         CA070216001      120070214G2820206040525101    HOUSING                                 BELL  206   206L4       1182110SW                                                               FUEL  SYS       DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) BYPASS INDICATOR BORE MISSING ONE 0.062 INCH DIA OIL PASSAGE AT BOTTOM OF BORE BREAKING THROUGH THE SMALLEST RECESSED BORE DIAMETER OF .375 INCH. PICTURE OF PART WITH THE MISSING HOLE ATTACHED. (TC NR 20070216001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U    NCH2SW                         
20070516001682007051600168CE  2007       5          16         CA070216002      120070214G2750100984040       MOTOR                                   BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  TE FLAP         FAILED          W      L   ABORTED APPROACH                                                                                F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) ON FINAL APPROACH, THE PILOT SELECTED FLAPS DOWN, WHEN THE FLAPS REACHED 5 DEGREES, THE ASSOCIATED CIRCUIT BREAKER POPPED. THE PILOT OVERSHOT TO EVALUATE THE SITUATION AND THEN CARRIED OUT AN UNEVENTFUL LANDING WITH 5 DEGREE OF FLAP. UPON INVESTIGATION BY MAINTENANCE, IT WAS FOUND THAT THE BEARING IN THE FLAP MOTOR HAD FAILED. THE MOTOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. AS THE FLAP MOTOR IS NOT CONTROLLED FOR HARD TIME, THE OPERATORS HAVE INDUCED A MANDATORY OVERHAUL OF THE MOTOR AND GEARBOX EVERY 5000 CYCLES. (TC NR 20070216002)                                                                                                                                                                  1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070516001692007051600169SO  2007       5          16         CA070216003      120070216G2730AN17422A        BOLT                                    PIPER PA31  PA31325     7103105SO  LYC   O540  TIO540J2BD  41532EA                              ELEVATOR        CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AT INSPECTION FOUND BOLTS (AN174-22A (6EA)) IN ELEVATOR TORQUE TUBE ASSEMBLY (40070-05) CORRODED. (TC NR 20070216003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A20SO   E14EA                
20080319001332008031900133CE  2008       3          19         CA070216004      120070209G7120829             SPACER                                  CESSNA172   172E        2072412CE  LYC   O360  IO360A1A    41514EA  HARTZLHCC2Y HCC2YR1     GL  ENGINE MOUNT    SHEARED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1000       15182                                               (CAN) A RATTLE NOISE WAS HEARD AT ENGINE START. CLOSE INSP OF THE ENGINE MOUNT ASSY REVEALED ALL 4 MOUNT SPACERS, P/N 829, HAD SHEARED THEIR ATTACHMENT RIVET HEADS. THIS AC WAS MODIFIED IN THE PAST WITH 180HP CONVERSION. DISASSEMBLY REVEALED THE USE OF VERY SOFT ALUMINUM ALLOY RIVETS TO ATTACH THE ALUMINUM SPACERS TO THE STEEL TUBE MOUNT STRUCTURE, PN 17201-1, WEAR DAMAGE PREVENTED POSITIVE VISUAL ID OF THE RIVET TYPE.  IT IS UNKNOWN IF THESE RIVETS ARE A FACTORY OR A FIELD INSTALLATION. FAILURE OF THESE RIVETS ALLOW  SPACER TO OSCILLATE LATERALLY ON THEIR MOUNTING PADS.  SUBMITTER RECOMMENDS TO EXAMINE THIS ENGINE MOUNT SPACER CLOSELY FOR SMOKING OR LOOSE RIVET HEADS AT INSP. (TC NR 20070216004)               1H71 3O3  ONT3A12    1E10    5  CP920     
20070516001702007051600170GL  2007       5          16         CA070216005      220070210G7261                OIL SYSTEM      ALLSN                   LKHEED382   382G        526414USO  ALLSN 501D  501D22A     03006GL  HAMSTD54H   54H60117    NE  NR 2 ENGINE     LOW PRESSURE    W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA            9453                                                      (CAN) IN CRUISE FLIGHT, THE CREW OBSERVED THAT THE OIL QUANTITY WAS DROPPING ON NR 2 ENGINE. AFTER VISUAL CONFIRMATION THAT OIL WAS EXITING THE OVERBOARD DRAIN, THE ENGINE WAS SHUTDOWN. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM.  MAINTENANCE REPLACED THE ENGINE SCAVENGE SYSTEM FILTER, THE ENGINE OIL COOLER, CHECKED THE ENGINE MAGNETIC DRAIN PLUGS AND REFILLED THE ENGINE WITH FRESH OIL. NO CONTAMINATION WAS OBSERVED OTHER THAN SOME CARBON IN THE SCAVENGE FILTER. THE AIRCRAFT WAS GROUND RUN AND THE RETURNED TO SERVICE. (TC NR 20070216005)                                                                                                                                                                                2H74 4T4  T  A1SO    E282    6  CP906     
20070516001712007051600171SW  2007       5          16         CA070216006      120070207G6320                GEARBOX         BELL                    BELL  427   427         1182207SW                                                               MAIN ROTOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1623       A37                                                 (CAN) FOUND A CRACK IN MAIN ROTOR TRANSMISSION, ON THE LT SIDE INPUT SHAFT. OIL STARTED TO SIP OUT OF THE TRANSMISSION. (TC NR 20070216006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U      R00001RC                     
20070530000102007053000010NE  2007       5          30         CA070216008      220070216G72305009T34P01      BLADE           GE                                                         GE    CT58  CT581401    30011NE                              COMPRESSOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            3971  258                                                 (CAN) ON INSPECTION, A STAGE 4 BLADE WAS FOUND TO HAVE A 0.080 INCH CRACK THROUGH THE DOVE TAIL AREA ON THE TRAILING EDGE SIDE.  OUR FILE NR SQID 07-00588 (TC NR 20070216008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         4  U          1E3                  
20070516001732007051600173NE  2007       5          16         CA070219001      220070216G7230                FAN BLADE                               CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              NR 2 ENGINE     BENT            W      A   UNSCHED LANDING                                                                                 C  F.O.D.                                                                        CLCLIMB          1                      CA       2520425204                         807217                      (CAN) FEB 16/07, AIR TURN BACK. THE CREW REPORTED THAT AFTER TAKEOFF A LOUD RUMBLING NOISE WAS HEARD.  CREW BELIEVED THAT ICE MAY HAVE BEEN INGESTED INTO THE RT ENGINE DURING LANDING ON THE PREVIOUS LEG INBOUND TO DESTINATION. MAINTENANCE CONFIRMED SEVERAL FAN BLADES WERE DAMAGED AT OUTER TIPS.  THE FAN BLADES WERE REMOVED AND REPLACED AND A COMPRESSOR INSPECTION WAS CARRIED OUT WITH NFF.  ENGINE RUNS WERE CARRIED OUT AND ALL PARAMETERS FOUND WITHIN LIMITS AND AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070219001)                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20070516001742007051600174EA  2007       5          16         CA070219003      120070218G2750                FLAP SYSTEM                             CNDAIRCL600 CL600*             EA                                                               TE FLAPS        JAMMED          W      L   ABORTED APPROACH                                                                                O  OTHER                                                                         APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH, CREW RECEIVED SLATS FAIL MESSAGE, ALSO, FLAPS  STOPPED AT 8 DEGREES. FLIGHT LANDED WITHOUT INCIDENT. INFORMATION WILL BE UPDATED AS SOON AS IS AVAILABLE.   (TC NR 20070219003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F    RTA21EA                        
20070516001752007051600175SW  2007       5          16         CA070219004      120070204G56102719442003      WINDSHIELD                              SWRNGNSA227 SA227AC     8780603SW                                                               COCKPIT         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA            3829                                                      (CAN) WHILE IN CRUISE FLIGHT ENROUTE, THE CAPTAINS WINDSCREEN CRACKED IN THE OUTER PANE. THE AIRCRAFT CONTINUED ON AND LANDED WITHOUT INCIDENT. THE WINDSHIELD WAS REPLACED WITH AN OVERHAULED ASSEMBLY AND THE AIRCRAFT RELEASED.   (TC 20070219004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4T    RTA8SW                         
20070516001762007051600176SW  2007       5          16         CA070219005      120070218G7120276211497       MOUNT                                   SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE33111U   01514WP                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            8945                                                      (CAN) DURING INSPECTION A CRACK WAS DISCOVERED IN THE UPPER AFT OUTBOARD WELD ASSEMBLY ON THE ENGINE MOUNT TRUSS REQUIRING REPLACEMENT OF THE MOUNT ASSEMBLY. (TC NR 20070219005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4T4  TRTA8SW    E4WE                 
20070516001772007051600177EA  2007       5          16         CA070219006      220070208G732134475523        FCU                                     BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  ENGINE          FAULTY          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) DURING GROUND RUN, RT POWER LEVER FOUND NOT CONTOLLING FCU. INSPECTED THROTLE LEVER LINKAGES AND CABLE TO FCU AND NO FAULTS FOUND. AFTER TROUBLESHOOTING WITH MFG TECH SUPPORT, SUSPECTED FAULTY FUEL CONTROL UNIT. FCU HAS BEEN REPLACED AND FAULT ELIMINATED. (TC NR 20070219006)                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070517001162007051700116EA  2007       5          17         CA070219008      120070218G5551C6TPM102228     BRACKET                                 DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  HORIZONTAL STAB LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE FLIGHT CREW WHERE CONDUCTING A GROUND RUN, MAINTENANCE ON THE GROUND NOTED THE RT ELEVATOR WAS MOVING UP AND DOWN EXCESSIVELY. UPON INVESTIGATION, MAINTENANCE FOUND BRACKET P/N C6TPM1022-28 WITH RIVETS WORKING AND SEVERAL WHERE ACTUALLY MISSING. THIS BRACKET IS THE PART OF THE ELEVATOR HINGE THAT IS RIVETED TO THE HORIZONTAL STABILIZER. ALL MISSING, LOOSE OR DAMAGED FASTNERS WHERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THE COMPANY HAS ISSUED A FLEET INSPECTION OF ALL OTHER TWIN OTTERS. (TC NR 20070219008)                                                                                                                                                                                              1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070530000112007053000011EA  2007       5          30         CA070219009      120070216G2750                FLAP SYSTEM                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                                              FAILED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       1758913354                                                     (CAN) DURING APPROACH WHEN FLAP SELECTED TO 8 DEG, CREW RECEIVED (FLAP FAIL) CAUTION MESSAGE ON EICAS, CONTROL POSITION DISPLAY SHOWED 2DEG ON LT FLAP AND 0 DEG ON RT FLAP. ZERO DEG FLAP LANDING CARRIED OUT.  AFTER LANDING CREW PERFORMED VISUAL INSPECTION OF THE FLAPS AND NOTED THAT LT FLAPS APPEARED TO BE AT 2 DEG AND RT FLAP LOOKED LIKE 2 DEG ON THE IB AND 0 DEG ON THE OB. FLAP CIRCUIT BREAKER RESET PROCEDURE CARRIED OUT. FLAPS FUNCTION CHECKED NORMAL. AIRCRAFT POSITIONED TO MAINTENANCE BASE. MAINTENANCE FOUND NO OBVIOUS FAULTS. ALL FLAP ACTUATORS REPLACED WITH REPLACEMENT UNITS, ALL FLAP DRIVE CABLES REMOVED AND INSPECTED AND RE-LUBRICATED. BOTH BPSU`S (FLAP BRAKE AND POSITION SENSOR UNITS) REPLACED. MAINTEN2L72 4F4  FRTA21EA   E15NE                
20070517001172007051700117EU  2007       5          17         CA070219010      120070219G5497                WIRE                                    BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33112UHR      WP  ROTOL R333  R333482F12  GL  NR 2 NACELLE    DAMAGED         W      A   UNSCHED LANDING                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) CREW REPORTED THAT THE AIRCRAFT NR 2 ENGINE STARTED TO SURGE AND THE TORQUE INDICATION FLUCTUATED BETWEEN 0-120 PERCENT. TTL AND SRL COMPUTERS TURNED OFF AND ENGINE SURGE STABILIZED AND CONTINUED TO RUN NORMALLY. INDICATION CONTINUED TO FLUCTUATE. TROUBLESHOOTING INDICATED DAMAGED WIRING IN THE NR 2 ENGINE COMPARTMENT. WIRING REPAIRED. INDICATION CALIBRATED AND NO FURTHER FAULTS FOUND. (TC NR 20070219010)                                                                                                                                                                                                                                                                                                                  2L72 4T4  TRTBA15CAA E4WE    6  CP61GL    
20070517001182007051700118    2007       5          17         CA070219011      420070217G2397M2430823F       CONNECTOR                               CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              P1RU            CORRODED        W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       5121 5121                                                      (CAN) CREW REPORTED PASSENGER ADDRESS CIRCUIT BREAKER 1Q5 POPPED , NON PA/CHIMES/CALL FUNCTION. MAINTENANCE INSPECTION FOUND STOWED CONNECTOR P1RU CORRODED AND SHORTING , CONNECTOR IS FOR AFT CABIN PA HANDSET ( NOT INSTALLED ON THIS TAIL) , CONNECTOR HAD BEEN BAGGED AND STOWED ABOVE CEILING PANEL. MAINTENANCE REMOVED CONNECTOR AND HEAT SHRUNK AND STOWED WIRING IAW AMM 20-17-10 . (TC NR 20070219011)                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20080319001342008031900134SW  2008       3          19         CA070220001      120070215G2913297037          SPLINE          VICKERS                 SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE33111U   01514WP  MCAULY4HFR344HFR34C652  NE  HYD PUMP        STRIPPED        W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA                  MX433286C                                           (CAN) LT HYD LIGHT ILLUMINATED BEFORE LANDING. THE DRIVE SPLINE ON THE PUMP WAS FOUND TO BE STRIPPED. IT IS MADE OF SOFTER MATERIAL AND MADE TO WEAR INSTEAD OF THE ENGINE. PUMP ASSY WAS REPLACED AND AC RETURNED TO SERVICE. THIS IS THE 3RD SPLINE REPLACED. ONE IN OCT- 06, ONE IN DC-06 AND NOW THIS ONE FEB-07. (TC NR 20070220001)                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4T4  TRTA8SW    E4WE    6  C3PNE     
20070517001192007051700119EA  2007       5          17         CA070220002      220070212G7200                ENGINE                                  BEECH 99    99          1154002CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  RIGHT           MAKING METAL    W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA            285                           40812100                    (CAN) CREW CALLED IN ON LANDING TO INFORM MAINTENANCE THAT THE RT CHIP LIGHT HAD ILLUMINATED.  MAINTENANCE FOUND ENGINE HAD METAL IN OIL.  ENGINE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.  THIS ENGINE WILL REQUIRE FURTHER INVESTIGATION AS TO THE CAUSE OF THE MIO.  IT IS A LOW TIME POWER SECTION THAT IS ON IT`S SECOND MIO.  THE FIRST TIME WAS 183 HOURS AND 341 CYCLES (TC NR 20070220002)                                                                                                                                                                                                                                                                                                                                       1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20070517001202007051700120WP  2007       5          17         CA070220003      120070218G6510C04111          BEARING         ROBSIN                  ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              DRIVESHAFT      DEFECTIVE       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       85         1062                                                (CAN) DAMPER HANGAR BEARING INNER RACE ROTATED ON DRIVESHAFT ASSY.  BEARING REPLACED ON DRIVE SHAFT ASSY WITH SERVICABLE UNIT. (TC NR 20070220003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1G71 3O3  O  H11NM   E295                 
20070517001212007051700121NE  2007       5          17         CA070220004      220070213G7200                ENGINE                                  AIRBUSA319  A319112     3930323EU  CFMINTCFM56 CFM565A1         NE                                              UNKNOWN         W      A   UNSCHED LANDING                                                                                 Y  ENGINE STOPPAGE                                                               CRCRUISE         1                      CA                                          731587                      (CAN) EARLY INVESTIGATIONS POINT TO A NR 4 BEARING FAILURE, AT THIS TIME THE ENGINE HAS NOT BEEN DISSASSEMBLED FOR CONFIRMATION OF FAILURE, PRESENTLY ENROUTE TO SHOP. (TC NR 20070220004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA28NM   E29NE                
20070517001222007051700122NM  2007       5          17         CA070220005      120070216G3230483023          SEQUENCE VALVE                          BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NLG             MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA       8173                                                           (CAN) ON GEAR EXTENSION GOT 3 GREEN AND DOOR AMBER.  TROUBLESHOOTING POINTED TO THE NOSE VALVE SOLENOID SEQUENCE.  VALVE REPLACED. (TC NR 20070220005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080319001352008031900135NE  2008       3          19         CA070220006      220070216G723031B525501       ACTUATOR                                GULSTM200   200         4500308NM  PWC   PW306 PW306A      52165NE                              IGV             LEAKING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA       525                                PCECC02423                  (CAN) AC PERFORMED NORMALLY FOR THE TAKEOFF AND INITIAL CLIMB TO 5000 FEET. APPROX (2) MINUTES INTO THE FLIGHT AFTER CLEARANCE TO 17000 FT WITH CLIMB PWR REAPPLIED TO COMMENCE THE CLIMB, THE RT ENG EXPERIENCED A COMPRESSOR STALL. AFTER (2) OR (3) SURGES THE ENGINE ROLLED BACK TO AROUND 50 PERCENT, N1 WITH FLUCTUATING RPM AND ITT. ROLLBACK WAS FOLLOWED BY A FADEC MAJOR FAIL FAULT LIGHT. THE PILOT REDUCED POWER ON THE RT ENGINE AND THE N1 STABILIZED AT FLIGHT IDLE. CHECKLIST WAS CALLED FOR AND THE RT ENG WAS SHUTDOWN IAW MFG CHECKLIST. FUEL DUMP WAS COMPLETED WITH CLEARANCE FROM THE DEPARTURE CONTROLLER AND THE AC WAS REDUCED TO LANDING WEIGHT AND RETURNED FOR LANDING AT AIRPORT WITH NO FURTHER INCIDENT.   THE AC2L72 4F4  FRTA53NM   E35NE                
20070517001232007051700123CE  2007       5          17         CA070220007      120070219G3233                SHAFT                                   BEECH 76    76          1153005CE  LYC   O360  LO360A1G6   41514EA  HARTZLHCM2Y HCM2YR      GL  MLG ACTUATOR    FRACTURED       W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            DEDESCENT        1                      CA       1329 1329                                                      (CAN) MAIN LANDING GEAR ACTUATOR SHAFT FRACTURED AT LAST THREAD FARTHEST FROM ROD END BEARING JAM NUT. SHAFT BENT SLIGHTLY THROUGHOUT ITS FULL LENGTH WITH AN APPROXIMATELY 40 DEGREE BEND AT FRACTURE POINT. (TC NR 20070220007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 3O3  O  A29CE   1E10    5  CP43GL    
20070517001242007051700124EA  2007       5          17         CA070221001      120070219G2720600902461       BUSHING                                 CNDAIRCL601 CL6012A12   1900303EA  GE    CF34  CF348E5A1   30015NE                              RUDDER          FAILED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA       7326 7326                                                      (CAN) DURING FLIGHT THE CO-PILOTS RUDDER PEDAL ADJUSTMENT MECHANISM FAILED ALLOWING THE RUDDER PEDALS TO FALL FORWARD TO THE LIMIT OF THEIR TRAVEL. INSPECTION REVEALED THAT THE THREADED BUSHING IN THE ADJUSTMENT MECHANISM HAD FAILED ALLOWING THE SYSTEM TO DICONNECT. NOTE: RUDDER CONTROL WAS STILL AVAILIBLE THOUGH RUDDER PEDAL POSITION ADJUSTMENT WAS NOT. (TC NR 20070221001)                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA21AE   E00063EN             
20070517001252007051700125EA  2007       5          17         CA070221002      120070218G27827663854         ACTUATOR                                CNDAIRCL600 CL600*             EA                                                               SLATS           FAILED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) SLAT FAIL MESSAGE, UNABLE TO MOVE SLATS AND FLAPS ONLY MOVED TO 8 DEGREES. MDC CODE B1-007772 INDICATES JAMMED SLAT ACTUATOR AND AIRCRAFT REMOVED FROM SERVICE FOR INVESTIGATION. BOTH LEFT HAND OUTBOARD ACTUATORS NR 5 AND NR 6 REPLACED AND TEST COMPLETED SUCCESSFULLY. WILL ASK FOR STRIP REPORTS FROM MANUFACTURER. INFORMATION WILL BE UPDATED AS SOON AS IS AVAILABLE. (TC NR 20070221002)                                                                                                                                                                                                                                                                                                                                        2L72 4F    RTA21EA                        
20070517001262007051700126CE  2007       5          17         CA070221003      120070205G25601101983         BUCKLE          PACIFICSCIEN            BEECH 90    C90A        1152911CE  PWA   PT6   PT6A21      52043EA  HARTZLHCB3T HCB3TN3     GL  SEAT BELT       MALFUNCTIONED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) COMPLIED WITH COMPANY CAMPAIGN NOTICE 010-25-10-011 NM-06-29.  THE CREW SEATBELT ROTARY LATCH CAN BE CONTACTED WITH THE CONTROL YOKE WITH THE SEAT FULL FORWARD AND THE YOKE FULL AFT. IT IS POSSIBLE TO UNLATCH THE SEATBELT BY ROTATING THE YOKE AND MAKING CONTACT WITH THE BUCKLE. THE FUNCTION TEST WAS CARRIED OUT IAW THE INSTRUCTIONS GIVEN IN NM-06-29.  (TC NR 20070221003)                                                                                                                                                                                                                                                                                                                                                     1L72 3T4  TRT3A20    E4EA    6  CP15EA    
20070517001272007051700127CE  2007       5          17         CA070221004      120070210G25601101983         BUCKLE          PACIFICSCIEN            BEECH 90    C90A        1152911CE  PWA   PT6   PT6A21      52043EA  HARTZLHCB3T HCB3TN3     GL  SEAT BELT       DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) COMPLIED WITH COMPANY CAMPAIGN NOTICE 010-25-10-011, NM-06-29.  THE CREW SEATBELT ROTARY LATCH CAN BE CONTACTED WITH THE CONTROL YOKE WITH THE SEAT FULL FORWARD AND THE YOKE FULL AFT. IT IS POSSIBLE TO UNLATCH THE SEATBELT BY ROTATING THE YOKE AND MAKING CONTACT WITH THE BUCKLE. THE FUNCTION TEST WAS CARRIED OUT IAW THE INSTRUCTIONS GIVEN IN NM-06-29.  (TC NR 20070221004)                                                                                                                                                                                                                                                                                                                                                    1L72 3T4  TRT3A20    E4EA    6  CP15EA    
20070808001432007080800143CE  2007       8          8          CA070221005      120070206G2560                BUCKLE                                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              SEATBELT        MALFUNCTIONED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) COMPLIED WITH COMPANY CAMPAIGN NOTICE 010-25-10-011/SAIB NM-06-29.  THE CREW SEATBELT ROTARY LATCH CAN BE CONTACTED WITH THE CONTROL YOKE LET DOWN HOLDER WITH THE SEAT FULL FORWARD AND THE YOKE FULL AFT. IT IS POSSIBLE TO UNLATCH THE SEATBELT BY ROTATING THE YOKE AND MAKING CONTACT WITH THE BUCKLE. THE FUNCTION TEST WAS CARRIED OUT IAW THE INSTRUCTIONS GIVEN IN SAIB NM-06-29.   (TC NR 20070221005)                                                                                                                                                                                                                                                                                                                          1L72 4F4  F  A22CE   E1NE                 
20070517001282007051700128NE  2007       5          17         CA070221006      120070213G32304546A           MOTOR                                   SKRSKYS61   S61N        8142104NE  GE    CT58  CT581402    30011NE                              LANDING GEAR    INOPERATIVE     W      O   OTHER                                                                                           J  WARNING INDICATION                                                            DEDESCENT        1                      CA       106181192  A019                                                (CAN) ON PRELANDING CHECK, MAIN LANGDNG GEAR FAILED TO EXTEND. EMERGENCY BLOW DOWN PROCEDURE WAS FOLLOWED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INVESTIGATION  DETERMINED THAT THE ELECTRIC MOTOR THAT DRIVES THE MLG HYDRAULIC PUMP HAD FAILED AND TRIPPED THE CIRCUIT BREAKER. (TC NR 20070221006)                                                                                                                                                                                                                                                                                                                                                                                                                                    2G72 4U4  U  1H15    1E3                  
20070517001292007051700129NM  2007       5          17         CA070221007      120070220G213314C3308         COUPLER         HYDROFLOW               BOEING737   737*               NM                                                               FS 967 S23R     LEAKING         W      A   UNSCHED LANDING                                                                                 KG FLUID LOSS                MULTIPLE FAILURE                                    CRCRUISE         1                      CA                                                                      (CAN) ALMOST AN HOUR INTO THE FIRST FLIGHT OF THE DAY, AIRCRAFT EXPERIENCED AUTOMATIC PRESSURIZATION FAULT WITH (AUTO-FAIL) LIGHT ON (WITH BOTH CPC`S FAIL). CREW RESORT TO MANUAL PRESSURIZATION CONTROL. AIRCRAFT ADVISED TO DIVERT TO MAIN BASE FOR RECTIFICATION.  UPON INVESTIGATION THE AFT OUT FLOW VALVE FOUND BLOCKED WITH ICE AND WATER SYSTEM QUANTITY LOW.  THIS WAS THE SECOND SIMILAR INCIDENT ON THIS AIRCRAFT.  FURTHER INVESTIGATION REVEALED WATER LEAKING FROM THE COUPLING (SIMILAR TO COUPLING) AT THE FITTING RT ABOVE THE AFT OUTFLOW VALVE. (SIMILAR TO PREVIOUS FINDING).  FITTING/LINES RE-ALIGNED TO RELIEVE POSSIBLE STRESS ON COUPLING. COUPLING TIGHTENED AND RESECURED WITH NEW PACKING. NO FURTHER LEAKS AND AIR2L72 4F    RTA16WE                        
20070517001312007051700131EA  2007       5          17         CA070222001      120070212G789722858222801     WIRE HARNESS                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              NR 1 ENGINE     CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2269622696                                                     (CAN) DURING ROUTINE MAINTENANCE INSPECTION , FOUND WIRING HARNESS ON NR1 ENGINE FOR THRUST REVERSER STOW SWITCH WIRING CHAFING ON EDGE OF LIGHTENING HOLE OF MOUNTING BRACKET. DAMAGED WIRING CUT OFF AND END RE-TERMINATED. MFG ILLUSTRATED PARTS CATALOG (CSP A-006) 78-37-01 FIG 1A PG 0 , ITEM 40 (BRACKET ASSY, STOW SWITCH MOUNTING). LIGHTNING HOLE ON THIS BRACKET CHAFED ON HARNESS FOR STOW SWITCH  (TC NR 20070222001)                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA21EA   E15NE                
20070517001322007051700132EA  2007       5          17         CA070222002      120070212G57306001201687S     SKIN                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              LT WING         DENTED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2595525955                                                     (CAN) CREW REPORTED BIRDSTRIKE ON APPROACH, MAINTENANCE INSPECTION FOUND DENT IN LT WING LEADING EDGE APPROX 6 FT OB FROM FUSELAGE. DENT ALLOWABLE IAW SRM LIMITS. (TC NR 20070222002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20070808001442007080800144CE  2007       8          8          CA070222003      120070222G551407321014        BRACKET                                 CESSNA185   A185E       2072818CE  CONT  O520  IO520D      17032SO  MCAULY2A34C D2A34C58    GL  HORIZONTAL STAB CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2383                                                           (CAN) HORIZONTAL STABILIZERS REMOVED FOR REPAIR.  AFT ATTACHMENT POINT REINFORCEMENT BRACKETS PN 0732101-4 REPLACED WITH NEW.  ADJACENT RIVETS REPLACED.  TAIL RE-ASSEMBLED.  DUAL INSPECTED. (TC NR 20070222003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  O  3A24    E5CE    5  CP3EA     
20070517001332007051700133NE  2007       5          17         CA070222004      220070219G720070BM031090      MODULE                                  SNIAS 350   AS350BA     8680817EU  TMECA ARRIELARRIEL1B    6OO30NE                              ENGINE          MALFUNCTIONED   W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) POSSIBLE T1 OR T2 MO3 TURBINE RUB. REMOVED MO3 AND SEND TO MFG FOR INVESTIGATION. THE TURBINE RUB WAS NOTICED AFTER SHUTDOWN OF THE ENGINE. (TC NR 20070222004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3U3  UNCH9EU    E19EU                
20070808001452007080800145CE  2007       8          8          CA070223001      120070220G21306621000000037   CHECK VALVE                             LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE731*     01518WP                              CABIN PRESSURE  BROKEN          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       2491                                                           (CAN) SHORTLY AFTER TAKEOFF, DURING INITIAL CLIMBOUT, THE CREW NOTICED THAT THE CABIN ALTITUDE RATE OF CLIMB INDICATOR SHOWED 600FT/MIN CLIMB.  USUALLY, THE CONTROLLER IS SET TO 400FT/MIN.  THEY CONTINUED TO CLIMB AND TO MONITOR THE PRESSURIZATION SYSTEM. A FEW MOMENTS LATER, THE INDICATOR SHOWED A 1500-2000FT/MIN CLIMB.  THE CABIN ALTITUDE FOLLOWED THE AIRPLANE ALTITUDE.  THE AIRPLANE WAS NOT PRESSURIZING THE CABIN. THE CREW CARRIED OUT THE APPROPRIATE CHECKLIST AND DECIDED TO DIVERT TO THEIR ALTERNATE AIRPORT.  MEANWHILE, NO WARNING OR CAUTION INDICATIONS/MESSAGES APPEARED ON EICAS AND THE CREW COULD NOW SMELL KIND OF ODOR OF A OVERHEATED DUCT.  THEY NOTICED ALSO THAT NO HEATED/CONDITIONED AIR WAS COMING FROM2L72 4F4  FRTT00008WIE6WE                 
20070530000122007053000012CE  2007       5          30         CA070223002      120070220G77978975294         WIRE HARNESS                            BEECH 100   100BEECH    1152916CE  GARRTTTPE331TPE3316252B 01514WP  HARTZLHCB4T HCB4TN5     GL  ENGINE ITT      FAILED          W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 TXTAXI/GRND HDL  1                      CA            495                           P27035                      (CAN) FLIGHT CREW DID ATTEMPTED AN ENGINE START NR 2 ENGINE WITH NO SUCCESS. AFTER MAINTENANCE HAD CORRECTED THE PROBLEM ASSOCIATED WITH THE FAILED START, THE CREW PROCEEDED TO CARRY OUT ANOTHER ENGINE START. ONCE THE ENGINE LIT OFF THE CREW NOTED THAT THE ITT WAS CLIMBING RAPIDLY TOWARDS THE RED BUT THEN WOULD DROP AND RISE AGAIN. THEY DECIDED TO CONTINUE WITH THE START. ONCE THE ENGINE HAD SETTLED AT IDLE, THE ITT BEGAN TO FLUCTUATE AND SLOWLY CLIMB TO THE REDLINE. THE CREW DECIDED AT THIS TIME TO SHUTDOWN THE ENGINE.  MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THAT THE ITT HARNESS WAS U/S. DUE TO THE FACT THAT THEY COULD NOT SPECIFICALLY STATE THAT THE PROBLEM WAS THE HARNESS AND NOT THAT THE HARNESS AND T1L72 3T4  T  A14CE   E2WE    6  CP40EA    
20070530000132007053000013EA  2007       5          30         CA070223003      220070221G8520UNK             SEAL                                    PIPER PA31  PA31350     7103110SO  LYC   O540  LTIO540J2BD 41533EA  MCAULY3DF36CB3DF36C526  GL  CRANKSHAFT      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       7000 1365                          L327861A                    (CAN) DURING A NORMAL WALK AROUND, OIL WAS OBSERVED ON THE COWLING. AN INVESTIGATION INTO THE OIL LEAK REVEALED THE CRANKSHAFT SEAL WAS BLOWN OUT. THE OIL SUMPS WERE DRAINED AND OIL FILTER CHECKED AND FOUND TO CONTAIN LARGE QUANTITIES OF METAL FILINGS. THE ENGINE WAS REMOVED FOR TEARDOWN REPORT AND OVERHAULED ENGINE INSTALLED. (TC NR 20070223003)                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  A20SO   E14EA   5  C         
20070517001602007051700160EA  2007       5          17         CA070223004      120070222G5330                SKIN                                    DHAV  DHC6  DHC6100     2802610EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  FUSELAGE        CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       35713                                                          (CAN) AIRCRAFT IS IN THE PROCESS OF GOING THROUGH ITS (5) YEAR CORROSION INSPECTION. DURING INSPECTION, SEVERAL AREAS OF CORROSION WERE NOTED IN AREAS WHERE CORROSION IS USUALLY NOT FOUND. THE HORIZONTAL STAB LOWER SKIN (CENTER) WAS CORRODED AROUND SOME ANCHOR NUTS (FOR THE FAIRINGS), THE SUPPORT BRACKET FOR THE LOWER RUDDER ATTACH POINT, AND AROUND ALL THE PASSENGER WINDOW FRAMES (WHERE SPOT WELDS ARE). THE SUPPORT BRACKET IS BEING REPLACED AND WE ARE WAITING FOR RD`S FROM VIKING FOR THE OTHER AREAS. (TC NR741 20070223004)                                                                                                                                                                                               1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070517001612007051700161SW  2007       5          17         CA070223005      120070220G6510204040608001    SPRING          BELL                    BELL  212   212         1181420SW  PWA   PT6T  PT6T3       52045EA                              TAIL ROTOR      BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  A512                                                (CAN) ENGINEER CARRYING OUT REQUIREMENTS OF CAMP CODE NR 650121 (INSPECT/LUBE T/R DRIVESHAFT FLEX COUPLING).  WHEN DISASSEMBLING THE T/R QUILL OUTPUT COUPLING IN SITU ON THE M/R TRANSMISSION.  UPON REMOVAL OF RETAINER AND PLATE, A SMALL SECTION OF SPRING PN 204-040-608-001 FELL INTO THE HAND OF THE ENGINEER.  REMAINDER OF SPRING WAS IN CORRECT POSITION.  FURTHER DISASSEMBLY OF COUPLING REVEALED DAMAGE TO COUPLING P/N 204-040-603-009.  NEW SPRING P/N 204-040-608-001 AND SERVICEABLE COUPLING P/N 204-040-603-009 S/N A12-42482 INSTALLED.  COMPLETE COUPLING ASSEMBLY LUBED AND REASSEMBLED IAW CHAPTER 65 OF MM, AND REASSEMBLED ONTO THE M/R TRANSMISSION. (TC NR 20070223005)                                              1G71 4U4  U  H4SW    E22EA                
20070517001622007051700162SW  2007       5          17         CA070223007      120070222G6210206010200133    BLADE                                   BELL  206   206B        1181511SW                                                               MAIN ROTOR      DENTED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       3224                                                           (CAN) WHILE IN HANGAR, METAL PIECE OUT OF HANGAR OVERHEAD HEATER FELL ON M/R BLADE AND DENTED THE BLADE. BLADE WAS REMOVED AND SENT FOR INSPECTION. HANGAR STAFF AND MANAGER WERE NOTIFIED AND REQUESTED TO INSPECT ALL OVERHEAD ACCESSORIES INCLUDING HEATERS FOR LOOSE OBJECTS.  (TC NR 20070223007)                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3U      H2SW                         
20070808001462007080800146CE  2007       8          8          CA070223008      120070214G32450923150         TUBE                                    CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  SNSNCH72C   72CK        EA  MAIN TIRE       FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA       1000                                                           (CAN) THE PILOT REPORTED A FLAT TIRE ON THE RUNWAY.  MAINTENANCE REMOVED THE AIRCRAFT FROM THE RUNWAY. FOUND NO DAMAGE TO THE TIRE, THE TUBE WAS FOUND SPLIT IN TWO PLACES AROUND THE OUTER CIRCUMFERENCE.  PART HAD BEEN INSTALLED APPROX 1000 HOURS AND APPROX 15 MONTHS.  REPLACED THE TUBE AND TIRE AND RETURNED TO SERVICE. (TC NR 20070223008)                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A19    E223    5  NP9045    
20070530000172007053000017EA  2007       5          30         CA070225001      120070212G56101393215         WINDSHIELD                              CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              COCKPIT         BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA       10130                                                          (CAN) INNER CORE OF CAPTAINS WINDSHIELD SHATTERED AT FL 330. MX REPLACED CAPTAINS WINSHIELD IAW 56-11-01. (TC NR 20070225001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA21EA   E15NE                
20070530000202007053000020    2007       5          30         CA070226001      420070221G3497                CONNECTOR       HONEYWELL               BOEING757   757236      1384971NM  RROYCERB211 RB211535E43754555NE                              DRIVE UNIT      BURNED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  4531                                                (CAN) CREW REPORTED EICAS STATUS MESSAGE, WXR SYSTEM. ON REPLACEMENT OF WXR DRIVE UNIT, FOUND BURNED ELECTRICAL CONNECTORS. (TC NR 20070226001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA2NM    E12EU                
20070530000212007053000021NM  2007       5          30         CA070226002      120070223G56105717623133      WINDSCREEN                              BOEING737   737522      138449FNM  CFMINTCFM56 CFM563C     13802EU                              COCKPIT         BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) CAPTAIN`S NR 2 WINDOW OUTER LAYER SHATTERED IN FLIGHT. WINDOW WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. REPORTED AS AN SDR DUE TO A SUSPECTED RELIABILITY ISSUE WITH SUBJECT WINDOWS. (TC NR 20070226002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA16WE   E21EU                
20070530000242007053000024CE  2007       5          30         CA070226005      120070208G52101014300327      PLATE                                   BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  DOOR            FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1328 1328                                                      (CAN) DISCOVERED DOOR MAKING NOISE WHEN RAISING OR LOWERING DOOR. INVESTIGATED FOR LOOSE HARDWARE INSIDE DOOR AND DETERMINED PIN AND ROLLER ASSY MIGRATED OUT OF LOWER AFT LATCH ASSY. THE DEFECTIVE PART IN QUESTION IS THE PLATE P/N 101-430032-7. THE PLATE IS THE FIXTURE FOR A PIN P/N 101-430032-9 AND ROLLER P/N 50-430037-7. THESE PARTS (PIN/ROLLER)ARE CONTAINED IN THE PLATE BY MEANS OF STAKING WAS NOT PROPERLY SET WHEN MFG CAUSING THE PIN MIGRATING OUT OF THE PLATE. ALL OTHER PLATES WERE INSPECTED TO ENSURE EACH PLATE`S SECURITY. THESE PLATES/LATCHES ARE CRUCIAL TO THE STRUCTURAL INTEGRITY OF THE DOOR AND FUSELAGE FRAME UNDER PRESSURIZATION LOADS. IPI REFERENCE 52-10-00 PG.16 ITEM 280, 285, 290 ILLUSTRATION SHEE2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070530000252007053000025SO  2007       5          30         CA070226006      220070219G8520626608          CAMSHAFT                                CESSNA150   150H        2071818CE  CONT  O200  O200A       17020SO  MCAULY1A101 1A101DCM    GL  ENGINE          WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1294                                                      (CAN) EXCESSIVE WEAR ON NR 1 AND NR 2 INTAKE LOBE.  CAUSED EXCESSIVE PITTING ON ALL LIFTER BODY ASSEMBLIES. (TC NR 20070226006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3O3  O  3A19    E252    5  NP918     
20070530000272007053000027EA  2007       5          30         CA070226008      120070226G57112151003268      SPAR CAP                                CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 CWASP       52016NE  HAMSTD43D   43D50       NE  RT WING         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4124                                                           (CAN) WHILE PERFORMING AD CF92-26R1, A CRACK WAS DETECTED ON THE RT REAR LOWER SPAR CAP JUST OB OF RBL 51.00.  WORK COMMENCED ON REPAIR IAW THE MFG SPEC. UPON REMOVAL OF REINFORCING STRIP (P/N 215-10032-76) AN ADDITIONAL CRACK WAS FOUND ON THE LOWER SPAR CAP AT RBL 49.50. FOLLOWING REMOVAL OF THE DAMAGED SPAR CAP AN ADDITIONAL CRACK WAS NOTICED ON THE WING SPAR WEB (P/N 215-10032-242) AT RBL 50.00 THAT EXTENDED FROM THE SECOND LOWER, WING TO FUSELAGE PICK UP ANGLE FASTENER HOLE THROUGH TO THE LOWER FASTENER HOLE AND OUT THE EDGE OF THE WEB. THESE CRACKS ARE BOTH LOCATED OUTSIDE OF THE DESIGNATED INSPECTION AREA. (TC NR 20070226008)                                                                                 2H72 4R3  RRTA14EA   ATC14   6  CP8879    
20070530000282007053000028EU  2007       5          30         CA070226009      120070131G5310350A3821003     CROSSBEAM                               SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1        NE                              FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            373                                                       (CAN) IAW THE AD 96-156-071 (B) R1 VISUAL INSPECTION EVERY 30 HOURS OR 150 LANDINGS. THE CRACKS WERE FOUND ON THE VISUAL. (TC NR 20070226009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H9EU    E19EU                
20070530000292007053000029CE  2007       5          30         CA070226010      120070225G3297                CONNECTOR                               BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  MLG             LOOSE           W      O   OTHER                                                                                           N  FALSE WARNING                                                                 APAPPROACH       1                      CA                                                                      (CAN) CREW REPORTED THAT THE GEAR INDICATION WOULD NOT INDICATE DOWN AND LOCKED ON APPROACH.   MAINTENANCE PERSONNEL LATER CARRIED OUT AIRCRAFT LANDING GEAR SWINGS AND FOUND RT SQUAT SWITCH CONNECTOR PLUG LOOSE ON BULKHEAD. CLEANED, SECURED AND GEAR SWINGS FUNCTION CHECKS CARRIED OUT.  NO FAULTS FOUND (TC NR 20070226010)                                                                                                                                                                                                                                                                                                                                                                                                              1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070530000302007053000030WP  2007       5          30         CA070226011      120070224G6310C1664           RETAINER        ROBSIN                  ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              CLUTCH          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       895        2043                                                (CAN) CRACKS AT OUTER RING BOLT HOLES. CLUTCH ASSY REMOVED AND IS BEING SENT TO MFG FOR WARRANTY. (TC NR 20070226011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3O3  O  H11NM   1E4                  
20080219001412008021900141SW  2008       2          19         CA070227001      120070222G6220204011121121    GRIP                                    BELL  212   212         1181420SW                                                               MAIN ROTOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) M/R GRIP TANG FOUND CRACK. COMPONENT ACCUMULATE 111 HRS SINCE LAST 150HRS NDT INSPECTION. (TC NR 20070227001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 4U      H4SW                         
20070530000312007053000031    2007       5          30         CA070227002      420070225G344220414440406     DRIVE UNIT                              BOEING757   757236      1384971NM  RROYCERB211 RB211535E4  54555NE                              WX RADAR ANTENNABURNED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) WXR RADAR DRIVE UNIT FOUND WITH TERMINAL 15 AND 16 BURNED (TC NR 20070227002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA2NM    E12EU                
20070530000322007053000032NE  2007       5          30         CA070227003      220070215G7210                GEARBOX                                 PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  REDUCTION       MAKING METAL    W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA                                          PCEPR0089                   (CAN) SHORTLY AFTER TAKEOFF THE ENGINE CHIP LIGHT ILLUMINATED. THE PILOT RETURNED TO BASE. THE REDUCTION GEARBOX CHIP DETECTOR WAS INSPECTED AND A FERROUS METAL FLAKE WAS FOUND ON THE DETECTOR, NO CONTAMINATION WAS FOUND IN ANY SCREENS OR THE MAIN OIL FILTER. THE ENGINE WAS RETURNED TO SERVICE AFTER COMPLETING THE MAINTENANCE REQUIREMENTS SPECIFIED IN MM CH. 79-20-02. AFTER 10 HRS OF OPERATION THE OIL FILTER WAS PULLED AND NO CONTAMINATION WAS FOUND. THE ENGINE HAS ACCUMULATED 101 HRS SINCE THE INCIDENT WITH NO FURTHER PROBLEMS. THE POWER SECTION NOW HAS 8788.3 TSN AND 652.9 TSO. (TC NR 20070227003)                                                                                                                  1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070530000332007053000033EA  2007       5          30         CA070227004      220070221G8550                TRANSFER TUBE                           BBAVIA8     8GCBC       1220803SW  LYC   O360  O360C2E     41514EA  MCAULY1A200 1A200*      GL  OIL SYSTEM      LOOSE           W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) CRANKSHAFT FWD CAVITY OIL TRANSFER TUBE LOOSE LATERALLY AND ROTATIONALLY. CRANKSHAFT WAS REPAIRED APPROX 500 HOURS AGO.   (TC NR 20070227004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  O  A21CE   E286    5  NP874     
20070808001472007080800147EU  2007       8          8          CA070227006      120070222G3234GH115TAREVE     HANDLE                                  GROB  120   G120A       1660208EU  LYC   O540  AEIO540D4D5      EA  HARTZLHCC3Y HCC3Y*      GL  LANDING GEAR    FAILED          W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CRCRUISE         1                      CA            97                                                        (CAN) LANDING GEAR HANDLE FAILED TO GIVE GEAR POSITION LIGHT AND IN-TRANSIT LIGHT INDICATIONS DURING A TRAINING MISSION. THE PILOT ELECTED TO FLY BY THE TOWER FOR ALL GEAR IN EXTENDED POSITION CONFIRMATION BEFORE AN UNEVENTFUL LANDING.  AFTER SHUTDOWN, THE LANDING GEAR POSITION LIGHTS BEGAN TO FUNCTION NORMALLY. MAINTENANCE PERSONNEL PLACED THE AIRCRAFT ON JACK AND TRIED UNSUCCESSFULLY TO DUPLICATE THE SNAG. THE WIRING AND TERMINALS WERE INSPECTED FOR FAULTS. NUMEROUS GEAR SWINGS WERE PERFORMED. THE AIRCRAFT WAS RELEASED SERVICEABLE. HISTORICALLY, THE LANDING GEAR HANDLE UNIT POSITION LIGHTS HAVE FAILED ON GROUND CHECKS AND THE UNITS (A FLEET OF 9 NEW (2006) AIRCRAFT) WERE SYSTEMATICALLY UPGRADED TO REVISION (E1L71 3O3  ORTA49CE   1E4     5  CP25EA    
20070530000352007053000035GL  2007       5          30         CA070227008      320070223G6111                BLADE           HARTZL      HCE4A3D     PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  PROPELLER       LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA            2234                                      KX130           (CAN) EXCESSIVE GREASE WAS NOTED LEAKING FROM PROPELLER BLADE ROOT ON ALL (4) BLADES. PROPELLER REMOVED AND SENT FOR REPAIR. (TC NR 20070227008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070808001482007080800148    2007       8          8          CA070227010      420070223G31600710143931      CONTROL PANEL                           PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  EFIS            FAILED          W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA                                                                      (CAN) MOVING THE HEADING KNOB ON THE CONTROL PANEL WOULD CAUSE A FAILURE INDICATION (RED X) THROUGH THE HEADING BUG, AND A TD WARNING ON THE BOTTOM RT CORNER OF THE EFIS SCREEN. THE CONTROL PANEL WAS REPLACED. (TC NR 20070227010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070808001492007080800149    2007       8          8          CA070227012      420070223G3455066107214       RECEIVER                                PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  ADF             ERRATIC         W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA                                                                      (CAN) THE VOLUME ON THE ADF WAS VERY HARD TO ADJUST AND ERRATIC.  ADF RECEIVER REPLACED (TC NR 20070227012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070530000382007053000038    2007       5          30         CA070227013      420070223G3100973321920       LIGHT                                   PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  CAUTION LIGHT   STUCK           W      O   OTHER                                                                                           N  FALSE WARNING                                                                 CRCRUISE         1                      CA                                                                      (CAN) WHEN RESETING THE CAUTION LIGHT, IT WOULD OCCASIONALY STICK ON. THE CAUTION LIGHT ASSY WAS REPLACED WITH NEW. (TC NR 20070227013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070530000392007053000039NE  2007       5          30         CA070227015      220070126G7210PT6T3B          GEARBOX                                 BELL  212   212         1181420SW  PWA   PT6T  PT6T3B      52045NE                              REDUCTION GB    MAKING METAL    W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       169831182                                                      (CAN) ENGINE NR 1 CHIP DETECTOR CAUTION LIGHT ILLUMINATED WHILE IN CRUISE FLIGHT AND PILOT RETURNED TO BASE. REDUCTION GEARBOX NR 1 SIDE CHIP DETECTOR FOUND WITH SMALL AMOUNT OF METAL. CHIP DETECTOR WAS CLEANED AND AIRCRAFT FLEW ANOTHER 2 HOURS BEFORE SECOND CHIP LIGHT AND RETURNED TO BASE.  SLIGHTLY MORE METAL FOUND ON PLUG. OIL WAS CHANGED AND AIRCRAFT WAS GROUND RUN 1 MINUTE BEFORE CHIP LIGHT ILLUMINATED. CHIP DETECTOR AND OIL FILTER CONTAINED MASSIVE AMOUNT OF METAL. REDUCTION GEARBOX WAS REPLACED AND SENT TO MFG FOR INVESTIGATION. NO REPORT HAS BEEN ISSUED AS YET. (TC NR 20070227015)                                                                                                                             1G71 4U4  U  H4SW    E22EA                
20070530000402007053000040    2007       5          30         CA070228002      420070221G612289741016        ARM             WOODWARD                MTSBSIMU2   MU2B60      5780460CE  GARRTTTPE331TPE33110    01514WP  HARTZLHCB4T HCB4TN5     GL  GOVENOR         STIFF           W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             LDLANDING        1                      CA       875  875   2131212                                             (CAN) WHEN AIRCRAFT LANDED IT WOULD PULL TO THE LT.   MAINTENANCE FOUND THAT THE PROP GOVERNOR ARM WAS STIFF AND WOULD NOT RETURN TO THE STOP. NOTE THIS GOVERNOR HAS SB TPE331-72-0567 RETURN SPRING INCORPORATED ON IT.  GOVERNOR WAS REPLACED AND CHECKED SERVICEABLE.  (TC NR 20070228002)                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H72 3T4  TRTA10SW   E4WE    6  CP40EA    
20070530000412007053000041    2007       5          30         CA070228003      420070228G6122AT210937        CONTROL ARM                             CESSNA206   U206        2073306CE  CONT  O520  IO520D      17032SO  MCAULY2A34C D2A34C58    GL  GOVERNOR        DEFECTIVE       W      A   UNSCHED LANDING                                                                                 FRJFLT CONT AFFECTED         PARTIAL RPM/PWR LOSS      WARNING INDICATION        CLCLIMB          1                      CA                                                                      (CAN) THE SUBJECT AIRCRAFT WAS CLIMBING OUT AFTER TAKEOFF AND EXPERIENCED A SIGNIFICANT LOSS OF CLIMB POWER RELATED TO A DROP IN ENGINE RPM FROM 2700 RPM TO 1600 RPM. THE PILOT EXECUTED ALL APPROPRIATE EMERGENCY PROCEDURES/ACTIONS WITH NO  IMPROVEMENT. THE PILOT DECLARED AN EMERGENCY AND WAS ABLE TO MANEUVER THE AIRCRAFT BACK TO THE AIRPORT,  LANDED WITHOUT FURTHER INCIDENT. UPON EXAMINATION, IT WAS DETERMINED THAT THE INTENTION OF THE DESIGN OF THE PROP GOVERNOR ARM ATTACHMENT WAS TO HAVE THE BOLT THAT COMPRESSES THE ARM ON TO THE SPLINED SHAFT WAS TO PASS THROUGH THE GROVE IN THE SHAFT THUS PREVENTING THE ARM FROM SEPARATING EVEN IF THE BOLT DOES NOT HAVE SUFFICIENT TORQUE. IN THIS CASE THE ARM IS MANUFACTURE1H71 3O3  O  A4CE    E5CE    5  CP3EA     
20070530000442007053000044CE  2007       5          30         CA070228006      120070228G71201299100471      MOUNT                                   BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  ENGINE          CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING ROUTINE MAINTENANCE A BLEED AIR LINE WAS FOUND CHAFING AN ENGINE TRUSS MOUNT TUBE. BLEED AIR LINE PN: 118-910033-93 TRUSS MOUNT PN: 129-910047-17. THE DAMAGE WAS FOUND TO BE WITHIN REPAIRABLE LIMITS IAW THE AIRCRAFT SRM. THE MOUNT WAS REPAIRED BY A QUALIFIED WELDER AND THE AIRCRAFT WAS RELEASED BACK INTO SERVICE. A FLEET CAMPAIGN WAS CONDUCTED AND ONE OTHER AIRCRAFT WAS FOUND WITH THE SAME PROBLEM WITH BOTH INCIDENTS ON THE LT ENGINE TRUSS MOUNT.  (TC NR 20070228006)                                                                                                                                                                                                                                            2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070530000452007053000045    2007       5          30         CA070228007      420070215G3452KT76A           TRANSPONDER                             CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL                  INTERMITTENT    W      A   UNSCHED LANDING                                                                                 H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA                                                                      (CAN) DURING CIRCUIT FLYING, TOWER REPORTED TO PILOT THAT HIS TRANSPONDER WAS INTERMITTENT.  PILOT CANCELLED REMAINDER OF FLIGHT AND RETURNED TO AIRPORT. DEFECT WAS NOT DUPLICATED ON THE GROUND. DEFECT OCCURED THE NEXT DAY WHILE AIRCRAFT WAS AGAIN IN THE CIRCUIT, PILOT CANCELLED AND RETURNED TO AIRPORT. MAINTENANCE REMOVED TRANSPONDER, CLEANED CONTACTS AND RE-RACKED TRANSPONDER. AIRCRAFT RETURNED TO SERVICE AND HAS NOT HAD ANOTHER OCCURANCE IN OVER 50 HOURS. (TC NR 20070228007)                                                                                                                                                                                                                                              1H71 3O3  ONT3A19    E223    5  NP50GL    
20070530000462007053000046CE  2007       5          30         CA070228008      120070208G563051116052        WINDOW                                  CESSNA421   421B        2076014CE  CONT  O520  GTSIO520H   17032SO  MCAULY3AF34C3AF34C92    GL  EMERGENCY EXIT  CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING MAJOR INSPECTION OF AIRCRAFT, REMOVED PLASTIC UPHOLSTERY COVER ON THE EMREGENCY EXIT HATCH. WINDOW FOUND CRACKED AT ALL LOWER ATTACH SCREW HOLES, ONLY THE SEALANT KEEPING THE WINDOW IN PLACE. (TC NR 20070228008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3O3  O  A7CE    E7CE    5  CP22EA    
20070530000472007053000047    2007       5          30         CA070228009      420070227G3400                SWITCH                                  CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA                              AVIONICS        FAILED          W      A   UNSCHED LANDING                                                                                 HJ ELECT. POWER LOSS-50 PC   WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) DURING TRAINING FLIGHT, PILOT EXPERIENCED COMPLETE AVIONICS FAILURE WHEN DEPRESSING THE PTT SWITCH. AIRCRAFT RETURNED TO BASE, MAINTENANCE DUPLICATED THE SNAG, DISCOVERED THE AVIONICS SWITCH DEFECTIVE AND REPLACED IT WITH NEW ONE, NO FURTHER FAULTS FOUND. (TC NR 20070228009)                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  ONT3A12    E274                 
20070530000482007053000048EA  2007       5          30         CA070301001      220070301G8530LW11901         INTAKE VALVE                            CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  ENGINE          CRACKED         W      A   UNSCHED LANDING                                                                                 RE PARTIAL RPM/PWR LOSS      VIBRATION/BUFFET                                    CLCLIMB          1                      CA       29                                                             (CAN) INVESTIGATING LOW COMPRESSION REVEALED SMALL CHUNK (ONE QUARTER INCH SQUARE) OF INTAKE VALVE MISSING ON EDGE, AND A CRACK IN ANOTHER AREA. (TC NR 20070301001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A19    E223    5  NP50GL    
20070530000492007053000049EA  2007       5          30         CA070301002      120070228G5343                FITTING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              LANDING GEAR    CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) BOTH MAIN LANDING GEAR FITTING FOUND CRACKED ON NDT INSPECTION IAW ADCF-1999-32R3. MAIN LANDING GEAR WILL BE REPLACED. LT P/N 5321103  S/N PO-422V5Q, RT P/N 3521104  S/N PO-BBBB10. (TC NR 20070301002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA21EA   E15NE                
20070524001942007052400194NM  2007       5          24         CA070301003      120070223G2761A44700009       ACTUATOR                                DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  SPOILER         CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    NRNOT REPORTED   1                      CA                                                                      (CAN) WHILE DOING A PRE-FLIGHT WALK AROUND THE PILOT NOTICED HYDRAULIC FLUID DRIPPING FROM THE RT FLAP TRACK NR 3 FAIRING. THE LEAK WAS FOUND TO BE COMING FROM THE OB ROLL SPOILER ACTUATOR. UPON REMOVAL OF THE ACTUATOR IT WAS FOUND THAT THE HOUSING HAD CRACKED IN THE AREA SUROUNDING ONE OF THE PLUGS CAUSING THE PLUG TO DISLODGE. THE CRACK EXTENDED AROUND THE ENTIRE CIRCUMFERENCE OF THE THREADED PORTION OF THE ACTUATOR BODY WHERE THE PLUG IS THREADED IN. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070301003)                                                                                                                                                                                   2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070524002082007052400208EA  2007       5          24         CA070301004      120070301G27606009260273      ROD                                     CNDAIRCL601 CL6012A12   1900303EA                                                               SPOILER         CORRODED        W      O   OTHER                                                                                           J  WARNING INDICATION                                                            ININSP/MAINT     1                      CA       10927                                                          (CAN) DURING THE PILOT PRE-FLIGHT CHECKS THE LT FLIGHT SPOILER INDICATED DEPLOYED WHEN STOW WAS SELECTED. THE FLIGHT SPOILER STOW/DEPLOY HANDLE WAS STIFF AT THE STOW EXTREMELY. VISUAL CONFIRMATION REVEALED THAT THE FLIGHT SPOILER WAS NOT FULLY STOWED BUT THE RT SPOILER WAS. INVESTIGATION REVEALED THAT THE ROD ENDS OF THE 15 DEGREE CONTROL ROD WERE CORRODED WITH RED RUST AND WERE NOT ABLE TO MOVE RESTRICTING THE FEEDBACK OF THE FLIGHT SPOILER CONTROL UNITS ON THE LT SIDE. OPERATIONS USING TYPE 4 ANTI-ICING FLUIDS HAVE SHOWN TO CAUSE RED RUST CORROSION ON UNPROTECTED STEEL. THERE CURRENTLY IS NO REQUIREMENT TO TREAT THE SURFACES WITH A CORROSION INHIBITOR. THE USE OF TYPE 4 ANTI-ICING FLUIDS CONTRIBUTING TO CORRO2L72 4F    RTA21AE                        
20070530000502007053000050EA  2007       5          30         CA070302001      120070228G2497                WIRE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                                              DAMAGED         W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AFTER A NORMAL LANDING AND WHILE TAXING TO THE GATE, THE FLT CREW REPORTED INTERMITTENT ARCING AND SMOKE COMING FROM BEHIND THE CAPTAINS SIDE CB PANEL.  AIRCRAFT DEPLANED NORMALLY.  ELECTRICAL POWER WAS SHUT DOWN AND FIRE CREW WERE CALLED TO CHECK OF FIRE.  NO FURTHER REPORTS OF SMOKE/FIRE AFTER POWER WAS REMOVED FROM THE AIRCRAFT.   UPON FURTHER INVESTIGATION, MAINTENANCE NOTED THAT (2) BUS FEEDER WIRES BECAME UNSECURED AND ARCED ON THE BULKHEAD WHICH RUNS PARALLEL TO B SCREEN TRAILING EDGE ON CAPTAINS SIDE AND APPROX FS280.  DAMAGE WAS NOTED TO WIRE TERMINAL ENDS AND WIRE INSULATION AND WELL AS BURN MARKS ON BULKHEAD/STRINGER AND 2 RIVETS.  NO DAMAGE TO EXTERNAL FUSELAGE SKIN.  BURN ON BULKHEAD IS 1 INC2L72 4F4  FRTA21EA   E15NE                
20070530000512007053000051EA  2007       5          30         CA070302002      120070225G5410                COWLING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              LT NACELLE      DEPARTED        W      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           CLCLIMB          1                      CA                                                                      (CAN) FLIGHT 3808, REPORTED A LOUD NOISE SHORTLY AFTER DEPARTURE, ON LANDING DISCOVERED COWLING MISSING AND UNKNOWN DAMAGE TO HORIZONTAL  STABILIZER, NO REPORTED INJURIES, SN 7849 (REG N456ZW).  WHAT COLLATERAL DAMAGE TO HZ STAB AND OTHER AREAS? HZ STAB LEADING EDGE AND HZ STAB CENTER BULLET CAP SIGNIFICANT IMPACT DAMAGE ASSUMED FROM LT UPPER FAN COWL DEPARTING THE AIRCRAFT.   WHAT POINT IN DEPARTURE WAS (LOAD NOISE) HEARD? (LOUD NOISE) ASSUMED TO BE (CARGO SHIFT) NOW SUSPECTED AS COWL DEPARTURE AT 2800 FEET ON INITIAL CLIMB OUT, ENROUTE.  BECAUSE PILOTS ASSESSED NOISE TO BE (CARGO SHIFT) THEY ELECTED TO CONTINUE.  LT UPPER FAN COWL WAS RECOVERED BY AND CURRENTLY RETAINED BY US COAST GUARD FROM LOCATION OUTSIDE2L72 4F4  FRTA21EA   E15NE                
20070530000522007053000052SW  2007       5          30         CA070302004      120070228G6230206010003001    CONE SET                                BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              MAIN ROTOR      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) MAIN ROTOR TORQUE CHECK WAS PERFORMED ON M/R MAST NUT BETWEEN 3 TO 8 FLIGHT HOURS IAW THE MM CHAPTER 5, AND MM, SECTION 62-7, PARAGRAPH 5.    INITIAL TORQUE CHECK OF MAST NUT TORQUE WAS FOUND BELOW MINIMUM SPECIFIED TORQUE OF 250 FT/LBS, IAW MM.  A SUBSEQUENT TORQUE CHECK WAS PERFORMED AFTER SECOND FLIGHT OF 3 HOURS WITH THE SAME RESULTS, MAST NUT TORQUE FALLING BELOW MINIMUM TORQUE VALUE OF 250FT/LBS.    UPON VISUAL INSPECTION IN THE AREA OF THE CONE SET TO TRUNNION,  IT WAS FOUND THAT ONE OF THE SPLIT CONES HALVES HAD MOVED.   THEREFORE DID NOT PROVIDE A TRUE SEAT FOR THE SPLIT CONES TO THE M/R TRUNNION AS CONE SET AND WAS PARTIALLY COCKED.    IT IS SUSPECTED THAT EACH OF THE 2 TORQUE CHECK ADJUSTMENTS 1G71 3U3  U  H2SW    E4CE                 
20070530000532007053000053NM  2007       5          30         CA070305001      120070303G2752NAS1611130      O-RING          BOEING                  BOEING727   727247      138408FNM                                                               DIRVE MOTOR     FAILED          W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  ININSP/MAINT     1                      CA       69942      84630D                                              (CAN) AIRCRAFT EXPERIENCED LOW PRESSURE WARNING LIGHT FROM THE (A)  HYD SYSTEM.  DUE TO WEATHER THE CREW DECIDED THAT A RETURN TO DEPARTURE POINT WOULD BE THE BEST OPTION. THE CREW DECLARED AN EMERGENCY AND RETURNED WHERE THEY HAD A SAFE LANDING AND THE AIRCRAFT WAS TOWED OFF THE RUNWAY TO THE RAMP.  MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE OB FLAP DRIVE HYD MOTOR WAS LEAKING HYD FLUID FROM THE CASE DRAIN TUBE. DUE TO WEATHER THE OB FLAP DRIVE HYD MOTOR WAS REPLACED THE NEXT DAY. SYSTEM WAS SERVICED AND THE SYSTEM WAS LEAK AND FUNCTION TESTED SERVICEABLE. THE AIRCRAFT DEPARTED ON MAR.3, 2007 WITH NO FURTHER FAULTS. (TC NR 20070305001)                                                                 2L73 4F      A3WE                         
20070530000542007053000054EA  2007       5          30         CA070305002      120070305G3233MS2125004012    BOLT                                    DHAV  DHC8  DHC8311     1386006EA                                                               ACTUATOR FITTINGSHEARED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING THE ACCOMPLISHMENT OF C-CHECK, THE NOSE ACTUATOR FUSELAGE FITTING WAS FOUND WITH (2) BOLTS SHEARED. SB 8-53-50 FOR THIS FAILURE. THE CUT IN S/N WAS 403 AND OUR A/C WAS S/N:410. THE MODIFICATION 8/2140 WAS TRULY ACCOMPLISHED. THE FITTING WAS INSTALLED WITH BIGGER BOLTS BUT (2) OF THOSE BOLTS WERE SHEARED.  (TC NR 20070305002)                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T    RTA13NM                        
20070530000552007053000055NM  2007       5          30         CA070305003      120070305G2497CL12068161      RELAY                                   DHAV  DHC8  DHC8102     2809003NM                                                               ECU             BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING THE ACCOMPLISHMENT OF THE INSPECTION TASK 7320/02, BOTH RELAY (RELAYS 7611-K3 AND K4) BASES WERE FOUND BROKEN AND BARELY MAKING CONTACT. SHOULD BOTH OF THEM HAVE FALLEN OFF AND DISCONNECTED IN FLIGHT, BOTH ECU`S WOULD HAVE HAD A COMPLETE POWER FAILURE. ECU SYSTEMS ARE DESIGNED TO HAVE POWER FED FROM NR 1 AND NR 2 ESSENTIAL BUSES. BOTH POWER SOURCES GO THROUGH THEIR RESPECTIVE RELAYS K3 AND K4, A BROKEN BASE WOULD COMPROMISE THE 2 POWER SOURCES SIMULTANEOUSLY, RESULTING IN EACH ECU REVERTING TO MANUAL MODE. THIS RELAY BASE PROBLEM WAS REPORTED BY ME FEW TIME FOR DIFFERENT SYSTEM ON DIFFERENT A/C AND DIFFERENT OPERATOR. (TC NR 20070305003)                                                              2H72 4T    RTA13NM                        
20070530000562007053000056CE  2007       5          30         CA070305004      120070228G561011438402522     WINDSHIELD                              BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  COCKPIT         FAILED          W      B   EMER. DESCENT                                                                                   O  OTHER                                                                         CRCRUISE         1                      CA       21017                                                          (CAN) CO-PILOTS WINDSHIELD SHATTERED IN CRUISE.  AIRCRAFT DESCENDED IAW ABNORMAL OCCURRENCE CHECKLIST AND BROUGHT CABIN DIFF DOWN TO BELOW 2PSI.  AIRCRAFT DESCENDED TO 11000 FT LOWERED CABIN ALTITUDE AT 500 FPM TO 11000FT.  PUT CABIN INTO DUMP MODE AND CONTINUED FLIGHT WITHOUT INCIDENT. WINDSHIELD WAS REPLACED WITH IMPROVED PART. (TC NR 20070305004)                                                                                                                                                                                                                                                                                                                                                                                 2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070530000572007053000057WP  2007       5          30         CA070306001      120070223G2916                RESERVOIR                               ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              HYD SYSTEM      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION HYDRAULIC FLUID FOUND VERY LOW, DETERMINED FLUID WAS LEAKING OUT OF THE VENT CAP ON HYDRAULIC RESERVOIR. FLUID TOPPED UP TO CENTER OF SIGHT GLASS. AIRCRAFT GROUND RAN, DETERMINED FLUID WAS RISING IN RESERVOIR AND VENTING OUT OF VENT CAP. RESERVOIR SENT TO MFG. REINSTALLED AFTER REPAIR, GROUND RAN AND FOUND HYDRAULIC LEVEL TO STAY AT CENTER OF SIGHT GLASS. (TC NR 20070306001)                                                                                                                                                                                                                                                                                                                               1G71 3O3  O  H11NM   1E4                  
20070530000582007053000058SW  2007       5          30         CA070306002      120070226G6310206040118001    COUPLING                                BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              GEARBOX         LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) C-GELT`S MAIN DRIVESHAFT P/N 206-040-015-103, S/N A-1331, 600 HR INSPECTION AND REPACK C/W FEB 22/07 AT 13635.5 HRS. TEST FLOWN 0.3 HRS, FLEW 7.1 HRS FEB 24 AND 25, ENGINEER FOUND TRANS. SIDE LEAKING GREASE AND COUPLING OVERHEATED. DRIVE SHAFT S/N A-2441 REMOVED FROM AC WITH FRESH 600 HR INSP. AND REPACK INSTALLED ON C-GELT. WHICH FAILED IN 11.7 HRS. WITH THE SAME PROBLEM. DRIVE SHAFT S/N A1331 OVERHAULED WITH NEW INNER GEAR, NEW OUTER COUPLING, NEW O-RINGS, AND GREASE (PN 204-040-755-5 EXP. NOV 2/08) INSTALLED ON YHY, FAILED IN 23 MINUTES FLYING TIME, SAME PROBLEM (TRANSMISSION SIDE) THE SAME TUBE OF GREASE WAS USED FOR ALL THE REPACKS. (TC NR 20070306002)                                                 1G71 3U3  U  H2SW    E4CE                 
20070530000592007053000059NM  2007       5          30         CA070306003      120070308G215020405010        ACM                                     BOEING737   737210C     1384459NM  PWA   JT8   JT8D9A      52048NE                              LEFT            ODOR            W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                                                      (CAN) SHORTLY AFTER DERPARTING, A SMOKE SMELL/HAZE WAS NOTICED IN THE CABIN AREA. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. THE CREW ADVISED MAINTENANCE THEY SUSPECTED THE LT PACK. THE SMOKE SMELL SOURCE WAS VERIFIED AS THE THE LT AIR CYCLE MACHINE. THE AIRCRAFT WAS RELEASED UNDER THE MEL. THE AIR CYCLE MACHINE WAS REPLACED THE FOLLOWING DAY. (TC NR 20070306003)                                                                                                                                                                                                                                                                                                                              2L72 4F4  F  A16WE   E2EA                 
20070530000602007053000060EU  2007       5          30         CA070306004      120070308G5610                WINDSHIELD                              AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  COCKPIT         FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         DEDESCENT        1                      CA                                                                      (CAN) ON DESCENT THE LT WINDSHIELD OUTER PANE FAILED. THE AIRCRAFT LANDED AT DESTINATION WITHOUT FURTHER PROBLEM. MAINTENANCE INSPECTED THE AIRCRAFT PRIOR TO RETURN UNDER MEL, WHERE THE WINDSHIELD WAS REPLACED. (TC NR 20070306004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20070530000612007053000061NE  2007       5          30         CA070306005      220070305G751082110588003     DUCT                                    DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF15      NE  BLEED AIR       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3823338233                                                     (CAN) DURING MAINTENANCE, TROUBLESHOOTING FOR LOW FLOW FROM CABIN GASPERS, MAINTENANCE, WHILE INSIDE THE AFT CARGO COMPARTMENT FELT THE REAR PRESSURE BULKHEAD AS BEING WARM/HOT. INVESTIGATION IN THE AFT EQUIPMENT BAY, FOUND THE ENGINE BLEED AIR / APU / AIR-CONDITIONING PACKS JUNCTION DUCT CRACKED, CRACK EXTENDED AT LEAST 50 PERCENT OF CIRCUMFERENCE AND WAS OPEN BY APPROX .2500 INCH.  DUCT ASSEMBLY REPLACED, FUNCTION CHECKS CARRIED OUT.  AIRCRAFT RETURNED TO SERVICE. (TC NR 20070306005)                                                                                                                                                                                                                                      2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070530000622007053000062EA  2007       5          30         CA070306006      120070304G3220498003          DAMPER                                  CNDAIRCL600 CL6002C10   1390015EA                                                               NLG             MALFUNCTIONED   W      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              LDLANDING        1                      CA       3750                                                           (CAN) ON LANDING CREW REPORTED AN AIRFRAME VIBRATION.  CREW INDICATED THAT THE VIBRATION DEMINISHED AS THE AIRCRAFT SPEED REDUCED.  AIRCRAFT TAXIIED TO GATE WITHOUT FURTHER INCIDENT.  MAINTENANCE INSPECTION REVEALED LOOSE APEX NUT ON LT SHIMMY DAMPER.  NEW SHIMMY DAMPER AND ASSOCIATED PARTS ARE BEING REPLACED. (TC NR 20070306006)                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F    RTA21EA                        
20070530000632007053000063EU  2007       5          30         CA070307001      120070302G324090002340PR      BRAKE ASSY                              EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF3410E6    30015NE                              MLG             ICED            W      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              LDLANDING        1                      CA                                                                      (CAN) ON LANDING, AT 90 KNOTS THE LT OB TIRE BLEW, DAMAGING PART OF THE GEAR DOOR ASSEMBLY. ACFT DEPARTED WHERE A SEVERE SNOW STORM WAS TAKING PLACE, IT WAS NOTED THAT WATER WAS RUNNING FROM THE BRAKE ASSEMBLY AND DRIPPING FOR HOURS, SUSPECT BRAKE BECAME PACKED WITH SNOW AND ICE. (TC NR 20070307001)                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA57NM   E00070EN             
20070530000642007053000064EA  2007       5          30         CA070307002      120070305G2560110124007       BUCKLE                                  DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  SEAT BELT       DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHEN COMPLYING WITH COMPANY CAMPAIGN NOTICE 010-25-10-011 AN INSPECTION FOR INTERFERENCE BETWEEN THE YOKE AND SEATBELT BUCKLE WAS CARRIED OUT IAW NM-06-29.THE RESTRAINT RELEASE MECHANISM ON PILOT AND COPILOTS SEAT BELTS CAN BE OPERATED UNINTENTIONALLY BY EXTREME NOSE UP AND ROLL COMMANDS OF THE CONTROL COLUMN. (TC NR 20070307002)                                                                                                                                                                                                                                                                                                                                                                                               1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070530000652007053000065EA  2007       5          30         CA070307003      120070305G5730C6W1017         SKIN PANEL                              DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  LT WING         DEBONDED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       17756                                                          (CAN) DEBONDING OF UPPER WING SKIN, OB OF NACELLE. DEBONDING DETECTED DURING ULTRA SONIC INSPECTION IAW SB 6/543. REPAIR CARRIED OUT IAW REO6-57-30-V013 REV A. (TC NR 20070307003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070530000662007053000066EA  2007       5          30         CA070307004      120070305G5730C6W1017         SKIN PANEL                              DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  RWS 72-97       DEBONDED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       17756                                                          (CAN) DEBONDING OF UPPER WING SKIN, IB OF NACELLE. DEBONDING DETECTED DURING ULTRA SONIC INSPECTION IAW SB 6/543. REPAIR CARRIED OUT IAW REO6-57-30-V012 REV A. (TC NR 20070307004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070530000672007053000067    2007       5          30         CA070307005      420070306G31600660312525      DISPLAY                                 PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  EFIS            INOPERATIVE     W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE, A (DU) WARNING APPEARED ON THE CO-PILOTS EADI DISPLAY INDICATING INSUFFICENT COOLING. THE DISPLAY UNIT WAS REPLACED. (TC NR 20070307005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070530000682007053000068EA  2007       5          30         CA070307006      120070305G5730                SKIN                                    DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  WING            CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       17756                                                          (CAN) SEVERAL CORRODED RIVET HEADS FOUND ON THE LOWER SURFACE OF WING. THE AREA OF CONCENTRATION IS THE GAS PATHS FROM THE EXHAUST STACKS. REPAIRS CARRIED OUT IAW REO6-57-30-V017 (YW 85-91.25) AND REO6-57-30-V018 (YW 127-146). (TC NR 20070307006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070530000692007053000069EA  2007       5          30         CA070307007      120070305G5730MS20470AD       SKIN                                    DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  WING            CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       17756                                                          (CAN) SEVERAL CORRODED RIVET HEADS FOUND ON THE LOWER SURFACE OF WING. THE AREA OF CONCENTRATION IS THE GAS PATHS FROM THE EXHAUST STACKS. REPAIRS CARRIED OUT IAW REO6-57-30-V019 (YW 85-91.25) AND REO6-57-30-V020 (YW 122-135). (TC NR 20070307007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070530000702007053000070EA  2007       5          30         CA070307008      120070305G5730C6W101427       SKIN PANEL                              DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  LT WING         CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       17756                                                          (CAN) SEVERAL CORRODED RIVET HEADS FOUND ON THE LOWER SURFACE OF WING. THE AREA OF CONCENTRATION IS THE GAS PATHS FROM THE EXHAUST STACKS. REPAIRS TO CORRODED RIVETS WAS INITIATED AND REVEALED CORROSION UNDER THE RIVET HEADS EXISTED TO A DEPTH OF 0.011. REPAIRS CARRIED OUT I.A.W. VIKING REO6-57-30-V025 (YW 85-97.25). I.C.A.`S PENDING D.T.A. BY VIKING. (TC NR 20070307008)                                                                                                                                                                                                                                                                                                                                                           1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070530000712007053000071SW  2007       5          30         CA070307009      120070305G291066D44           REGULATOR                               FRCHLDSA227 SA227CC     3377522SW  GARRTTTPE331TPE33111U   01514WP  MCAULY4HFR344HFR34C652  NE  HYD SYSTEM      MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AC DEPARTED BASE AND UPON GEAR RETRACTION BOTH LT AND RT HYD PRESSURE LIGHTS ILLUMINATED FOR 3-4 SECONDS THEN WENT OUT.  AIRCRAFT RETURNED TO BASE AND UPON INVESTIGATION IT WAS FOUND THAT NO RESIDUAL HYD PRESSURE WAS PRESENT AFTER ENGINE SHUTDOWN.  UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE 31 PSI REGULATOR WAS CONTAMINATED WITH HYD FLUID.  THE REGULATOR CHECK VALVE HAD BEEN INSTALLED INCORRECTLY.  THE CHECK VALVE WAS REPOSITIONED AND THE REGULATOR WAS REPLACED.  GEAR WINGS WERE CARRIED OUT SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070307009)                                                                                                                                              2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20070530000722007053000072NE  2007       5          30         CA070307010      220070307G7497WIRE            WIRE                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              MAGNETO         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       286        E051A254                                            (CAN) GOVERNOR WAS LAZY AND SNAGGED BY PILOT.  UPON FURTHER INVESTIGATION, THE MAGNETO WAS REMOVED AND PRIMARY COIL WIRE WAS TOUCHING AND CHAFING ON TACH POINT CONNECTOR. THIS MAY BE THE POSSIBLE CAUSE FOR LAZY GOVERNOR.  NEW MAGNETO INSTALLED PROBLEM RECTIFIED. MAGNETO SENT BACK FOR WARRANTY. (TC NR 20070307010)                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 3O3  O  H11NM   1E4                  
20080324004122008032400412EU  2008       3          24         CA070307011      120070307G6710                CYCLIC CONTROL                          UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              MAIN ROTOR      MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) CYCLIC CONTROLS JAMMED IN NEUTRAL POSITION, CYCLIC WAS ABLE TO MOVE AFT, FWD, AND LT BUT WAS UNABLE TO MOVE CYCLIC TO THE RT DURING LEVEL CRUISE AT 2500 FT AGL. REDUCED AIRSPEED TO 65 KNOTS AND CONTROLS BROKE FREE AND OPERATED NORMALLY.  THEN FLEW BACK TO THE HANGER AT AN AIRSPEED OF 65 KNOTS AND CONTROLS FELT NORMAL UNTIL AT ABOUT 200 FT AGL AND AIRSPEED AT ABOUT 40 KNOTS WITH 300 FT IAW MINUTE DESCENT RATE THE CYCLIC JAMMED ON THE RT SIDE AGAIN. THE AC SLOWLY STARTED A BANK AND AN OVERSHOOT AND PROCEEDED TO THE RUNWAY. DURING THE OVERSHOOT, BROUGHT AIRSPEED BACK UP TO AROUND 65 KNOTS AND JOINED A RT DOWNWIND FOR RUNWAY 13. ON A BASE LEG, SHUTOFF HYD AND PERFORMED A NORMAL HYD FAILURE APPROACH. CONTROLS 1G72 3U3  UNCR0001RD E34NE                
20070530000732007053000073SO  2007       5          30         CA070308001      120070302G284268101002        FLOAT                                   PIPER PA28  PA28R200    7102811SO  LYC   O360  IO360C1C    41514EA  HARTZLHCC3Y HCC3YF1     GL  FUEL CELL       WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7968                                                           (CAN) HOLE IN FLOAT WAS EXTREMELY WORN AND FLOAT FELL OFF. (TC NR 20070308001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 3O3  O  2A13    1E10    5  CP25EA    
20070530000742007053000074    2007       5          30         CA070308002      420070306G2397J176037         WIRE            COLLINS                 BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  NR 2 COMM HEAD  SHORTED         W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA       16604      14617                                               (CAN) FLIGHT CARRIED OUT MAR. 5, 2007, NR 2 COMM DISPLAY WENT BLANK.  CONTROL HEAD REPLACED WITH LOANER UNIT, GROUND TESTED OK. NEXT FLIGHT AIRCRAFT TOOK OFF AND UPON ROTATION THE CREW SMELLED SOMETHING BURNING AND SAW SMOKE COMING FROM THE  NR 2 COMM CONTROL HEAD. AIRCRAFT RETURNED TO BASE.  CONTROL HEAD REMOVED FOR REPAIR AND INVESTIGATION. FOUND WIRE P/N J176037 IN NOSE AVIONICS BAY GOING FROM RELAY J304 TO TRANSCEIVER TRAY WITH CONTINUITY TO GROUND.  WIRE REPAIRED AND ORIGINAL CONTROL HEAD INSTALLED AFTER REPAIR, COMM OPERATED FOR 2 HOURS ON THE GROUND WITHOUT FAULT. NO PROBLEMS REPORTED THE SUBSEQUENT FLIGHT. (TC NR 20070308002)                                                                               2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070530000752007053000075EA  2007       5          30         CA070308003      120070307G76032100140007      GEARBOX                                 CNDAIRCL604 CL604       1900301EA  GE    CF34  CF343B1          NE                              THROTTLE        FAILED          W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA       1740                                                           (CAN) DURING CLIMB, THE RT ENGINE WAS NOT ABLE TO ACHIEVE CLIMB POWER. THE AIRCRAFT DIVERTED TO ANOTHER AIRPORT AND LANDED UNEVENTFULLY. INVESTIGATION REVEALED THAT THE THROTTLE GEARBOX HAS AN AREA WHERE MOVEMENT OF THE THROTTLE HAS NO EFFECT ON THE MFC. THIS CONDITION WOULD NOT ALLOW THE MFC TO REACH THE MAX POWER STOP. MFG SB 604-76-004 HAD NOT BEEN COMPLIED WITH AT THIS TIME NOR WAS IT REQUIRED AT THIS TIME BUT WAS PLANNED TO BE COMPLETED. THERE ARE (2) AD`S FOR THROTTLE GEARBOX WEAR ON THE RJ FLEET.  REF: AD 2005-06-04, AD 2004-05-12.  AFTER REPAIR AND RETURN OF THE AIRCRAFT TO THE MAIN BASE AND EXAMINATION OF THE FAILED PART THEN MORE INFORMATION WILL BE PROVIDED. (TC NR 20070308003)                       2L72 4F4  FRTA21EA   E15NE                
20070530000762007053000076WP  2007       5          30         CA070308004      120070306G2430                CONTROL SWITCH                          CVAC  340   340CVAC     242270AWP  ALLSN 501D  501D22      03005GL  HAMSTD54H   54H60       NE                  SHORTED         W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) WHILE CARRYING OUT FLIGHT TRAINING THE LT GENERATOR WAS TURNED OFF. WHEN SELECTED BACK ON, IT WAS NOTED THAT SMOKE WAS COMING FROM THE VOLTAGE REGULATOR. THE GANG BAR WAS SELECTED TO SHUTOFF DC POWER. DURING TROUBLESHOOTING THE MAINTENANCE CREW DISCOVERED AN AN960-10L WASHER HAD SHORTED OUT THE WIRE ATTACHMENT LUGS ON THE BACK OF THE GENERATOR CONTROL SWITCH. A REPLACEMENT VOLTAGE REGULATOR WAS INSTALLED AND THE WIRING SYSTEM WAS INSPECTED. NO FURTHER DAMAGE WAS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070308004)                                                                                                                                                                                       2L72 4R4  T  6A6     E282    6  CP906     
20070530000772007053000077EU  2007       5          30         CA070309001      120070303G2820110BR02         VALVE                                   BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R408  CR4086123F17EU  FUEL CROSSFEED  MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) AC WAS IN CRUISE FLIGHT, WHEN THE FLIGHT CREW OPENED THE FUEL CROSSFEED VALVE TO BALANCE THE FUEL LOAD. WHEN THE FLIGHT CREW SELECTED THE LT BOOST PUMPS TO OFF, THE NR 1 ENGINE FLAMED OUT. THE FLIGHT CREW FEATHERED ENGINE NR 1. THE PILOT THEN CLOSED THE FUEL CROSSFEED VALVE, SWITCHED THE LT FUEL BOOST PUMPS TO ON AND SUCCESSFULLY RELIT ENGINE NR 1. THE AIRCRAFT CONTINUED WITH OUT FURTHER DIFFICULTY.  UPON ARRIVAL, MAINTENANCE BLED THE FUEL SYSTEM, CHECKED FOR FUEL CONTAMINATION AND EXTENSIVELY GROUND RAN ENGINE NR 1. NO FAULTS WERE FOUND. FURTHER INVESTIGATION HAS DETERMINED HS SB 28/27 WHICH PREVENTS ACCUMULATION OF AIR IN THE CROSSFEED LINE HAS NOT BEEN ACCOMPLISHED ON THIS AIRCRAFT. IT IS BELIEVED AIR 2L72 3T4  T  A24EU   A196    6  CP17BO    
20080219001472008021900147EU  2008       2          19         CA070309002      120070308G6210C621A1006103    BLADE                                   UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              MAIN ROTOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       995  995                                                       (CAN) BLADE CRACKED BY TRAILING EDGE OF TRIM TAB, IB SIDE. (TC NR 20070309002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G72 3U3  UNCR0001RD E34NE                
20070530000782007053000078WP  2007       5          30         CA070309003      120070302G6210500P2100101     BLADE                                   HUGHES369   369D        4470706WP  ALLSN 250C  250C20      03013GL                              MAIN ROTOR      CRACKED         W      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA       2597                                                           (CAN) PILOT FELT A VIBRATION AND UPON LANDING CHECKED MAIN ROTOR BLADES. A CRACK APPROXIMATELY 18 INCHES FROM THE ROOT, RUNNING PERPENDICULAR TO THE TRAILING EDGE WAS DISCOVERED. IT APPEARS AS IF THE BLADE DEBONDED AT A RIB, AS THE CRACK FOLLOWS STRAIGHT FROM THE RIB TOWARD THE C-CHANNEL BEFORE IT TRAILS OFF TO THE SIDE.  MDHI )OEM) HAS SUGGESTED THAT THE CAUSE WAS TOO MUCH TENSION ON THE BLADES AT TIE-DOWN, OIL-CANNING BETWEEN THE RIBS PUTTING PRESSURE ON THE BOND. (TC NR 20070309003)                                                                                                                                                                                                                                      1G71 3U3  U  H3WE    E4CE                 
20070530000792007053000079EU  2007       5          30         CA070310001      120070302G27529787320309      ACTUATOR                                PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  TE FLAPS        FROZEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA       2242 2242                                                      (CAN) FLAPS WOULD WORK AS NORMAL, EVEN AFTER 4 HOUR FLIGHT AT -45. AFTER LANDING & SELECTING FLAPS UP,  (FLAPS) CAUTION WOULD COME ON NR FLAPS WOULD NOT MOVE. NORMAL GROUND RESET WOULD NOT WORK. FLAP CONTROL 1 AMP C/B APPEARED TO BE (BLOWN) BUT NOT POPPED. AFTER RESETTING C/B, NORMAL FLAP RESET WOULD WORK. TRYING TO MOVE FLAPS AGAIN WOULD CAUSE THE SAME PROBLEM. NOTE THIS DEFECT WOULD ONLY OCCUR IF THE GROUND TEMP WAS -5 TO -12. AFTER WARMING THE AIRCRAFT IN A HANGAR FLAPS WOULD RESET NR WORK. UPON INSPECTION OF THE ACTUATORS IT WAS DISCOVERED THAT 3 OF THE 4 ACTUATORS WERE HEATING UP. +40 TO +50 C. ACTUATORS WERE REMOVED FROM SERVICE. ALSO NOTED WAS FLAP CONTROL WARNING UNIT FAILURE CODES INCLUDED TOO HIGH CUR1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070530000802007053000080EU  2007       5          30         CA070310002      120070302G275297897320309     ACTUATOR                                PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  TE FLAPS        FROZEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA       2242 2242                                                      (CAN) FLAPS WOULD WORK AS NORMAL, EVEN AFTER 4 HOUR FLIGHT AT -45. AFTER LANDING AND SHUTDOWN (FLAPS) CAUTION WOULD COME ON AND FLAPS WOULD NOT MOVE. NORMAL GROUND RESET WOULD NOT WORK. FLAP CONTROL 1 AMP C/B APPEARED TO BE (BLOWN) BUT NOT POPPED. AFTER RESETTING C/B, NORMAL FLAP RESET WOULD WORK. TRYING TO MOVE FLAPS AGAIN WOULD CAUSE THE SAME PROBLEM. NOTE THIS DEFECT WOULD ONLY OCCUR IF THE GROUND TEMP WAS -5 TO -12. AFTER WARMING THE AIRCRAFT IN A HANGAR FLAPS WOULD RESET AND WORK. UPON INSPECTION OF THE ACTUATORS IT WAS DISCOVERED THAT 3 OF THE 4 ACTUATORS WERE HEATING UP. +40 - +50 C. ACTUATORS WERE REMOVED FROM SERVICE. ALSO NOTED WAS FLAP CONTROL WARNING UNIT FAILURE CODES INCLUDED TOO HIGH CURRENT DRAW1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070530000812007053000081EU  2007       5          30         CA070310003      120070302G27529787320309      ACTUATOR                                PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  TE FLAPS        FROZEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA       2242 2242                                                      (CAN) FLAPS WOULD WORK AS NORMAL, EVEN AFTER 4 HOUR FLIGHT AT -45. AFTER LANDING AND SHUTDOWN (FLAPS) CAUTION WOULD COME ON AND FLAPS WOULD NOT MOVE. NORMAL GROUND RESET WOULD NOT WORK. FLAP CONTROL 1 AMP C/B APPEARED TO BE (BLOWN) BUT NOT POPPED. AFTER RESETTING C/B, NORMAL FLAP RESET WOULD WORK. TRYING TO MOVE FLAPS AGAIN WOULD CAUSE THE SAME PROBLEM. NOTE THIS DEFECT WOULD ONLY OCCUR IF THE GROUND TEMP WAS -5 TO -12. AFTER WARMING THE AIRCRAFT IN A HANGAR, FLAPS WOULD RESET AND WORK. UPON INSPECTION OF THE ACTUATORS IT WAS DISCOVERED THAT 3 OF THE 4 ACTUATORS WERE HEATING UP. +40 - +50 C. ACTUATORS WERE REMOVED FROM SERVICE. ALSO NOTED WAS FLAP CONTROL WARNING UNIT FAILURE CODES INCLUDED TOO HIGH CURRENT DRA1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070530000822007053000082NM  2007       5          30         CA070312001      120070220G2913                SHAFT                                   DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  HYD PUMP        SHEARED         W      D   RETURN TO BLOCK                                                                                 J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA       209548792  MX422697                                            (CAN) AFTER START OF THE NR 1 ENGINE, THE HYDRAULIC PUMP CAUTION LIGHT REMAINED ON WITH ZERO PRESSURE INDICATED ON THE ASSOCIATED HYDRAULIC SYSTEM PRESSURE GAUGE. AIRCRAFT ENGINES WERE SUBSEQUENTLY SHUTDOWN AND ENGINEERING CONTACTED TO CONDUCT DEFECT RECTIFICATION PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. ENGINEERING DEFECT INVESTIGATION REVEALED THAT THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP DRIVE SHAFT WAS SHEARED. THE HYDRAULIC PUMP WAS REPLACED WITH A SERVICEABLE ASSY IAW AMM 29-10-11 AND THE AIRCRAFT SUBSEQUENTLY RETURNED TO SERVICE.  (TC NR 20070312001)                                                                                                                                                             2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070530000832007053000083NE  2007       5          30         CA070312002      220070306G7230                BLADES                                  AIRBUS320   A320211     3930320EU  CFMINTCFM56 CFM565A1         NE                              COMPRESSOR      DAMAGED         W      A   UNSCHED LANDING                                                                                 RA PARTIAL RPM/PWR LOSS      FLAME/FIRE                                          CLCLIMB          1                      CA       4021418251                         731775                      (CAN) ON TAKEOFF AT 500 AGL, 3 TO 4 STALLS ON NR 2 ENGINE, LOUD POPPING NOISE, ATC SAW FLAMES COMING OUT. AIRCRAFT RETURNED TO DEPARTURE, ENGINE BOROSCOPE FOUND DAMAGED COMPRESSOR BLADES FROM STAGE 6 TO STAGE 9. ENGINE REMOVED FROM AIRCRAFT AND SENT TO SHOP FOR INVESTIGATION. (L-4298804) (TC NR 20070312002)                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA28NM   E29NE                
20070530000842007053000084NM  2007       5          30         CA070312003      120070312G4940360581217       STARTER                                 BOEING737   73735B      13844BMNM  GE    CFM56 CFM563B1    13802NE                              APU             FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) APU SHUTDOWN ON ITS OWN AND WOULD NOT RE-START. NEW STARTER INSTALLED. NEW STARTER BLEW APART ON FIRST START ATTEMPT. SECOND STARTER INSTALLED AND OPERATED SERVICEABLE. (TC NR 20070312003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA16WE   E2GL                 
20070530000852007053000085NM  2007       5          30         CA070312004      120070307G3810                LINE                                    BOEING767   767306      1385148NM  GE    CF6   CF680C2B6F  30025NE                              POTABLE WATER   FAILED          W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                                                                      (CAN) DURING NORMAL WALK AROUND FOUND WATER LEAKING OUT OF THE BELLY OF THE AIRCRAFT, FORWARD AREA. SUBSEQUENT INVESTIGATION FOUND CLAMSHELL (CLAMP) P/N CA62505-56BL HOLDING POTABLE WATER LINE THAT RUNS OVER FWD. E&E COMPARTMENT TOWARD THE FWD. LAVATORY FAILED RESULTING IN THE TWO EICAS COMPUTERS BEING SOAKED WITH WATER.  BOTH COMPUTERS CHANGED, CLAMP REPLACED WITH APPROVED P/N 14C33-08, METAL NOT  THE ORIGINAL PLASTIC. (TC NR 20070312004)                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA1NM    E13NE                
20070530000862007053000086EA  2007       5          30         CA070312005      120070225G52201196411         HOUSING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              ECAPE HATCH     CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       11157                                                          (CAN) CREW ESCAPE HATCH HANDLE HOUSING FOUND CRACKED AND OUTER HANDLE WAS CORRODED. THE PART OF THE HOUSING THAT FITS INSIDE OF THE INNER HANDLE WAS CRACKED COMPLETELY OFF. (TC NR 20070312005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20080219001562008021900156CE  2008       2          19         CA070312006      120070222G32301225P363        PRESSURE SWITCH             ADI7999001  BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  LANDING GEAR    MALFUNCTIONED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING LANDING GEAR SWINGS IT WAS NOTICED THAT THE LANDING GEAR PUMP WAS HESITATING. PROBLEM WAS TRACED BACK TO THE PRESSURE SWITCH. SWITCH WAS REPLACED AND GEAR SWUNG, FAULT FEE. (TC NR 20070312006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20080219001712008021900171SO  2008       2          19         CA070312007      120070303G324616102100        WHEEL HALF                              PIPER PA30  PA30        7103002SO  LYC   O320  IO320B1A    41508EA  HARTZLHCE2Y HCE2YL2     GL  LANDING GEAR    DESTROYED       W      K   NONE                                                                                            O  OTHER                                                                         NRNOT REPORTED   1                      CA       2203                                                           (CAN) SUSPECT HARD LANDING WITH SIDE MOVEMENT STRESSED WHEEL HALF CASTING. THE BACK STOP PORTION OF HUB CASTING HAS A NEW CLEAN BREAK. WITH RACE BROKEN, BEARING CONE FAILED. WHEEL ASSEMBLY TIPPED IN MOUNTING FORK AND RODE ON BRAKE CALIBER TORQUE PLATE. BRAKE DISK WORE ON INSIDE OF MOUNTING FORK. (TC NR 20070312007)                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  A1EA    1E12    5  CP9EA     
20070530000872007053000087NM  2007       5          30         CA070312008      120070222G323010134501        TORQUE LINK                             DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  LT MLG          BROKEN          W      C   ABORTED TAKEOFF                                                                                 O  OTHER                                                                         TOTAKEOFF        1                      CA       5304                                                           (CAN) DURING TAKEOFF A SEVERE VIBRATION WAS NOTICED ON THE ENTIRE AC, THE CREW ABORTED THE TAKEOFF SUCCESSFULLY. MAINTENANCE FOUND THE LT MLG TORQUE LINK BROKE INTO 2 PARTS ALONG WITH DAMAGE TO LT IB AND LT OB TIRES, BRAKE UNITS NR 1 AND 2, WIRING AND BRAKE LINES, AND STRUCTURE DAMAGE TO THE NACELLE. MFG TO CARRY OUT INVESTIGATION AS TO THE CAUSE OF TORQUE LINK FAILURE.  (TC NR 20070312008)                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080219001872008021900187SO  2008       2          19         CA070312009      120070220G2420587857          ALTERNATOR                              PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  LEFT            FAILED          W      O   OTHER                                                                                           HP ELECT. POWER LOSS-50 PC   NO WARNING INDICATION                               CRCRUISE         1                      CA                                                                      (CAN) LT ALTERNATOR FAILED AT CRUISE, FAULT-FIELD POWER FUSE BLOWER.  RT ALTERNATOR FAILED/NOT ON LINE, FAULT, BAD ALTERNATOR MASTER SWITCH OR NOT ON.  RT INOP ALTERNATOR SWITCH/RELAY FAILED SO NO COCKPIT INOP LIGHT.  AC CONTINUED FLIGHT ON BATTERY POWER TO DESTINATION.  FLIGHT AT NIGHT -30C AND IFR CONDITIONS.  CONCLUSIONS/RECTIFICATIONS:  LT FIELD FUSE REPLACED. RT ALTERNATOR INOP SWITCH REPLACED. ALTERNATOR MASTER SWITCH CLEANED/TESTED.  BATTERY CHARGED AND TESTED.  AC AND ALTERNATOR SYS OPS CHECKED AND AC RETURNED TO SERVICE. (TC NR 20070312009)                                                                                                                                                                     1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070530000882007053000088EA  2007       5          30         CA070312010      220070307G7320                COTTER PIN      HONEYWELL               BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  FUEL CONTROL    MISINSTALLED    W      E   ENGINE SHUTDOWN                                                                                 W  INADEQUATE Q C                                                                DEDESCENT        1                      CA            2504  A63002                                              (CAN) ON DESCENT FROM 21000 FEET, THE RT POWER LEVER WAS PULLED BACK BUT THE ENGINE DID NOT RESPOND TO THE COMMAND. ENGINE WAS THEN SHUTDOWN TO PREVENT OVERTORQUING.   ON INSPECTION OF FCU LINKAGES, MECHANICS FOUND THE COTTER PIN GOING THROUGH INPUT SHAFT AFT OF MAX STOP ARM HAD ONLY ONE LEG BENT OVER.  OTHER LEG, IN CERTAIN POSITIONS WOULD HANG UP ON MIN STOP SCREW, PREVENTING FCU ARM FROM RETURNING TO IDLE.  COTTER PIN WAS PROPERLY SECURED AND AIRCRAFT WAS TEST FLOWN WITH NO FURTHER INCIDENTS. (TC NR 20070312010)                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070530000892007053000089EA  2007       5          30         CA070313001      220070312G8530LW16812         LIFTER                                  CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA  MCAULY1C160 1C160DTM    GL  INTAKE          UNLOCKED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1778 1778                          RL326476T                   (CAN) DURING THE REAMING OF A STICKY EXHAUST VALVE GUIDE IN CYLINDER NR 4, IT WAS FOUND THAT THE NR 4 CYLINDER INTAKE HYDRAULIC LIFTER HAD LOST ITS SNAP RING.  THE WEAR PATTERN SHOWED THAT THE SNAP RING HAD MIGRATED ALONG BETWEEN THE PUSHROD AND THE SHROUD TUBE (THE SNAP RING SHOWED WEAR ON ITS INSIDE DIAMETER WERE IT HAD MOVED ALONG THE PUSHROD, AND WEAR ON ITS OUTSIDE DIAMETER, WHERE IT HAD WORN ALONG THE INSIDE OF THE PUSHROD SHROUD TUBE). THE SNAP RING WAS FOUND INTACT (SAME SHAPE), IN THE NR 4 CYLINDER ROCKER BOX.  ONE EXPLANATION IS THAT WHEN THE CYLINDER WAS CHANGED 525.0 HRS PREVIOUS, THE SNAP RING WAS NOT PROPERLY INSTALLED IN THE HYDRAULIC LIFTER WHEN IT WAS BLED DOWN BEFORE INSTALLATION, AND IT POPPE1H71 3O3  ONT3A12    E274    5  NP910     
20070530000902007053000090    2007       5          30         CA070313002      420070312G611305503214        BULKHEAD        CESSNA                  CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA  MCAULY1C160 1C160DTM    GL  SPINNER         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       373                                                            (CAN) THIS AIRCRAFT HAS HAD ALL THE AFT BULKHEAD AND HEAVIER SPINNER UPGRADES AND HAS HAD IT ALL ASSEMBLED IAW THE LATEST SB. CRACKS WERE FOUND FORMING PARALLEL FROM THE PROP BOLT HEAD CONTACT SURFACE ON (3) OF THE (6) HOLES. YOU HAVE TO LOOK VERY CAREFULLY AS THE CRACKS RADIATING FROM THE PROP BOLT HOLES ARE VERY FINE AND HIDE UNDER THE FACTORY PRIMER.  THE TORQUE OF THE PROP BOLTS IS SHEAR STRESSING THE BULKHEAD. A COVER PLATE IS NEEDED TO OFFSET THE BOLTS FROM THE THIN ALUMINUM SHEET METAL BULKHEAD. THIS PROBLEM IS RE-OCCURRING WITH THIS SPINNER ASSY ON SEVERAL OF OUR AC THAT WE MAINTAIN. (TC NR 20070313002)                                                                                                      1H71 3O3  ONT3A12    E274    5  NP910     
20070601001172007060100117EU  2007       6          1          CA070313003      120070312G33208ES00375200     POWER SUPPLY                            AIRBUS310   A310300     3930305EU  GE    CF6   CF680C2*         GL                              CABIN LIGHTS    OVERHEATED      W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE, FLIGHT CREW OBSERVED WHAT APPEARED TO BE WHITE SMOKE EMANATING FROM READING LIGHT (PSU) PANEL ASSEMBLY ABOVE SEAT 30 AB. CREW SWITCHED OFF READING LIGHTS AND SMOKE STOPPED. ON ARRIVAL TO THE STATION, MAINTENANCE FOUND ONE TRANSFORMER PRINTED CIRCUIT BORD SEVERELY OVERHEATED. POWER SUPPLY REPLACED AND SYSTEM TESTED SERVICEABLE.   (TC NR 20070313003)                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA35EU   E23EA                
20070601001182007060100118NM  2007       6          1          CA070313004      120070313G3230                LANDING GEAR                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NOSE            INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA                                                                      (CAN) DURING APPROACH TO BASE, THE NLG DOORS DID NOT OPEN AND THE NLG DID NOT EXTEND.  APPROACH CANCELLED, AIRCRAFT ENTERED HOLDING PATTERN. GEAR CYCLED WITHOUT SUCCESS NLG EXTENSION. MLG OPERATED NORMALLY. ALTERNATE EXTENSION PROCEDURE CONDUCTED. NLG REMAINED RETRACTED AND NLG DOORS REMAINED CLOSED. AIRCRAFT PERFORMED A TOUCH AND GO TO SHOCK THE NLG DOWN, WITHOUT SUCCESS.  AIRCRAFT CONDUCTED A 60-DEGREE BANK TO APPLY POSITIVE G IN AN EFFORT TO EXTEND THE NLG WITHOUT SUCCESS. AIRCRAFT LANDED WITH NLG RETRACTED.  TO COMPLETE FULL INVESTIGATION. AOM NR 210 ISSUED. (TC NR 20070313004)                                                                                                                                    2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070601001192007060100119CE  2007       6          1          CA070313005      120070312G534005521335        SUPPORT                                 CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160DTM    GL  LANDING LIGHT   CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2647                                                           (CAN) THE SUPPORT WAS CRACKING AT THE MOUNTING FLANGE BEND RADII AT THE (4) AND (8) O`CLOCK POSITIONS. THE CRACKS HAD PREVIOUSLY BEEN STOPDRILLED BUT HAD CONTINUED PAST THE STOPDRILLING.  SUSPECT THAT CRACKING STARTS AT SHARP/ROUGH ALUMINUM EDGES AND IS AGGRAVATED BY THE PROPELLERS PROXIMITY CAUSING PULSATION AGAINST THE LIGHT. (TC NR 20070313005)                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    E274    5  NP910     
20070601001202007060100120EA  2007       6          1          CA070313006      220070308G852013F1773585      CRANKSHAFT                              RKWELL700   700         7630520SW  LYC   O540  TIO540R2AD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          BROKEN          W      E   ENGINE SHUTDOWN                                                                                 EJ VIBRATION/BUFFET          WARNING INDICATION                                  CRCRUISE         1                      CA            1289                          RL352361A                   (CAN) APPROXIMATELY 45 MILES OUT, THE CREW NOTED A VIBRATION FROM THE LT ENGINE. THE CREW SECURED THE ENGINE AND FEATHERED THE PROP IAW THE CHECK LIST.  THE FLIGHT CONTINUED TO DESTINATION WITHOUT INCIDENT.   WITH COWLINGS REMOVED,  NOTED THE CASE HAD BEEN BREACHED AND THE CAMSHAFT HAD BROKEN.  WITH NR 5 CYL. REMOVED WE COULD SEE THAT THE CRANKSHAFT WAS BROKEN AFT OF THE MAIN BEARING BETWEEN CYLINDER BANKS 2-4 AND 5-6.  THIS PERMITTED THE CRANK SEGMENT WITH CONNECTING RODS FOR CYL`S 5 AND 6 TO FLAIL AROUND, BREAKING THE CRANKCASE AND CAMSHAFT.   THE ENGINE WILL BE SENT OUT FOR FURTHER TEARDOWN. PARTS AVAILABLE FOR INSPECTION. (TC NR 20070313006)                                                                  1L72 3O3  O  A12SW   E14EA   5  CP33EA    
20070601001212007060100121NE  2007       6          1          CA070313008      220070313G75303024606         FITTING                                 AIRTRCAT802 AT802       0390305SW  PWA   PT6   PT6A67A     52043NE  HARTZLHCB5M HCB5MA3     GL  ENGINE          CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1761                               PCE107017                   (CAN) UPON INSPECTION OF THE P3 AIR LINES, IT WAS DISCOVERED THAT THERE WAS NO CLEARANCE BETWEEN THE P3 FILTER HOUSING NIPPLE FITTING (P/N 3024606) AND THE ENGINE REAR FIRE SEAL PLATES (P/N 3031003 AND 3031004).  UPON REPOSITIONING OF THE FIRE SEAL PLATES, IT WAS DISCOVERED THAT THE PLATES HAD CHAFED INTO THE NIPPLE FITTING APPROXIMATELY 0.020 INCH. THE FITTING WAS REMOVED AND REPLACED.  THE OTHER AIRCRAFT IN OUR FLEET WERE INSPECTED WITH NO OTHER DEFECTS NOTED. (TC NR 20070313008)                                                                                                                                                                                                                                          1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20080219001942008021900194SW  2008       2          19         CA070313009      120070313G5411804501          FRAME                                   AIRTRCAT802 AT802A      0390308SW  PWA   PT6   PT6A65AG    52043NE  HARTZLHCB5M HCB5MA3     GL  FIREGATE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       568                                                            (CAN) DURING ANNUAL INSPECTION, THE LOWER LONGITUDINAL FRAME OF THE STAINLESS STEEL FIREGATE P/N 80450-1 WAS NOTED TO BE CRACKED AT THE FWD END AND BULGED AT THE AFT END.  (2) OTHER AC HAVE SIMILAR DAMAGE. WATER WAS FOUND IN THE TUBE AND THE DAMAGE APPEARS TO BE CAUSED BY WATER FREEZING. (TC NR 20070313009)                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3T4  TNCA19SW   E4EA    6  CP44GL    
20080129000132008012900013SO  2008       1          29         CA070314001      120070314G3233WTC21151        ACTUATOR                                PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  MLG             BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ACTUATOR BROKEN, FOUND DURING REPAIRS TO AIRCRAFT. (TC NR 20070314001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070601001222007060100122EA  2007       6          1          CA070314002      220070117G7200                ENGINE                                  BEECH 1900  1900D       1154162CE  PWA   PT6   PT6*        52043EA                                              MAKING METAL    W      E   ENGINE SHUTDOWN                                                                                 A  FLAME/FIRE                                                                    CLCLIMB          1                      CA                                          114390                      (CAN) ON CLIMB FOLLOWING TAKE-OFF, FLAMES WERE SEEN EXITING THE ENGINE EXHAUST ACCOMPANIED BY A LOUD NOISE.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL AND ROTOR SEIZURE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314002)                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T3  TRTA24CE   E2NE                 
20070601001232007060100123NE  2007       6          1          CA070314004      220070125G7321311717804       FUEL CONTROL                            AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                                              UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  APAPPROACH       1                      CA       9077                                                           (CAN) ON APPROACH, ENGINE TORQUE FELL TO ZERO WHEN POWER LEVER WAS RETARDED. SUBSQUENT THROTTLE INPUT RESULTED IN TORQUE FLUCTUATION AND THE ENGINE WAS SUBSEQUENTLY SHUTDOWN IN FLIGHT.  TROUBLESHOOTING LED TO REPLACEMENT OF THE ENGINE FUEL CONTROL UNIT. (TC NR 20070314004)                                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4T4  TRT        E20NE                
20070601001242007060100124WP  2007       6          1          CA070314005      220070217G7200FE73121C        ENGINE                                  AMD   FALC10FALCON10    2730101EU  GARRTTTFE731TFE7312     01518WP                              NR 1            VIBRATION       W      E   ENGINE SHUTDOWN                                                                                 EJ VIBRATION/BUFFET          WARNING INDICATION                                  CRCRUISE         1                      CA                                          P73114                      (CAN)  NR1 ENGINE FAILED, TEMPERATURE SPIKE ABOVE 1000 DEGREES C. AS VIBRATION INCREASED, THEN INDICATIONS (ITT, FIFY N2) DECREASED. N1 TURNED, SECURITY, PULLED FIRE HANDLE.  ON ARRIVAL, COULD NOT TURN N1, FOUND OIL AND METAL PIECES IN EXHAUST, ENGINE REMOVED FROM AIRCRAFT.  PRIOR OIL ANALYSIS WERE NORMAL (16 DEC.2006 AND 21 SEPT, 2005).  NO METAL ON MAG PLUG.  A FEW SLIVERS IN FILTER.  (TC NR 20070314005)                                                                                                                                                                                                                                                                                                                       2L72 4F4  F  A33EU   E6WE                 
20080131000142008013100014SO  2008       1          31         CA070314006      120070307G5720                STRUCTURE                               PIPER PA28  PA28140     7102802SO  LYC   O320  O320E3D     41508EA  SNSNCH74D   74DM        EA  RT WING ROOT    CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       8000                                                           (CAN) RT FORWARD WING WALK ASSEMBLY, P/N 62061-002. RT ROOT WAS CRACKED. (TC NR 20070314006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3O3  O  2A13    E274    5  NP88614   
20070613001232007061300123EU  2007       6          13         CA070314007      120070130G7930310595801       RELIEF VALVE                            AEROSPATR42 ATR42500    8680948EU  PWA   PW120 PW127            NE                              ENGINE OIL      UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB THE ENGINE LOW OIL PRESSURE WARNING ACTIVATED AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION LED TO REPLACEMENT OF THE ENGINE COLD-OIL PRESSURE RELIEF VALVE. (TC NR 20070314007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA53EU   E20NE                
20070601001252007060100125EU  2007       6          1          CA070314008      120070313G27529787320309      ACTUATOR                                PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  TE FLAPS        FROZEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA       2259 2259                                                      (CAN) FLAP ACTUATOR WOULD TEMPORARILY FREEZE/SEIZE AT THE END OF A FLIGHT WHILE WAITING ON THE GROUND AT OAT-5-12C. AFTER WARMING A/C, FLAPS WOULD RESET AND FUNCTION NORMALLY. ACTUATOR REMOVED FROM SERVICE.  FLAP WARNING UNIT FAILURE CODES INDICATED HIGH CURRENT DRAW. FLAPS SYSTEM TESTED WITHIN CURRENT DRAW LIMITS AFTER REPLACEMENT OF ACTUATOR. MFG TECH REP HAS REQUESTED TEARDOWN REPORTS. (TC NR 20070314008)                                                                                                                                                                                                                                                                                                                     1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070613001242007061300124EA  2007       6          13         CA070314009      220070129G7200                ENGINE                                  PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A6       52043EA                                              FLAMED OUT      W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                          103238                      (CAN) DURING ATTITUDE RECOVERY TRAINING, THE ENGINE FLAMED OUT.  THE ENGINE WAS SUCCESSFULLY RE-STARTED IN FLIGHT BUT SUFFERED AN OVER TEMPERATURE DURING THE RE-LIGHT.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3T3  TRTA78EU   E4EA                 
20070601001262007060100126EU  2007       6          1          CA070314010      120070313G2752                ROD END                                 PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  ACTUATOR        LOOSE           W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA            17                                                        (CAN) ROD END WAS FOUND LOOSE/WORN OUT ON OVERHAULED ACTUATOR. TEMPORARILY INSTALLED IN AIRCRAFT WHILE AWAITING REPLACEMENT. REMOVED WITH 16.8 HRS TSO BEFORE RETURNING TO SUPPLIER. (TC NR 20070314010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070613001252007061300125NE  2007       6          13         CA070314011      220070208G7260                SHAFT                                   DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE                              ACCESSORY DRIVE DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          CRCRUISE         1                      CA                                          12383                       (CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION IN CRUISE AND WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED ACCESSORY DRIVE TOWER SHAFT DAMAGE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070314011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E20NE                
20070615001882007061500188NE  2007       6          15         CA070314012      220070213G7261PW545B          ENGINE                                  CESSNA500   560CESSNA   2076750CE  PWC   545   PW545B           NE                                              OIL CONSUMPTION W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          DD0351                      (CAN) THE ENGINE LOW-OIL-PRESSURE WARNING ACTIVATED IN FLIGHT.  SUBSEQUENT INVESTIGATION REVEALED HIGH OIL CONSUMPTION.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA22CE   E00059EN             
20070613001262007061300126NE  2007       6          13         CA070314013      220070213G7250                BLADES                                  AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE                              POWER TURBINE   DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                          121276                      (CAN) DURING CLIMB, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN POWER.  THE ENGINE WAS SHUTDOWN IN FLIGHT.   GROUND INSPECTION REVEALED A SEIZED PROPELLER AND DAMAGED POWER TURBINE BLADES.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC  20070314013)                                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA53EU   E20NE                
20070613001272007061300127NE  2007       6          13         CA070314014      220070202G7230                COMPRESSOR                              BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                              ENGINE          SEIZED          W      E   ENGINE SHUTDOWN                                                                                 A  FLAME/FIRE                                                                    CRCRUISE         1                      CA                                          114109                      (CAN) FLAMES WERE SEEN EXITING THE ENGINE EXHAUST AND THE ENGINE WAS SHUT DOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED COMPRESSOR SEIZURE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4T4  TRTA24CE   E26NE                
20070613001282007061300128NE  2007       6          13         CA070314015      220070210G7250                TURBINE BLADES                          AEROSPATR72 ATR72              EU  PWA   PW120 PW124B           NE                              ENGINE          DAMAGED         W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CLCLIMB          1                      CA                                          124662                      (CAN) THE ENGINE FLAMED OUT OUT FOLLOWING TAKEOFF.  SUBSEQUENT INSPECTION REVEALED DAMAGED POWER TURBINE BLADES AND METAL DEBRIS IN THE ENGINE OIL SYSTEM.   MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314015)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRT        E2ONE                
20070613001292007061300129NE  2007       6          13         CA070314016      220070215G7200                ENGINE                                  BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                                              VIBRATION       W      E   ENGINE SHUTDOWN                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA                                          100180                      (CAN) ENGINE EXHIBITED HEAVY VIBRATION DURING CRUISE AND WAS SHUTDOWN IN FLIGHT.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070314016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4F4  FRTA16SW   E25EA                
20070601001272007060100127NM  2007       6          1          CA070314017      120070312G49004503067A        APU                                     BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  APU BAY         MALFUNCTIONED   W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) CREW MADE A NORMAL APU START REQUEST, A FEW SECONDS LATER HEARD A LOUD BANG AND GOT THE APU FAIL ADVISORY LIGHT. APU ENCLOSURE SUFFERED STRUCTURAL DAMAGE AFTER FUEL VAPOR IGNITED. NO FIRE LIGHT OR FIRE NOTED.  EXAMINATION OF APU COMPARTMENT AREA REVEALED THAT APU ACCESS DOORS DEPARTED THE TAILCONE. TAIL CONE TO BE REPLACED.  (TC NR 20070314017)                                                                                                                                                                                                                                                                                                                                                                                2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070613001302007061300130NE  2007       6          13         CA070314018      220070216G7230                ACTUATOR                                GULSTM200   200         4500308NM  PWC   PW306 PW306A      52165NE                              INLET GUIDE VANEFAILED          W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) ON APPLICATION OF POWER IN CLIMB, THE ENGINE EXPERIENCED A COMPRESSOR STALL ACCOMPANIED BY AN UNCOMMANDED POWER REDUCTION, PARAMETER FLUCTUATIONS AND A FADEC FAULT INDICATION.  SUBSEQUENT INVESTIGATION LED TO REPLACEMENT OF THE ENGINE INLET GUIDE VANE ACTUATOR. (TC NR 20070314018)                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA53NM   E35NE                
20070613001312007061300131NE  2007       6          13         CA070314019      220070216G73103033981         LINE                                    PIPER PA46  PA46500TP   7104622SO  PWA   PT6   PT6A42      52043NE                              FCU             FRACTURED       W      O   OTHER                                                                                           RXJPARTIAL RPM/PWR LOSS      ENGINE FLAMEOUT           WARNING INDICATION        CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION IN FLIGHT AND FLAMED OUT ON LANDING ROLL-OUT.   SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL DELIVERY TUBE. (TC NR 20070314019)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 3O4  TRTA25SO   E4EA                 
20070613001322007061300132EA  2007       6          13         CA070314020      220070122G7250                TURBINE BLADES                          AGUSTAA109  A119        0261102EU  PWA   PT6T  PT6T3       52045EA                              ENGINE          FRACTURED       W      E   ENGINE SHUTDOWN                                                                                 O  OTHER                                                                         LDLANDING        1                      CA                                          TH0727                      (CAN) ON LANDING FOLLOWING A TRAINING FLIGHT, THE ENGINE EMITTED A LOUD NOISE.  SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES.   MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314020)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G72 3U4  U  H7EU    E22EA                
20070613001332007061300133NE  2007       6          13         CA070314021      220070223G7200                ENGINE                                  RAYTHN36    G36         7150061CE  PWA   PT6   PT6A68           NE                                              MAKING METAL    W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) DURING A TRAINING MISSION, THE ENGINE EXPERIENCED AN UNCOMMANDED REDUCTION IN POWER ACCOMPANIED BY A NOISE AND A CHIP DETECTOR INDICATION.  SUBSEQUENT INSPECTION REVEALED METALLIC DEBRIS IN THE ENGINE OIL SYSTEM.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314021)                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O4  TRT3A15    E26NE                
20070613001342007061300134NE  2007       6          13         CA070314022      220070222G7200                ENGINE                                  AYRES S2    S2RHGT65    0970110SO  PWA   PT6   PT6A65AG    52043NE                                              FLAMED OUT      W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE WAS REPORTED TO HAVE FLAMED OUT IN FLIGHT.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070314022)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3T4  TNC        E4EA                 
20070601001282007060100128EU  2007       6          1          CA070315001      120070306G3000                HEATER                                  AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE                              CCAS PROBE      FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) DEPARTING, THE CREW OBSERVED A STICK PUSHER/ STICK SHAKER FAULT. AFTER A FAILED, RESET THE AIRCRAFT, RETURNED TO POINT OF DEPARTURE WITH OUT FURTHER PROBLEM. MAINTENANCE VERIFIED THE NR 1 CCAS ALPHA PROBE HEAT FUNCTION HAD FAILED. THE PROBE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE (TC NR 20070315001)                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRTA53EU   E20NE                
20070601001292007060100129EA  2007       6          1          CA070315002      120070313G3320BB100200258     SOCKET                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              CABIN LIGHTS    BURNED          W      HK  DEACTIVATE SYST/CIRCUITSNONE                                                                    B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                                                                      (CAN) REF LOG PAGE NR 593976. F/A REPORTS ELECTRICAL SMELL IN FORWARD CABIN, AROUND ROW 2 AND 3. 4FD SIDEWALL LIGHT HOLDER FOUND AT FAULT, CBP2 C/B S5 OPENED AND SECURED.  SIDEWALL LIGHT INOP, DEFERRED IAW MEL 33-21-01 CAT (C). SOCKET ASSY P/N BB1-0020-02-58 (TC NR 20070315002)                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20070604000032007060400003EU  2007       6          4          CA070315003      120070310G3297                CONNECTOR                               AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE                              MLG             UNSECURE        W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) DEPARTING, THE CREW OBSERVED A FAIL TO RETRACT INDICATION ON THE RT MAIN LANDING GEAR. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM.  MAINTENANCE FOUND A CONNECTOR IN THE INDICATION SIGNAL HARNESS WITH A CONNECTOR NOT FULLY LOCKED. THE CONNECTOR WAS SECURED SYSTEM INTEGRITY VERIFIED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070315003)                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA53EU   E20NE                
20070604000042007060400004    2007       6          4          CA070315004      420070312G34107004544713      HSI                                     AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE                              NR 1            MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) DEPARTING THE CREW OBSERVED A CIRCUIT BREAKER TRIP ON THE NR 1 EADI, RESET SUCCESSFUL. THIS WAS FOLLOWED BY A CIRCUIT BREAKER TRIP ON THE NR 1 EHSI. THE RESET ATTEMPT FAILED AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE NR 1 SYMBOL GENERATOR UNIT.  THE SYSTEM FUNCTION CHECKED SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070315004)                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA53EU   E20NE                
20070604000052007060400005NM  2007       6          4          CA070315005      120070215G324629685           BEARING                                 BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NR 4 MAIN WHEEL DAMAGED         W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AFTER LANDING, A PIECE OF NR4 BRAKE DISK WAS FOUND AT THE SPOT WHERE THE A/C WAS PARKED. A/C WAS INSPECTED AND THE FOLLOWING ARE REPORTED. FOUND DAMAGE AT INNER BEARING AFTER THE INSPECTION WITH NR 4 WHEEL ASSEMBLY WAS REMOVED. WHEEL BRAKE AND AXLE ASSYS REPLACED. (TC NR                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080131000152008013100015EU  2008       1          31         CA070316001      120070315G6340MS2771923       SWITCH                                  SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              LOW ROTOR       INTERMITTENT    W      K   NONE                                                                                            N  FALSE WARNING                                                                 ININSP/MAINT     1                      CA       8171                                                           (CAN) LOW ROTOR HORN NOT WORKING BUT LIGHT ON 4ALPHA PANEL WOULD COME ON.  SYSTEM TROUBLESHOT AND FOUND SWITCH TO BE INTERMITENT.  A/C GROUNDED TILL NEW SWITCH HAD BEEN REPLACED. THE POTENTIAL FOR GIVING A FALSE READ TO THE PILOT DURING FLIGHT MAY HAVE OCCURED.  AIRCRAFT WAS GROUNDED. SWITCH HAS BEEN REPACED AND A/C RETURN TO SERVICE. (TC NR 20070316001)                                                                                                                                                                                                                                                                                                                                                                            1G71 3U3  U  H9EU    E19EU                
20080131000162008013100016SW  2008       1          31         CA070316002      120070316G3610                LINE                                    AIRTRCAT802 AT802       0390305SW  PWA   PT6   PT6A67A     52043NE  HARTZLHCB5M HCB5MA3     GL  BLEED AIR       BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1437                                                           (CAN) DURING ANNUAL INSPECTION, THE BLEED AIR LINE FOR THE CABIN HEATER WAS FOUND UNSECURED UNDER THE COCKPIT FLOOR. FURTHER INVESTIGATION FOUND THE MUFFLER FOR THE LINE BROKEN IN (2) PIECES AT THE FWD END. THE PARTS WERE REPLACED. THE REMAINING AIRCRAFT IN THE FLEET WERE INSPECTED. ONE ADDITIONAL AIRCRAFT WAS FOUND WITH THE SAME DEFECT. THE PARTS WERE REPLACED WITH SERVICEABLE UNITS. (TC# 20070316002)                                                                                                                                                                                                                                                                                                                           1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20080201000992008020100099CE  2008       2          1          CA070316003      120070313G7714MS250384        TACH GENERATOR                          BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL                  FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) N1 TACH GENERATOR FAILED IN FLIGHT. (TC NR 20070316003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070613001362007061300136EA  2007       6          13         CA070316004      220070212G7322                CARBURETOR                              CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  ENGINE          OUT OF ADJUST   W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      CA            455                                                       (CAN) ENGINE WAS RUNNING ROUGH, UNABLE TO ADJUST IDLE ON CARBURETOR.  ENGINE WANTED TO SHUTDOWN ON APPROACH WHEN THROTTLE WAS RETARDED. (TC NR 20070316004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  ONT3A19    E223    5  NP50GL    
20070604000062007060400006EU  2007       6          4          CA070319001      120070312G2140BAS30198        PRESSURE SWITCH                         BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R408  CR4086123F17EU  HEATER          MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) DURING DEPARTURE THE AIRCRAFT`S HEATER FAILED AND THE CREW WAS UNABLE TO RESTART THE HEATER. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE HEATER PRESSURE SWITCH AND THE AIRCRAFT RETURNED TO SERVICE AFTER SATIFACTORY GROUND CHECK. (TC NR 20070319001)                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 3T4  T  A24EU   A196    6  CP17BO    
20070604000072007060400007NE  2007       6          4          CA070319004      220070316G7310263451          DUMP VALVE                              DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF15      NE  FLOW DIVIDER    LEAKING         W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA       4065 1179                                                      (CAN) AFTER TAKEOFF DURING CLIMB, NR1 ENGINE LOST POWER AND TRQ ROLL BACK, CREW ELECTED TO SHUT ENGINE DOWN AND RETURN TO DEPARTURE AIRPORT. MAINTENANCE INSPECTION FOUND FUEL SUPPLY LINE TO FLOW DIVIDER/DUMP VALVE (B-NUT) NOT LOCKWIRED AND BACKED OFF, ALLOWING HIGH PRESSURE FUEL LEAK. O-RINGS REPLACED, FUEL LINE (B-NUT) TIGHTENED AND LOCKWIRED. ENGINE RUNS CARRIED OUT, AIRCRAFT RETURNED TO SERVICE. (TC NR 20070319004)                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070604000082007060400008WP  2007       6          4          CA070319005      220070316G72308934825         IMPELLER                                FRCHLDSA227 SA227CC     3377522SW  GARRTTTPE331TPE33111U   01514WP  MCAULY4HFR344HFR34C652  NE  ENGINE          FRACTURED       W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA       2065020650                         P44721C                     (CAN) ENGINE WAS REMOVED DUE TO NOT MAKING TARGET TAKEOFF TORQUE.  UPON DISASSEMBLY THE 2ND STAGE COMPRESSOR IMPELLER FAILED AND HAS EXPERIENCED A FATIGUE TYPE FAILURE. THE PRESENT TIME ON THE IMPELLER IS 20,650.2 HOURS AND 28,175 CYCLES.  A LARGE PIECE OF THE LEADING EDGE BROKE OFF AND WAS DISCOVERED FURTHER DOWN IN THE ENGINE.  IT HAS BEEN RETAINED.  IT HAS EXTENSIVE DAMAGE DUE TO SECONDARY IMPACT DAMAGE.  NO RUB DAMAGE, AS WOULD TYPICALLY CAUSE A PROBLEM, FOR THE IMPELLER WAS FOUND SUGGESTING THAT THE COMPRESSOR WAS BUILT PROPERLY. THE DAMAGE NOTED IN PHOTOGRAPH IS BELIEVED TO BE SECONDARY RUB DAMAGE DUE TO THE CRACKED PIECE GETTING LODGED BETWEEN THE SHROUD AND THE IMPELLER.  ALL DIMENSIONS FOR ENGINE SHIMM2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20070604000092007060400009EA  2007       6          4          CA070319006      220070314G853077672           TAPPET                                  BEECH 60    B60         1153605CE  LYC   O541  TIO541E1C4  41536EA  HARTZLHCF3Y HCF3YR2     GL  ENGINE          SPALLED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       443                                                            (CAN) ENGINE MODIFIED IAW FIREWALL FORWARD CENTRILUBE STC. PREVIOUS EXPERIENCE WITH THIS ENGINE SERIES PROMPTS REGULAR TAPPET INSPECTIONS. TAPPETS INSPECTED AND SPALLING WAS FOUND, EVEN ON THIS STC`D ENGINE.  TAPPETS SENT TO FIREWALL FORWARD FOR EXAMINATION, AND ONLY 3 OF THE 12 TAPPETS WERE JUDGED REUSABLE.  THIS TAPPET-BODY MANUFACTURING PROCESS HAS BEEN HIGHLY SUSPECT FOR MANY YEARS BY THIS SUBMITTER. (TC NR 20070319006)                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A12CE   E10EA   5  CP31EA    
20070604000102007060400010EA  2007       6          4          CA070319008      220070315G8520                CAMSHAFT                                PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            136                           L521861A                    (CAN) THIS ENGINE WAS JUST PUT ON WING TO REPLACE AN ENGINE THAT HAD CAMSHAFT WEAR. DURING A ROUTINE INSPECTION THE OIL WAS DRAINED AND A SUBSTANTIAL AMOUNT OF FERROUS METAL WAS DISCOVERED IN THE FILTER. AN OIL SAMPLE WAS SENT IMMEDIATELY TO PROGRESSIVE FOR ANALYSIS. THEY REPORTED BACK THAT IT WAS THE CAMSHAFT FAILING. WE ARE SENDING THE ENGINE TO THEM FOR TEARDOWN AND WILL NOT KNOW UNTIL THEN WHETHER IT IS AN OPERATIONAL PROBLEM OR A COMPONENT PROBLEM. (TC NR 20070319008)                                                                                                                                                                                                                                                   1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070604000112007060400011NM  2007       6          4          CA070319009      120070209G3297                WIRE HARNESS                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NLG WOW         DAMAGED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKE OFF, ALL THREE GEAR FAILED TO RETRACT. (3) RED AND (3) GREEN LIGHTS REMAINED ILLUMINATED.  RAN CHECKLIST, NO HELP.  HANDLE DID ILLUMINATE AMBER. FLIGHT WAS DIVERTED BACK TO BASE.  MAINTENANCE REMOVED AND REPLACED NLG WOW 2 CENTERING WIRING HARNESS. (TC NR 20070319009)                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070604000122007060400012NM  2007       6          4          CA070320001      120070207G561080260006        WINDSHIELD                              BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       12216                                                          (CAN) RT WINDSHIELD SPIDER WEBBED AT 24,000 FT CRUISE. WINDSHIELD HEAT ON. NO CAUTION LIGHTS. FLIGHT WAS DIVERTED BACK TO BASE. MAINTENANCE REPLACED RT WINDSHIELD IAW AMM 56-10-01. (TC NR 20070320001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070604000132007060400013NE  2007       6          4          CA070320002      220070317G73133038589         STUD                                    CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  FUEL NOZZLE     LOOSE           W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       349  349                           PCEPC0700                   (CAN) DURING FIRST FUEL NOZZLE INSPECTION FROM OVERHAUL -9 OF 28 FUEL NOZZLE STUDS WERE REMOVED WITH NUTS ON STUDS P/N 3038589.  HAVE A CODE H19 STAMPED ON THE END -DURING A PHONE CONVERSATION WITH AN EMPLOYEE AT MFG, THEY INDICATED THAT OVERSIZED STUDS WERE PROBABLY NOT USED AT THE OVERHAUL. MFG ACKNOWLEDGED THE PROBLEM, AND ARE INTERNALLY LOOKING INTO IT, AND PROVIDING THE PROPER HARDWARE TO BE INSTALLED. (TC NR 20070320002)                                                                                                                                                                                                                                                                                                  1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20070604000142007060400014EA  2007       6          4          CA070320003      120070317G2120X8905           MANIFOLD                                CNDAIRCL600 CL6002B19   1900309EA                                                               CABIN AIR       SPLIT           W      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                CRCRUISE         1                      CA                                                                      (CAN)  A/C IS UNDERGOING MODIFICATION TO FREIGHTER CONFIGURATION,AND WAS BEING TEST FLOWN FOR COLLECTING CABIN VENTILATION SYSTEM PRESSURES, UNDER VARIOUS OPERATIONAL CONDITIONS.THE A/C WAS CONFIGURED FOR THE TEST; SPECIFICALLY (2) TEST PORTS WERE FITTED TO THE A/C VENTILATION SYSTEM DUCTING TO MEASURE DUCT PRESSURE IN FLIGHT. THE DUCT PRESSURES WERE MEASURED SUCCESSFULLY UNDER SEVERAL OPERATING CONDITIONS, BUT IT WAS NOTED THAT THE DISTRIBUTION MAIN FEED MANIFOLD WOULD NOT WITHSTAND THE PRESSURE FROM THE PACK FLOW, WITH MAX CLIMB POWER APPLIED. THE FLIGHT WAS CONCLUDED AND THE A/C RETURNED UNEVENTFULLY. UPON INSPECTION OF THE SYSTEM,THE THE MAINFEED MANIFOLD WAS FOUND TO HAVE A SPLIT AT ONE OF THE JOINTS.  (TC2L72 4F    RTA21EA                        
20070604000162007060400016EA  2007       6          4          CA070320005      120070319G7830                THRUST REVERSER                         CNDAIRCL600 CL600*      1900302EA  GE    CF34  CF348C1          NE                                              UNKNOWN         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                                                      (CAN) AFTER TAKEOFF AND CLIMBING THROUGH 25000 FEET, CREW RECEIVED RED THRUSTER REVERSER ICON IN THEIR N1 GAUGE. SHORTLY THEREAFTER CREW RECEIVED REVERSER STATUS MESSAGE. AFTER DISCUSSION WITH MTC, ELECTED TO RETURN TO DEPARTURE TO LOCK OUT THRUST REVERSER. THRUST REVERSER DEFERRED IAW MEL 78-30-01 WILL PROVIDE MORE INFORMATION WHEN IT BECOMES AVAILABLE.  WITH THE SUPPORT OF MFG WE HAVE CONCLUDED THAT THE CAUSE OF THE INDICATION PROBLEMS IS RELATED TO A PYLON CONNECTOR THAT IS BEING CONTAMINATED WITH MOISTURE. THE IMMEDIATE SHORT TERM FIX IS TO APPLY A WATER RESISTANCE FILLER TO THE BACK OF THE CONNECTOR TO PREVENT WATER INGRESS. THE LONG TERM FIX IS TO REPLACE THE CONNECTOR WITH A NEW WATER TIGHT CONNECTOR. MF2L72 4F4  FRTA21EA   EOOO63EN             
20070604000172007060400017SW  2007       6          4          CA070320006      120070226G275019023           CONTROL CABLE                           BBAVIA8     8GCBC       1220803SW  LYC   O360  O360C2E     41514EA  MCAULY1A200 1A200*      GL  LT WING TE DLAP FRAYED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       535                                                            (CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN LT WING GAP AREA.  (TC NR 20070320006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  A21CE   E286    5  NP874     
20070604000182007060400018CE  2007       6          4          CA070320007      120070316G32457008006         TUBE                                    CESSNA207   207         2073602CE  CONT  O520  IO520F      17032SO  HARTZLHCC3Y HCC3YF1     GL  TIRE            CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA       374                                                            (CAN) MAINTENANCE WAS DISPATCHED AND THE WHEEL ASSEMBLY WAS REPLACED UPON INSPECTION, VALVE STEM FOUND CRACKED DUE TO EXTREME COLD.  (TC NR 20070320007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  O  A16CE   E5CE    5  CP25EA    
20070604000192007060400019SW  2007       6          4          CA070320008      120070226G275019023           CONTROL CABLE                           BBAVIA8     8GCBC       1220803SW  LYC   O360  O360C2E     41514EA  MCAULY1A200 1A200*      GL  RT WING TE FLAP FRAYED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       535                                                            (CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN RT WING GAP AREA.  (TC NR 20070320008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  A21CE   E286    5  NP874     
20070604000202007060400020    2007       6          4          CA070320009      420070320G83009408308902      BEARING                                 PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  ACCESSORY DRIVE DETERIORATED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       477                                                            (CAN) TRYING TO DIAGNOSE A NR 2 GENERATOR HOUSING DRAIN LINE OIL LEAK ,THE NR 2 GEN  HOUSING ASSY WAS REMOVED TO REPLACE THE ENGINE ACCESSORY DRIVE SEAL WHICH WAS SUSPECT LEAKING. UPON REASSEMBLY OF NR 2 GEN HOUSING PLAY WAS NOTED ON PULLEY END OF DRIVE SHAFT. DISASSEMBLY REVEALED THAT THE OUTER BEARING P/N:940.83.08.902 OR P202PP/FS5000 HAD BEGUN TO DISINTEGRATE. THERE WERE 3 BALLS MISSING AND THE REMAINING BALLS STILL WERE CARRYING LOAD. THERE WAS ENOUGH SIDE PLAY IN THE SHAFT WHICH WOULD CAUSE THE SHAFT NOT TO RUN TRUE WHICH IN TURN CAUSED THE ENGINE ACCESSORY SEAL TO FAIL. ALL AFFECTED PARTS REPLACED WITH NEW AND OIL LEAK IS GONE. (TC NR 20070320009)                                                          1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070604000212007060400021EA  2007       6          4          CA070320010      120070314G5350CL6002D15       RADOME                                  CNDAIRCL600 CL600*      1900302EA  GE    CF34  CF34*            NE                              FUSELAGE        BURNED          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA       4522 4522                                                      (CAN) DURING CRUISE AIRCRAFT STRUCK BY LIGHTENING. MAINTENANCE INSPECTION FOUND SCORCH MARKS ON RADOME, ALONG CENTER EDGES OF NLG DOORS, AND ALONG FORWARD FUSELAGE UP TO WING ROOT FAIRINGS. ALSO MINOR BURN MARK ON RT WINGLET TIP. NO DAMAGE TO ANY STATIC DISCHARGE WICKS. ADF WILL NOT POINT, ADF LOOP ANTENNA REPLACED. FUSELAGE BURN MARKS REPAIRED IAW MFG INSTRUCTIONS. WINGLET DAMAGE ALLOWABLE AS IAW MFG REO. AIRCRAFT RETURNED TO SERVICE. (TC NR 20070320010)                                                                                                                                                                                                                                                                     2L72 4F4  FRTA21EA   E15NE                
20070604000222007060400022CE  2007       6          4          CA070321001      120070307G3230115811020651    GEARBOX                                 BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA                              MLG             FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      CA       9220 2576                                                      (CAN) GEAR WOULD NOT COME UP WHEN SELECTED, LANDING GEAR GEARBOX REPLACED. OVERHAUL FACILITY REPORTED THAT A INTERNAL GEAR MAY HAVE BEEN SHIMMED IMPROPERLY THAT CAUSED PREMATURE WEAR (TC# 20070321001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T4  T  A14CE   E4EA                 
20070604000232007060400023SO  2007       6          4          CA070321002      120070320G8120                BEARING                                 PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  TURBOCHARGER    FAILED          W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA       2110                               L147768A                    (CAN) RT ENGINE LOST BOOST AT ALTITUDE. PILOT ELECTED TO DESCEND TO LOWER ALTITUDE.  AT LOWER ALTITUDE, RT ENGINE HAD NORMAL POWER.  APPROXIMATELY 20 MINUTES LATER, RT OIL PRESSURE WAS OBSERVED LOWER THAN NORMAL.  ENGINE WAS SECURED AND SHUTDOWN.  UNEVENTFUL SINGLE-ENGINE LANDING WAS CARRIED OUT. (TC NR 20070321002)                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070604000242007060400024NE  2007       6          4          CA070321003      320070320G6114S8462           BARREL                                                                                                      HAMSTD2D    2D30        NE  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            855                                       112779          (CAN) LOWER BARREL HALF FOUND WITH 5.5 INCH CRACK AT FLANGE AREA. (TC NR 20070321003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        5  CP206     
20070604000252007060400025EA  2007       6          4          CA070321004      220070316G8510                CRANKCASE                               PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1033                          L11868AA                    (CAN) THE AIRCRAFT WAS BROUGHT INTO THE HANGAR DURING AN INTERMEDIATE STOP TO WORK ON SOME SNAGS.  THE ENGINEER NOTICED A QUANTITY OF OIL ON THE OUTSIDE OF THE IB NACELLE OF THE RT ENGINE.  AFTER CLEANING THE ENGINE AND RUNNING IT AGAIN A CRACK WAS NOTICED EMANATING FROM THE LOWER FORWARD STUD OF THE NR 2 CYLINDER.  IT RAN FORWARD TO THE THREADED HOLE FOR THE PROP GOVERNOR BRACE.  THE CRACK WAS NDT`D AND FOUND TO ALSO BE RUNNING BACKWARDS ALONG THE CASE UNDER THE STARTER AREA.  IT ALSO RAN HALFWAY UP THE EDGE OF THE CYLINDER BOSS.  THE ENGINE HAS GONE FOR REPLACEMENT OF THE CASE. (TC NR 20070321004)                                                                                                                  1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070604000262007060400026EA  2007       6          4          CA070321005      120070228G2497PA204D8         WIRE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              COCKPIT         BURNED          W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA       2679926799                                                     (CAN) AFTER LANDING ELECTRICAL SHORT/ARCING BEHIND CAPTAINS SEAT IN CIRCUIT BREAKER PANEL. SOME SMOKE OBSERVED. AC TAXIED CLEAR OF ACTIVE RUNWAY. SMOKE AND SPARKS STOPPED, AIRCRAFT TAXIED TO RAMP, PRIOR TO ARRIVAL AT GATE SPARKS RE-OCCURRED. AIRCRAFT STOPPED AND DEPLANED. MAINTENANCE INSPECTION FOUND BUSS FEEDER JUMPER WIRE DISCONNECTED AND HAD MADE CONTACT WITH BULKHEAD BEHIND CB PANEL. ARCING DAMAGE BURNED THROUGH STRINGER AND BULKHEAD SKIN. BULKHEAD BURN THROUGH APPROX 1 INCH BY .5 INCH . (2) FEEDER WIRES BURNED INSULATION. FEEDER WIRES PA204D8 AND PA204E8 REPLACED. WIRE PA204C8 CONNECTION FOUND LOOSE AT CB 1-H2, ALL SCREWS ON BUS BAR H FROM H2 TO H13 FOUND NOT TIGHT. SB601R-34-096 (PROVISIONAL GPS INSTALLAT2L72 4F4  FRTA21EA   E15NE                
20070604000272007060400027CE  2007       6          4          CA070321006      120070320G5410S32471          LATCH                                   CESSNA208   208         2073702CE  PWA   PT6   PT6A114     52043NE  MCAULY3AF34C3GFR34C703  GL  LT NACELLE      LOOSE           W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA       14254                                                          (CAN) LT ENGINE UPPER COWL OPENED IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS FLYING THROUGH TURBULENCE WHEN THE COWL OPENED. DURING THE INSPECTION OF THE COWL, IT WAS FOUND THAT ALL 3 LATCHES WERE LOOSE. THE LATCHES WERE RE-ADJUSTED.   (TC NR 20070321006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3T3  TNTA37CE   E4EA    5  CP60GL    
20070604000282007060400028NM  2007       6          4          CA070321007      120070320G3260                PSEU                                    DHAV  DHC8  DHC8103     1386005NM  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF7       NE  MLG             MALFUNCTIONED   W      O   OTHER                                                                                           N  FALSE WARNING                                                                 APAPPROACH       1                      CA                                                                      (CAN) DURING APPROACH TO AIRPORT, THE PILOTS SELECTED GEAR DOWN AND HAD A GEAR (UNSAFE) LIGHT BUT NO GEAR EXTENSION. ALTERNATE EXTENSION WAS PERFORMED IAW CHECK LIST WITHOUT FURTHER REMARKS.   PSEU (PROXIMITY SWITCHING ELECTRONIC UNIT) REPLACED AS PRECAUTION.   FURTHER INVESTIGATION FOUND OUT THE MAIN CAUSE OF THE EVENT WAS LOOSE WIRING/TERMINAL ON THE MLG INHIBIT SWITCH.  MFG ISSUED DASH 8 Q100/200/300 AOM 828 TO PROVIDE DETAILS OF THIS EVENT. (TC NR 20070321007)                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070604000292007060400029SW  2007       6          4          CA070321008      120070321G5310205030163395    BEAM                                    BELL  205   205A1       1181414SW  LYC   T53   T5313B      41549NE                              FUSELAGE        CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       1231                                                           (CAN) WEB P/N 205-030-163-395 FOUND CRACKED AT INDUCTION BAFFLE SUPPORT WL 80.13. THE CRACK WAS APPROX 1 INCH IN LENGTH AND .5 INCH DOWN . REPAIR SCHEME IN PROGRESS THROUGH MFG. (TC NR 20070321008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 4U4  U  H1SW    E17EA                
20070604000302007060400030EU  2007       6          4          CA070321009      320070305G6197697070212       BUSS BAR                                BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  PROP HUB        SHORTED         W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) NR 2 ENGINE SHUTDOWN MANUALLY IN FLT DUE PEC FAIL CAUTION AND PROP SPEED AT 1060 RPM. FAULT CODES RT CH A/B 160 AND 162. MAINT DISPATCHED TO T/S. FOUND BUSBAR FOR PROPELLER DEICE CHAFFING ON MPU BRACKET, CAUSING MPU TO PICKUP SENS FROM BUSBAR. MPU ADJUSTED AND NEW BUSBAR INSTALLED. ENGINE GROUND RUNS C/O NORMAL. (TC NR 20070321009)                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070613001372007061300137NE  2007       6          13         CA070321010      220070316G7321430109817       FCU                                     SNIAS 350   AS350D      8680803EU  LYC   LTS101LTS101600A2 41560NE                              ENGINE          FAILED          W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  DEDESCENT        1                      CA            1082                                                      (CAN) THE ENGINE FLAMED OUT WHILE THE THROTTLE WAS BEING RETARDED DURING A PRACTICE AUTOROTATION. THE POSITION OF THE THROTTLE AT THE TIME OF THE FLAME OUT WAS NO WHERE NEAR THE POSITION IT NORMALLY CUTS OFF THE FUEL DURING NORMAL SHUTDOWN. AFTER CONDUCTING A NORMAL AUTOROTATION, THE PILOTS RESTARTED THE ENGINE AND PERFORMED A TEST HOVER AND FLIGHT. THEY PERFORMED (3) MORE PRACTICE AUTOROTATIONS WITHOUT ANY MORE INCIDENT OR SYMPTOMS.  NO FUEL LEAKS OR VISIBLE MECHANICAL ISSUES WERE FOUND.  THE FCU WAS REPLACED AS A PRECAUTION AND IS BEING SENT TO AN APPROVED FACILITY FOR BENCH TESTING.     (TC NR 20070321010)                                                                                                        1G71 3U3  U  H9EU    E5NE                 
20070604000312007060400031SW  2007       6          4          CA070321011      120070321G6230206010332121    MAST                                    BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              MAIN ROTOR      CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            2213                                                      (CAN) DURING ANNUAL INPECTION OF INTERIOR OF MAST, CORROSION AND PITTING WERE DISCOVERED.  MAST WAS REMOVED AND SENT TO AN OVERHAUL FACILITY FOR REPAIR. (TC NR 20070321011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3U3  U  H2SW    E4CE                 
20070604000322007060400032EA  2007       6          4          CA070321012      120070321G5330                SKIN                                    CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 CWASP       52016NE  HAMSTD43E   43E60       NE  FS 388          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3765                                                           (CAN) DURING A REGULAR SCHEDULED MAINTENANCE B-CHECK, THE MAINTENANCE GUIDE CHECKLIST CALLED FOR A VISUAL INSPECTION IN ZONE 330/340 FUSELAGE TO WING AREA, BS 388-434.  A SMALL 1 INCH CRACK WAS FOUND STEMMING FROM UNDERNEATH THE SHEAR PLATE AT BS 388. AFTER REMOVAL OF THE PRC, PAINT STRIPPING, AND COMPLETING A LIQUID DYE PENETRANT INSPECTION, (2) CRACKS AT STA 388 BETWEEN WL216 AND WL210 WERE IDENTIFIED. ONE CRACK WAS APPROXIMATELY 3.5 INCH AND THE OTHER APPROXIMATELY 0.5 INCH.  PICTURES AND INFORMATION SENT TO THE MFG FOR DIRECTION TO COMPLETE THIS REPAIR. (TC NR 20070321012)                                                                                                                                         2H72 4R3  RRTA14EA   ATC14   6  CP871     
20070604000332007060400033EA  2007       6          4          CA070321013      120070319G493021188002        ECU                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              APU             MALFUNCTIONED   W      O   OTHER                                                                                           A  FLAME/FIRE                                                                    NRNOT REPORTED   1                      CA       5330 5330                                                      (CAN) GROUND CREW REPORTED FLAMES FROM APU EXHAUST DURING PUSHBACK. COCKPIT HAD NO FIRE INDICATIONS. CREW SHUTDOWN AND PASSENGERS DEPLANED. MAINTENANCE INSPECTED AND APU MEL`D. LATER MAINTENANCE TROUBLESHOOTING FOUND APU ECU WITH FAULT/ERROR CODES. APU ECU REPLACED. AIRCRAFT RETURNED TO SERVICE. (TC NR 20070321013)                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20070604000342007060400034CE  2007       6          4          CA070322001      120070321G54141019800013      PANEL                                   BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  NACELLE         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       1375 1375                                                      (CAN) PANEL IS INSTALLED ON RT IB SIDE OF NACELLE. IT COVERS THE FUEL FIREWALL SHUTOFF VALVE. THE PANEL IS MANUFACTURED WITH A BULGE TO ACCOMMODATE THE VALVE.  IN THIS INSTALLATION THE VALVE CONNECTOR PLUG CHAFFED AGAINST THE PANEL CAUSING A STRESS RISER RESULTING IN A 1.5 CRACK VISIBLE FROM THE OUTSIDE OF THE PANEL.  PANEL WAS REPAIRED IAW THE SRM 54-00-01.  A NEW PANEL P/N 101-980001-41 WAS ORDERED.  THIS ALTERNATE PANEL HAS A LARGER/DEEPER DEPRESSION TO BETTER ACCOMMODATE THE VALVE. (TC NR 20070322001)                                                                                                                                                                                                                  2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070604000372007060400037EA  2007       6          4          CA070322004      120070321G7897                CONNECTOR                               CNDAIRCL600 CL600*      1900302EA  GE    CF34  CF348C1          NE                              THRUST REVERSER DAMAGED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) ENROUTE, CREW RECEIVED RED THRUST REVERSER ICON IN THEIR N1 GAUGE. AFTER DISCUSSIONS WITH MAINTENANCE AND DISPATCH, ELECTED TO DIVERT FOR MAINTENANCE TO LOCK OUT THE THRUST REVERSER. LANDED WITHOUT INCIDENT AND MAINTENANCE CARRIED OUT THE PROCEDURE. RT THRUST REVERSER LOCKED OUT. MEL 78-30-01 APPLIED WILL PROVIDE MORE INFORMATION WHEN IT BECOMES AVAILABLE  CORRECTIVE ACTION, DATED 29 MARCH 2007: WITH THE SUPPORT OF MFG WE HAVE CONCLUDED THAT THE CAUSE OF THE INDICATION PROBLEMS IS RELATED TO A PYLON CONNECTOR THAT IS BEING CONTAMINATED WITH MOISTURE. THE IMMEDIATE SHORT TERM FIX IS TO APPLY A WATER RESISTANCE FILLER TO THE BACK OF THE CONNECTOR TO PREVENT WATER INGRESS. THE LONG TERM FIX IS TO REPLACE THE2L72 4F4  FRTA21EA   EOOO63EN             
20070604000382007060400038    2007       6          4          CA070322005      420070313G61228210410         GOVERNOR                                BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  PROPELLER       MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) AIRCRAFT DEPARTED FOR DESTINATION, WHEN THE CREW ATTEMPTED TO SET CLIMB POWER, THE RT PROP DROPPED TO 1200 RPM AND THE TORQUE WENT TO 2200 LBS.  THE CREW DECLARED AN EMERGENCY AND LANDED UNEVENTLY .   MAINTENANCE WENT TO SITE THE FOLLOWING DAY AND CHANGED THE RT PROPELLER, RIGGED IT AND PERFORMED GROUND RUNS .THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. (TC NR 20070322005)                                                                                                                                                                                                                                                                                                                                 2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070604000392007060400039SO  2007       6          4          CA070322006      220070128G731464936849A1      PUMP                                    DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  FUEL SYSTEM     OUT OF ADJUST   W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA       69                                 806498                      (CAN) PILOT REPORTED ENGINE STOPPED DURING POWER OFF STALL.  RECORDS INDICATED (2) SID97-3C FUEL SET UP ADJUSTMENTS CARRIED OUT IN THE PREVIOUS FIVE DAYS OR 13.1 HRS PRIOR TO THE INCIDENT. SID CHECK REVEALED UNMETERED PRESSURE OUT OF LIMITS BY -1.1 PSI, LIMIT IS +/- 0.2 PSI.  MECHANICAL FUEL PUMP REPLACED, PUMP OFF S/N B06LA110, NEW PUMP S/N B06LA111 INSTALLED, FUEL INJECTORS, INLINE FILTER AND ALL FUEL LINE REMOVED CLEANED INSPECTED AND RE-INSTALLED. AIRCRAFT RELEASED CONDITIONAL TO SATISFACTORY TEST FLIGHT AND TEST FLOWN UNSATISFACTORY. EITHER PUMP WAS UNABLE TO BE ADJUSTED TO OBTAIN LEANING SCHEDULE LIMITS OR UNABLE TO RE-ADJUST  TO MEET SID SPEC AFTER TEST FLIGHT.  MECHANICAL FUEL PUMP REPLACED ONCE AGAIN W1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
             20081107     GL  2008       11         7          CA070322007      120070108G3245                TIRE                                    DIAMONDA20  DA20C1      2990001GL                                                               MLG             MISMANUFACTURED W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN)  AFTER 2 FLAT TIRES WITHIN APPROX. 30 HRS. ASSOCIATED WITH A SMALL MANUFACTURE LABEL ADHERED TO THE INSIDE OF THE TIRE DURING THE MANUFACTURING PROCESS.  THE GLUE OR LABEL MATERIAL WAS REACTING WITH THE TUBE AND CAUSING SMALL CRACKS AND EVENTUALLY ALLOWING AIR TO ESCAPE.  FAILURES DID NOT SEEM TO BE RELATED TO ANY PARTICULAR FLIGHT SEGMENT AS SOME WERE GOING FLAT OVERNIGHT, OTHERS WERE GOING FLAT WHILE TAXIING AND SOME SHORTLY AFTER LANDING ON ROLL OUT. SINCE THE TIRE REPLACEMENTS TO DATE WE HAVE HAD NO RECURRENT ISSUES DUE TO THE LABEL. APPROX. 35 TIRES AND TUBES HAVE BEEN REPLACED, SOME WERE REPLACED AS A PRECAUTION NOT NECESSARILY A FAILURE.                                                              1L71 3O    NTTA4CH                        
             20081113     GL  2008       11         13         CA070322008      120070309G3245500X56PLY       TIRE            CLEVELANDPNU4078E       DIAMONDA20  DA20C1      2990001GL                                                               LANDING GEAR    SPLIT           W      O   OTHER                                                                                           O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) SINCE OUR PLAGUED REPORTED UNDER SDR 20070322007, WE HAVE ENCOUNTERED MORE FLAT TIRES. THIS TIME WE ARE FINDING SPLITS IN THE TUBE OUTER EDGE CENTRE LINE. NOT THE SAME PROBLEM WE WERE HAVING WITH THE MCCREARY TIRES. THE COMMONALITY IN THESE FAILURES SEEMS TO BE RELATED TO MICHELIN TUBES. WE HAVE SINCE RETURNED 5 TUBES TO MICHELIN FOR THEIR INSPECTION. A CONVERSATION WITH AN AVIALL REPRESENTATIVE WHO HAS BEEN IN CONTACT WITH MICHELIN TODAY CONFIRMS THEY HAVE RECEIVED THE TUBE AND HAVE BEGUN PRELIMINARY INSPECTION. THEY HAVE INDICATED THAT THEY ARE ALSO DEALING WITH ANOTHER CUSTOMER WITH SIMILAR PROBLEMS AND WILL GET BACK TO US WITH THE DETAILS OF THE ANALYSIS. WE HAVE SINCE PURCHASED TUBES FROM A DIFFERENT1L71 3O    NTTA4CH                        
20070604000402007060400040EA  2007       6          4          CA070322009      320070314G6111                TAPE                                                                                                        SNSNCHW69EK W69EK63     EA  PROPELLER       DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       71         AG7471                                              (CAN) DURING VISUAL INSPECTION, IT WAS FOUND THAT THE TAPE USED ON THE LEADING EDGE OF THIS PROP WHICH WAS INSTALLED BY THE MFG, UNDER SPEC SP-127, WAS STARTING TO BLISTER AND SEPARATE FROM THE LEADING EDGE, WORSE AT THE TIPS. TAPE WAS REMOVED AND LOG ENTRIES CARRIED OUT. NO WEIGHT AND BALANCE CHANGES AND THOUGH DISCUSSIONS WITH BOTH MFGS.  THERE IS NO ILL EFFECT ON BALANCE AS LONG AS BOTH BLADE TAPES ON BOTH BLADES ARE REMOVED.  COULD NOT SEEM TO ENTER THAT THIS IS A W69EK-63 MODEL PROP. (TC NR 20070322009)                                                                                                                                                                                                                                            5  NTA4CH    
             20081104     EA  2008       11         4          CA070322010      320070314G6110                TAPE                                                                                                        SNSNCHW69EK W69EK63     EA  PROPELLER       BLISTERED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       48                                                             (CAN) DURING VISUAL INSP, IT WAS FOUND THAT THE TAPE USED ON THE L/E OF THIS PROP WHICH WAS INSTALLED BY THE MFG UNDER SPECIFICATION SP-127 WAS STARTING TO BLISTER AND SEPERATE FROM THE L/E, WORSE AT THE TIPS. TAPE WAS REMOVED AND LOG ENTRIES CARRIED OUT. NO WEIGHT AND BALANCE CHANGES AND THOUGH DISCUSSIONS WITH BOTH PROP MFG AND ACFT MFG, THEIR IS NO ILL EFFECT ON BALANCE AS LONG AS BOTH BLADE TAPES ON BOTH BLADES ARE REMOVED.. (TC NR 20070322010)                                                                                                                                                                                                                                                                                                         5  NTA4CH    
20070604000412007060400041CE  2007       6          4          CA070322011      120070322G561035410291652     WINDOW                                  BEECH 95    E95         1153410CE  LYC   O360  IO360B1B    41514EA  HARTZLHCC2Y HCC2YK2     GL  COCKPIT         BROKEN          W      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE FLIGHT, AT 6000 FT, THE MAJORITY OF THE LT SIDE COCKPIT WINDOW DEPARTED THE AC. THE AC BEING CLOSE TO ITS INTENDED DESTINATION CONTINUED ON AND LANDED WITHOUT INCIDENT. A FLIGHT PERMIT WAS ISSUED AND THE AIRCRAFT FLOWN TO MAIN BASE FOR EVALUATION AND REPAIR. SPEAKING WITH THE PILOT THE WINDOW DID NOT APPEAR DAMAGED OR CRACKED PRIOR TO THE EVENT. THE SAME PILOT WHO FLEW THE SAME AIRCRAFT DAYS EARLIER MENTIONED HIS HEAD HIT THE WINDOW DURING AN ENCOUNTER WITH TURBULENT AIR BUT DID NOT FEEL IT WAS SEVERE ENOUGH TO CAUSE DAMAGE TO THE WINDOW. THE ONLY SUBSEQUENT DAMAGE TO THE AIRCRAFT WAS A SMALL CUT IN THE LT HORIZONTAL STABILIZER DE-ICE BOOT. THE AIRCRAFT IS AN UNPRESSURIZED AIRCRAFT. (TC NR 200701L72 3O3  O  3A16    1E10    5  CP920     
20070604000422007060400042EU  2007       6          4          CA070323001      220070301G7240RK47289         COMBUST CHAMBER                                                            RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  ENGINE          FAILED          W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA            2479                                                      (CAN) PILOTS NOTICED THE LT ENGINE OPERATING APPROX. 100 POUNDS OF TORQUE LOW.  UPON LANDING MAINTENANCE WAS NOTIFIED.  IT WAS FOUND THAT THE NR 2 COMBUSTION CAN ASSEMBLY HAD LOST A SECTION OF ITS OUTSIDE AIR CASING. A GENERAL INSPECTION OF THE AREA GAVE NO CLUES AS TO WHY THIS HAPPENED. IAW THE MM ALL APPLICABLE INSPECTIONS WERE COMPLETED TO ENSURE THE ENGINE WOULD BE SAFE TO CONTINUE IN SERVICE.  FURTHERMORE, DUE TO A HOT SECTION INSPECTION COMING DUE ALL OTHER COMBUSTION CANS WERE REPLACED.  THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO ISSUES SINCE. (TC NR 20070323001)                                                                                                                                                     4  T          A196    6  CP899     
             20081104     NM  2008       11         4          CA070323002      120070321G52808233101003      PUSHROD                                 DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  MLG DOOR        BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) NR 1 MLG, AFT DOOR OPEN IN FLIGHT. FOUND BOTH GEAR DOOR PUSH ROD, P/N: 8323101-003 AND SPRING, P/N: 83231020-003, BROKEN. PUSH ROD AND SPRING REPLACED. (TC NR 20070323002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070604000432007060400043NE  2007       6          4          CA070323003      220070321G72614115T43PO3      CARBON SEAL                             CNDAIRCL600 CL600*      1900302EA  GE    CF34  CF34*            NE                              NR 1 ENGINE     MISSING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA       5302                                                           (CAN) AFTER DEPARTURE AND CLIMBING THOUGH 16,000 FT, CREW RECEIVED (OIL LEVEL LOW) MESSAGE FOR NR 1 ENGINE. QUANTITY WAS 50 PERCENT AND DROPPING. AFTER DISCUSSION WITH MAINTENANCE ELECTED TO RETURN TO BASE.  ANNOUNCED TO PASSENGERS THAT THEY WERE RETURNING DUE TO OIL QUANTITY INDICATION. JUST PAST THE OUTER MARKER CREW RECEIVED RED OIL LEVEL WARNING AND SHUTDOWN NR 1 ENGINE.  NO EMERGENCY WAS DECLARED AS THEY WERE SO CLOSE TO LANDING AT THIS POINT. DID A FLAP 20 LANDING WITHOUT INCIDENT AND ADVISED PASSENGERS THAT THEY DID HAVE TO SHUTDOWN ENGINE DUE OIL LEVEL. NO ADVERSE PASSENGER REACTION.  FDR READOUT WAS TAKEN AND NO HEAVY LANDING INSPECTION WAS REQUIRED.  EARLIER THAT DAY THE NR 1 EDP HYDRAULIC PUMP HAD BE2L72 4F4  FRTA21EA   E15NE                
20070604000442007060400044NM  2007       6          4          CA070323004      120070322G3260387             BULB                                    BOEING727   727247      138408FNM                                                               MLG INDICATOR   FAILED          W      O   OTHER                                                                                           P  NO WARNING INDICATION                                                         APAPPROACH       1                      CA                                                                      (CAN) AIRCRAFT ON MARCH 22, 2007 WAS ON APPROACH WHEN THE CREW EXTENDED THE LANDING GEAR FOR LANDING. WHEN THE GEAR WAS DOWN, THE CREW NOTICED THAT THE LT MAIN GEAR GREEN LOCKED LIGHT WAS NOT ILLUMINATED. THE CREW REJECTED THE LANDING AND CONTACTED ATC FOR A NEW APPROACH LINE-UP. THE SECOND APPROACH REVEALED THE SAME RESULTS. THE CREW REMOVED AND REPLACED A FAULTY BULB AND THE AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE CHECKED THE SYSTEM AND CHECKED THAT THE CORRECT BULB WAS USED. NO FURTHER PROBLEMS. (TC NR 20070323004)                                                                                                                                                                                      2L73 4F      A3WE                         
20070613001382007061300138EA  2007       6          13         CA070323005      220070322G7300                CONTROLLER                              PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA                              FUEL SYSTEM     LEAKING         W      A   UNSCHED LANDING                                                                                 KERFLUID LOSS                VIBRATION/BUFFET          PARTIAL RPM/PWR LOSS      CRCRUISE         1                      CA            1069                          L91568A                     (CAN) DURING A TRAINING FLIGHT WHEN POWER WAS APPLIED, THE RT ENGINE ACCELERATED NORMALLY TO 40 INCHES AND THEN STARTED TO SURGE BETWEEN 20 AND FORTY INCHES.  THE PILOT WAS ABLE TO STABILIZE THE ENGINE AT ABOUT 25 INCHES OF MANIFOLD PRESSURE.  ALL GAUGES WERE NORMAL ALTHOUGH THEY COULD NOT GAIN ANY MORE THAN 30 INCHES OF MANIFOLD PRESSURE.   A LOT OF BLACK SMOKE WAS OBSERVED UNDER THE WING OF THE AIRCRAFT. AS THE AIRCRAFT LANDED, THE RIGHT ENGINE QUIT. A QUANTITY OF FUEL WAS POURING OUT THE `SNIFFLE` VALVE OF THE ENGINE.    MAINTENANCE REMOVED THE DENSITY AND DIFFERENTIAL CONTROLLERS.  THE DENSITY CONTROLLER APPEARED TO HAVE AN INTERNAL LEAKAGE WHICH HAD CONTAMINATED BOTH THE DIFFERENTIAL CONTROLLER AND THE FCU1L72 3O3  O  A20SO   E14EA                
20070604000452007060400045NM  2007       6          4          CA070326001      120070322G2497                WIRE HARNESS                            DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE                  CHAFED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       13589                                                          (CAN) AN OPERATOR HAS REPORTED FINDING SOME WIRE LOOMS THAT WE HAVE DAMAGED DUE TO CHAFING. THIS CHAFING IS OCCURRING WITH THE CABIN FLOOR WIRE TROUGH ON AN A/C THAT IS POST MOD 8/2705, S/B 8-53-66. THE BULK OF THE CHAFING HAS BEEN OBSERVED IN THE REAR OF THE FUSELAGE WHERE THE LOOM TIE MOUNTS ARE GREATLY REDUCED.  MFG IS REVIEWING WIRING INSTALLATION. (TC NR 20070326001)                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070604000462007060400046EU  2007       6          4          CA070326002      120070322G2741                RELAY                                   PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  TRIM SYS        MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) A/C WAS CLIMBING OUT. THE PILOT MADE A MANUAL TRIM UP SELECTION WHEN A HZ STAB TRIM RUNAWAY OCCURRED. THE PILOT SELECTED THE TRIM INTERRUPT SWITCH TO STOP THE RUNAWAY AND RETURNED. THE TRIM RELAY K 022 WAS REPLACED AND SYSTEM WAS GROUND CHECKED SERVICEABLE AND THE A/C RETURNED TO SERVICE. NO FURTHER PROBLEMS HAVE BEEN REPORTED. (TC NR 20070326002)                                                                                                                                                                                                                                                                                                                                                                             1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070604000472007060400047CE  2007       6          4          CA070326003      120070214G531111543008435     FRAME                                   BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  FUSELAGE        CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) FRAME SEGMENT P/N 115-43008-35 CRACKED AT OB ENDS. AIRCRAFT IS AN EMS MACHINE. DEFECT APPEARS TO BE RELATED TO HIGH FLOOR LOADING.  (TC NR 20070326003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070604000482007060400048CE  2007       6          4          CA070327001      120070326G3010                BOOT                                    BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  DE ICE SYSTEM   ARCED           W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) PILOTS REPORTED THAT THE IB LEADING EDGE DEICE BOOT WAS NOT FUNCTIONING.  THE DEICE SYSTEM WAS TESTED AND THE SNAG WAS CONFIRMED.   WHEN THE LEADING EDGE WAS REMOVED TO CHECK THE BOOT SYSTEM EVIDENCE OF SEVERE ARCING WAS FOUND IN THE VICINITY OF THE START RELAYS.  IT IS SUSPECTED THAT THE DEICE HOSE WAS ROUTED IMPROPERLY TO THE LEADING EDGE.  OVER TIME THE HOSE CHAFED ON THE WIRING FROM THE RELAYS.    MAINTENANCE REPLACED THE LEADING EDGE AS WELL AS ANY CONNECTORS THAT WERE DAMAGED.  (TC NR 20070327001)                                                                                                                                                                                                              1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070604000492007060400049NM  2007       6          4          CA070327002      120070322G38106BS10011        DRAIN VALVE                             AMD   FALC50FALCON2000  2730170NM  HNYWL AS907 AS90711A    33908WP                              POTABLE WATER   DAMAGED         W      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      CA       3626 3626                                                      (CAN) THE AIRCRAFT POTABLE WATER SYSTEM WAS DAMAGED DUE TO HAVING THE WATER SYSTEM FULL OF WATER. THEN HAVING THE AIRCRAFT LEFT ON THE RAMP FOR 8 HOURS AT -14C WITH NO ADDITIONAL HEAT TO KEEP THE WATER SYSTEM FROM FREEZING. UPON ARRIVAL THE PILOTS REPORTED (WATER APPEARS TO BE LEAKING FROM THE BELLY). THE MAINTENANCE PERSONNEL INVESIGATED THE SNAG AND FOUND THE WATER SYSTEM DRAIN VALVE WAS DAMAGED DUE TO THE SEVERE FREEZING. A REMINDER TO ALL CORPORATE PILOTS TO MONITOR THE POTABLE WATER SYSTEM AND THE OAT IN WINTER.  (TC NR 20070327002)                                                                                                                                                                                 2K72 4F4  FRTA50NM   E00010LA             
20070604000502007060400050SW  2007       6          4          CA070327003      120070319G2435230321910       FRICTION CUP                            BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              STARTER GEN     CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA            660   10481                                               (CAN) DURING INSPECTON STARTER-GENERATOR FRICTION CUP PLATE WAS FOUND TO BE CRACKED. NEW PART ORDERED AND INSTALLED WHEM IT ARRIVED. (TC NR 20070327003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3U3  U  H2SW    E4CE                 
20070604000522007060400052SO  2007       6          4          CA070327005      120070322G3260487862          PROXIMITY SWITCH                        PIPER PA31  PA31325     7103105SO  LYC   O540  TIO540F2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  MLG             FAILED          W      K   NONE                                                                                            N  FALSE WARNING                                                                 ININSP/MAINT     1                      CA                                                                      (CAN)  MAINTENANCE COULD NOT DUPLICATE FAULT ON GROUND WITH AIRCRAFT ON JACKS. CYCLED GEAR 20 TIMES FAULT FREE. WIRING CHECKED,OK, RIGGING CHECKED OK, HYDRAULIC POWER PACK CHECKED, OK. CORRECTIVE ACTION TO REPLACE ALL 6 LANDING GEAR PROXIMITY SWITCHES. (TC NR 20070327005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3O3  O  A20SO   E14EA   5  CP33EA    
             20081104     EA  2008       11         4          CA070327006      220070323G741410391584        DISTRIBUTOR BLK BENDIX                  PIPER PA28  PA28R200    7102811SO  LYC   O360  IO360C1C    41514EA  HARTZLHCC3Y HCC3YR      GL  MAGNETO         UNSERVICEABLE   W      D   RETURN TO BLOCK                                                                                 RE PARTIAL RPM/PWR LOSS      VIBRATION/BUFFET                                    TXTAXI/GRND HDL  1                      CA            1130                                                      (CAN) DISTURBER BLOCK CENTER BUSHING WAS LOOSE IN THE PLASTIC MOLDING. (TC NR 20070327006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  O  2A13    1E10    5  CP25EA    
20070604000542007060400054EA  2007       6          4          CA070327008      220070312G8500                ENGINE                                  PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL                  FAILED          W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA       2145                                                           (CAN) ENGINE FAILURE, PROP STOPPED IN FLIGHT. NO EXTERNAL DAMAGE TO ENGINE.  SUSPECT CRANKSHAFT FAILURE. (TC NR 20070327008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070604000552007060400055SW  2007       6          4          CA070327009      120070313G6520206040402003    GEARBOX                                 BELL  206   206L        1181522SW  ALLSN 250C  250C20R2         GL                                              LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       5118                                                           (CAN) OIL LEAK. SHIPPED TO AUTHORIZED SERVICE CENTER FOR REPAIR AND RE-INSTALLATION.  (TC NR 20070327009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3U3  U  H2SW    E4CE                 
20070604000562007060400056CE  2007       6          4          CA070327010      120070208G27301260505406      CONTROL CABLE                           CESSNA206   U206F       2073333CE  CONT  O550  IO550F      17042SO  MCAULY3A32C D3A32C*     GL  ELEVATOR        CUT             W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2664                                                           (CAN) A SCREW FROM THE AVIONIC EQUIPMENT LOOSENED, FELL AND LODGED  BETWEEN THE PULLEY AND CABLE FOR THE ELEVATOR FLIGHT CONTROL. WITH TIME, THE CABLE WAS DAMAGED AS IT ROLLED OVER THE SCREW. (TC NR 20070327010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  O  A4CE    E3SO    5  CP21EA    
20070604000572007060400057EU  2007       6          4          CA070327011      120070327G3500D2475           COUPLING                                SAAB  SF340 340B        7860101EU  GE    CT7TP CT79B       30030NE  ROTOL R390  R3904123F27 NE  BLEED AIR SYS   DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE A BLEED AIR LEAK INDICATION WAS OBSERVED FOR THE RT ENGINE. THE ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE. AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE INSPECTION FOUND NO EVIDENCE OF A BLEED AIR LEAK. FURTHER INVESTIGATION SHOWED THAT A FIRE WIRE COUPLING WAS LOOSE IN THE RT WING. WHEN THE COUPLING WAS REMOVED IT WAS FOUND THAT A CRUSH WASHER WAS MISSING FROM THE ASSEMBLY. THE COUPLING WAS CLEANED, INSPECTED AND REASSEMBLED CORRECTLY WITH (2) CRUSH WASHERS. AFTER INSTALLATION THE FIRE WIRE ELECTRICALLY TESTED SATISFACTORY. THE AIRCRAFT WAS SUBJECT TO FULL ENGINE RUNS AND NO BLEED AIR LEAK WAS EVIDENT. ALL COCKPIT INDICATIONS WERE NORMAL. (TC NR 20070327011)                                  2L72 4T4  TRTA52EU   E8NE    6  CP31NE    
20070604000582007060400058    2007       6          4          CA070328001      420070325G3418350A230083      COMPUTER                                AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF5       NE  STALL WARNING   MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) FOLLOWING DEPARTURE, THE CREW OBSERVED A STICK PUSHER/ STICK SHAKER FAULT. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE CREW ALERTING COMPUTER, SYSTEM GROUND CHECKED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070328001)                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20070604000592007060400059CE  2007       6          4          CA070328002      120070312G2120651510314       DUCT                                    CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              CABIN AIR SYS   DEBONDED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) COMPANY CAMPAIGN NOTICE 851-21-20-034 WAS CARRIED OUT. INSPECTION FOUND THE CLAMP PORTION OF THE BLEED AIR WELD ASSEMBLY LOOSE. THE WELD ASSEMBLY WAS REPAIRED BY COLD BONDING IAW INSTRUCTIONS RECEIVED FROM MFG CUSTOMER SUPPORT. UNIT RETURNED TO SERVICE. (TC NR 20070328002)                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 4F4  F  A22CE   E1NE                 
20070604000602007060400060EA  2007       6          4          CA070328003      120070323G2910600752406       LINE                                    CNDAIRCL601 CL6012A12   1900303EA  GE    CF34  CF348E5A1   30015NE                              HYD SYSTEM      FAILED          W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1505415054                                                     (CAN) DURING ROUTINE SERVICING AFTER A/C ARRIVAL, HYD FLUID WAS NOTICED LEAKING OUT OF THE BOTTOM OF THE RUDDER AND RUNNING DOWN THE TAILCONE AND TO THE GROUND. PANELS WERE REMOVED TO LOCATE THE LEAK, FIGURING THAT THERE WAS A BAD RUDDER PCU LEAKING. WHAT WAS FOUND IT WAS THE NR 3 HYDRAULIC RETURN SYSTEM LINE P/N 600-75240-6 CHAFED THREW AT THE BOTTOM OF THE HORIZONTAL STAB REAR SPAR. 3 MONTH PREVIOUS A 15,000 HOUR INSP WAS C/O AND THE CENTER BOTTOM HINGE BEARING WAS FOUND WORN OUT, SO THE HOLE BRACKET ASSY WAS REPLACED. TO REPLACED THIS BRACKET THE HYD LINE OF THE NR 3 RETURN SYSTEM HAD TO BE DISASSEMBLE TO GAIN ACCESS TO THE BRACKET. WHEN THE RUDDER WAS REMOVED TO DO THE REPAIR, AS THIS LINE IS ON THE REAR SP2L72 4F4  FRTA21AE   E00063EN             
             20081104     CE  2008       11         4          CA070328004      120070327G792110656D          OIL COOLER                              BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  LT ENGINE       LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      CA                                                                      (CAN) EXCESSIVE OIL NOTED ON LT ENGINE NACELLE. OIL LEAK TRACED TO LT ENGINE OIL COOLER. NEW OIL COOLER INSTALLED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
             20081104     NM  2008       11         4          CA070328005      120070317G2520VL200307A       ACTUATOR        BOEING                  BOEING767   767333      1385301NM  PWA   4060  PW4060      52119NE                              LEG REST        FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) SEAT LOCATION ON THE ACFT WAS 7F, AND FAILED IN FLIGHT. LEG REST ACTUATOR KEPT DRIVING THE FOOTREST BACKWARD, AND PUNCTURED THE REAR SPAR OF THE SEAT. THERE IS A CONCERN THAT ECU SOFTWARE 2.8 MAY BE TO BLAME, BUT INVESTIGATION IS ON GOING. THERE HAS BEEN A PREVIOUS CASE OF A BENT SPAR, PRIOR TO THIS LEVEL OF SOFTWARE, SO IT IS POSSIBLE THAT THERE IS STILL AN UNKNOWN FAILURE MODE THAT CAUSES THE FEEDBACK FROM THE FOOTREST POSITION TO BE LOST, AND DRIVE THE FOOTREST UNTIL FAILURE.                                                                                                                                                                                                                                       2L72 4F4  FRTA1NM    E24NE                
20070503000012007050300001EU  2007       5          3          CA070329001      120070326G6310350A35105901    COUPLING        SNIAS                   SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1        NE                              M/R DRIVESHAFT  CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CRACK IN DISC LAMINATE FOUND DURING POST FLIGHT (DAILY) INSPECTION. (TC NR 20070329001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H9EU    E19EU                
20070511000012007051100001EA  2007       5          11         CA070329002      120070323G5340CN6272017203    BRACKET                                 CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C1          NE                              HYD LINE        BROKEN          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CRCRUISE         1                      CA       5723                                                           (CAN) AC EXPERIENCED A COMMANDED IFSD DUE TO OIL PRESSURE LOSS DURING CRUISE. DURING FLIGHT, PILOT NOTICED OIL PRESSURE DECREASING STEADILY DURING CRUISE. AT 36 PSI OIL PRESSURE, PILOT INITIATED A COMMANDED SHUTDOWN OF THE NR 2 ENGINE AND DIVERTED INTO BILLINGS FOR AN UNEVENTFUL SINGLE ENGINE LANDING.  UPON INSPECTION OF ENGINE, MECHANICS NOTICED A STATIC OIL LEAK FROM THE BOTTOM OF GEARBOX. AFTER FURTHER INSPECTION, IT WAS NOTICED THAT THE BRACKET HOLDING THE HYD LINE TO GEARBOX AT 6:30 ON THE AFT AGB FLANGE HAD BROKEN OFF, AND CONTACTED THE BOTTOM OF THE GEARBOX JUST ABOVE THE BRACKET LOCATION, HAD WORN A HOLE IN THE AGB HOUSING, RESULTING IN THE OIL LOSS. ENGINE IS BEING REMOVED AND REPLACED, ANOTHER ENGINE 2L72 4F4  FRTA21EA   EOOO63EN             
20070503000022007050300002CE  2007       5          3          CA070329005      120070329G2560110195203       BUCKLE                                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              SEATBELT        INTERFERENCE    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CONTROL YOKE INTERFERENCE WITH ROTORY SEAT BUCKLES INSPECTED IAW INTERNAL CAMPAIGN NOTICE 010-25-10-011. OPERATION OF EITHER PILOTS AND CO-PILOTS YOKES WITH SEATS FULL FORWARD CONFIRMS THAT INTERFERENCE CAN CAUSE UNLATCHING OF THE SEATBELT ROTARY BUCKLES. (TC NR 20070329005)                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 4F4  F  A22CE   E1NE                 
20070503000032007050300003SO  2007       5          3          CA070329006      220070313G8530                CYLINDER                                CESSNA150   150L        2071826CE  CONT  O200  O200A       17020SO  MCAULY1A102 1A102OCM    GL  NR 4            DETACHED        W      A   UNSCHED LANDING                                                                                 ER VIBRATION/BUFFET          PARTIAL RPM/PWR LOSS                                CRCRUISE         1                      CA       1587                                                           (CAN) ENGINE VIBRATION AND POWER LOSS IN FLIGHT, ENGINE CAME TO TOTAL STOP ON TAXIWAY. CYLINDER NR 4 FOUND DETACHED. ENGINE (2587.4 HOURS). ENGINE REMOVED FOR OVERHAULED. (TC NR 20070329006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  O  3A19    E252    5  NP918     
20070613001392007061300139    2007       6          13         CA070329007      420070314G61228210004         GOVERNOR                                DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  PROPELLER       UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 S  AFFECT SYSTEMS                                                                TXTAXI/GRND HDL  1                      CA            2862                          PCE40320                    (CAN) A GROUND INCIDENT OCCURRED WHERE ONE AC TAXIED INTO ANOTHER.  BOTH AIRCRAFT WERE ON STRAIGHT SKIS. AFTER START-UP THE AC  MOVED FORWARD FROM ITS PARKING SPOT, THEN WHEN THE PILOT MOVED THE POWER LEVER INTO REVERSE THE NR 2 PROP WENT INTO REVERSE MOMENTARILY BUT THEN WENT INTO FORWARD PITCH WITH THE POWER LEVER STILL IN REVERSE.  AS A CONSEQUENCE THE RT WING MOVED FORWARD CAUSING THE AIRCRAFT TO SWING TO THE LT AND THE AIRCRAFT ENDED UP WITH ITS LT WING UNDER THE RT WING OF THE PARKED AC, ITS LT SPINNER INTO THE RT WINDSHIELD OF THE PARKED AC, AND THE NR 1 PROP DAMAGED THE NOSE OF THE PARKED AIRCRAFT. AFTER TEMPORARY REPAIRS WERE COMPLETED AND THE NR 1 PROP AND ENGINE WERE CHANGED ON THE AIRCRAFT THAT HA1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070504000832007050400083CE  2007       5          4          CA070329008      120070327G32501018100327      TORQUE KNEE                             BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCD4N3HCD4N3A     GL  MLG             WORN            W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       7020 7020                                                      (CAN) WHILE TAXING BACK TO THE RAMP, THE PILOT NOTICED THAT THE STEERING WAS MORE DIFFICULT AND INEFFECTIVE. HE SHUTDOWN BOTH ENGINES AND ON INVESTIGATION FOUND THE LT LANDING GEAR TORQUE KNEE BOLT DISCONNECTED. THE CAUSE OF THE DISCONNECTION WAS A WORN OUT RETAINING WASHER. MAINTENANCE REPLACED THE WASHER AND RETURNED THE AIRCRAFT TO SERVICE. THIS AREA WAS RECENTLY INSPECTED. THE MM DOES NOT SPECIFY DISASSEMBLING THIS AREA TO INSPECT. THE ONLY WAY THIS COULD HAVE BEEN DETECTED WAS BY DISASSEMBLY.  OUR MAINTENANCE PROGRAM TRACKING SHEETS HAVE BEEN AMENDED TO INCLUDE DISASSEMBLY OF THE TORQUE KNEES EACH 800 HOURS. (TC NR 20070329008)                                                                                1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070503000042007050300004CE  2007       5          3          CA070329009      120070329G2897                WIRE                                    BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  SHUTOFF VALVE   CHAFED          W      H   DEACTIVATE SYST/CIRCUITS                                                                        J  WARNING INDICATION                                                            CRCRUISE         1                      CA       434                                                            (CAN) 5 AMP ANNUNCIATOR INDICATION (CB4) POPPED IN FLIGHT AND THE CREW LOST THE GREEN AND WHITE ANNUNCIATOR LIGHTS. THE CREW ATTEMPTED TO RESET THE 5 AMP CIRCUIT BREAKER, BUT COULD NOT BE RESET.  PROBLEM WAS IN FOUND ON WIRE PIN D WIRE NR Q62A20 ON THE RT FUEL SHUTOFF VALVE HAD CHAFED TO GROUND ON ONE OF THE SCREWS THAT HOLDS ON THE INSPECTION PANEL ON. DID A REPAIR ON WIRE NR Q62A20 AND THE SYSTEM WAS FUNCTION TESTED NORMAL. (TC NR 20070329009)                                                                                                                                                                                                                                                                               2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070504000862007050400086NE  2007       5          4          CA070330002      320070216G611458462           BARREL          HAMSTD                  DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            855   112779                                              (CAN) PROPELLER HISTORY  - AUG 28 06 TTSOH 712.8 PROPELLER REPAIRED. - JAN 19 07 TTSOH 839.6 PROPELLER FLY WEIGHT ROLLER STIFF, ROLLER LUBRICATED AND RETURNED TO SERVICE. - FEB 16 07 TTSOH 854.9 PROPELLER REMOVED FROM SERVICE AND RETURNED TO O/H SHOP FOR REPAIR, SLOW TO CHANGE PITCH. - MAR 13 07 TTSOH 854.9 PROPELLER REPAIRED BY O/H SHOP, NEW CYLINDER AND COUNTER WEIGHT ROLLER KITS INSTALLED. - MAR 15 07 TTSOH 854.9 PROPELLER INSPECTED BEFORE INSTALLATION ON AIRCRAFT AND THE REAR PORTION OF THE PROPELLER BARREL (HUB) WAS FOUND TO BE CRACKED FROM THE BOLT BOSS 90` TO THE REAR OF THE BARREL ALONG THE OUTSIDE RADIUS.  CONTINUED OPERATION OF THE UNIT IN THIS CONDITION WOULD HAVE LED TO A CATASTROPHIC FAILURE.  THIS1H71 3R3  RRCA806    5E1     5  CP206     
20070504000922007050400092WP  2007       5          4          CA070330003      120070329G2780N547E           RELAY                                   CVAC  340   340CVAC     242270AWP  ALLSN 501D  501D13D     03004GL  ALLSN A6441 A6441FN606  GL  TE FLAP         FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION, THE FLAPS WERE SELECTED DOWN. THEY STOPPED  MOVING APPROXIMATELY HALF WAY DOWN. THE FLAP SOLENOID CIRCUIT BREAKER WAS OBSERVED TO BE OPEN. UPON INVESTIGATION  THE FLAP RELAY LOCATED IN THE GENERAL RELAY PANEL WAS FOUND TO HAVE FAILED. THE RELAY WILL BE REPLACED WITH A SERVICEABLE UNIT. (TC NR 20070330003)                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4R4  T  6A6     E282    6  CP898     
20070504000942007050400094NM  2007       5          4          CA070330004      120070329G3230                LANDING GEAR                            DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE                  MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       4800748007                                                     (CAN) DURING CRUISE CREW RECEIVED INTERMITTENT LANDING GEAR INOP CAUTION LIGHT. CREW ELECTED TO RETURN TO ORIGINATING AIRPORT. ALTERNATE GEAR EXTENSION USED TO LOWER LANDING GEAR.  NORMAL LANDING.  MAINTENANCE INSPECTION FOUND NO FAULTS. AIRCRAFT WILL BE RETURNED TO SERVICE SUBJECT TO A SATISFACTORY TEST FLIGHT. (TC NR 20070330004)                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070503000052007050300005NE  2007       5          3          CA070330005      220070326G7261                ENGINE                                  BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  RIGHT           MAKING METAL    W      D   RETURN TO BLOCK                                                                                 J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA       144916131                          PS0149                      (CAN) PILOTS LOADED PAX DEPARTED THE GATE. AFTER RECEIVING TAXI CLEARANCE THE PILOT NOTICED THE RIGHT LOW OIL PRESSURE WARNING LIGHT,THE AIRCRAFT WAS TURNED AROUND AND THE ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO THE GATE AND THE PASSENGERS UNLOADED. THE AIRCRAFT WAS TOWED BACK TO THE MAINTENANCE HANGER AND INSPECTED. WHEN THE OIL FILTER WAS REMOVED THERE WAS A LARGE AMOUNT OF SILVER COLORED MAGNETIC PARTICLES IN THE FILTER. THE ENGINE HAS BEEN REMOVED AND WILL BE SENT BACK TO MFG FOR INSPECTION/OVERHAUL, (TC NR 20070330005)                                                                                                                                                                                             2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070503000082007050300008NM  2007       5          3          CA070402001      120070329G6120666000459       CONTROL UNIT                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NR 2 PROPELLER  MALFUNCTIONED   W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) DURING LEVEL FLIGHT FL. 250, ENGINE NR 2 PROPELLER SPEED WENT TO 1051 RPM, FOLLOWED BY POWERPLANT ON ED. THIS CASE WAS TREATED AS AN OVERSPEED AND QRH CONSULTED, ENDING UP WITH ENGINE SHUTDOWN, ON NR 2 ENGINE. EMERGENCY DECLEARED AND A NORMAL DESCENT TOWARDS BASE WAS INITIATED. LANDING PERFORMED AND TAXI TO REMOTE GATE WAS DONE.  MAINTENANCE ARRIVED AND FOUND FAULT CODE 160 CH A AND B. FIM TASK 61-20-04-810-813 PERFORMED. NO CONTACT WITH MPU AND BUSS BARS. REMOVE AND REPLACED MPU.  (TC NR 20070402001)                                                                                                                                                                                                                2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070503000102007050300010EU  2007       5          3          CA070402002      120070402G29107229160003      LINE                                    SAAB  SF340 340B        7860101EU  GE    CT7TP CT79B       30030NE  ROTOL R390  R3904123F27 NE  HYD SYSTEM      CHAFED          W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) HYDRAULIC FLUID WAS NOTICED ROUND ACCESS PANEL 151CB RT. INVESTIGATION REVEALED A WEAR MARK AND PIN HOLE IN A HYDRAULIC LINE UNDER THE PANEL. FURTHER INVESTIGATION INDICATED THAT AN AJACENT PANEL BONDING STRAP HAD LOOPED WHEN THE PANEL WAS CLOSED AND HAD BEEN RUBBING ON THE HYDRAULIC LINE. THAT THE STRAP WOULD CHAFE ON THE HYDRAULIC LINE WAS NOT OBVIOUS WHEN THE PANEL WAS CLOSED. (TC NR 20070402002)                                                                                                                                                                                                                                                                                                                        2L72 4T4  TRTA52EU   E8NE    6  CP31NE    
20070503000192007050300019EU  2007       5          3          CA070402003      120070322G2917973811430       PRESSURE SWITCH                         PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  HYD SYSTEM      LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       165                                                            (CAN) DURING INSPECTION IT WAS NOTED THAT THIS HYDRAULIC PRESSURE SWITCH WAS LEAKING FLUID AT THE SWAGED SEEM OF THE SWITCH. THE SWITCH WAS REPLACED WITH NEW. (TC NR 20070402003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070503000232007050300023EU  2007       5          3          CA070402004      120070330G7700304544902       CHIP DETECTOR                           PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  ENGINE          BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6574                                                           (CAN) WHEN THE CONNECTOR WAS REMOVED FROM THE CHIP DETECTOR AT INSPECTION, IT WAS NOTED THAT ONE OF THE PINS OF THE CHIP DETECTOR HAD BROKE, AND STAYED IN THE CONNECTOR. THE CHIP DETECTOR WAS REPLACED. (TC NR 20070402004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070503000262007050300026SW  2007       5          3          CA070402006      120070315G561036004314SS      WINDSHIELD                              GULSTM690TP 690D        3970405SW  GARRTTTPE331TPE3315     01514WP  ROTOL R306  R306382F7   GL  COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       6350                                                           (CAN) DURING A ROUTINE MEDIVAC FLIGHT AT AN ALTITUDE OF 12,000 FEET, THE FLIGHT CREW VISUALLY NOTED THAT THE RT WINDSHIELD WAS CRACKED ACROSS THE UPPER OB CORNER.  AIRCRAFT RETURNED TO BASE. INSPECTION OF THE WINDSHIELD FOUND THE OUTER WINDOW PANE CRACKED APPROXIMATELY 2.5 INCHES LENGTH ACROSS THE CORNER.  NEW WINDSHIELD INSTALLED AND AIRCRAFT RETURNED TO SERVICE.  (TC NR 20070402006)                                                                                                                                                                                                                                                                                                                                             1H72 3T4  T  2A4     E4WE    6  CP8EU     
20070503000302007050300030CE  2007       5          3          CA070403001      120070328G5740SPS8178510      BOLT                                    BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  WING ATTACH     CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7540                                                           (CAN) DURING A SCHEDULED NDT INSPECTION OF THE WING ATTACHMENT BOLTS THE FWD UPPER BOLT ON THE RT SIDE WAS REJECTED AFTER THE LIQUID PENETRANT INSPECTION REVEALED A CRACK AT THE HEAD OF THE BOLT. THE BOLT HAD 7540.5 TSN. THIS INSPECTION IS DUE EVERY 1000 HRS. (TC NR 20070403001)                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070503000312007050300031SW  2007       5          3          CA070403002      120070401G56102719442004      WINDSHIELD                              SWRNGNSA226 SA226AT     8780405SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCB3T HCB3TN5     GL  COCKPIT         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA            5049                                                      (CAN) THE FLIGHT CREW OBSERVED THE LT HEATED WINDSHEILD DELAMINATE AND CRACK DURING FLIGHT. THEY CARRIED OUT THEIR EMERGENCY PROCEDURES AND LANDED AT THEIR POINT OF DESTINATION. MAINTENANCE REPLACED THE WINDSHEILD. NO REASON FOR THE FAILURE (IE IMPACT) COULD BE DETERMINED. THIS IS ONE OF MANY FAILURES OF THIS WINDSHEILD PN INCURRED BY THIS OPERATOR. MULTIPLE ATTEMPTS TO CONTACT THE MFG HAS RESULTED IN NO RESPONSE. (TC NR 20070403002)                                                                                                                                                                                                                                                                                           2L72 4T4  TRTA5SW    E4WE    6  CP15EA    
20070503000332007050300033    2007       5          3          CA070403003      420070321G61223020094         DRIVE GEAR      WOODWARD                                                   GARRTTTPE331TPE331*     01514WP                              PROPELLER GOV   MAKING METAL    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  1754695                                             (CAN) CONSTANT SPEED, SINGLE ACTING PROPELLER GOVERNOR P/N 895490-10 WAS RECEIVED AT MFG WITH REPORTED PROBLEM CUSTOMER RETURNED ON IN TRANSIT B69894 AND IRR NR 5170 STATING PROP GOVERNOR HAS NO RESET PRESSURE AND SHAFT STICKS AND WILL NOT RETURN TO MINIMUM STOP. THE FAULT WAS NOT CONFIRMED BY AN EXTERNAL VISUAL INSPECTION. A (RUN AS RECEIVED) WAS PERFORMED AND THE FOLLOWING WAS NOTED: ( PUMP CAPACITY WAS 7.8 QPM, SHOULD HAVE BEEN 9.0 QPM ) RELIEF VALVE PRESSURE WAS 440 PSI, SHOULD HAVE BEEN 465 +/- 20 PSI  MAGNETIC PICKUP WAS 3.2 VOLTS AT 3700 RPM, SHOULD HAVE BEE 4.5 +/- 0.2 VOLTS THE UNIT WAS SYSTEMATICALLY DISASSEMBLED IAW COMPONENT MM (CMM 33091C, 1986), AND SIGNIFICANT DAMAGE WAS FOUND TO SEVERAL INTERNAL       3  T          E2WE                 
20070503000342007050300034SO  2007       5          3          CA070403004      120070331G3250AN3H7A          ATTACH BOLT     PIPER                   PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  STEERING ARM    SHEARED         W      C   ABORTED TAKEOFF                                                                                 E  VIBRATION/BUFFET                                                              TOTAKEOFF        1                      CA                                                                      (CAN) DURING T/O ROLL DEPARTING CREW ABORTED T/O DUE A VIBRATION AND PULLING TO THE RIGHT. A/C TAXIED OFF RUNWAY, SHUTDOWN AND CREW VISUALLY INSPECTED A/C, NO DEFECTS NOTED. TAXIED BACK TO HANGER, MTCE WAS NOTIFIED.  MAINTENANCE INSPECTION REVEALED (2) STEERING ARM ATTACH BOLTS SHEARED. NLG INSPECTED FOR OVER STEERAGE FROM GROUND HANDLING, NO OBSERVED DEFECTS NOTED.  STEERING BOLTS REPLACED WITH NEW AND SYSTEM/TRAVEL/LANDING GEAR FUNCTION TESTS C/W .  (TC NR 20070403004)                                                                                                                                                                                                                                                     1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070503000352007050300035EA  2007       5          3          CA070403005      120070331G3820060150C1        WATER HEATER                            CNDAIRCL601 CL6013A     8070802EA  GE    CF34  CF343A      30015NE                              LAVATORY        ODOR            W      BA  EMER. DESCENT           UNSCHED LANDING                                                         B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA       5057                                                           (CAN) WHILE EN ROUTE, A BURNING ODOR WAS NOTICED BY THE CREW AND PASSENGERS.  NO SMOKE WAS APPARENT IN THE CABIN OR COCKPIT.  THEN SEARCHED THE LAVATORY AND BAGGAGE COMPARTMENT.  A TRACE OF SMOKE WAS FOUND IN THE BAGGAGE COMPARTMENT.  A QUICK VISUAL INSPECTION OF THE LUGGAGE WAS CARRIED OUT TO SEE IF THIS WAS THE SOURCE OF THE SMOKE.  IT WAS NOT.  UPON EXITING THE LUGGAGE COMPARTMENT THE SMOKE WAS SEEN SLOWLY ADVANCING TO THE PASSENGER CABIN.  CLOSED THE DOOR TO THE BAGGAGE AREA AS WELL AS TO THE LAVATORY.  BRIEFED THE PASSENGERS TO NOT OPEN THE DOORS AND MOVED THEM TO THE MOST FORWARD SEATING POSITIONS.  DECLARED AN EMERGENCY AND REQUESTED TO LAND.  A RAPID DESCENT WAS INITIATED AND THE QRH PROCEDURE FOR SMOKE2L72 4F4  FRTA21EA   E15NE                
20070503000362007050300036CE  2007       5          3          CA070404001      120070325G561010138402521     WINDSHIELD                              BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE FLIGHT THE L/H OUTER WINDSHIELD PANE CRACKED IN SEVERAL PLACES. THE CREW CARRIED OUT THE APPLICABLE PROCEDURES AND LANDED AT THE NEAREST AIRPORT. THE WINDSHIELD WAS INSPECTED BY MAINTENANCE AND THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY WHERE THE WINDSHIELD WAS REPLACED. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (TC NR 20070404001)                                                                                                                                                                                                                                                                                                                                                                      2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070503000372007050300037GL  2007       5          3          CA070404002      120070402G5511C2TP39ND        RIB             DHAV                    DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HARTZLHCB3R HCB3R304    GL  HORIZONTAL STAB CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  112                                                 (CAN) DURING MAIN SPAR REPLACEMENT AFTER COMPLETION OF SB 2/47, A SINGLE NOSE RIB WAS FOUND TO BE HEAVILY CORRODED.  AIRCRAFT TT 22235.0. THE AIRCRAFT OPERATES ON FLOATS IN A CORROSIVE ENVIRONMENT.  PREVIOUS CORROSION TREATMENT WAS NOT IN EVIDENCE (TC NR 20070404002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3R3  RRCA806    5E1     5  CP28EA    
20070503000382007050300038EA  2007       5          3          CA070404003      120070403G2797UK              WIRE HARNESS                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              RUDDER POSITION DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       30222                                                          (CAN) DURING AN INSPECTION, THE RUDDER POSITION TRANSMITTER HARNESS WAS FOUND TO BE DAMAGED. THE CAUSE OF THE DAMAGE WAS FOUND TO BE IMPROPER ROUTING BY COMPARING WITH ANOTHER A/C S/N 7163. THE ACTUAL ROUTING DRAWING WHERE REQUESTED FROM BOMBARDIER AND THE HARNESS WILL BE REPAIRED AND REROUTED PROPERLY. (TC NR 20070404003)                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA21EA   E15NE                
20070503000402007050300040EU  2007       5          3          CA070404004      120070404G2910AE2463774G0164  HOSE                                    AIRBUS310   A310304     3930339EU  GE    CF6   CF680C2A5        NE                              HYD SYSTEM      PUNCTURED       W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) GREEN HYDRAULIC ECAM MESSAGE LOW LEVER WARNING CAME ON AFTER TAKE OFF. ON ARRIVAL, MAINTENANCE FOUND THE RT MAIN LANDING GEAR DOWN LOCK ACTUATOR FLEX LINE HOSE LEAKING. FOUND HOLE IN FLEX LINE. FLEX LINE WAS REPLACED WITH BOTH HYDRAULIC PUMPS, CASE DRAIN FILTERS AND GREEN SERVO CONTROL MANIFOLD FILTERS.   (TC NR 20070404004)                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA35EU   E13NE                
20070504001072007050400107NM  2007       5          4          CA070404006      120070329G2781H1010262        SWITCH                                  BOEING727   727243      138408DNM  PWA   JT8   JT8D9A      52048NE                              NR 3 KRUGER     MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) ON FLAP RETRACTION THE CREW NOTICED THE NR 3 KRUGER FLAP INDICATED (IN TRANSIT).  CREW RETURNED TO BASE. NR 3 KRUGER FLAP RETRACT SWITCH WAS REPLACED AND A/C RETURNED TO SERVICE.  (TC NR 20070404006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L73 4F4  FRTA3WE    E2EA                 
20070504001092007050400109SW  2007       5          4          CA070404007      120070404G28102060636321      FUEL CELL                               BELL  206   206L1       1182107SW  ALLSN 250C  250C28      03013GL                              LEFT            LEAKING         W      O   OTHER                                                                                           KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            CRCRUISE         1                      CA                                                                      (CAN) RETURNING FROM A FLIGHT IT WAS NOTED THERE WAS A FUEL ODOR IN THE REAR CABIN. INVESTIGATING DETERMED THE LT FWD FUEL CELL HAD A SMALL LEAK. FUEL CELL WAS CHANGED OUT. (TC NR 20070404007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3U3  U  H2SW    E1GL                 
20070504001122007050400112CE  2007       5          4          CA070404008      120070329G571097430000150     CROSS TIE                               BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  BS 187          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       10546                                                          (CAN) THE STRUCTURAL PIECE CALLED A CROSSTIE P/N 97-430000-150 WAS FOUND CRACKED DURING INSPECTION. IPC / REF: 53-10-20 FIG. 20 ITEM NR 26. THE CRACK IS LOCATED LT SIDE OF AIRCRAFT AT FS 187.383 AND WL 119 ( LOWER LONGERON ). REPLACED WITH NEW. (TC NR 20070404008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4T4  T  A24CE   E4EA    6  CP56GL    
20070507000762007050700076EA  2007       5          7          CA070404009      120070401G2740706010          CONTROL UNIT                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              HORIZONTAL STAB MALFUNCTIONED   W      BA  EMER. DESCENT           UNSCHED LANDING                                                         F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) SHORTLY AFTER TAKEOFF, FLIGHT EXPERIENCED A HSTA RUNAWAY. ACFT HAD JUST DEPARTED RUNWAY  AND FLAPS WERE RETRACTED TO 0 DEGREES. AUTOPILOT DISENGAGED. TRIM SELECTION INPUT MADE.  STABILIZER TRIM CONTINUED TO RUN & ASSOCIATED AURAL ALERT SOUNDED.  IMMEDIATE ACTION CHECKLIST WAS COMPLETED, AS WAS QRH PROCEDURE.   MODERATE CONTROL PULL FORCES WERE REQUIRED TO FLY ACFT AT 10,000 & 250 KNOTS. CREW USED ACARS SYSTEM TO CALCULATE A WEIGHT & BALANCE, & REDISTRIBUTED CABIN LOAD TO ALLEVIATE CONTROL FORCES. ICE ENCOUNTERED AT 10,000 FT & REQUIRED DESCENT TO 8,000 FT.   EMERGENCY DECLARED.  ACFT RETURNED.    FLAPS SELECTED TO 20 DEGREES WHILE BETWEEN 8000 & 6000 FT.   CONTROL FORCES WERE SIGNIFICANTLY LIGHTER ONCE FL2L72 4F4  FRTA21EA   E15NE                
20070504001142007050400114EA  2007       5          4          CA070404010      120070328G5610NP13932113      WINDSHIELD                              CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C1          NE                              COCKPIT         FAILED          W      B   EMER. DESCENT                                                                                   O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) ON CLIMB OUT THROUGH 11000` PILOTS WINDSHIELD SHATTERED.  REMARKS FROM PILOT (TOOK OFF CLIMBING THROUGH 11000 OR 12000) THE LT FRONT PILOT WINDSHIELD SPIDERWEBBED AND SHATTERED.  IT SPIDERWEBBED ALL AT ONCE VERY QUICKLY.  WE DECLARED AN EMERGENCY, DESCENDED TO 8000 FT AND SLOWED THE AIRCRAFT DOWN TO 190 KNOTS.  COMPLETED THE QRH FOR LT WINDSHIELD HEAT.  TRANSFERRED THE CONTROLS TO THE FIRST OFFICER AND PREPARED FOR AN EMERGENCY LANDING.  BRIEFED THE FLIGHT ATTENDANTS AND SENT A MESSAGE TO DISPATCH VIA ACARS.  NEXT WE ADVISED OPS WE WERE RETURNING AND WERE ASSIGNED GATE.  FIRST OFFICER AND BRIEFED AN OVERWEIGHT LANDING AND COMPLETED IN RANGE AND BEFORE LANDING CHECKLIST.  CONDITIONS WERE GUSTY WINDS GUSTIN2L72 4F4  FRTA21EA   EOOO63EN             
20070504001182007050400118EA  2007       5          4          CA070404011      120070330G490038004883        APU                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                                              FAILED          W      F   ACTIVATE FIRE EXT.                                                                              B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA       4510                                                           (CAN) TECHNICIAN WAS TROUBLESHOOTING THE APU FOR APU AUTO SHUTDOWN, LOSS OF APU DOOR POSITION ON STATUS PAGE.  ECU CODE: 109,224,91  MAINTENANCE FOUND THE ELECTRICAL CONNECTOR FOR OIL TEMP SENSOR PARTIALLY INSTALLED ( CODE 91). RESECURED THE CONNECTOR AND PROCEEDED TO START THE APU. AT THAT TIME NO FUEL LEAK / OIL LEAK WERE NOTED IN THE APU ENCLOSURE.  START THE APU WITH NO PROBLEM AND WITH BOTH A/C PACKS RUNNING, A STRONG SMELL OF FUEL IN THE COCKPIT AND GALLEY AREA WAS NOTED. SOME FUEL ON THE GROUND AT THE DRAIN AREA WAS NOTED.  SHUTDOWN THE APU, CLIMBED IN THE AFT EQUIPMENT BAY, START TO OPEN THE OIL SERVICING PANEL ONCE A FEW FASTENERS WERE LOOSE THEN A FIRE FLARED UP. ASKED THE CREW TO DISCHARGE THE ONBOAR2L72 4F4  FRTA21EA   E15NE                
20070613001412007061300141CE  2007       6          13         CA070405001      120070404G7830LA7139A         BEARING                                 CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              THRUST REVERSER CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7285       2537                                                (CAN) WATER INFILTRATED BETWEEN SLEEVE P/N LA7140 AND BEARING P/N  LA7139A CAUSING PIN HOLE CORROSION IN THE BEARING JACKET, ALLOWING WATER TO COME IN CONTACT WITH THE DRIVER LINK P/N 202-0007-3 PIVOT POINT CORRODING IT BEYOND REPAIR. (TC NR 20070405001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 4F4  F  A22CE   E1NE                 
20070808001502007080800150CE  2007       8          8          CA070405003      120070215G272004310031        BELLCRANK                               CESSNA150   150         2071802CE  CONT  O200  O200A       17020SO  SNSNCH69CK  M69CK       EA  RUDDER          CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       10000                                                          (CAN) FOLLOWING ITEMS FOUND INSTALLED: TRIANGLE DOUBLERS IAW SL 150-27; ANGLE STIFFENER NOT INSTALLED IAW SL 65-10. ANGLE STIFFENER MIGHT BE INSTALLED IAW PERSONAL PLANE SERVICE LTD (OTTAWA). DRAWING NR PPS.161. HAVE NOT BEEN ABLE TO FIND A COPY OF PPS 161, AT THIS TIME (MARCH 29, 2007). IF CRACKED PART IS A NON CONFORMING PART, NO FURTHER ACTION IS NEEDED. MY CONCERNS IS THIS: IF PART IS IAW PPS 161, AND NO FURTHER ACTION IS REQUIRED AFTER INSTALLATION (A VERY LONG TIME AGO) AND THEY ARE CRACKING IN SERVICE IT COULD BE QUITE SERIOUS, IN MY OPINION TO LOSE RUDDER CONTROL. THE AREA IN QUESTION IS ALSO VERY DIRTY AND HARD TO LOOK AT DUE TO OIL ACCUMULATION AND DIRT. (TC NR 20070405003)                            1H71 3O3  ONT3A19    E252    5  NP9045    
20070504001202007050400120EA  2007       5          4          CA070405005      120070405G2120C6VF11531       FLAPPER VALVE   DHAV                    DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA                              RAM AIR DUCT    OBSTRUCTED      W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       14                                                             (CAN) THE RAM AIR FLAPPER VALVE, P/N C6VF1153-1, BECAME JAMMED IN IT`S DUCT. ATTEMPTS BY THE PILOT TO RECTIFY THE PROBLEM BY MOVING THE CONTROL LEVER BACK AND FORTH RESULTED IN THE CONTROL CABLE, P/N 130-032A22.75B29.0, BECOMING KINKED AND UNSERVICEABLE.  DIS-ASSEMBLY OF THE SYSTEM REVEALED THAT THE RUBBER-LIKE MATERIAL USED TO SEAL THE PERIMETER OF THE FLAPPER VALVE HAD BECOME DISTORTED AND ENLARGED, POSSIBLY DUE TO EXPOSURE TO HEAT. THIS CAUSED THE SEAL TO CONTACT THE INNER WALLS OF THE DUCT BEFORE THE FLAPPER WAS AT A 90-DEGREE ANGLE TO THE DUCT, IE: BEFORE THE FLAPPER WAS IN THE CLOSED POSITION.  REMOVAL AND REPLACEMENT OF THE DAMAGED CABLE AND FLAPPER VALVE REQUIRED REMOVAL AND REPLACEMENT OF MUCH OF THE A1H72 3T4  TRTA9EA    E4EA                 
20070504001222007050400122EA  2007       5          4          CA070405006      120070405G32507116111         COLLAR                                  DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  STEERING SYS    CRACKED         W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) STEERING COLLAR CRACKED AT RADIUSED AREA OF ATTACH STUD TO STEERING ACTUATOR. FOUND AT ROUTINE MAINTENANCE INSPECTION (TC NR 20070405006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20080221000032008022100003CE  2008       2          21         CA070405007      120070321G7603565549012       THROTTLE CONTROL                        CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A105 1A105*      GL                  BROKEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA       4475                                                           (CAN) PILOT REPORTED STRANGE, SPRINGY FEELING TO THROTTLE CONTROL. IT WAS DISCOVERED THAT THE OUTER PART OF THE CONTROL HAD SEPARATED WHERE IT WAS SWAGED TO THE FLEXIBLE, SPIRAL ROUND PART OF THE CONTROL. (TC NR 20070405007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A19    E223    5  NP918     
20070504001232007050400123EA  2007       5          4          CA070405008      120070405G3220713381          TORQUE LINK                             DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  NLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) LOWER TORQUE LINK CRACKED AT ATTACHMENT LUG TO UPPER TORQUE LINK. CRACK FOUND ON ROUTINE MAINTENANCE INSPECTION (TC NR 20070405008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070511000022007051100002EA  2007       5          11         CA070405009      120070403G2450VS643           RELAY                                   CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              JUNCTION BOX NR6BURNED          W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE IB, FLIGHT CREW NOTICED AN AC ESSENTIAL BUS MESSAGE FOLLOWED BY A POPPING SOUND AND A BURNED ODOR ON THE FLT DECK. LOOKED AT AC ELECTRICAL SYNOPTIC PAGE AND EVERYTHINGS WAS NORMAL BUT THE F/A NOTICED THAT THE EMERGENCY LIGHTS WERE ON. FLIGHT CREW APPLIED QRH AND CARRIED ON FLIGHT.  ON ARRIVAL AT THE GATE, BURNED ODOR WAS STRONGER AND THEY SHUTDOWN EVERYTHING INCLUDING THE APU.  AFTER INVESTIGATION, MAINTENANCE FOUND AC ESSENTIAL RELAY K1XD BURNED IN JB6 AND CARBON TRACES WERE FOUND ON THE RELAY SOCKET AND JB6 BRACKET/CASING.  REF LOG NR 565535 AC ESSENTIAL SENSE RELAY K1XD P/N VS 643 AND RELAY SOCKET PN S0-1021-7127 WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070405009)     2L72 4F4  FRTA21EA   E15NE                
20070504001242007050400124SO  2007       5          4          CA070405010      120070405G3220203601042       AXLE            CURTIS                  CURTISC46   C46DAIRLIFT        SO  PWA   R2800 R280051     52026NE  HAMSTD23E   23E50       NE  TAIL GEAR       FRACTURED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING TAXI TO RUNWAY POSITION, TAIL WHEEL AXEL FRACTURED RESULTING IN TAIL WHEEL DEPARTING TAIL GEAR ASSEMBLY.  TAXI WAS AT SLOW SPEED BUT TAIL FORK DAMAGED DURING AXEL FAILURE.  TAIL WHEEL FORK AND AXEL ASSEMBLY, WERE REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070405010)                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4R4  R  3A2     5E8     6  CP603     
             20080520     CE  2008       5          20         CA070405011      120070403G711005521335        SUPPORT                                 CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160DTM    GL  ENGINE COWL     CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       48                                                             (CAN) THE ORIGINAL PART WAS FOUND CRACKED AND WAS REPLACED LESS THAN 50 HOURS AGO. THE CRACKS ORIGINATE AT THE 4 OCLOCK AND 8 OCLOCK POSITIONS, AT THE END OF THE FLANGED SECTION OF THE SUPPORT. SUBMITTER SUSPECTS THAT THE PULSATING AIRFLOW FROM THE PROPELLER, WHICH IS IMMEDIATELY IN FRONT OF THIS ASSEMBLY, IS RESPONSIBLE FOR THE FATIGUE CRACKING.                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    E274    5  NP910     
20070504001252007050400125NM  2007       5          4          CA070407001      120070404G5280                DOOR                                    DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  NLG             DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4480344803                                                     (CAN) MAINTENANCE CARRIED OUT A LIGHTENING STRIKE INSPECTION IAW AMM 05-50-31 AND DAMAGE WAS NOTED ON THE RT FWD NOSE GEAR DOOR, BURN AND PITTING MARKS ON BELLY FUSELAGE AND LT ELEVATOR STATIC WICK WAS BURNED OFF.  NDT WAS CARRIED OUT AND THE BELLY SKIN WAS REPAIRED IAW MFG RD8-53-9556 ISSUE 1, TEMP REPAIR FOR 1000 HRS.  THE ELEVATOR TIP FAIRING FASTENERS WERE REPLACED IAW SRM AND THE STATIC WICK WAS REPLACED AND BONDING CHECKS WERE CARRIED OUT.  RT NOSE GEAR DOOR A SCREW WAS REPLACED.  ALL SYSTEMS AND FLIGHT CONTROLS FUNCTION CHECKED SERVICEABLE AND THE A/C WAS RETURNED TO SERVICE. (TC NR 20070407001)                                                                                                               2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070511001012007051100101NE  2007       5          11         CA070409001      220070330G7200                ENGINE                                  CNDAIRCL600 CL6002D24   1390016EA  GE    CF34  CF348E5     30015NE                              NR 1            MALFUNCTIONED   W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                          194243                      (CAN) ON TAKEOFF ROLL, 1ST OFFICER NOTICE A MOMENTARY FLUCTUATION OF ABOUT 2% ON NR 1 N1 GAGE JUST AFTER THE 80 KNOTS CALL.  N1 THEN STABILIZED UNTIL REACHING JUST OVER 100 KNOTS, FLUCTUATED AGAIN.  DID NOT HEAR OR FEEL ANY CHANGES IN ENGINE.  THERE WERE NO EICAS MSG AND ALL OTHER ENGINE READOUTS WERE STABLE AND NORMAL.  THIS WAS POSSIBLY A ERRONEOUS N1 READOUT, ELECTED TO CONTINUE TAKEOFF.  EVERYTHING NORMAL ON CLIMB UNTIL SHORTLY AFTER ACCELERATION ALTITUDE WHEN NR 1 N1 BEGAN TO FLUCTUATE MORE SIGNIFICANTLY.   COULD NOW HEAR AND FEEL NR 1 ENGINE SURGING. WITHIN SECONDS, ENGINE WENT INTO AN OVERSPEED CONDITION ACCOMPANIED BY A FADEC FAULT 1 STATUS MSG. BROUGHT THRUST LEVER TO IDLE, NO EFFECT.  DECLARED AN EMER2L72 4F4  FRTA21EA   E00063EN             
20070507001762007050700176EA  2007       5          7          CA070409002      120070404G2913R1309P216       PLUG                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              RT EDP          MISSING         W      B   EMER. DESCENT                                                                                   KJYFLUID LOSS                WARNING INDICATION        ENGINE STOPPAGE           CRCRUISE         1                      CA       8717                                                           (CAN)  AFTER TAKEOFF FROM SOUTH BEND (SBN), THE AIRCRAFT CLIMBED TO FL 290. SHORTLY AFTER REACHING CRUISE ALTITUDE, THE RT ENGINE OIL PRESS WARNING ILLUMINATED FOLLOWED BY A DROP IN THE OIL PRESSURE ON THE RT OIL PRESSURE GAUGE. THE FLIGHT CREW PERFORMED THE QRH PROCEDURES AND REDUCED POWER ON THE RT ENGINE. SEEING THAT THE OIL PRESSURE CONTINUED TO DROP, THE CAPTAIN ELECTED TO SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL APPROACH AND LANDING WAS MADE AT MSP.  UPON LANDING, MAINTENANCE FOUND THAT THE AIRCRAFT HAD A MEL OPENED FOR NR 2 ENGINE DRIVEN HYDRAULIC PUMP. FURTHER INVESTIGATION REVEALED THE RT EDP HAD NOT BEEN PROPERLY MEL`D AND THAT THE OIL LOSS WAS THE RESULT OF A MISSING SPLINE PL2L72 4F4  FRTA21EA   E15NE                
20070504001262007050400126CE  2007       5          4          CA070409003      120070404G291025800           SELECTOR VALVE                          BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  HYD SYSTEM      LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    DEDESCENT        1                      CA            2                                                         (CAN) VALVE WAS OVERHAULED BY VENDOR. AFTER OVERHAUL IT WAS INSTALLED IN THE AIRCRAFT. AFTER 2 HOURS OF OPERATION A LEAK DEVELOPED. THE VALVE WAS REMOVED AND DISTRIBUTION MANIFOLD DISASSEMBLED. WHEN CHECKING THE IPC IT WAS NOTED THAT AT OVERHAUL, THE OVERHAUL FACILITY FAILED TO INSTALL 2 O-RINGS. THE O-RINGS WERE INSTALLED AND RE-ASSEMBLED, THE AIRCRAFT GEAR SWING CARRIED OUT SATISFACTORY (TC NR 20070409003)                                                                                                                                                                                                                                                                                                                     1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070808001512007080800151CE  2007       8          8          CA070409004      120070402G5610551127517       WINDOW                                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              COCKPIT         DELAMINATED     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) PILOT`S STORM WINDOW DELAMINATED AT UPPER EDGE, RESULTING IN A CRACK FROM ATTACH HOLE RADIUS TO AFT EDGE. (TC NR 20070409004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 4F4  F  A22CE   E1NE                 
20070504002212007050400221SO  2007       5          4          CA070409005      120070406G2823                SELECTOR                                PIPER PA23  PA23250     7102308SO  LYC   O540  IO540C4B5   41532EA  HARTZLHCE2Y HCE2YR2     GL  FUEL            FAILED          W      D   RETURN TO BLOCK                                                                                 Y  ENGINE STOPPAGE                                                               TXTAXI/GRND HDL  1                      CA                                                                      (CAN) DURING FUNCTIONAL TEST PRIOR TO TAKEOFF, WHEN MOVING FUEL SELECTOR FROM OB TO IB TANKS THE ROLL PIN CONNECTING THE FUEL SELECTOR HANDLE TO THE LINKAGE FAILED.  THIS FAILURE LEFT THE RT ENGINE FUEL SELECTOR IN THE OFF  POSITION, STARVING THE ENGINE FOR FUEL.  THE AIRCRAFT RETURNED TO THE RAMP FOR REPAIRS.    (TC NR 20070409005)                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3O3  O  1A10    1E4     5  CP9EA     
20080219003672008021900367CE  2008       2          19         CA070409006      120070405G3230508103385       DRAG BRACE                              BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  LT MLG          FAILED          W      O   OTHER                                                                                           Z  SIGNIFICANT FAILURE REPORT                                                    TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AC WAS DISCOVERD OUTSIDE HANGER WITH THE LT MLG COLLAPSED.  THE FAULT OF THE PROBLEM WAS THE LT MLG DRAG BRACE. IT WAS REPLACED RECENTLY WHEN A SIMILIAR INCIDENT OCCURED TO THE RT MLG DRAG BRACE CAUSING THE LT MLG TO COLLAPSE WHILE BEING TOWED. DAMAGE CAUSED FROM THIS INCIDENT WAS AS FOLLOWS, DAMAGE TO LT WING TIP, LT MLG DOORS, LT MLG ACTUATOR, VHF ANTENNA. THE AIRCRAFT WAS LIFTED AND JACKED AND A LOCALLY MFG DOWNLOCK WAS INSTALLED. THE AIRCRAFT IS IN THE PROCESS OF BEING INSPECTED FOR OTHER DAMAGE. THIS IS ONLY A PRELIMINARY REPORT, A MORE CONCLUSIVE REPORT WILL BE ADDED WHEN FINDINGS ARE COMPLETE. (TC NR 20070409006)                                                                                       1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070507000772007050700077WP  2007       5          7          CA070409007      220070228G7314                GEAR                                                                       GARRTTTPE331TPE33110UG  01514WP  ROTOL R333  R333482F12  GL  FUEL PUMP       UNKNOWN         W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                          P63259                      (CAN) GEARS DRIVING THE FUEL PUMP FAILED CAUSING THE ENGINE TO SHUTDOWN IN FLIGHT. (TC NR 20070409007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 4  T          E4WE    6  CP61GL    
20070507000782007050700078NE  2007       5          7          CA070410001      220070408G7260                CASE                                    DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF15      NE  ACC GEARBOX     CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       3019810612                         PW123150                    (CAN) ON MARCH 28TH/07 IT WAS REPORTED AN OIL LEAK ON NR 2 ENGINE. THE OIL LEVEL WHEN DOWN 2L IN 5.55 HOURS OF FLIGHT TIME. THE PROPELLER ASSY AND THE LT SIDE OF THE ENGINE WAS REPORTED TO HAVE BEING WASHED WITH OIL AND BOTH THEY WERE INSPECTED FOR LEAKAGE. NO SIGNS OF DETERIORATION FOUND AT THE TIME AND IT WAS DECIDED TO DO A POWER RUN CHECK. AGAIN NO SIGNS OF LEAKAGE FOUND. ON MARCH 29TH/07 WAS REPORTED ANOTHER OIL LEAKAGE FROM NR 2 ENGINE. PERSONNEL INVESTIGATED THE PROPELLER AND THE ENGINE AND IT WAS FOUND AN APPROXIMATE 2. (TC NR 20070410001)                                                                                                                                                                       2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070507000792007050700079EU  2007       5          7          CA070410002      120070408G27501700637         DRIVE SHAFT                             EMB   ERJ170ERJ170100          EU  GE    CF34  CF348E5A1   30015NE                              FLAP DRIVE      DAMAGED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) DURING APPROACH, THERE WAS A FLAP FAIL MSG. ACFT LANDED WITH FLAPS LOCKED OUT.  TROUBLESHOOTING REVEALED THAT GEARBOX SPLINED SHAFT AND DRIVE SHAFT WERE NOT LOCKED INTO PLACE BY LOCK SCREW.  SIMILAR SCENARIO OCCURRED ON RHS, WHERE THE IB MOST FLAP ACTUATOR DISCONNECTED WITH THE SPLINE IN THE SAME WAY.  THE LOCKBOLT WAS IN PLACE AND SAFETIED, BUT WAS NOT INSTALLED THROUGH THE HOLE IN THE SPLINED SHAFT. ANGLED GEARBOX PN IS AS ABOVE, BUT FLAP ACTUATOR PN IS C154814-2. (TC NR 20070410002)                                                                                                                                                                                                                                2L72 4F4  FRTA56NM   E00063EN             
20070808001522007080800152CE  2007       8          8          CA070410003      120070327G3233NAS464P4A29     BOLT                                    CESSNA210   210L        2073448CE  CONT  O520  IO520L      17032SO  HARTZLHCJ3Y PHCJ3YF1    GL  LT MLG ACTUATOR BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ON SCHEDULED INSPECTION APPRENTICE FOUND ONE ATTACH BOLT BACKED OUT OF HOLE. ON REMOVING THE BOLT FULLY HE FOUND THE BOLT TO BE BROKEN. THE AIRCRAFT WAS JACKED UP AND THE ACTUATOR WAS REMOVED. THE OTHER 2 ATTACH BOLTS WERE INSPECTED AND FOUND WORN. THE ACTUATOR WAS INSPECTED FOR CRACKS. NONE FOUND. THE ATTACH BULKHEAD WAS INSPECTED ALSO. NO FAULTS WERE FOUND. THE ACTUATOR WAS REINSTALLED WITH NEW BOLTS. GEAR WAS SWUNG AND AIRCRAFT RETURNED TO SERVICE. SUSPECT THAT AS THERE ARE NO LOCKING DEVICES OTHER THAN TORQUE, BOLTS LOOSENED OVER TIME AND BOLT BROKE DUE TO GEAR TRANSIT FORCES. (TC NR 20070410003)                                                                                                           1H71 3O3  O  3A21    E5CE    5  CP36EA    
20070507001782007050700178EU  2007       5          7          CA070410004      120070406G5753                BELLCRANK                               PZLWARWILGA PZL104W35A  7360104EU  LYC   O540  IO540K1B5   41532EA  HARTZLHCE3Y HCE3YR1     GL  TE FLAPS        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       276                                                            (CAN) LOWER LT FLAP ACTUATOR BELLCRANK SUPPORT BRACKET CRACKED AT UPPER END. WHEN FLAP IS SUBJECTED TO A SIMULATED AIR LOAD, THE SUPPORT BRACKET FLEXES AND THE CRACK VISIBLY OPENS.  THIS BRACKET HAS EVIDENCE OF PREVIOUS REPAIR (A DOUBLER IS PRESENT AT THE LOWER END). NONE OF THE OTHER (3) SUPPORT BRACKETS HAVE ANY DOUBLERS OR SHOW ANY EVIDENCE OF CRACKS. (TC NR 20070410004)                                                                                                                                                                                                                                                                                                                                                        1H71 3R3  ONCEXPA1H711E4     5  CP33EA    
20070507001802007050700180SW  2007       5          7          CA070411001      120070409G6310209340265103    SEAL                                    BELL  407   407         1182206SW                                                               FREEWHEEL UNIT  LEAKING         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA       395                                                            (CAN) TRANSMISSION OIL PRESSURE DROP (2) BARS BELOW THE GREEN.  ON ROUTE BACK TO BASE THE TRANSMISSION OIL LOW PRESSURE LIGHT CAME ON UPON LANDING.  THE ENGINE DECK IS COVERED WITH OIL. THE FREEWHEEL AFT SEAL HAD POPPED OUT OF ITS BORE, RESULTING IN A LOSS OF OIL. (TC NR 20070411001)                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3U    O H2SW                         
20070507000802007050700080EU  2007       5          7          CA070411002      120070405G3230A2757040500200  SWITCH                                  AIRBUS310   A310304     3930339EU  GE    CF6   CF680C2A5        NE                              MLG             STICKING        W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB THE AIRCRAFT HAD A (KRUGER) FAULT ECAM WARNING.QAH CARRIED OUT BUT WARNING REMAINED ON. AIRCRAFT RETURNED TO THE STATION. DURING TROUBLESHOOTING THE BITE TEST ON THE SFCC 1 AND 2 FAULTED THE RT RETRACT SWITCH. THE SWITCH WAS FOUND DIRTY AND STICKING AND TARGET WAS FOUND WORN. SWITCH WAS CLEANED AND TARGET ADJUSTED IAW MM. SYSTEM WAS TESTED SERVICEABLE.  (TC NR 20070411002)                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA35EU   E13NE                
20080220000072008022000007SW  2008       2          20         CA070411003      120070317G6320                DRIVE GEAR      KAMAN       K974002103  KAMAN K1200 K1200       05625F6SW  LYC   T53   T5317A1LYC  41615NE                              TRANSMISSION    DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 JZ WARNING INDICATION        SIGNIFICANT FAILURE REPORT                          ININSP/MAINT     1                      CA       7556 2748  AA1825                                              (CAN) DURING THE INITIAL START UP OF THE DAY, AT APPROX 10 PERCENT ROTOR RPM, AN ABNORMAL NOISE WAS HEARD COMING FROM THE POWER TRAIN AND A TRANSMISSION CHIP WARNING LIGHT INDICATION. THE START WAS THEN ABORTED. THE ATTENDING AME INSPECTED THE TRANSMISSION SYS CHIP PLUGS AND FOUND AN ABUNDANCE OF PARTICLES OF ON THE LT SUMP CHIP PLUG.  PRODUCT SUPPORT WAS CONTACTED AND WANTED US TO REMOVE THE OIL PUMP AND THE OIL PUMP DRIVE ASSY AND INSPECT THE OIL PUMP DRIVE GEAR FOR DAMAGE. THIS INSPECTION REVEALED THE DRIVE GEAR HAD SUSTAINED SIGNIFICANT DAMAGE. THIS GEAR IS INSIDE THE TRANSMISSION MAIN HOUSING AND IS NOT FIELD REPAIRABLE ITEM. THE TRANSMISSION WAS SUBSEQUENTLY REPLACED ON LOCATION WITH TSO 0.0 UNIT INSTALLE1G71 4F4  UNTTR7BO   E17EA                
             20081104     WP  2008       11         4          CA070411004      120070408G6310V31001          SWITCH                                  ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              CLUTCH ASSY     UNSERVICEABLE   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA       507                                                            (CAN) DURING GROUND RUN AND PRE-TAKEOFF CHECKS, THE CLUTCH FAILED TO ENGAGE. SWITCH V3-1001 IS SPRING LOADED AND BREAKS AND THE CLUTCH WILL NOT ENGAGE. THESE SWITCHES ARE A WEAK PART OF THE SYSTEM. (TC NR 20070411004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3O3  O  H11NM   1E4                  
20070507000812007050700081EA  2007       5          7          CA070411005      120070410G5310C3FS249         STRUT                                   DHAV  DHC3  DHC3        2800202EA  PWA   R1340 R1340*      52016NE  HAMSTD23D   23D40       NE  WINDSCREEN      CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING REPLACEMENT OF THE LT WINDSCREEN, CORROSION WAS FOUND ON THE STRUT PN C3FS2-49.  AFTER REMOVAL OF SEALANT IT WAS NOTED THE STRUT WAS CORRODED COMPLETELY THROUGH ONE OF THE WALLS OF THE STRUT.   RT STRUT INSPECTED AND NO FAULT FOUND (TC NR 20070411005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3R3  R  A815    5E2     6  CP719     
20070507000822007050700082    2007       5          7          CA070411006      420070411G230052611           CONTROL PANEL                           DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF15      NE  AUDIO CONTROL   BURNED          W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA       325134328                                                      (CAN) ENROUTE CREW NOTICED SMOKE COMING FROM AUDIO CNTRL PANEL, PULLED CIRCUIT BREAKER, SMOKE STOPPED. CREW DONNED O2 MASKS AND ELECTED TO RETURN TO ORIGINATING AIRPORT FOR NORMAL LANDING. MAINTENANCE REPLACED LT AUDIO CNTRL PANEL AND AIRCRAFT RETURNED TO SERVICE (TC NR 20070411006)                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070507000832007050700083SW  2007       5          7          CA070412001      120070320G7120206062102001    MOUNT                                   BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ON A ROUTINE ENGINE REPLACEMENT, IT WAS FOUND THAT THE LT LOWER ENGINE MOUNT WAS CRACKED AT THE ATTACH POINT. AFTER CLOSER INSPECTION THE MOUNT WAS COMPLETELY SEPARATED FROM THE AIRFRAME. THERE WAS NO INITIAL INDICATION OF A PROBLEM. IT WAS FOUND THAT THERE WAS EXCESSIVE TORQUE ON THE ATTACH BOLT TO THE AIRFRAME. THE ATTACH POINT WAS ALSO CUPPED TO INDICATE THAT THE PROPER PROCEDURE WAS NOT USED TO REMOVE THE ENGINE IE; LOOSENING THE ENGINE MOUNTS FIRST. (TC NR 20070412001)                                                                                                                                                                                                                                            1G71 3U3  U  H2SW    E4CE                 
             20081104     EA  2008       11         4          CA070412002      120070411G324650105844        WHEEL                                   CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              MLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6421 1492                                                      (CAN) DURING ROUTINE NDT HFEC INSP OF MAIN WHEELS, ACCORDING TO ABSC NDT MANUAL PART 1, CH. 32-42-03, CRACKS WERE FOUND IN THE LOCKING RING GROOVE. THE DEPTH OF 3 CRACKS IS GREATER THAN .040 INCH AND THE LENGTH OF THE CRACKS ARE 30MM, 20MM AND 5MM. ONE CRACK HAS A DEPTH OF .020 INCH AND A LENGTH OF 20MM. COMPONENT COULD BE SENT FOR MACHINING, BUT THE DEFECT DEPTH IS ALREADY GREATER THAN THE MACHINING LIMITS.                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA21EA   E15NE                
             20081104     EA  2008       11         4          CA070412003      120070411G324650105844        WHEEL                                   CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              MLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6421 1492                                                      (CAN) DURING ROUTINE NDT HFEC INSP OF RJ MAIN WHEELS, ACCORDING TO NDT MANUAL PART 1, CH. 32-42-03, CRACKS WERE FOUND IN THE LOCKING RING GROOVE. THE DEPTH OF 3 CRACKS IS GREATER THAN .040 INCH AND THE LENGTH OF THE CRACKS ARE 30MM, 20MM AND 5MM. ONE CRACK HAS A DEPTH OF .020 INCH AND A LENGTH OF 20MM. COMPONENT COULD BE SENT FOR MACHINING, BUT THE DEFECT DEPTH IS ALREADY GREATER THAT THE MACHINING LIMITS.                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA21EA   E15NE                
20070507000842007050700084NE  2007       5          7          CA070412004      220070330G7323116085023       GOVERNOR                                BELL  205   205A1       1181414SW  LYC   T53   T5317A      41549NE                              ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2920 1160                          LE07576                     (CAN) DURING THE DAILY INSPECTION PERFORMED BY THE ENGINEER, THE SCREW HOLDING THE GOV SERVO LEVER PLATE IN PLACE WAS ENTIRELY BACKED OUT OF THE HOLE.  THIS PART HAD BEEN REPLACED, TESTED AND ADJUSTED AT TSN 2346.3 FOR LOOSE SCREWS.  THE SCREWS ARE STAKED IN PLACE AND YET WERE STILL ABLE TO BACK OUT. THE GOVENOR WAS SENT FOR REPAIR. THE SCREW MAY POISE A RISK IN JAMMING THE SERVO LEVER. (TC NR 20070412004)                                                                                                                                                                                                                                                                                                                       1G71 4U4  U  H1SW    E17EA                
20070507000852007050700085NM  2007       5          7          CA070412005      120070407G3110B030302104C94   HOSE                                    BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  INSTRUMENT PANELCUT             W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       908                                                            (CAN) CREW REPORTED THAT THE INTEGRATED STANDBY ELECTRONIC INSTRUMENT WAS NOT READING THE SAME AS THE PRIMARY FLYING DISPLAYS.  INVESTIGATION REVEALED THAT THE LINES TO THE INSTRUMENT HAVE TO BE REMOVED TO PERFORM AD CF2005-15 PART B.  ON REASSEMBLY IF THE LINES ARE NOT ORIENTED PROPERLY THAT WILL CHAFE ON STRUCTURE. (TC NR 20070412005)                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070507000972007050700097EA  2007       5          7          CA070413001      120070407G7830                COWLING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              THRUST REVERSER DEPARTED        W      BA  EMER. DESCENT           UNSCHED LANDING                                                         DE INFLIGHT SEPARATION       VIBRATION/BUFFET                                    CRCRUISE         1                      CA                                                                      (CAN) A/C EXPERIENCED A THRUST REVERSER UNLOCK IN FLIGHT AT A CRUISE FLIGHT LEVEL OF 16000 FEET WITH AN APPROXIMATE SPEED OF 280 KNOTS.  A SMALL VIBRATION IN THE AIRFRAME WAS FELT BY THE CREW PRIOR TO RECEIVING THE (REVERSER UNLOCK) MSG, FOLLOWED BY A LOUD BANG, WITH THE AIRCRAFT PITCHING UP AND ROLLING LT. THE CREW STOWED THE REVERSER AND VIBRATIONS SUBSEQUENTLY STOPPED.  UPON LANDING INTO ORD UNDER A DECLARED EMERGENCY, IT WAS NOTE THAT T/R TRANSLATING COWLS WERE MISSING, ALONG WITH THE STRUCTURAL DAMAGE TO THE VERTICAL AND HORIZONTAL STAB.  LIST OF AFFECTED COMPONENT TO FOLLOW. (TC NR 20070413001)                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20070507000982007050700098NM  2007       5          7          CA070413002      120070409G323069141061        CYLINDER                                BOEING727   727233      138408ANM  PWA   JT8   JT8D15      52051NE                              NLG             FAILED          W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) THE CREW OBSERVED AN A SYSTEM DEPLETION CONDITION AFTER EXTENDING THE LANDING GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NOSE LANDING GEAR SYSTEM TRANSFER CYLINDER HAD FAILED. THE CYLINDER HAD FAILED AT THE LAST END CAP THREAD. THE UNIT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070413002)                                                                                                                                                                                                                                                                                                                                                                                         2L73 4F4  FRTA3WE    E2EA                 
20080219003682008021900368EA  2008       2          19         CA070413003      120070411G3240B121            PEDAL                                   FOUND FBA   FBA2C1      3640103EA                                                               COCKPIT         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       147                                                            (CAN) DURING CLEAN UP AFTER THE REPLACEMENT OF THE FUEL GAUGE ON AC 52 MECHANIC NOTICED THAT THE CO-PILOTS BRAKE-PEDAL ASSY WAS CRACKED. AFTER DISCUSSION WITH CHIEF ENGINEER HE NOTED THAT THIS WAS THE SECOND TIME, IT HAD HAPPENED PREVIOUSLY TO AC 53. FOUND MFG HAS INITIATED A MATERIAL REVIEW BOARD, A SB WILL BE MAILED OUT. THE SB WILL REQUIRE AN IMMEDIATE VISUAL INSPECTION TO THE BRAKE PEDAL AND A VISUAL INSPECTION EVERY 100 HOURS AFTERWARDS. IF A CRACK IS FOUND OR TO TERMINATE THE SB, A DOUBLER WILL BE INSTALLED. A TEST FIXTURE WILL BE FABRICATED TO TEST THE CRACKED BRAKE PEDAL TO FIND THE RESIDUAL LOAD. THE FIXTURE WILL ALSO BE USED TO TEST A REPAIRED PEDAL AND A NEW DESIGN OF BRAKE PEDAL. (TC NR 20070413003)1H71 3O    NCA7EA                         
20070507000992007050700099EA  2007       5          7          CA070413004      120070410G6120C6NF1117        CONTROL BOX                             DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  BETA SYSTEM     FAILED          W      C   ABORTED TAKEOFF                                                                                 FJ FLT CONT AFFECTED         WARNING INDICATION                                  TOTAKEOFF        1                      CA                                                                      (CAN) THE AIRCRAFT WAS BEING USED FOR CREW TRAINING WHEN, ON TAKEOFF, THE RT PROPELLER RPM DROPPED TO 30 PERCENT. THE PILOTS ABORTED THE TAKEOFF AND RETURNED TO THE RAMP. THE PILOTS NOTED THAT NP WAS STILL AT 30 PERCENT WITH THE POWER LEVER AT IDLE. THE PROPELLER WAS FEATHERED WITH THE PROP LEVER AND IT DID SO. WHEN THE PROP LEVER WAS SELECTED FULLY FWD THE PROPELLER WOULD NOT UNFEATHER. TROUBLESHOOTING REVEALED THAT THERE WAS POWER TO THE BETA BACKUP SOLENOID VALVE. FURTHER TROUBLESHOOTING LED BACK TO THE BETA BACKUP CONTROL BOX P/N C6NF1117. THIS WAS REPLACED AND THE AIRCRAFT CHECKED SERVICEABLE.  IT IS SUSPECTED THAT RELAY K4 MAY HAVE MALFUNCTIONED. THE CONTROL BOX IS BEING RETURNED TO THE OEM FOR EXAMINATIO1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
             20081104     CE  2008       11         4          CA070416001      120070413G8011PM2401          HOUSING         LAMAR                   CESSNA172   172R        2072401CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  STARTER         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       965                                                            (CAN) PILOT ATTEMPTED TO START THE ACFT. ALL THAT COULD BE HEARD WAS A CLICKING NOISE. FURTHER INVESTIGATION REVEALED THE FWD HSG WAS CRACKED CAUSING THE INCORRECT ENGAGEMENT OF THE STARTER BENDIX. STARTER WAS REPLACED AND ACFT RETURNED TO SERVICE. (TC NR 20070416001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  ONT3A12    1E10    5  NP857     
20070507001012007050700101CE  2007       5          7          CA070416002      120070413G77203034389         PROBE                                   BEECH 99    99          1154002CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  ENGINE T5       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) 7 OUT OF 8 T5 INDICATION PROBES WERE FOUND WITH LOOSE OR BROKEN TERMINALS AND MISSING CERAMIC INSULATION.  THE PROBES APPEAR TO QUITE FRAGILE IN COMPARISON TO THE OEM PART.  THE PARTS IN QUESTION ARE PMA PARTS, THEIR PN 26584.  PROBES REPLACED AND AIRCRAFT RETURNED TO SERVICE (TC NR 20070416002)                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20070507001022007050700102NM  2007       5          7          CA070416003      120070415G3297471515          WIRE HARNESS                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NLG             DAMAGED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER T/O LANDING GEAR WOULD NOT RETRACT WHEN SELECTED.  A/C RETURNED TO BASE FOR MAINTENANCE INSPECTION. HARNESS WOW NR 2 REPLACED IAW AMM. A/C RTS (TC NR 20070416003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070507001052007050700105NM  2007       5          7          CA070416004      120070413G6120699018002       CONTROL UNIT                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NR 2 PROP       FAILED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         FJ FLT CONT AFFECTED         WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) CREW COMPLETED A NR 2 ENGINE SHUTDOWN MANUALLY (IFSD) DUE POWERPLANT MESSAGE AND PEC CAUTION. MAINT ARRIVED AND FC 161 CH A AND B. FIM TASK PERFORMED. NO CONTACT WITH MPU AND BUSS BARS. REMOVED & REPLACED PEC. (TC NR 20070416004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070507001062007050700106EA  2007       5          7          CA070416005      120070413G3297                CONNECTOR                               CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              SELECTOR VALVE  CONTAMINATED    W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA       149778924  1999                                                (CAN) ON APPROACH NOSE LANDING GEAR DID NOT EXTEND.  CREW CARRIED OUT A GO-AROUND AND COMPLETED A MANUAL EXTENSION.  THE GEAR LOWERED AND LOCKED-CREW RECEIVED 3 GREENS IN THE COCKPIT.  THE AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE WAS DISPATCHED TO TROUBLESHOOT.  PSEU CODES READ AND FORWARDED TO TECH OPS.  AFTER CONSULTATION WITH TECH OPS, SUSPECT THE NLG SELECTOR VALVE AT FAULT.  AFTER FURTHER INSPECTION IT WAS NOTED THAT THE NLG SELECTOR VALVE HAD A SLIGHT LEAK NR THE SOLENOID CONNECTOR PLUG WAS CONTAMINATED WITH HYD FLUID.  THE SELECTOR VALVE WAS REPLACED AND GEAR SWINGS WERE CARRIED OUT WITH NFF AND A/C WAS RETURNED TO SERVICE WITHOUT ANY FURTHER INCIDENTS.  (TC NR 20070416005)                         2L72 4F4  FRTA21EA   E15NE                
20070507001072007050700107NM  2007       5          7          CA070416006      120070315G2750C1486742003     CONTROL UNIT                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  TE FLAPS        MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 FJ FLT CONT AFFECTED         WARNING INDICATION                                  CRCRUISE         1                      CA       1613                                                           (CAN) ENROUTE BASE, THE FLAP POWER CAUTION LIGHT ILLUMINATED. RESET WAS CARRIED OUT IAW QRH 10.11 HOWEVER ONE MINUTE LATER THE CAUTION LIGHT RE-ILLUMINATED.  IAW THE QRH FLAPS RENDERED UNAVAILABLE FOR LANDING. FLAPLESS LANDING WAS CARRIED OUT WITHOUT INCIDENT. ENGINEERING INVESTIGATION REVEALED FAILURE OF THE FLAP CONTROL UNIT. UNIT REPLACED AND TESTED IAW MAINTENANCE MANUAL REQUIREMENTS. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. AS DEFECT CONFIRMED WITH REPLACEMENT OF THE FCU. (TC NR 20070416006)                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070507001082007050700108SO  2007       5          7          CA070416007      120070416G2910OAS229307       POWERPACK                               PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  HYD SYSTEM      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1091              317552010                               (CAN) DURING A MAINTENANCE RUN AFTER WORK ON AN ENGINE THE MECHANICS DID A HYDRAULIC PUMP CHECK BY SELECTING HANDLE TO GEAR DOWN POSITION.  THE HANDLE WOULD NOT RETURN TO THE NEUTRAL POSITION AS IS NORMAL.  WHEN GEAR SWINGS WERE CARRIED OUT IN THE HANGAR THE OB GEAR DOORS WOULD ONLY PROCEED HALFWAY AND THEN SIT AND SHUDDER.  A LOUD BANG WAS HEARD FROM THE POWERPAK AND THEN THE DOORS WOULD CLOSE OR OPEN AS SELECTED.  THERE WAS NO PRIOR INDICATION OF PROBLEMS WITH THE POWERPACK. (TC NR 20070416007)                                                                                                                                                                                                                           1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070507001092007050700109    2007       5          7          CA070416008      420070324G3460101741111       COMPUTER                                DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  FMS             MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CRCRUISE         1                      CA       534                                                            (CAN) CREW REPORTED FMS FAILED THEN FLIGHT DECK EXPERIENCED SMOKE AND FUMES. CREW ELECTED TO RETURN THE AIRCRAFT TO BASE WHERE A LANDING WAS CARRIED OUT WITHOUT INCIDENT.  ENGINEERING REPLACED THE FMS UNIT. INITIAL INVESTIGATION OF THE REMOVED UNIT INDICATES AN ELECTRICAL FAILURE OF AN INTERNAL CIRCUIT BOARD. UNIT HAS BEEN RETURNED TO THE MFG FOR REPAIR AND WITH A REQUEST TO PROVIDE A STRIP REPORT. (TC NR 20070416008)                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070507001102007050700110NM  2007       5          7          CA070416009      120070327G242131708001A       GENERATOR                               DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  NR 2 AC SYSTEM  MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) ON INITIAL CLIMB AFTER TAKEOFF THE AC GENERATOR `HOT` CAUTION LIGHT ILLUMINATED. CREW ELECTED TO RETURN THE AIRCRAFT TO BASE WHERE AN APPROACH AND LANDING WAS CARRIED OUT WITHOUT INCIDENT. ENGINEERING REPLACED THE AC GENERATOR AND RETURNED THE AIRCRAFT TO SERVICE. (TC NR 20070416009)                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070615001892007061500189SW  2007       6          15         CA070417001      120070412G3242A032            VALVE           PARAMOUNT               SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP                              MASTER CYLINDER STUCK           W      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                LDLANDING        1                      CA            5282  13026                                               (CAN) THE AC RT MLG TIRES WERE BLOWN UPON LANDING. DURING INSPECTION IT WAS FOUND THAT THE RT BRAKE ASSY WERE DRAGGING AND OVERHEATED CAUSING THE WHEELS NOT TO TURN FREELY UPON TOUCHDOWN.  TIRES, BRAKES AND AFFECTED BRAKE MASTER CYLINDERS WERE REPLACED. AN INITIAL TEARDOWN OF THE MASTER CYLINDERS INDICATED THAT THE CAPTAIN`S RT CYLINDER WAS AT FAULT DUE TO MALFUNCTIONS OF INTERNAL COMPONENTS. AD 2002-08-01 DEALS WITH A SPECIFIC FAILURE MODE OF THESE MASTER CYLINDERS AND HAVE A OVERHAUL LIMIT OF 15000 HRS TIS. THESE MASTER CYLINDERS HAD 5282.00 HRS TT SINCE OVERHAUL.  FURTHER INVESTIGATION REVEALED THAT THE COTTER PIN (AN380-2C2) WHICH HOLDS THE VALVE IN THE MASTER CYLINDER TO THE ACTUATING ARM WAS BENT NOT ALLO2L72 4T4  TRTA8SW    E4WE                 
20070511000032007051100003EA  2007       5          11         CA070417002      120070417G57512151500080680   RIB                                     CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 CWASP       52016NE  HAMSTD43E   43E60       NE  AILERON         DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DAMAGE FOUND TO BOTH AILERONS ON THE (2) FIRST CENTER HINGE RIBS ASSEMBLY, ADJACENT TO THE FIXED STOPS.  A/C HOURS;  4658.7, CYCLES;   2973  (TC NR 20070417002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4R3  RRTA14EA   ATC14   6  CP871     
             20081104     EU  2008       11         4          CA070417003      120070409G3240RFS1010         DISK                                    BAG   JETSTMJETSTM3101  1500215EU                                                               MLG BRAKE       BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DISC WAS FOUND BROKEN IN HALF. NEW BRAKE UNIT INSTALLED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4T    RTA21EU                        
20070507001252007050700125GL  2007       5          7          CA070418001      120070416G38104E32612         POTABLE WATER                           BOMBDRBD700 BD7001A10   1390006GL  RROYCEBR700 BR700710A22009500NE                              GALLEY          LEAKING         W      D   RETURN TO BLOCK                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       422                                                            (CAN) FOLLOWING THE ADVISORY WIRE FROM MFG, THE WATER SYSTEM VENT VALVES (6) WHERE REPLACED IN MFG. ON THE NEXT CUSTOMER FLIGHT, ONE VENT VALVE FROM THE GALLEY HAS STARTED TO LEAK. END RESULT, AVIONICS BAY FLOODED, BLACK BOXES FULL OF WATER. INVESTIGATION SHOWED THAT THE 2 VALVES ARE ACTING REVERSE. AS A TEMPORARY MEASURE, MFG DRAWING NR BAS67038670 INCORPORATED. (REMOVED VENT VALVES AND INSTALLED PLUGS) (TC NR 20070418001)                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTT00003NYE00061EN             
             20081104     EA  2008       11         4          CA070418002      120070227G32400860162001      ACCUMULATOR                             DHAV  DHC8  DHC8311     1386006EA                                                               PARKING BRAKE   CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       3345821048                                                     (CAN) WHILE PERFORMING AN LPI ON THE LANDING GEAR (PARKING BRAKE ACCUMULATOR), (3) AXIAL CRACKS WERE FOUND IN THE BOTTOM PORTION OF THE INSPECTION AREA. THIS INSPECTION WAS IN SUPPORT OF SB A8-32-162. THE CRACKS EXTEND OUTSIDE THE TAPERED SECTION AND ARE .75, .50, AND .25 IN LENGTH. RETURNED TO STORES FOR REPAIR.                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T    RTA13NM                        
             20081104     SW  2008       11         4          CA070418003      120070321G7120205060105001    MOUNT                                   BELL  205   205A1       1181414SW  LYC   T53   T5317A      41549NE                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       91                                                             (CAN) ENGINE MOUNT WAS INSTALLED NEW IAW  STC SH99-11. POWER PLANT WAS ALIGNED IAW MM SUPPLEMENT. THE MM SUPPLEMENT INCLUDES AN INSP EVERY 100 HRS OR ANNUALLY. NOTE TO INSPECT ENGINE MOUNTS FOR CRACKS, DAMAGE, CORROSION AND SECURITY. THE CRACK STARTED BELOW THE MOUNT BETWEEN THE WELDS AND MOVES INWARD. ACFT WAS CHECKED FOR VIBRATION AND ALIGNMENT NO DEFECTS NOTED.                                                                                                                                                                                                                                                                                                                                                                  1G71 4U4  U  H1SW    E17EA                
             20081104     EA  2008       11         4          CA070418004      120070301G32400860162001      ACCUMULATOR                             DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  PARKING BRAKE   CORRODED        W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       349335783                                                      (CAN) WHILE PERFORMING AN LPI INSPECTION ON THE LANDING GEAR (PARK BRAKE ACCUMULATOR) IAW SB A8-32-162 A .015 CORROSION PIT WAS FOUND IN THE RADIUS OF THE TOP CAP,BETWEEN THE TAPERED SECTION AND THE SHAFT OF THE CAP.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070507001292007050700129    2007       5          7          CA070418005      420070416G3497M227591622      WIRE                                    DOUG  DC3   DC3C        3021457WP  PWA   PT6   PT6A67R     52043NE  HAMSTD23E   23E50       NE  AIRSPEED WARNINGARCED           W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                                                                      (CAN) THE AIRSPEED AURAL WARNING CIRCUIT BREAKER WAS FOUND TO BE (POPPED).  WHEN THE UPPER PANEL WAS LOWERED EVIDENCE OF ARCING WAS FOUND ON AIRFRAME STRUCTURE.  THE WIRE WAS REPAIRED THROUGH PARTIAL REPLACEMENT, CHAFE PROTECTOR WAS ADDED TO THE AIRFRAME STRUCTURE AND THE WIRE BUNDLE AND THE WIRE BUNDLE WAS RE-POSITIONED. (TC NR 20070418005)                                                                                                                                                                                                                                                                                                                                                                                         2L72 4R4  T  A669    E26NE   6  CP603     
20070507001302007050700130NE  2007       5          7          CA070418006      220070322G8530CH90ER          CYLINDER HEAD                                                              PWA   R985  R985AN14B   52008NE                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            586                                                       (CAN) ON 100 HR INSPECTION DURING A DIFFERENTIAL CHECK CYLINDER WAS READING LOW. USING A SOAP SOLUTION IT WAS DETERMINED THAT THERE WAS A LEAK ACROSS THE HEAD DUE TO A CRACK BETWEEN THE COOLING FINS. (TC NR 20070418006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            3  R          5E1                  
20070507001332007050700133GL  2007       5          7          CA070418007      120070417G5341VALTB12091      FITTING                                 DHAV  DHC1  DHC1        2801702GL  PWA   R985  R985AN14B   52008NE  HARTZLHCB3R HCB3R304    GL  WING TO BODY    CORRODED        W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       6052                                                           (CAN) A CURSORY INSPECTION REVEALED CORROSION ON THE LT PORK CHOP FITTING. BOTH LT AND RT FITTINGS WERE REPLACED WITH NEW UNITS. DEPTH OF CORROSION WAS APPROX 25 PERCENT OF PART OVERALL THICKNESS. THE MANUFACTURE WAS CONTACTED. THE PART IN QUESTION IS APPROX 11 YEARS OLD. (TC NR 20070418007)                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3O3  R  EXPA1L715E1     5  CP28EA    
20070808001532007080800153    2007       8          8          CA070419001      420070418G3197                WIRE                                    CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              NR 1 FEEDER     CHAFED          W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      NRNOT REPORTED   1                      CA                                                                      (CAN) DURING AN ATTEMPT TO RUN THE AIRCRAFT TO FUNCTION CHECK THE WINDSHIELD ANTI-ICE BLEED AIR (SNAG-NO BLEED AIR TO THE WINDSHIELD FOR ANTI-ICE UNTIL WINDSHIELD ANTI-ICE CB IS PULLED). WHEN THE BATTERY SWITCH WAS TURNED ON THE LT CB PANEL 35 AMP CIRCUIT BREAKER (LOCATED ON THE RT HAND CB PANEL) POPPED.  IT WAS DISCOVERED THAT THE NR 1 FEEDER WIRE (P10A6) FOR THE LT BUSS, THE INSULATION HAD ABRADED THROUGH AND MADE CONTACT WITH A SCREW ON THE BACK OF THE DE-ICE PANEL ASSY.  THIS WAS THE DIRECT CAUSE OF THE ABOVE MENTIONED 35AMP CIRCUIT BREAKER POPPING.  WHEN THIS DE-ICE SIDE CONSOLE PANEL ASSY IS INSTALLED. (3) 6 GAUGE WIRES (ALL LT BUS FEED WIRES P10A6, P11A6 AND P12A6) ARE ROUTED IN BEHIND THIS PANEL.  THE F1L72 4F4  F  A22CE   E1NE                 
20070507001362007050700136EA  2007       5          7          CA070419002      220070413G7230                BLADES          PWC                     BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  COMPRESSOR      DEPARTED        W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      CA            4538                          PCE51225                    (CAN) LT ENGINE EXPERIENCED A SUDDEN POWER LOSS ON CLIMB OUT. THE ENGINE WAS SHUTDOWN AND THE A/C RETURNED TO BASE WITHOUT ANY FURTHER INCIDENT. THE POWER SECTION WAS REMOVED FOR INVESTIGATION.   THE INVESTIGATION REVEALED THAT PIECES WERE MISSING FROM SEVERAL CT IGV`S, MULITPLE CT BLADES BEING DAMAGED (IE. MISSING PIECES) AS WELL AS DAMAGE TO SEVERAL PT BLADES AND GUIDE VANES. THE ENGINE HAS 4538.3 HRS AND 4622 CYCLES SINCE O/H AND IS ON CONDITION FOR HOT SECTION INSPECTIONS. THE LAST HSI WAS COMPLETED 2068.6 HRS AND 2695 CYCLES AGO WHEN 0.0 TSO CT BLADES P/N 3039901 WERE RE-INSTALLED.  THE ENGINE HAS BEEN SENT FOR O/H AND FURTHER INFO WILL BE AVAILABLE AFTER WHEN A TEARDOWN REPORT BECOMES AVAILABLE (TC# 200701L72 3T4  T  A14CE   E4EA    5  CSTC      
20070507001372007050700137CE  2007       5          7          CA070419003      120070418G55401145240253      TORQUE SHAFT                            BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  RUDDER          CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       15917                                                          (CAN) DURING A PHASE INSPECTION IT WAS DISCOVERED THAT THE RUDDER TORQUE SHAFT WAS CORRODED. IT IS BELIEVED THAT THE CORROSION OCCURRED DUE TO WATER MIGRATION FROM THE VERTICAL STABILIZER. THE TORQUE SHAFT WAS REPLACED. (TC NR 20070419003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070507001382007050700138SW  2007       5          7          CA070419004      120070419G6520476206297       BEARING                                 BELL  47    47G2        1181008SW  LYC   O435  VO435A1D    41516EA                              TAIL ROTOR GB   MAKING METAL    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3111 685                                                       (CAN) DURING ROUTINE 100 HR INSPECTION THE OIL WAS FOUND TO BE DARKER IN COLOR THAN NORMAL, AFTER CLOSER INSPECTION AND CHECKING FOR STEEL WITH A MAGNET THE DARKNESS IN COLOR WAS ATTRIBUTED TO METAL CONTAMINATION IN THE OIL SO FINE THAT IT LOOKED LIKE METALLIC PAINT. THE GEARBOX IS IN FOR TEARDOWN AND WILL ADVISE THE FINDINGS AFTER INSPECTION.  (TC NR 20070419004)                                                                                                                                                                                                                                                                                                                                                                  1G71 3O3  O  H1      E279                 
20070808001542007080800154CE  2007       8          8          CA070419005      120070412G554005310181        BRACKET                                 CESSNA172   172D        2072410CE  LYC   O360  O360A1A     41514EA  HARTZLHCC2Y HCC2YK1     GL  RUDDER          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3717                                                           (CAN) DURING THE ANNUAL INSPECTION, BOTH RUDDER HINGE BRACKETS WERE FOUND TO BE CRACKED.  RUDDER WAS REMOVED AND REINSTALLED AFTER REPAIRS.  PN 0531018-1 AND 0531018-2 WERE REPLACED WITH NEW IAW THE MM. (TC NR 20070419005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A12    E286    5  CP920     
20070507001402007050700140NE  2007       5          7          CA070420001      220070419G8530153084          CYLINDER                                DOUG  DC4   DC4         3021502WP  PWA   R2000 R20007M2    52023NE                              NR 4 ENGINE     CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) REPLACED NR 14 CYLINDER ON NR 4 ENGINE, DUE TO CRACK.  AIRCRAFT RETURNED TO SERVICE. (TC NR 20070420001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L74 4R4  R  A762    5E5                  
20070507001422007050700142EA  2007       5          7          CA070420002      220070417G8520SL12596         BOLT                                                                       LYC   O540  LTIO540J2BD 41533EA                              CONNECTING ROD  FAILED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      CA       671                                                            (CAN) BOLT FAILED CAUSING CONNECTING ROD TO BECAME DETACHED FROM CRANKSHAFT CAUSING MAJOR DAMAGE TO LOWER END OF ENGINE. (TC NR 20070420002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           3  O          E14EA                
20070507001432007050700143EA  2007       5          7          CA070420003      120070418G5220                DOOR                                    DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF15      NE  EMERGENCY EXIT  STIFF           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3470434704                                                     (CAN) ON GROUND, WHEN FLIGHT ATTENDANTS UNDERGOING RECURRENT TRAINING ATTEMPTED TO OPEN FWD RT EMERG EXIT DOOR, WERE UNABLE TO GET DOOR OPEN. MAINTENANCE CALLED TO ASSIST AND REQUIRED TWO ENGINEERS (ONE ON INSIDE HANDLE AND ONE ON OUTSIDE HANDLE) TO GET DOOR OPEN . MAINTENANCE INSPECTED AND LUBRICATED INTERNAL DOOR MECHANISM, DOOR RE-INSTALLED AND FUNCTIONED WITH NORMAL OPENING FORCE. (TC NR 20070420003)                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070507001932007050700193EU  2007       5          7          CA070423001      120070420G6220601741          BEARING                                 BOLKMS105   BO105S      5626006EU  ALLSN 250C  250C20B     03013GL                              MAIN ROTOR      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING PERFORMANCE OF A 100/300 HOUR INSPECTION OF THE AIRCRAFT AND IN PARTICULAR THE MAIN ROTOR BLADES.  THE ENGINEER FOUND THAT THE PENDULUM ABSORBER OF THE RED MAIN ROTOR BLADE WAS EXTREMELY ROUGH.     UPON DISASSEMBLY OF THE PENDULUM ABSORBER IT WAS FOUND THAT THE BEARINGS WERE DRY, WITH NO TRACE OF OIL PRESENT.  ONE BEARING CAGE HAD FAILED, AND THE BALL BEARINGS HAD WORN TO WELL BEYOND ANY CIRCULAR SHAPE.  JUST A NOTE TO SAY THAT THERE HAD BEEN NO TRACE OF OIL ON THE HEAD IN PREVIOUS INSPECTIONS TO INDICATE A LEAK.     ONE BEARING AND SEAL WERE REPLACE, THE ASSEMBLY REASSEMBLED AND INSTALLED ONTO THE ROTOR BLADE.  AIRCRAFT RETURNED TO SERVICE UPON COMPLETION OF THE INSPECTION. (TC NR 20070423001)    1G72 3U3  U  H3EU    E4CE                 
20070507001942007050700194EA  2007       5          7          CA070423002      220070423G8530LW12427         CYLINDER                                BEECH 23    C23         1151242CE  LYC   O360  O360A4K     41514EA  SNSNCH76E   76EM8S5     EA  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1397                                                           (CAN) CRACK FOUND IN CYLINDER. (TC NR 20070423002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  A1CE    E286    5  NP4EA     
20070711002902007071100290NE  2007       7          11         CA070423004      220070421G72976015091017      WIRE HARNESS                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              RT ENGINE       CHAFED          W      A   UNSCHED LANDING                                                                                 H  ELECT. POWER LOSS-50 PC                                                       CLCLIMB          1                      CA                                                                      (CAN) SHORTLY AFTER T/O, THE RT ENGINE VIBRATION INDICATOR FLUCTUATED ERRATICALLY THE WENT TO DASHES MOMENTARILY THEN RETURNED TO NORMAL OPERATION.  FLIGHT RETURNED FOR MAINTENANCE TROUBLESHOOTING.  AFTER CHANGING THE ENGINE ACCELEROMETER AND SIGNAL CONDITIONER WITH NO FIX, THE ENGINE VIBRATION HARNESS SHIELDED WIRE WAS FOUND CHAFFING AGAINST ENGINE CLOSE TO THE ENGINE DISCONNECT PLUG.  THE VIBRATION HARNESS WAS REPLACED AND THE AIRCRAFT WAS FUNCTION CHECKED SERVICEABLE. (TC NR 20070423004)                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
20070508001972007050800197EA  2007       5          8          CA070423005      220070419G8530LW12966         CYLINDER                                PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1702                          RL145668A                   (CAN) OIL WAS NOTICED LEAKING FROM THE PUSHROD AREA.  THE PUSHROD WAS REMOVED TO REPLACE THE SEALS.  THE CRACK IN THE CYLINDER HEAD WAS FOUND THEN.  THE CRACK RAN FROM THE BOTTOM OF THE CYLINDER HEAD SEAM TO ABOUT 4-5 INCHES ALONG THE HOLLOW WHERE THE PUSHROD TUBE RESIDES.  THE CYLINDERS WERE MANUFACTURED NEW STEEL AT OVERHAUL. (TC NR 20070423005)                                                                                                                                                                                                                                                                                                                                                                                   1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070808001552007080800155CE  2007       8          8          CA070423006      120070419G251005142043        SEAT                                    CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160CTM    GL  COCKPIT         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4224                                                           (CAN) WHILE PERFORMING AD CF87-15R2 A CRACK WAS NOTED IN THE RADIUS OF THE MACHINED FORK AT THE LT FRONT LOCATION. THE FORK IS MADE OF RATHER THIN RECTANGULAR ALUMINUM TUBING AND IS SUBJECT TO SOME FLEXING AS OCCUPANTS ENTER OR EXIT THE AIRCRAFT. (TC NR 20070423006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    E274    5  NP910     
20070508001992007050800199CE  2007       5          8          CA070423007      120070418G2430290143          PROBE                                   BEECH 99    99          1154002CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  TEMP MONITOR    INTERMITTENT    W      O   OTHER                                                                                           N  FALSE WARNING                                                                 APAPPROACH       1                      CA                                                                      (CAN) BATTERY TEMP MONITOR WAS INDICATING HIGHER THAN NORMAL ON APPROACH.  AIRCRAFT LANDED WITHOUT INCIDENT.  BATTERY WAS LUKEWARM TO THE TOUCH.  MONITOR WAS UNRESPONSIVE. BATTERY AND PROBE WERE REPLACED ALONG WITH WIRING INSPECTED AND AIRCRAFT RETURNED TO SERVICE.  NO FAULTS WERE FOUND DURING DEEP CYCLE OF BATTERY AT BATTERY SHOP.  PROBE REPLACED DUE TO POSSIBLE INTERMITTENT OPERATION. (TC NR 20070423007)                                                                                                                                                                                                                                                                                                                       1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20070711002892007071100289WP  2007       7          11         CA070423008      220070416G73218978015         FUEL CONTROL                            SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE33111U   01514WP  MCAULY4HFR344HFR34C652  NE  ENGINE          LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  NRNOT REPORTED   1                      CA            3600                                                      (CAN) NOTED LARGE FUEL LEAK UNDER THE AIRCRAFT IN THE HANGER.  DETERMINED THE FUEL WAS COMING FROM AN ENGINE DRAIN.  GROUND RAN THE ENGINE, FOUND THE FUEL CONTROL DRAIN LEAKING.  REMOVED AND REPLACED THE FUEL CONTROL WITH AN OVERHAULED UNIT, NO FURTHER DEFECTS NOTED. (TC NR 20070423008)                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4T4  TRTA8SW    E4WE    6  C3PNE     
20070508002012007050800201CE  2007       5          8          CA070423009      120070422G53229743000015      CROSS TIE                               BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7390                                                           (CAN) THE INTERIOR WAS REMOVED FOR REFURBISHMENT.  MAINTENANCE DISCOVERED A CRACK IN THE CROSS TIE, A STRUCTURAL MEMBER AROUND THE EMERGENCY EXIT ON THE LT SIDE OF THE AIRCRAFT.  CONTACTED MFG FOR A REPAIR. (TC NR 20070423009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070615001902007061500190EU  2007       6          15         CA070424001      120070420G2910571191          PTU                                     AIRBUS310   A310304     3930339EU  GE    CF6   CF680C2*         GL                              HYD SYSTEM      LEAKING         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) DURING FLIGHT, CREW NOTICED LOSS OF GREEN SYSTEM HYDRAULIC FLUID. FLIGHT DIVERTED TO MAIN MAINTENANCE BASE FOR INVESTIGATION. DURING INVESTIGATION, THE GREEN/YELLOW SYSTEM PTU WAS FOUND LEAKING AT THE CHECK VALVE DUE TO A DAMAGED O RING. PTU UNIT WAS REPLACED AND SYSTEM TESTS SERVICEABLE.  (TC NR 20070424001)                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA35EU   E23EA                
20070615001912007061500191EU  2007       6          15         CA070424002      120070421G2121X76451          FAN                                     AIRBUS310   A310304     3930339EU  GE    CF6   CF680C2*         GL                              CABIN           ODOR            W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) DURING FLIGHT CABIN CREW REPORTED ELECTRICAL BURN ODOR FROM THE AFT CABIN.  FAULT ISOLATED TO THE AFT RT FAN HEATER FIN NR 28HC. CBS WERE PULLED AND ODOR DISAPPEARED.  SYSTEM WAS PLACED ON MEL DUE PART IS NIL STOCK.  (TC NR 20070424002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA35EU   E23EA                
20070618001142007061800114EU  2007       6          18         CA070424003      120070412G2800                UNKNOWN                                 AIRBUS310   A310304     3930339EU  GE    CF6   CF680C2*         GL                              FUEL SYSTEM     UNKNOWN         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE, CREW NOTICES A FUEL DISCREPANCY OF ONE TON BETWEEN FUEL ON BOARD AND FUEL USED. AFTER RECALCULATION SHORTLY THEREAFTER THE FUEL DISCREPANCY HAD GROWN TO 1.4 TONS. CREW PROCEEDED WITH QRH PROCEDURES AND SPOTTED FUEL SPAYING FROM THE RIGHT WING TIP VENT BOX. SHORTLY THEREAFTER THE FUEL VENTING CEASED. THE FLIGHT WAS DIVERTED TO THE MAIN STATION. DURING INVESTIGATION MAINTENANCE ATTEMPTED TO DUPLICATE THE PROBLEM WITH NO SUCCESS. AIRBUS WAS CONTACTED FOR THEIR RECOMMENDATION. THE FOLLOWING UNITS WERE REPLACED AND ROUTE TO THE VENDOR FOR SHOP CHECK AND STRIP REPORT: (A) RT INNER TANK VENT FLOAT VALVE (B) 2 RT OB BOOST PUMP CHECK VALVES  (C) RT WING REFUEL/DEFUEL VALVE (D)  FUEL TRANSFER VALVE A2L72 4F4  FRTA35EU   E23EA                
20080219003692008021900369CE  2008       2          19         CA070424004      120070419G291310138800517     POWERPACK                               BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCD4N3HCD4N3A     GL  HYDRAULIC SYSTEMFAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA       9010 9010              BB1281                                  (CAN) DURING A ROUTINE MEDEVAC AND TEN MINUTES AFTER  DEPARTURE THE RED LIGHT IN THE IN THE LANDING GEAR HANDLE ILLUMINATED.VISUAL CONFIRMATION OUT CAPT SIDE WINDOW OF LANDING GEAR PARTIALLY DOWN.  A MANUAL GEAR EXTENSION WAS INITIATED AND A UNEVENTFUL LANDING WAS COMPLETED. TELCOM WITH MTCE. AND FLIGHT CREW CONFIRMED, LANDING GEAR MOTOR WAS NON FUNCTIONING. VISUAL INSP WAS C/O BY CREW FOR DAMAGE OR EXCESSIVE FLUID LOSS, WITH NONE OBSERVED.  AC WAS RETURNED WITH LANDING GEAR IN THE DOWN/ LOCKED POSITION, ESSENTIAL CREW ONLY ON BOARD.  MAINT INSPECTION REVEALED,THE L/G HYD POWERPACK HAD INTERNALLY FAILED TO MAINTAIN SYS PRESSURE,CAUSING THE PUMP TO RUN AND EXCEEDED OPERATIONAL TOLERANCE WHICH POPPED THE C/B. REP1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070509000622007050900062EA  2007       5          9          CA070424005      220070424G7230                COMPRESSOR WHEEL                                                           PWA   PT6   PT6A27      52043EA                              ENGINE          MAKING METAL    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) OPERATOR REPORTED THAT WHEN THE ENGINE WAS STARTED, THE PROPELLER DID NOT ROTATE. AFTER SHUTDOWN, THE ENGINE AND PROP COULD BE ROTATED BY HAND. HOWEVER, SEVERAL SMALL PIECES OF METALLIC DEBRIS WAS REMOVED FROM THE EXHAUST AREA.  DISASSEMBLY OF THE ENGINE REVEALED SEVERE IMPACT DAMAGE ON THE FWD FACE OF THE CT DISC ASSY AND 4 MISSING CT VANE RETAINING BOLTS. FURTHER INVESTIGATION REVEALED IMPACT DAMAGE ON THE CT VANE LOCK PLATE, CT VANE, CT BLADES AND PT BLADES. (TC NR 20070424005)                                                                                                                                                                                                                                            4  T          E4EA                 
20070618001152007061800115EA  2007       6          18         CA070424006      120070420G2497C030722         DIODE                                   DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  LT DC ESS BUSS  MISWIRED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3540435404                                                     (CAN) DURING GRD RUN LEAK CHECKS, AFTER ROUTINE MAINTENANCE,  NOTED NO DISCHARGE SHOWING ON THE BATTERY MONITOR FOR THE AUX BATTERY. INVESTIGATION FOUND WIRING BACKWARDS AT DIODE 2431-CR5; THIS IS THE POWER SUPPLY TO THE BUS FROM THE AUX BATTERY.  IN THIS CONDITION NO POWER IS AVAILABLE FROM THE AUX BATTERY UNDER ANY CONDITIONS. THE ONLY INDICATION OF THIS MISCONNECTION WAS BATTERY MONITOR SHOWING NO DISCHARGE FROM THE AUX BATTERY, WHEN BOTH MAIN AND AUX BATTERIES WERE SELECTED ON.  (NORMAL OPERATING PROCEDURE IS TO HAVE BOTH BATTERIES SELECTED ON) ALL OTHER ELECTRICAL SYSTEM INDICATIONS WERE NORMAL. WIRING CORRECTED SYSTEM FUNCTION CHECKED NORMAL. (TC NR 20070424006)                                            2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070618001162007061800116NE  2007       6          18         CA070424007      220070423G7230JT8D15QM        BLADE           PWA                     BOEING727   727247      138408FNM  PWA   JT8   JT8D15      52051NE                              COMPRESSOR      FAILED          W      C   ABORTED TAKEOFF                                                                                 RY PARTIAL RPM/PWR LOSS      ENGINE STOPPAGE                                     TOTAKEOFF        1                      CA       573393677                          696622                      (CAN) DURING TAKEOFF ROLL AT 80KTS, THE TOWER ADVISED THE CREW THAT FLAMES WERE VISIBLE OUT OF ONE OF THE ENGINES. THE CREW REJECTED THE TAKEOFF AND ENGINES WERE SHUTDOWN. THE AIRCRAFT WAS TOWED BACK TO THE RAMP.   MAINTENANCE INSPECTED THE ENGINES AND FOUND NR 2 ENGINE TO HAVE TURBINE DAMAGE. SOME INTERNAL ENGINE PARTS HAD EXITED THE ENGINE AND WERE FOUND ON THE RUNWAY. (16 IN YYC). AT THIS TIME IT LOOKS AS THOUGH THE FAILURE STARTED WITHIN THE COMPRESSOR SECTION.  THE ENGINE IS CURRENTLY BEING REMOVED FROM THE AIRCRAFT AND A FOLLOW-UP TO THIS SDR SHALL BE ACCOMPLISHED ONCE THE ENGINE HAS BEEN DISASSEMBLED FOR INSPECTION. (TC NR 20070424007)                                                                      2L73 4F4  F  A3WE    E2EA                 
20080219003702008021900370CE  2008       2          19         CA070424008      120070422G2910124F0016CR0164  HYDRAULIC LINE                          BEECH 99    99          1154002CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  HYDRAULIC SYSTEMRUPTURED        W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  LDLANDING        1                      CA                                                                      (CAN) DURING APPROACH TO LAND THE CREW EXTENDED THE LANDING GEAR AND NOTICED THE NOSE GEAR WAS NOT DOWN AND LOCKED. THE EMERGENCY GEAR EXTENSION WAS ACTIVATED AND THE NOSE GEAR WAS LOCKED IN THE DOWN POSITION. THE AC LANDED WITHOUT INCEDENT. UPON INSP BY MAINT IT WAS DETERMINED THE HYDR SYS ACCUMULATOR LINE HAD RUPTURED PURGING THE HYDRAULIC FLUID FROM THE SYS OVERBOARD. NO DEFINITIVE CAUSE FOR THE RUPTURE OF THE LINE COULD BE DETERMINED. THE AGE OF THE LINE IS UNKNOWN. IT IS SUSPECTED CYCLIC FATIGUE IS THE CAUSE OF THE RUPTURE. NO LIFE LIMIT OR REPLACEMENT INTERVAL IS MANDATED BY THE AC MFG. (TC NR 20070424008)                                                                                                     1L72 3T4  T  A14CE   E4EA    6  CP15EA    
             20081104     CE  2008       11         4          CA070424010      120070418G3297973106A12SL64   CONNECTOR       RAYTHN      623372      BEECH 1900  1900C       1154161CE                                                               SELECTOR VALVE  CORRODED        W      L   ABORTED APPROACH                                                                                O  OTHER                                                                         APAPPROACH       1                      CA                                                                      (CAN) ON (GEAR DOWN) SELECTION, CIRCUIT BREAKER FOR THE GEAR CONTROL POPPED AND THE GEAR REMAINED RETRACTED. AFTER A MISSED APPROACH THE NORMAL SOP`S WERE CARRIED OUT AND THE GEAR MANUALLY EXTENDED. AN UNEVENTFUL LANDING WAS THEN CARRIED OUT. ON INVESTIGATION THE CONNECTOR TO THE GEAR SELECTOR VALVE ON THE HYDRAULIC POWER PACK WAS FOUND TO BE CORRODED AND HAD A BROKEN WIRE. THE CONNECTOR WAS REPLACED AND THE WIRE REPAIRED. THE GEAR SWINGS WERE NORMAL AND THE ACFT HAS SINCE FLOWN WITH NO REOCCURRENCE OF THE DEFECT.                                                                                                                                                                                                         2L72 4T    RTA24CE                        
20070508002032007050800203SW  2007       5          8          CA070424011      120070418G7712                IDLER GEAR                              SWRNGNSA226 SA226*             SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  TORQUE SENSOR   LOOSE           W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA       3115 3115  P8640C                                              (CAN) FOUND ON TAKEOFF ROLL, THE RT CHIP LIGHT CAME ON THROUGH 70 KTS. THE TAKEOFF WAS ABORTED AND THE AC TAXIED BACK TO THE RAMP WITHOUT ANY FURTHER INCIDENT.  AT THIS TIME MAINT HAD DONE A SOAP SAMPLE AND FOUND METAL IN THE OIL FILTER.  WHEN THE ENGINE WAS TAKEN APART THE TORQUE SENSOR IDLER GEAR WAS NOTICED TO BE LOOSE DUE TO THE BEARING HAD FAILED ON THE IDLER GEAR THAT IS ATTACHED TO THE TORQUE SENSOR. (TC NR 20070424011)                                                                                                                                                                                                                                                                                                  2L72 4T4  TRTA56W    E4WE    5  CP10NE    
20070808001562007080800156CE  2007       8          8          CA070425001      120070423G323355275042        ACTUATOR                                CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              MLG             MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            DEDESCENT        1                      CA       7518                                                           (CAN) AIRCRAFT EXPERIENCED UNSAFE GEAR EXTENSION WHILE DOING CIRCUITS.  GEAR SELECTION WAS MADE WHILE IN DOWNWIND TURN AND RT MAIN GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE, (GEAR UNLOCKED) AND (HYD PRESS ON) LIGHTS REMAINED ON. GEAR WAS RECYCLED IN LEVEL FLIGHT AND NORMAL INDICATION RESULTED.  AIRCRAFT WAS FLOWN UNDER FERRY FLIGHT PERMIT WITH GEAR VERIFIED DOWN AND LOCKED. MAINTENANCE CONDUCTED SEVERAL GEAR SWINGS TO ENSURE PROPER OPERATION AND DOWNLOCK SWITCH CONTINUITY, WHICH REVEALED NO FAULTS.  WHEN A LOWER THAN NORMAL HYDRAULIC PRESSURE WAS APPLIED AND GEAR DOWN SELECTION MADE, THE NOSE AND LT GEAR RELEASED BUT THE RT MAIN REMAINED IN THE UPLOCK.  PRESSURE WAS THEN INCREASED TO NORMAL WITH NO EFFECT O1L72 4F4  F  A22CE   E1NE                 
20070620000022007062000002NM  2007       6          20         CA070425002      120070421G321383210301001     STRUT                                   DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  LT MLG          SEPARATED       W      O   OTHER                                                                                           WZ INADEQUATE Q C            SIGNIFICANT FAILURE REPORT                          LDLANDING        1                      CA                                                                      (CAN) LT MLG SEPARATED FROM AIRCRAFT DURING LANDING. THE LOWER OLEO STRUT WITH THE WHEELS AND AXLE DEPARTED THE AIRCRAFT; AIRCRAFT LANDED ON DRAG STRUT WHICH THEN COLLAPSED AND SHEARED OFF. SUBSTANTIAL DAMAGE WAS DONE TO THE LOWER FUSE, LT NACELLE, ENGINE AND PROP, AND LT WING TIP. PILOT REPORTED THAT THERE WAS NOT A HARD LANDING. MFGS ARE INVESTIGATING THE EVENT.  (TC NR 20070425002)                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070618001172007061800117NM  2007       6          18         CA070425003      120070419G242111522184        GENERATOR                               BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NR 1            LACK OF LUBE    W      E   ENGINE SHUTDOWN                                                                                 GJ MULTIPLE FAILURE          WARNING INDICATION                                  APAPPROACH       1                      CA       3760 1620                                                      (CAN) DURING APPROACH TO BASE AT 1000 FEET, THE NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. PILOT CYCLED THE NR 1 AC GENERATOR AND THEN THE AC GENERATOR HOT CAUTION LIGHT ILLUMINATED AS WELL AS THE AC GENERATOR CAUTION LIGHT.  AFTER TOUCHDOWN WHEN PLA RETARDED TO DISC THE NR 1 OIL PRESS WARNING LIGHT ILLUMINATED AND THE ENGINE WAS SHUTDOWN.  GROUND INSPECTION REVEALED: AC GEN OVERHEATED, AC GEN QUILL SHAFT SEPARATED, NO OIL ON THE SIGHT GAGE, NO EXTERNAL LEAK, METAL TRAPPED ON THE AC GEN MCD 41 SEC, LOW OIL PRESS EXCEEDED, RECORDED IN EMU.  NR 1 ENGINE REPLACED DUE TO THE EXCEEDING. (TC NR 20070425003)                                                                                                              2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080220000082008022000008SO  2008       2          20         CA070425004      120070405G322167054803        TRUNNION                                PIPER PA44  PA44180     7104402SO  LYC   O360  O360E1A6D   42305EA  HARTZLHCC3Y HCC3YR2     NE  NLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       10636                                                          (CAN) DURING A PREFLIGHT INSP THE PILOT NOTICED THE NOSE GEAR TRUNNION CRACKED. THE CRACK STARTS FROM THE UPPER PART OF THE CASTING AND GOES DOWN HALFWAY AT WHICH POINT IT SPREADS INTO 3 OTHER CRACKS. THE IDENTICAL CRACK CAN BE FOUND ON THE REAR SIDE OF THE CASTING .THE CRACK IS 5 INCHES LONG.  SUSPECT A HARD LANDING, A HARD LANDING INPS WAS CARRIED OUT AND NO FURTHER DAMAGE WAS FOUND. THE NOSE TIRE SHOWED EVIDENCE OF A HARD LANDING. THE PART IS BEING KEPT, CAN SEND A PICTURE OR MAKE THE PART AVAILABLE FOR INSP. (TC NR 20070425004)                                                                                                                                                                                       1L72 3O3  O  A19S0   E286    5  CP25EA    
20080220000092008022000009EU  2008       2          20         CA070425005      120070425G2913593733          BEARING                     350A35109223SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                              HYDRAULIC PUMP  WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1188       4KMVA                                               (CAN) DURING DI, HYDRAULIC PUMP PULLEY WAS NOTICED TO BE LOOSE LATERALLY WHEN MOVED SIDE TO SIDE. WHEN MAIN ROTOR WAS ROTATED HYDRAULIC PUMP PULLEY WAS FOUND NOT SPINNING SQUARE AND THE HYDRAULIC BELT WAS OFF SET FROM CENTER. HYDRAULIC PUMP PULLEY WAS REMOVED AND BEARING INNER RACE WAS FOUND SPINNING ON SHAFT AND WORE A SUBSTANTIAL GROOVE IN PULLEY SHAFT.  (TC NR 20070425005)                                                                                                                                                                                                                                                                                                                                                      1G71 3U3  U  H9EU    E00054EN             
20070508002042007050800204NE  2007       5          8          CA070426002      220070424G73146078T39P04      PUMP                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              FUEL SYSTEM     LEAKING         W      ED  ENGINE SHUTDOWN         RETURN TO BLOCK                                                         KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       24818683                           872485                      (CAN) DURING ENGINE START UP, GROUND CREW OBSERVED A LEAK COMING FROM BELOW THE ENGINE NR 2.  LINE MAINTENACE FOUND A FUEL LEAK FROM A MICROSCOPIC PIN HOLE CLOSE TO A PLUGGED FITTING ADAPTOR ON ENGINE NR 2 FUEL PUMP AFT CASING. THE EXACT PIN HOLE LOCATION WAS NOT FOUND DUE TO THE HIGH FUEL PRESSURE MIST. FUEL PUMP SN CGWT0202. (TC NR 20070426002)                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20070508002122007050800212EA  2007       5          8          CA070426003      220070426G853072242           ROCKER COVER                            RKWELL700   700         7630520SW  LYC   O540  TIO540R2AD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          SEPARATED       W      A   UNSCHED LANDING                                                                                 RE PARTIAL RPM/PWR LOSS      VIBRATION/BUFFET                                    CRCRUISE         1                      CA            24                            L633761A                    (CAN) SHORTLY AFTER TAKEOFF, THE PILOTS EXPERIENCED A POWER LOSS IN THE LT ENGINE, HOWEVER THE ENGINE REMAINED RUNNING.  THEY RETURNED TO THE NEARBY AIRPORT WITHOUT INCIDENT.   MAINTENANCE INSPECTED THE ENGINE AND FOUND THAT NR 6 CYLINDER ROCKER COVER HAD BEEN DAMAGED. THE COVER WAS REMOVED AND FOUND THAT THE RETAINING CLIP THAT HOLDS THE ROCKER SHAFTS IN PLACE FOR THE INTAKE AND EXHAUST VALVES HAD FALLEN OFF.  THE ROCKER SHAFT FOR THE INTAKE VALVE HAD FALLEN OUT ALLOWING  THE ROCKER TO BECOME DISLODGED THEREBY DISABLING THAT CYLINDER. THE VALVE ASSEMBLY WAS INSPECTED AND REINSTALLED WITH A REPLACEMENT VALVE COVER AND GASKET.  GROUND RUNS COMPLETED AND ALL CHECKS FOUND SERVICEABLE.   AS NOTED ABOVE, THE ENGINE 1L72 3O3  O  A12SW   E14EA   5  CP33EA    
20070618001182007061800118NM  2007       6          18         CA070426005      120070420G5753RD8457049       SEAL                                    BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  RT OB FLAP      MISSING         W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) AFTER 30 MINS INTO FLIGHT, CREW REPORT AILERON MISMATCH, AP DISCONNECTED AND AILERON STUCK.  PILOT USED FORCE TO RELEASE AILERONS.  REST OF FLT SYSTEM, OPS NORMAL.  THIS WAS THE FIRST FLT OF THE DAY AND THE TEMP AT FL250 WAS -45 DEG C.  FOUND RT FLAP SEAL LOOSE, PART MISSING AND LT FLAP SEAL LOOSE. LT AND RT FLAP SEALS REPLACED. (TC NR 20070426005)                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070808001572007080800157CE  2007       8          8          CA070426007      120070420G2910S217840114      CONNECTOR                               CESSNA177   177RG       2073709CE                                                               NLG             LEAKING         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) AIRCRAFT PLANNING ON LANDING WHEN UNDERCARRIAGE LIGHT FAILED TO INDICATED GEAR DOWN AND LOCKED. DECLARED AN EMERGENCY. AFTER SEVERAL ATTEMPTS AT TRYING TO PUMP GEAR DOWN BY HAND THE PILOT GOT A GEAR DOWN AND LOCKED LIGHT. AIRCRAFT LANDED WITH NO EVENT TAKING PLACE. MAINTENANCE LATER FOUND THE NOSE GEAR ACTUATOR HOSE HAD SLID PARTIALLY FROM ITS SWAGED END CONNECTOR AND WAS LEAKING BADLY. HOSE REPLACED. (TC NR 20070426007)                                                                                                                                                                                                                                                                                                  1H71 3O      A20CE                        
20070618001192007061800119EU  2007       6          18         CA070426008      120070419G308045150560        PROBE                                   AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  AOA             MALFUNCTIONED   W      D   RETURN TO BLOCK                                                                                 J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                                                      (CAN) WHILE TAXIING TO POSITION FOR DEPARTURE THE CREW OBSERVED AN ICE DETECTOR FAULT. THE AIRCRAFT RETURNED TO THE RAMP FOR TROUBLESHOOTING. MAINTENANCE REPLACED THE CAPTAINS ALPHA PROBE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070426008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20070618001202007061800120GL  2007       6          18         CA070426009      120070420G5521C2TE83ND        RIB                                     DHAV  DHC2  DHC2MKI     2801830GL  PWA   PT6   PT6A34      52043EA  HARTZLHCB3T HCB3TN3     GL  ELEVATOR        CRACKED         W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       89                                                             (CAN) THIS ELEVATOR LEADING EDGE RIB WAS FOUND CRACKED WHILE CARRYING OUT ANNUAL INSPECTION.  IT WAS DETERMINED THAT THE CRACK WAS THE RESULT OF TOO SHARP OF A BEND RADIUS IN THE AREA WHERE THE PART GETS  RIVETED TO THE ELEVATOR LEADING EDGE SKIN.  THIS DEFECT WAS COMMUNICATED AND THE TOOLING HAS BEEN REPAIRED ALLOWING FOR A MOVE UNIFORM RADIUS ON THE PART IN QUESTION. (TC NR 20070426009)                                                                                                                                                                                                                                                                                                                                         1H71 3R4  TRCA806    E4EA    6  CP15EA    
20080320000022008032000002EU  2008       3          20         CA070427001      120070416G5210332A2213010006  DOOR                                    SNIAS AS332 AS332L      8680809EU  TMECA MAKILAMAKILA1A    60040EU                              MAIN PAX        SEPARATED       W      A   UNSCHED LANDING                                                                                 D  INFLIGHT SEPARATION                                                           CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKING OFF FROM AN OFFSHORE RIG AT 300 FT, 70 KNOTS, CREW HEARD A STRONG NOISE AND ONE OF THE PASSENGERS ADVISED THAT DOOR WAS MISSING. P/C NOTICED NO CAUTION LIGHTS. AC RETURNED TO THE RIG AND LANDED WITHOUT FURTHER INCIDENT. AC SUBSEQUENTLY RETURNED TO CHC`S OPS MAIN BASE WITHOUT PASSENGERS AND IS PRESENTLY QUARANTINED AWAITING INVESTIGATION TEAM.  CAPTAIN`S STATEMENT: FIRST FLIGHT OF THE DAY. BEFORE TAKEOFF DOOR CAUTION LIGHT FLICKERING. P/C CHECKED MEL AND ALL DOORS LOCKED. ENGINEER ON DUTY INFORMED, HE INSPECTED DOORS LOCKERS. SECOND FLIGHT. BEFORE TAKEOFF FROM (OFFSHORE RIG), DOORS WERE CONFIRMED LOCKED AND NO CAUTION LIGHTS. PASSING 00 FT AFTER TAKEOFF STRONG NOISE, PAX ADVISE DOOR MISSING, P2G72 4U4  U  H4EU    E12NE                
20070618001212007061800121EA  2007       6          18         CA070427003      120070425G7897B080201500398S  CONNECTOR                               CNDAIRCL600 CL600*      1900302EA  GE    CF34  CF34*            NE                              THRUST REVERSER SHORTED         W      K   NONE                                                                                            J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA       6005 6005                                                      (CAN) ON GROUND, EICAS SHOWED (PROX SYS FAULT 2).  MAINTENANCE INSPECTION FOUND PYLON CONNECTOR WITH INTERNAL SHORT, INDICATING FAILURE OF THRUST REV PROX SENSOR. CONNECTOR P/N B0802015-003-98SA (REF: WIRING MANUAL 71-50-01 J508) REPLACED, SYSTEM FUNCTION TEST NORMAL, AIRCRAFT RETURNED TO SERVICE (TC NR 20070427003)                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA21EA   E15NE                
20070618001942007061800194CE  2007       6          18         CA070427004      120070423G243599121252        STARTER GEN                             CESSNA525   525         2076601CE  WILINTFJ44  FJ44        66000GL                              ENGINE          FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA       756                                                            (CAN) GENERATOR OUTPUT FAILURE, NO OUTPUT.  (TC NR 20070427004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 4F4  FRTA1WI    E3GL                 
20070618001902007061800190SW  2007       6          18         CA070427005      120070416G6220407310104103    SPRING                                  BELL  407   407         1182206SW  ALLSN 250C  250C47B          GL                              MAIN ROTOR      BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) UPON SCHEDULED INSPECTION IT WAS NOTICED THAT ONE OF THE EIGHT SPRINGS IN THE MAIN ROTOR FRAME ASSEMBLY WAS BROKEN. (TC NR 20070427005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  UO H2SW    E1GL                 
20070613001422007061300142NM  2007       6          13         CA070427006      120070410G5754                ATTACH BRACKET                          BOEING727   727225      1384077NM  PWA   JT8   JT8D15      52051NE                              NR 7 SLAT       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A AND B5 INSPECTION NR 7 SLAT ATTACH BRACKET UPPER MOUNT ON FRONT SPAR CRACKED.  P/N TO BE DETERMINED FROM MFG ENGINEERING DRAWINGS. RDA ISSUED BY DECA ENGINEERING TO REPAIR. (TC NR 20070427006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L73 4F4  F  A3WE    E2EA                 
20070618001962007061800196SO  2007       6          18         CA070427007      120070425G322016667000        LINK                                    PIPER PA23  PA23250     7102308SO  LYC   O540  IO540C4B5   41532EA  HARTZLHCE2Y HCE2YK2     GL  NOSE GEAR       BROKEN          W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) DURING GEAR RETRACTION THE PILOTS DID NOT GET A GEAR UP AND SAFE LIGHT, UPON VISUALLY INSPECTING THE GEAR WITH THE MIRRORS THE NOSE GEAR WAS SEEN TO BE DANGLING AT AN APPROXIMATE 60 DEGREE ANGLE.  GEAR WAS SELECTED DOWN, DOWN AND LOCKED INDICATION WAS PROVIDED AND THE AIRCRAFT LANDED UNEVENTFULLY.  DURING INSPECTION OF THE GEAR SYSTEM THE NOSE GEAR DOWN LOCK LINK ASSEMBLIES WERE FOUND TO BE BROKEN IN HALF.  THEY ARE MADE OF STEEL.  THE LINK ASSEMBLIES WERE REPLACED NEW AND THE GEAR SWUNG NUMEROUS TIMES SATISFACTORILY. (TC NR 20070427007)                                                                                                                                                                           1L72 3O3  O  1A10    1E4     5  CP9EA     
20070618001972007061800197EA  2007       6          18         CA070427008      120070425G271082740220101     GUARD                                   DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE                  WORN            W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA       3475734757                                                     (CAN) FLIGHT CREW REPORTED ROLL CONTROL INPUTS SEEMED STIFF, ESPECIALLY LT TO RT IN-FLIGHT. ON GROUND NO INDICATION OF STIFFNESS AND NOTHING ADVERSE WITH ROLL DISCONNECT. MAINTENANCE INSPECTION FOUND LT OB AILERON CABLE ROUTED AROUND WRONG SIDE OF CABLE GUARD. CABLE ROUTING WAS RECTIFIED, CABLE GUARD REPLACED, CABLE INSPECTED WITH NO SIGNS OF DETERIORATION. AILERON CABLES RE-TENSIONED AND INDEPENDENT INSPECTION COMPLETED. AIRCRAFT RETURNED TO SERVICE. REF: DHC-83 IPC 27-12-00 FIG 10 ITEM 350 P/N 82740220-101 CABLE GUARD , REF: DHC-83 IPC 27-12-00 FIG. 25 ITEM 470 P/N 82700563-S001 CABLE,  REF: DHC SERIES 300 MAINT. TASK CARD 2710/02 PG 3 OF 6 VIEW H,  PG 6 OF 6 FIGURE 4 CABLE ROUTING. (TC NR 20070427008)       2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070618002072007061800207EA  2007       6          18         CA070502001      120070502G2810K215T6400212    FUEL TANK                               CNDAIRCL215 CL2156B11215       EA                                                                               LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) TESTED BEFORE INSTALLATION, THE NEW TANK HAS BEEN FOUND LEAKING BY ONE OF PROBE ATTACHMENT.  THE PROBE ATTACHMENT NUT HAS BEEN REPLACED, RETIGHTENED AND TANK INSTALLED IN A/C.  (TC NR 20070502001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T    RTA14EA                        
20070618001982007061800198SW  2007       6          18         CA070502002      120070426G6510222044003107    HANGER ASSY                             BELL  230   230         1182149SW                                                               TAIL ROTOR DRIVEFAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) T/R HANGAR BEARING ASSY FAILURE WAS DISCOVERED AFTER THE PILOT WAS ALERTED BY AN UNUSUAL NOISE UPON ENGINE START. (TC NR 20070502002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G72 3U    NCH9SW                         
20070618002062007061800206EA  2007       6          18         CA070502003      120070502G2810K215T6400212    FUEL TANK                               CNDAIRCL215 CL2156B11215       EA                                                                               LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) TESTED BEFORE INSTALLATION, THE NEW TANK HAS BEEN FOUND LEAKING BY ONE OF THE PROBE ATTACHMENT PATCH INSTALLATION. THE NEW TANK HAS BEEN REJECTED. (TC NR 20070502003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T    RTA14EA                        
20070808001582007080800158CE  2007       8          8          CA070502005      120070410G531224120111        BULKHEAD                                CESSNA172   172RG       2072438CE  LYC   O360  O360F1A6    41514EA                              BS 108          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       8484                                                           (CAN) PARTS WERE CRACKED AT ATTACH POINTS OF WHEEL WELL COVER SKIN 2412011-1 AND BULKHEADS STATION 108 AND 124 AND CRACK ON WHEEL WELL COVER AT RT FRONT CORNER WHERE IT ATTACHES TO BULKHEAD STATION 108.  TIEDOWN RINGS ALSO ATTACH IN THIS AREA.  (TC NR 20070502005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  O  3A17    E286                 
20080220000102008022000010SW  2008       2          20         CA070502006      120070426G6320                CASE            BELL        427040006107BELL  427   427         1182207SW                                                               TRANSMISSION    CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       450        56024                                               (CAN) ON INVESTIGATING AN OIL LEAKAGE, A CRACK WAS FOUND ON THE TRANSMISSION LOWER CASE (SIMILAR LOCATION AS SDR 20070216006) (TC NR 20070502006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3U      R00001RC                     
             20081104     EA  2008       11         4          CA070502007      220070501G74144371            MAGNETO                                 CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA                              LEFT            MALFUNCTIONED   W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       2458 475                                                       (CAN) UPON RUN-UP, THE LT MAGNETO WAS SELECTED CAUSING THE ENGINE TO STOP. THE MAGNETO WAS REPLACED, AND AFTER SATISFACTORY GROUND RUNNING, THE A/C WAS RELEASED FOR RETURN TO SERVICE. (TCNR 20070502007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    E274                 
20080220000462008022000046SO  2008       2          20         CA070502008      120070427G7602455361          CONTROL CABLE                           PIPER PA28  PA28R201T   7102813SO  CONT  O360  TSIO360F    17025SO  HARTZLHCC2Y BHCC2YF1    GL  MIXTURE CONTROL DAMAGED         W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             ININSP/MAINT     1                      CA                                                                      (CAN) MIXTURE CONTROL WAS FOUND TO BE STIFF BY MAINT ON AN ENGINE START FOR TAXI TO HANGER. CABLE WAS REMOVED. THE CABLE ROUTING POSITIONS THE CABLE LESS THAN (6) INCHES FROM THE TURBOCHARGER. AN ASBESTOS COVER HAD PREVIOUSLY BEEN PLACED OVER THE CABLE AND STITCHED TOGETHER WITH LOCK WIRE TO PROTECT THE CABLE. ( NOT DONE AT OUR SHOP). ONCE THE COVER WAS REPLACED WE DISCOVERED THE ENTIRE OUTER CABLE SHIELD DETERIORATED AND MISSING A TWO INCH SECTION. (TC NR 20070502008)                                                                                                                                                                                                                                                       1L71 3O3  O  2A13    E9CE    5  CP920     
20070618001222007061800122EA  2007       6          18         CA070502009      220070410G8500                ENGINE                                  PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  NR 2            FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) NR 2 ENGINE FAILED SEVEN MINUTES PRIOR TO LANDING AT AIRPORT. NR 2 CYLINDER DROPPED DOWN INSIDE THE COWLING AND APPROXIMATELY 2 QUARTS OF OIL WAS LOST. THE ENGINE WAS SECURED WITHIN A FEW SECONDS AND A LANDING WAS SAFELY EXECUTED AT AIRPORT.  THE ENGINES WERE BOTH SET AT 31 INCHES HG, 2200 RPM AND APPROXIMATELY 1500F EGT, PRIOR TO THE NR 2 ENGINE FAILURE. THE FAILURE OCCURRED ON THE 30 MARCH 2007. (TC NR 20070502009)                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070808001592007080800159CE  2007       8          8          CA070502010      120070418G27100510105365      CONTROL CABLE                           CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  AILERONS        FRAYED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2392                                                           (CAN) DURING INSPECTION RT WING AILERON CONTROL CABLES FOUND TO BE FRAYED WITH BROKEN STRANDS AT WING STATION 100 WHERE CABLES TRAVEL ON TOP OF FAIRLEAD PN 0522647-10 CABLES WERE REPLACED WITH NEW UNITS FROM MFG. (TC NR 20070502010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A12    1E10    5  NP857     
20070618001912007061800191NE  2007       6          18         CA070502011      220070420G7250                TURBINE WHEEL                           BELL  212   212         1181420SW  PWA   PT6T  PT6T3B      52045NE                              NR 1            DAMAGED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA       3238 469                                                       (CAN) IN FLIGHT SHUTDOWN OF NR 1 ENGINE. POWER TURBINE WHEEL SHED BLADES. DAMAGE FOUND ON MAIN ROTOR BLADES AND TAIL ROTOR BLADES.  LARGE AMOUNTS OF METAL ON CHIP DETECTOR. (TC NR 20070502011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 4U4  U  H4SW    E22EA                
20070618001952007061800195    2007       6          18         CA070502012      120070424G32469546            WHEEL                                                                      LYC   O540  IO540E1B5   41532EA  HARTZLHCA3V HCA3VK2     GL  NLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AXLE PLUG 9546 WHICH IS USED TO SECURE AXLE IN NOSE WHEEL SEPARATED ALLOWING AXLE BOLT TO COME HALF WAY OUT OF AXLE WHICH THE PILOT NOTICED ON WALK AROUND. ON INSPECTION IT WAS NOTICED THAT WHEEL HALF RETAINING BOLTS/NUTS HAD LOOSENED CAUSING WHEEL HALVES TO SEPARATE, PUTTING ADDED FORCE ON PLUG 9546 WHICH IN TURN SHEARED PLUG CAUSING BOLT TO EXIT AXLE PART WAY. (TC NR 20070502012)                                                                                                                                                                                                                                                                                                                                                 3  O          1E4     5  CP6EA     
20070808001612007080800161NM  2007       8          8          CA070502014      120070424G2497                FEEDER CABLE                            DORNERDO32  DO328300           NM  PWA   306   PW306B           NE                              ALTERNATOR      CHAFED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) DURING TROUBLESHOOTING OF INTERMITTENT AC ALTERNATOR FOUND FEEDER WIRE CHAFED AND ARCED TO COWL STRUCTURE.  STRUCTURE AFFECTED IS RETAINER FOR COWL SUPPORT ARM. (TC NR 20070502014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  FRTA55NM   E35NE                
20070618002052007061800205EU  2007       6          18         CA070502015      120070430G78101379049H401     EXHAUST PIPE                            BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33112UHR      WP  ROTOL R333  R333482F12  GL  ENGINE          BROKEN          W      FA  ACTIVATE FIRE EXT.      UNSCHED LANDING                                                         RBJPARTIAL RPM/PWR LOSS      SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION        CLCLIMB          1                      CA                                          P66042C                     (CAN) ON CLIMB PILOTS EXPERIENCED TORQUE FLUCTUATIONS ON RT ENGINE. THEY RETURNED TO THE AIRPORT WITH NO FURTHER PROBLEMS. ON TAXI THEY BLEW THE FIRE BOTTLES ON THE RT ENGINE.  WHEN MAINTENANCE REMOVED THE COWLS THEY DISCOVERED HEAT DAMAGE TO SOME WIRING. ON FURTHER INVESTIGATION THEY DISCOVERED THAT THE EXHAUST PIPE STUB HAD BROKEN AND FOLDED OVER PARTIALLY BLOCKING THE EXHAUST GAS FLOW. FURTHER INVESTIGATION IS REQUIRED. (TC NR 20070502015)                                                                                                                                                                                                                                                                                  2L72 4T4  TRTBA15CAA E4WE    6  CP61GL    
20070618002012007061800201EU  2007       6          18         CA070502016      120070426G324018942           CLEVIS                                  SAAB  SF340 340B        7860101EU  GE    CT7TP CT79B       30030NE  ROTOL R390  R3904123F27 NE  RT BRAKE PEDAL  BROKEN          W      D   RETURN TO BLOCK                                                                                 S  AFFECT SYSTEMS                                                                TXTAXI/GRND HDL  1                      CA                                                                      (CAN) ON RUN UP THE RT BRAKE PEDAL CLEVIS FORKEND AT THE BRAZE JOINT BROKE. ON TROUBLESHOOTING THIS SNAG, IT WAS FOUND THAT SB 340-32-078 HAD NOT BEEN COMPLETED ON THIS A/C, THE NEW SOLID FORKEND P/N 250704 WAS INSTALLED IAW SB. (TC NR 20070502016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4T4  TRTA52EU   E8NE    6  CP31NE    
20070613001402007061300140EA  2007       6          13         CA070503001      120070207G274283963           ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              HORIZONTAL STAB UNSERVICEABLE   W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA       6392       1114                                                (CAN) SHORTLY AFTER DEPARTURE, RUNWAY 27L, AT APPROXIMATELY 3000 FEET, THE AC ROLLED TO 45 DEGREES, AND PITCHED UP > 18 DEGREES. THE CREW RECOVERED THE AIRCRAFT AT AN ALTITUDE OF 4500 FEET.   POST INCIDENT INVESTIGATION FOUND NO ANOMALIES WITH THE AILERON CONTROL SYSTEM, AILERON TRIM SYSTEM, ELEVATOR CONTROL SYSTEM, AND THE HSTA SYSTEM. SUBSEQUENT PRE-FLIGHT PREPARATION DETECTED A MALFUNCTION WITHIN THE HSTA. THE HSTA WAS REPLACED.   AIR SAFETY IS IN CONTACT WITH THE TSBC WHO IN TURN ARE IN CONTACT WITH THE GERMAN BFU. CRJ 7901 APPEARS TO HAVE OPERATED WITHOUT FURTHER INCIDENT SINCE REPLACEMENT OF THE HSTA. CRJ 7901 WAS EQUIPPED WITH A 9 HSTCU DURING THE INCIDENT FLIGHT, THIS UNIT WAS NOT SUSPECTED AND WAS NOT2L72 4F4  FRTA21EA   E15NE                
20070618002042007061800204NE  2007       6          18         CA070503002      320070430G61118173861         SLEEVE                                  DHAV  DHC8  DHC8106     2809020NM  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF7       NE  MR 3 BLADE      WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            7571                                                      (CAN) DURING ACTUATOR CHANGE FOUND THAT THE BLADE PIN BEARING ON THE NR 3 BLADE HAD EXCESSIVE MOVEMENT. UPON FURTHER INVESTIGATION, FOUND THAT THE BEARING SLEEVE WAS WORN THRU TO THE BEARING AND THAT THE BLADE PIN WAS WORN AS WELL. MFG SB 14SF-61-134 ADDRESSES THE PROBLEM ENCOUNTERED AND WAS NOT BEEN INCORPORATED ON THIS BLADE. (TC NR 20070503002)                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070618002082007061800208EA  2007       6          18         CA070503003      220070503G8530LW19332S        CONNECTING ROD                          RKWELL700   700         7630520SW  LYC   O540  TIO540R2AD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          BROKEN          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA            670                           L528761A                    (CAN) IT WAS REPORTED TO MAINTENANCE THAT THE RT ENGINE HAD EXPERIENCED SOME TROUBLE.  THE ENGINE WAS SHUTDOWN (DURING FLIGHT) AND PROP WAS FEATHERED. THE AIRCRAFT COMPLETED THE FLIGHT TO THE NEAREST AIRPORT AND LANDED WITHOUT INCIDENT.  THE PRELIMINARY INSPECTION INDICATES THAT THE NR 4 CYLINDER CONNECTING ROD BROKE THROUGH THE PISTON PIN HOLE.  THIS PERMITTED THE PISTON TO BECOME DISLODGED AND THE CYLINDER ASSEMBLY WAS SUBSEQUENTLY FORCED FREE OF THE ENGINE BREAKING ALL THE CYLINDER BASE HOLD DOWN STUDS. THE ENGINE WILL REQUIRE MAJOR REPAIRS. (TC NR 20070503003)                                                                                                                                                      1L72 3O3  O  A12SW   E14EA   5  CP33EA    
20070618002002007061800200WP  2007       6          18         CA070503004      220070426G732189777026        FUEL CONTROL                            MTSBSIMU2   MU2B36      5780412CE  GARRTTTPE331TPE33110    01514WP  HARTZLHCB3T HCB3TN5     GL  ENGINE          WORN            W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA       4283 4283                          P106684                     (CAN) ENGINE WAS SHUTDOWN DUE TO ABNORMAL INDICATIONS. ENGINE REMOVED AND SENT TO OVERHAUL FACILITY, FCU AND FUEL PUMP REMOVED, DAMAGE FOUND TO THE FUEL CONTROL QUILL SHAFT AND THE STUB SHAFT INTERNAL SPLINES. FCU AND FUEL PUMP REPLACED.  NOTE: FCU HAD 780.4 HOURS SINCE LAST SPLINE INSPECTION.  NOTE: FUEL PUMP P/N 897400-5 WAS REPLACED AT THIS TIME DUE TO SPLINE CHECK OUT OF LIMITS.  (TC NR 20070503004)                                                                                                                                                                                                                                                                                                                          1H72 3T4  TRTA10SW   E4WE    6  CP15EA    
20070618001892007061800189EA  2007       6          18         CA070503005      220070413G852076786           DRIVE GEAR                              PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2B   41532EA  HARTZLHCE3Y HCE3YR2A    GL  CRANKSHAFT      FAILED          W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA       2340                               RL118861                    (CAN) LT ENGINE FAILED IN CRUISE FLIGHT. AIRCRAFT RETURNED TO BASE. ENGINE REMOVED AND REPLACED. THE ACCESSORY CASE WAS REMOVED AND FOUND THAT THE CRANKSHAFT DRIVE GEAR HAD FAILED (TEETH STRIPPED OFF DRIVE GEAR). (TC NR 20070503005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070618002022007061800202EA  2007       6          18         CA070503006      220070426G8520C3317228        SEAL                                    PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  CRANKSHAFT      LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                          L521861A                    (CAN) RECEIVED ENGINE, AFTER A REPAIR FOR PREMATURE CAMSHAFT FAILURE (REF: SDR 20070319008).  AFTER INSTALLATION AND RUN-UPS, AN OIL LEAK WAS DISCOVERED AT THE CRANKSHAFT SEAL. WHEN THE SEAL WAS REMOVED IT WAS NOTED THAT IT WAS A (SPLIT) TYPE SEAL NOT THE ONE-PIECE AS CALLED FOR IN THE IPC.  AFTER SPEAKING WITH REPAIR STATION, THEY AGREED TO COVER THE LABOR AND NEW SEAL COSTS. A NEW SEAL WAS INSTALLED AND THERE HAVE BEEN NO LEAKS SINCE. WE RETURNED THE DEFECTIVE SEAL, AS THEY REQUESTED IT FOR QUALITY PURPOSES. (TC NR 20070503006)                                                                                                                                                                                         1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070625000022007062500002NM  2007       6          25         CA070503007      120070428G3240530425          LOCK            BFGOODRICH              DHAV  DHC5  DHC5A       2803018NM                                                               BRAKE           MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            24    347                                                 (CAN) DURING A ROUTINE DAILY INSPECTION, IT WAS NOTED ON ONE OF THE BRAKE UNITS WEAR INDICATOR PINS WAS NO LONGER PROTRUDING FROM THE BRAKE. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE LOCKING CLIP FOR THE END OF THE PIN WAS MISSING ALLOWING THE PIN TO SLIDE IN AND OUT OF THE UNIT. THE BRAKE UNIT HAD JUST BEEN RETURNED FROM REPAIR BY CONDOR AVIATION AND INSTALLED ON THE AIRCRAFT 24.3 HOURS BEFORE. THE DEFECTIVE UNIT WAS REMOVED AND REPLACED WITH A SERVICEABLE ONE. (TC# 20070503007)                                                                                                                                                                                                                                2H72 4T    RT                             
20070618002032007061800203NE  2007       6          18         CA070503008      220070429G8530LW13622         VALVE STEM                              ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          BENT            W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA       466                                                            (CAN) AIRCRAFT WAS FLYING DURING A SEISMIC JOB.  ENGINE LOST POWER AND ENGINE WAS RUNNING ROUGH.  EMERGENCY LANDING TOOK PLACE.  MAINTENANCE INVESTIGATED AND FOUND NR 1 CYLINDER DEFECTIVE.  UPON FURTHER INVESTIGATION INTAKE VALVE STUCK OPEN AND CONTACTED PISTON.  CYLINDER AND PISTON WERE REPLACED AND AIRCRAFT WAS PUT BACK IN SERVICE. (TC NR 20070503008)                                                                                                                                                                                                                                                                                                                                                                             1G71 3O3  O  H11NM   1E4                  
20070618001922007061800192EU  2007       6          18         CA070503009      120070422G27429787314203      ACTUATOR                                PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  PITCH TRIM      INOPERATIVE     W      O   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA       7794 5773                                                      (CAN) THE SECONDARY ELECTRIC MOTOR, WHICH ACTUATES THE PITCH TRIM ACTUATOR IN RESPONSE TO AUTO PILOT COMMANDS WAS NOT OPERATIVE. THIS RENDERED THE AUTOPILOT SYSTEM U/S. THE ACTUATOR WAS REPLACED AND THE SYSTEM WAS CHECKED AIRWORTHY. THE O/H INTERVAL ON THESE ACTUATORS IS 6000 HRS. OR 5 YEARS INSTALLED TIME. (TC NR 20070503009)                                                                                                                                                                                                                                                                                                                                                                                                        1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070618001932007061800193SW  2007       6          18         CA070503010      120070423G7603C8102413        CONTROL CABLE                           SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCB3T HCB3TN5     GL  POWER LEVER     FAILED          W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) CONTROL CABLE FAILED WHERE IT MAKES A BEND COMING OUT OF THE CENTER PEDESTAL.  COMMON FAILURE POINT.  REPLACED WITH NEW PART, REPLACED OTHER SIDE AS A PRECAUTION AS WELL. (TC NR 20070503010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4T4  TRTA8SW    E4WE    6  CP15EA    
20070619001272007061900127NM  2007       6          19         CA070503011      120070428G29103811374102      CABLE                                   DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  INDICATOR       SEPARATED       W      O   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA            127   0193                                                (CAN) THE ORIGINAL RESERVOIR WAS REPLACED DUE TO FAULTY DIAPHRAGM INTERNALLY.  NEW O/H UNIT WAS INSTALLED. APPROXIMATELY 127 HOURS LATER AS THE AIRCRAFT WAS PREPARING FOR DEPARTURE THE HYD. LOW PRESS. LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO THE DEPARTURE RAMP AND SHUTDOWN. DURING THE INVESTIGATION OF THE FAULT THE HYD LEVEL WAS CHECKED USING THE GAUGES WHICH BOTH SHOWED FULL. THE PUMP WAS REMOVED TO SEE IF THE SHAFT HAD SHEARED BUT IT DID NOT. UPON FURTHER TROUBLESHOOTING IT WAS DISCOVERED THAT THE HYDRAULIC SYSTEM WAS EMPTY. IT WAS THEN NOTICED UPON CLOSER INVESTIGATION OF THE INDICATOR CABLE ASSY. THAT THERE WAS A KINK IN THE CABLE NEXT TO THE NUT WHICH SECURES IT TO THE TOP OF RESERVOIR PREVENTING FREE 2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070619001282007061900128NM  2007       6          19         CA070504001      120070501G5400312N570138      LINE                                    BOEING757   757236      1384971NM  RROYCERB211 RB211535E43754555NE                                              LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) FORWARD PYLON PRESSURE LINE FOUND CHAFED THROUGH CAUSING LEAK.  DAMAGE CAUSED BY A DEFECTIVE HOSE CLAMP. (TC NR 20070504001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA2NM    E12EU                
20080129000142008012900014SW  2008       1          29         CA070504002      120070503G6220471401241       TUBE            BELL                    BELL  47    47G2        1181008SW  LYC   O435  VO435A1D    41516EA                              STABILIZER BAR  CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       141261108  54C                                                 (CAN) ON NORMAL WALK AROUND PILOT NOTICED STABILIZER BAR TUBE CRACKED AT SLEEVE AT IB END OF TUBE. STAB BAR ASSEMBLY WAS REPLACED AND MACHINE RETURNED TO SERVICE. AD 74-08-02 COVERS THIS ISSUE ON SOME OF THE LATER MODEL STAB BARS BUT NOT THE EARLIER MODELS OF STAB BARS. ALTHOUGH WE CHECK THIS AS PART OF OUR NORMAL PREFLIGHT CHECK AND THIS IS HOW IT WAS FOUND. (TC NR 20070504002)                                                                                                                                                                                                                                                                                                                                                   1G71 3O3  O  H1      E279                 
20080319001362008031900136EA  2008       3          19         CA070504003      220070502G72503024711         TURBINE WHEEL                           BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       14878                              PCE85202                    (CAN) DURING A HOT SECTION INSPECTION, A CRACK WAS DISCOVERED ON THE CT HUB FROM ONE UNUSED BALANCE HOLE, AROUND THE FLANGE AND BACK TO THE SAME BALANCE HOLE.THE CRACK WAS ADJACENT TO (1) OF THE (3) PROTRUDING LOCK LUGS. (TC NR 20070504003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070619001292007061900129NM  2007       6          19         CA070504004      120070430G5330                SKIN                                    BOEING737   7372L9      1384497NM  PWA   JT8   JT8D17      52049NE                              BS 727          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING WASHING PROCEDURE MAINTENANCE DETECTED A SKIN CRACK AT BS727, WL215, APPROXIMATELY 1.5 INCHES LONG. THIS IS KNOWN AREA ADDRESSED BY SB 737-53-1065. THE AREA WAS REPAIRED IAW THE MANUFACTURERS SRM AND RETURNED TO SERVICE (TC NR 20070504004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA16WE   E2EA                 
20070619001302007061900130SO  2007       6          19         CA070504006      120070501G534336058711        FITTING                                 LKHEED382   382G        526414USO  ALLSN 501D  501D22A     03006GL  HAMSTD54H   54H60117    NE  TRUNNION SUPPORTCRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION, A CRACKED LT NLG TRUNNION SUPPORT WAS DETECTED AND THE AIRCRAFT IS CURRENTLY UNDERGOING REPLACEMENT OF THE FITTING.  (TC NR 20070504006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2H74 4T4  T  A1SO    E282    6  CP906     
20070808001622007080800162CE  2007       8          8          CA070504007      120070507G32457008006         TUBE                                    CESSNA207   207         2073602CE  CONT  O520  IO520D      17032SO  HARTZLHCC3Y HCC3YF1     GL  TIRE            LEAKING         W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       185  185                                                       (CAN) AIRCRAFT LANDED, DURING TAXI RT MAIN WHEEL WENT FLAT AIRCRAFT WAS REMOVED FROM RUNWAY WHEEL ASSY REMOVED, TUBE FOUND TO HAVE A PIN HOLE, TUBE REPLACED, AIRCRAFT RETURNED TO SERVICE (TC NR 20070504007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  O  A16CE   E5CE    5  CP25EA    
20080131000182008013100018CE  2008       1          31         CA070504008      120070503G28221013640867      PUMP            BEECH                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  FUEL TRANSFER   MALFUNCTIONED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  PC112                                               (CAN) RT FUEL PUMP RUNNING EVEN AFTER MASTER SWITCH OFF.  (TC NR 20070504008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070619001312007061900131    2007       6          19         CA070504009      420070503G2210                COMPUTER                                BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  FLT DIRECTOR    MALFUNCTIONED   W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) FLIGHT DIRECTOR CB TRIPPED AND WILL NOT RESET. (TC NR 20070504009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070619001322007061900132NM  2007       6          19         CA070504010      120070502G3234MS253831        SWITCH                                  BOEING737   737201      1384454NM  PWA   JT8   JT8D17      52049NE                              MLG HANDLE      INTERMITTENT    W      L   ABORTED APPROACH                                                                                N  FALSE WARNING                                                                 APAPPROACH       1                      CA                                                                      (CAN) ON FINAL APPROACH, THE FLIGHT CREW SELECTED LANDING GEAR DOWN. THE LAND GEAR INDICATORS ILLUMINATED 3 GREEN AND 3 RED. THIS INDICATED A DISAGREEMENT BETWEEN LANDING GEAR HANDLE POSITION AND LANDING GEAR POSITION. THE FLIGHT CREW SELECTED GEAR UP AND ABORTED THE LANDING. ON THE DOWNWIND LEG THE FLIGHT CREW SELECTED LANDING GEAR DOWN AND ALL ILLUMINATION WAS NORMAL (3 GREEN AND NO RED ILLUMINATION). THE FLIGHT CREW LANDED UNEVENTFUL.  MAINTENANCE INSERTED THE LANDING GEAR PINS AND SELECTED GEAR UP AND DOWN NUMEROUS TIMES AND WAS NOT ABLE TO DUPLICATE THE PROBLEM. THE AIRCRAFT WAS RELEASED AND CONTINUES TO FLY WITHOUT REOCCURRENCE OF THE PROBLEM. OPERATOR HAS ORDERED AN NEW LANDING GEAR HANDLE SWITCH AND WIL2L72 4F4  F  A16WE   E2EA                 
20070622000512007062200051EA  2007       6          22         CA070505001      120070501G5610NP1393225       WINDOW                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              COCKPIT         CRACKED         W      BG  EMER. DESCENT           O2 MASK DEPLOYED                                                        O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) THE CAPTAIN`S SIDE WINDSCREEN OUTER PANE CRACKED. THE FLIGHT WAS AT 34000FT, WHEN THE INCIDENT OCCURRED, THEN THEY DESCENDED AND DAWNED THEIR OXYGEN MASKS AS A PRECAUTION. THERE WAS NO PRESSURE LOSS AND NO EMERGENCY DECLARED. MAINTENANCE INSPECTED THE AIRCRAFT AFTER LANDING AND REPLACED THE CRACKED WINDOW. (TC NR 20070505001)                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA21EA   E15NE                
20070619001332007061900133SW  2007       6          19         CA070506001      120070423G6510204010765001    NUT                                     BELL  204   204B        1181404SW  LYC   T53   T5313B      41549NE                              TAIL ROTOR      DAMAGED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) ON APRIL 23, 2007 DURING A TEST FLIGHT FOR MAINTENANCE THAT WAS PERFORMED, THE PILOT EXPERIENCED AN UNCONTROLLED YAW TO THE RIGHT WHILE IN A 4 FOOT HOVER.  THE HELICOPTER WAS IMMEDIATELY SET DOWN ON THE TARMAC.  THERE APPEARED TO BE A STEP WORN IN THE INTERNAL WORM GEAR SPLINE OF NUT ASSEMBLY P/N 204-010-765-001 THAT MAY HAVE AFFECTED THE RIGGING PROCEDURE THAT WAS ACCOMPLISHED THE NIGHT BEFORE.  NO DAMAGE TO HELICOPTER, CARS 625 APPENDIX G WAS PERFORMED AT THE SCENE WITH NO REPORTED DEFECT.  ENTIRE QUILL ASSEMBLY WAS REPLACED; AIRCRAFT RECEIVED FURTHER INSPECTION AND RE-RIGGED TAIL ROTOR ASSEMBLY AND TEST FLOWN WITH NO DEFECT.   TSB WAS NOTIFIED AND HAVE NOT FINISHED THEIR INVESTIGATION.  PRODUCT SUPPORT1G71 4U4  U  H1SW    E17EA                
20070619001342007061900134EA  2007       6          19         CA070506002      120070505G711022850020113     NOSE COWL                               CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              RT ENGINE       DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A SCHEDULED MAINTENANCE CHECK, AFTER FAN COWL RT REMOVAL, STRUCTURAL DAMAGE WAS OBSERVED ON THE INLET COWL BY THE CAPPED 14TH STAGE BLEED AIR DUCT.  DAMAGE WAS OBSERVED ON THE REMOVED FAN COWL, SAME AREA, AS WELL. MAINTENANCE PROCEED TO REPLACE THE FAN COWL AND THE INLET COWL. AIRFRAME HOURS=26110:41. CYCLES= 21307. (TC NR 20070506002)                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA21EA   E15NE                
20070619001352007061900135NM  2007       6          19         CA070507005      120070507G276082742339001     PULLEY                                  DHAV  DHC8  DHC8*              NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  SPOILER CABLE   MISINSTALLED    W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       8935                                                           (CAN) AN OPERATOR HAS REPORTED THE FOLLOWING FINDINGS DURING THE C2 INSPECTION BEING PERFORMED ON AN AIRCRAFT. DURING INSPECTION OF THE SPOILER CABLE DISCONNECT SENSING SYSTEM ASSY, THE FAIRLEAD ROLLER AND SPRING ATTACHMENT HAVE BEEN FOUND INSTALLED INCORRECTLY. THE OPERATOR STATE THAT THEY HAD NO REASON TO BELIEVE THAT THIS COULD HAVE BEEN CARRIED OUT IN SERVICE, AND THE ERROR WOULD HAVE OCCURRED DURING AIRCRAFT PRODUCTION.  THE OPERATOR IS CURRENTLY CONDUCTING A FLEET-WIDE INSPECTION AND WILL ADVISE US ON THEIR FINDINGS.  (TC NR 20070507005)                                                                                                                                                                           2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070619001362007061900136CE  2007       6          19         CA070507007      120070504G8011642085A4        ADAPTER                                 CESSNA402   402C        207590RCE  CONT  O520  TSIO520VB   17040SO  MCAULY3AF32C3AF32C505   GL  NR 1 STARTER    FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA            10                                                        (CAN) UNABLE TO ROTATE ENGINE DURING WALKAROUND INSPECTION PRIOR TO ENGINE START. FAULT ISOLATED TO STARTER ADAPTER ASSY. STARTER ADAPTER FAILED ONLY 9.6 HRS IN SERVICE AFTER OVERHAUL. OVERHAUL FACILITY CONTACTED. UNIT TO BE SHIPPED TO FACILITY FOR TEARDOWN INSPECTION.  STARTER ADAPTER REPLACED. (TC NR 20070507007)                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  A7CE    E8CE    5  CP22EA    
20070619001372007061900137SW  2007       6          19         CA070507008      120070506G7120276211495       TRUSS                                   FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  RT ENGINE MOUNT CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A PHASE 6 INSPECTION, A GAPING CRACK WAS FOUND ON THE RT ENGINE TRUSS MOUNT AT THE UPPER IB WELD JOINT OF THE FIREWALL ATTACH FITTING. (TC NR 20070507008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20070619001382007061900138CE  2007       6          19         CA070507009      120070503G79313020958         RELIEF VALVE                            CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  ENGINE OIL      MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       7508 125                           PCE19412                    (CAN) IN CRUISE FLIGHT, OIL PRESSURE BEGAN TO FLUCTUATE FROM BOTTOM TO MIDDLE OF GREEN RANGE, 80 TO 90 PSI.  FAULT CONFIRMED ON GROUND RUN, NOT RELATED TO INDICATION. CONSULTATION WITH ENGINE OVERHAULER, OIL PRV VALVE TO BE CHECKED. PARTS AT TOOLS DISPATCHED, THIS REPORT OPEN. (TC NR 20070507009)                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3T3  T  A37CE   E4EA    5  CP60GL    
             20081104     EA  2008       11         4          CA070507010      120070502G324650105844        WHEEL                                   CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              MLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       14976                                                          (CAN) DURING ROUTINE NDT HFEC INSP ON RJ MAIN WHEEL, ACCORDING TO ABSC NDT MANUAL PART 1, 32-42-03, CRACKS WERE FOUND IN THE LOCKING RING GROOVE. THE CRACKS HAVE A DEPTH OF .040 INCH, .020 INCH AND .010.INCH.  COMPONENT COULD BE SENT FOR MACHINING, BUT THE DEFECT DEPTH IS ALREADY GREATER THAN THE MACHINING LIMITS.                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA21EA   E15NE                
20070622000012007062200001EU  2007       6          22         CA070507011      120070504G3297                WIRE HARNESS                            BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  LT MLG WW       DAMAGED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) DEPARTING THE LANDING GEAR SELECT LEVER WOULD NOT MOVE TO THE GEAR UP POSITION. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE DETERMINED THE SOURCE OF THE PROBLEM WAS IN THE LT GEAR HARNESS WHEELWELL CONNECTOR. THE WIRING WAS REPAIRED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070507011)                                                                                                                                                                                                                                                                                                                                                                                        2L72 3T4  T  A24EU   A196    6  CP899     
20070622000022007062200002EU  2007       6          22         CA070507012      120070503G3610                SHUTOFF VALVE                           AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF5       NE  BLEED AIR SYS   MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) DEPARTING THE CREW OBSERVED THAT THE ARCRAFT WAS FAILING TO PRESSURIZE NORMALLY. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE REPLACED THE NR 1 BLEED AIR SHUTOFF VALVE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070507012)                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20070619000762007061900076EA  2007       6          19         CA070507013      220070412G7414                ROTOR           BENDIX      S4LN20      CESSNA172   172K        2072430CE  LYC   O320  O320E2D     41508EA  MCAULY1A175 1A175*      GL  MAGNETO         FAILED          W      D   RETURN TO BLOCK                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA            1995                                                      (CAN) PILOT OF AC ON FLOATS DETECTED A DEAD MAGNETO ON HIS PRE-TAKEOFF INSPECTION, AND RETURNED TO THE DOCK. (TC NR 20070507013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A12    E274    5  NP857     
             20081104     CE  2008       11         4          CA070508001      120070507G8011MHB4016R        STARTER                                 CESSNA172   172RG       2072438CE  LYC   O360  O360F1A6    41514EA  MCAULY2D34C B2D34C220   GL  ENGINE          MALFUNCTIONED   W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA            440                                                       (CAN) PILOT DID RUN-UP, ALL ENGINE INDICATIONS WERE NORMAL SO HE COMMENCED HIS TAKE-OFF. JUST AFTER HE STARTED TO CLIMB HE NOTICED THAT THE ACFT DID NOT WANT TO CLIMB AS IT SHOULD. ALL ENGINE INSTRUMENTS WERE WHERE THEY WERE SUPPOSED TO BE. HE ABORTED HIS TAKE-OFF WITHOUT INCIDENT. ACFT WAS RUN UP BY MAINT, ALL ENGINE INDICATIONS WERE CORRECT. COWLINGS WERE REMOVED AND ENGINE WAS INSPECTED, NOTHING WAS NOTED AS BEING WRONG. COMPRESSION CHECK WAS COMPLETED ON ENGINE AND WHILE DOING THE TEST. THE STARTER BENDIX ENGAGED BY ITS SELF (NO POWER WAS ON). TALKED TO ENGINE SHOP AND CONCLUDED THAT THE STARTER MUST HAVE ENGAGED ITS SELF ON TAKE-OFF AND THIS CAUSED LOSS OF POWER. SERVICABLE STARTER INSTALLED AND ACFT WAS F1H71 3O3  O  3A17    E286    5  CP7EA     
20070619000782007061900078SW  2007       6          19         CA070508002      120070507G7120206064106001    LEG ASSY        BELL        206064106   BELL  206   206L1       1182107SW  ALLSN 250C  250C30      03013GL                              ENGINE MOUNT    BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       11747                                                          (CAN) ON STARTING A 200HR SCHEDULED INSPECTON FOUND LT ENGINE MOUNT LEG BROKEN IN (2) PIECES AND UPON REMOVAL FOUND SEVERE INTERNAL CORROSION THAT CAUSED THE WALL THICKNESS TO DEGRADE TO THE POINT OF COLLAPSE AND FAILURE. (TC NR 20070508002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3U3  U  H2SW    E1GL                 
20070619000792007061900079WP  2007       6          19         CA070508003      120070508G6220369X10045       PIN                                     HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              MAIN ROTOR      BENT            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1333                                                           (CAN) DURING AN INSPECTION THE ENGINEER NOTICED THE THE M/R BLADE FOLDING PIN LOOKED BENT. UPON TAKING THE UNIT APART HE NOTICED THAT THE THREADS OF THE PIN WERE NOT ON THE PIN STRAIGHT, KIND OF LOPSIDED. (TC NR 20070508003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3U3  U  H3WE    E4CE                 
20070808001632007080800163CE  2007       8          8          CA070508004      120070411G2750S19061          CONTROL SWITCH                          CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  TE FLAPS        FAULTY          W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             NRNOT REPORTED   1                      CA                                                                      (CAN) DURING CIRCUITS, PILOTS SELECTED FLAPS UP AND THEY REMAINED IN THE FULL DOWN POSITION. FOUND UP CONTROL SWITCH AT FLAP SELECTOR IN COCKPIT FAULTY, REPLACED SWITCH, OPS CHECKED OK WITH NO FURTHER OCCURANCES. (TC NR 20070508004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A19    E223    5  NP50GL    
20070619000822007061900082SO  2007       6          19         CA070508005      120070504G2913268028          HOUSING                                 PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  HYD PUMP        CRACKED         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA                                                                      (CAN) 2ND MAINTENANCE GROUND RUN WAS COMPLETED ON AIRCRAFT AND ENGINES SHUTDOWN. HAD LUNCH AND RETURNED TO A/C AND OBSERVED POOL OF HYDRAULIC FLUID BENEATH THE RT ENGINE. POST INSPECTION OF HYD PUMP REVEALED A CRACKED HOUSING.  REPLACED THE HYDRAULIC PUMP.   (TC NR 20070508005)                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070619000832007061900083NM  2007       6          19         CA070509001      120070507G561080260008        WINDSHIELD                              BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       69                                                             (CAN) IN CRUISE FLIGHT AT 25,000, THE FO`S WINDSHIELD CRACKED. REMOVED AND REPLACED FO`S WINDSHIELD I/A/W Q 400 TASK 56-10-01-000-801 AND TASK 56-10-01-400-801, REMOVED AND REPLACED FO`S WINDSHIELD ANTI-ICE CONTROLLER I/A/W Q 400 TASK 30-41-01-00-801 AND TASK 30-41-01-400-801 OP`S TEST GOOD.  (TC NR 20070509001)                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080220000472008022000047CE  2008       2          20         CA070509002      120070509G213310138001313     CONTROL VALVE                           BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  CABIN PRESSURE  INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WORK WAS DONE TO THE AC THAT OPENED THE PRESSURE VESSEL. WHEN THIS WORK WAS STARTED THE AC WOULD HOLD MAX DIFF. THE WORK DONE LED TO A PRESSURIZATION PROBLEM, WHICH, WHILE TROUBLESHOOTING, LED TO THE DISCOVERY OF FLOW CONTROL VALVE THAT WAS WORKING INCORRECTLY. THE CABIN LEAK CAUSED BY THE WORK DONE WAS CORRECTED AND AN O/H FLOW PACK INSTALLED. THE AC STILL WOULD NOT HOLD MAX  DIFF, MORE CABIN LEAKS WERE DISCOVERED AND REPAIRED. OUTFLOW AND SAFETY VALVES WERE CHANGED. PROBLEM STILL REMAINED. A SERVICEABLE CONTROL VALVE FROM AN IN SERVICE AC WAS INSTALLED FOR TROUBLESHOOTING, AND THE AIRCRAFT WOULD PRESSURIZE TO MAX  DIFF.  A SECOND O/H FLOW CONTROL VALVE WAS INSTALLED ON THE LT SIDE AS WELL AS AN O/H UNIT1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070808001642007080800164EU  2007       8          8          CA070509003      120070504G2841360930001       SIGNAL COND UNIT                        AMD   FALC10FALCON10    2730101EU  GARRTTTFE731TFE73121C        NE                              FUEL INDICATOR  MALFUNCTIONED   W      O   OTHER                                                                                           N  FALSE WARNING                                                                 CRCRUISE         1                      CA            7                                                         (CAN) IN FLIGHT, ON THE WAY BACK TO BASE THE CREW NOTICED THE RT FUEL GAUGE WAS INTERMITTENT AND NOT WORKING MOST OF THE TIME.  THE DEFECTIVE PART WAS JUST REPLACED 7 HOURS PRIOR WITH THE SAME ISSUE.  ANOTHER SIGNAL CONDITIONER HAS BEEN INSTALLED AND CALIBRATED.  THERE HAS BEEN NO FAULTS SINCE THE REPLACEMENT. (TC NR 20070509003)                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  F  A33EU   E6WE                 
20070622000032007062200003EA  2007       6          22         CA070509004      120070503G71102285008114      COWLING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              NR 1 ENGINE     SEPARATED       W      K   NONE                                                                                            DE INFLIGHT SEPARATION       VIBRATION/BUFFET                                    DEDESCENT        1                      CA       5855                                                           (CAN) ON DESCENT, THROUGH FL280, CREW FELT SLIGHT VIBRATION TO THE AIRCRAFT.  FIRST OFFICER (FO) FELT A SLIGHT SHUDDER IN THE CABIN.   ON ARRIVAL, IT WAS FOUND NR 1 LOWER ENGINE COWL HAD SEPARATED FROM THE AIRCRAFT.  UPON MAINTENANCE INITIAL INSPECTION, IT WAS NOTED THAT 75 PERCENT OF THE CAMLOC FASTENERS THAT HOLD THE COWL WERE STILL INSTALLED IN THE COWL RETAINERS. THE COWL SEPARATION CAUSED DAMAGE TO THE UPPER ACCESS NOSE COWL, NOSE COWL, LOWER TORQUE BOX, LOWER OB T/R CASCADE, AND SOME T/R PDU LINES.  (2) RETAINERS WERE REPLACED, THE LOWER CASCADE VANE WAS REPLACED, P2 SENSE LINE WAS REPLACED AND THE UPPER AND LOWER COWLS WERE REPLACED.   THE A/C WAS THEN FERRIED FOR FULL INSPECTION AND REPAIR.  AFTER FURTH2L72 4F4  FRTA21EA   E15NE                
20070619000852007061900085NM  2007       6          19         CA070510001      120070506G2920DSC1896         CHECK VALVE                             DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  NR 2 HYD SYS    CRACKED         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    APAPPROACH       1                      CA                                                                      (CAN) AN OPERATOR EXPERIENCED A LOSS OF NR 2 HYD FLUID SYSTEM DUE TO A FRACTURED CHECK VALVE WHEN THE LANDING GEAR WAS SELECTED DOWN DURING APPROACH. THE CAUSE OF THE EVENT IS A CIRCUMFERENTIAL CRACK AROUND NR 2 HYD SYSTEM MANIFOLD CHECK VALVE. (TC NR 20070510001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070820000382007082000038CE  2007       8          20         CA070510002      120070117G5512                SKIN                                    CESSNA441   441         2076020CE                                                               STABILATOR      DELAMINATED     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9440                                                           (CAN) FOUND DELAMINATION (OF 8 INCH X 16 INCH) ON TOP OF LT SIDE IB HORIZONTAL STABILIZATOR.  DELAMINATION FOUND WHEN DOING PHASE 2 AND 3 INSPECTION.  HORIZONTAL STABILIZATOR REPLACED, NO REPAIR IS ALLOWED ON HORIZONTAL STABILIZATOR IAW SRM.  (TC NR 20070510002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3T    RTA28CE                        
20080220000482008022000048CE  2008       2          20         CA070510003      120070428G3260                SQUAT SWITCH                            BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  RT MLG          FAILED          W      O   OTHER                                                                                           G  MULTIPLE FAILURE                                                              DEDESCENT        1                      CA                                                                      (CAN) OUR 1900D WAS ON APPROACH, PILOT SELECTED THE LANDING GEAR DOWN. NOTHING HAPPENED, AC RETURNED TO ITS MAIN BASE. WHEN MAINT RECEIVED THE AC THE FAULT COULDNT BE DUPLICATED. DURING TROUBLESHOOTING ON THE GROUND THE MAINT WAS ABLE TO FIND A CONSTANT FAULT ON THE GROUND, IT WAS FOUND THAT THERE WAS A CONSTANT 28 VOLTS APPLIED TO THE (UP) SOLENOID OF THE HYDR POWERPACK, PREVENTING THE (DOWN) SOLENOID FROM MOVING THE SELECTOR VALVE TO THE DOWN POSITION WHEN THE LANDING GEAR HANDLE IS PLACED IN THE (DOWN) SELECTION. THE VOLTAGE SOURCE ORIGINATED FROM THE PROP GOVERNOR TEST CIRCUIT THROUGH THE RT MLG SQUAT SWITCH. THE SQUAT SWITCH WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070510003)      2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20080319001372008031900137SO  2008       3          19         CA070510004      220070420G8530TISN73OCA221    CYLINDER                                CESSNA421   421C        2076016CE  CONT  O520  GTSIO520L   17032SO                              NR 2            BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            103                           150045H                     (CAN) WHEN DOING 100 HRS INSP, FOUND DAMAGE ON COVER VALVE ROCKER CYLINDER NR 4, COVER (PN : 631834) REMOVED AND FOUND RETAINER ROCKER SHAFT (PN: 646032) BROKEN. NEW CYLINDER WAS INSTALLED IN POSITION NR 4. ALSO FOUND CYLINDER NR 2 WITH LOW COMPRESSION (50 PSID), THE CYLINDER WAS REPLACED BY NEW ONE. (TC NR 20070510004)                                                                                                                                                                                                                                                                                                                                                                                                               1L72 3O3  O  A7CE    E7CE                 
20070619000862007061900086WP  2007       6          19         CA070510005      220070507G7250                TURBINE BLADES                          LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       607                                P116662C                    (CAN) DURING POST/PREFLIGHT INSPECTION, MAINTENANCE PERSONNEL NOTICED NICKS ON 2 OF THE 3RD STAGE TURBINE BLADES. NO FOD DAMAGE WAS NOTICED ON THE COMPRESSOR END OF THE ENGINE, SUSPECT FIRST STAGE BLADE RETAINER COMING LOOSE FROM TURBINE DISC AS ON SDR NR 20061110007 AND SDR NR 20060618001.   WILL NOTIFY WHEN HAVE CONFIRMATION.  ENGINE HAS BEEN REMOVED AND SENT TO AN HEAVY MAINTENANCE FACILITY FOR INVESTIGATION AND REPAIR. A RENTAL ENGINE HAS BEEN INSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070510005)                                                                                                                                                                                                         2L72 4F4  FRTT00008WIE6WE                 
20070619000872007061900087EU  2007       6          19         CA070510006      120070510G6520350A33100021    GEAR                                    SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              T/R GEARBOX     WORN            W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      CA       691  691   MA1110                                              (CAN) GEAR SET, PINION GEAR AND BEVEL GEAR WEAR AND PRODUCED METAL.  GEAR SET SCRAPPED DUE TO SPALLING. GEAR SET INSTALLED AT LAST OVERHAUL OF THE GEARBOX. TGB TSN 4632.8 / TSO 691.2 GEAR SET TSN 691.2 (TC NR 20070510006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H9EU    E19EU                
20070619000882007061900088NM  2007       6          19         CA070510007      120070504G323385311176009     ACTUATOR                                DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  NLG             CRACKED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH, THE NOSE LANDING GEAR WOULD NOT EXTEND TO THE DOWN AND LOCKED POSITION. CREW DID A FLY-BY PASS THE ATC CONTROL TOWER, WHO CONFIRMED THAT THE GEAR WAS EXTENDED, BUT DID NOT APPEAR TO BE LOCKED.  GEAR WAS CYCLED AND ALL (3) GEARS WERE CONFIRMED DOWN AND LOCKED. AIRCRAFT THEN LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS THEN FERRIED WITH GEAR PINNED DOWN TO A MAINTENANCE BASE FOR FURTHER INSPECTION AND REPAIR. THE FOLLOWING DAMAGE WAS FOUND. THE NLG UPLOCK ACTUATOR FITTING ASSY P/N 85311176-009 WAS FOUND CRACKED AT THE ACTUATOR ATTACH POINT. DISCOLORATION OF PART OF THE CRACK INDICATES PROPAGATION OCCURRED OVER A PERIOD OF TIME. RECOMMEND A MORE FOCUSED SPECIFIC VISUAL OR NDT INSPECTION OF THIS2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
             20081104     WP  2008       11         4          CA070511001      120070508G8010C0531           SWITCH          ROBSIN      C0512       ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              CLUTCH ACTUATOR DEFECTIVE       W      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                TXTAXI/GRND HDL  1                      CA       487                                                            (CAN) ACFT SHUTDOWN AT LEASE SITE. PILOT ATTEMPTED TO START THE ACFT TO CARRY OUT DAY AND ACFT FAILED TO START. FURTHER INVESTIGATION CONDUCTED BY AN AME FOUND ENGAGING SWITCH HAD FAILED. THE ACTUATOR ASSY WAS VERY DUSTY AND DIRTY FROM BELT DEBRIS. THE ACFT WAS FERRIED BACK TO A MAINT BASE AND THERE CLUTCH ASSY WAS REPLACED AND ACFT RETURNED TO THE FLIGHT LINE. (TC NR 20070511001)                                                                                                                                                                                                                                                                                                                                                 1G71 3O3  O  H11NM   1E4                  
20070808001652007080800165CE  2007       8          8          CA070511002      120070510G3210504501025       TORQUE TUBE                             CESSNA310   310R        2074245CE  CONT  O520  IO520M      17032SO  MCAULY3AF32C3AF32C*     GL  MLG             BROKEN          W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKE-OFF PILOT RETACTED GEAR ALL 3 GREEN LIGHTS WENT OUT AND UNLOCKED LIGHT WAS OUT.  RADIO CALL FROM TOWER INFORMED PILOT THAT LT MAIN GEAR WAS NOT RETRACTED.  PILOT PUT GEAR DOWN AND GOT ALL 3 GREEN LIGHTS. SHUT DOWN LT ENGINE IN CASE GEAR COLLAPSED ON LANDING AND MADE UNEVENTFUL LANDING. AIRCRAFT INSPECTED AND IT WAS NOTED THAT THE LT MAIN RETRACT TORQUE TUBE WAS BROKEN. NEW PART ON ORDER. (TC NR 20070511002)                                                                                                                                                                                                                                                                                                     1L72 3O3  O  3A10    E5CE    5  CP22EA    
20070618001232007061800123EA  2007       6          18         CA070511003      220070410G8520                BUSHING                                 PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          WORN            W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA            1208                          L739061A                    (CAN) DURING CRUISE PORTION OF THE FLIGHT, THE PILOT NOTICED A VIBRATION FOLLOWED BY A NOISE AND LOSS OF OIL. THE PILOT SHUTDOWN THE ENGINE AND DIVERTED TO A NEARBY AIRPORT AND LANDED SAFELY. THE ENGINE WAS REMOVED AND SENT TO AN ENGINE SHOP FOR A TEARDOWN.   IT WAS DETERMINED THAT THE COUNTERWEIGHT BUSHING WAS WORN THUS CAUSING EXCESSIVE PLAY. THIS EXCESSIVE PLAY CAUSED THE COUNTERWEIGHT CHEEK TO BREAK AND THE COUNTERWEIGHT COMING LOOSE INSIDE THE ENGINE WHICH CAUSED SUBSTANTIAL DAMAGE.  THE POSSIBLE REASON FOR THE FAILURE COULD BE DUE TO ENGINE OVERSPEED AT SOMETIME OR ANOTHER. (TC NR 20070511003)                                                                                                                  1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070618001242007061800124EU  2007       6          18         CA070511004      120070405G32309740926112      RELAY                                   PILATSPC12  PC1245      7090551EU                                                               MLG             MALFUNCTIONED   W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) ON A RETURN FLIGHT, GEAR DOWN WAS  SELECTED BY PILOT. AFTER GEAR DOWN AND LOCKED, THE HYDRAULIC PUMP REMAINED OPERATING. PILOT LANDED AIRCRAFT AND MAINTENANCE WAS NOTIFIED.  DURING TROUBLESHOOTING MAINTENANCE DISCOVERED WHEN POWER APPLIED TO AIRCRAFT, THE HYDRAULIC PUMP REMAINED OPERATIONAL. PULLING THE HYDRAULIC CONTROL 5 AMP CIRCUIT BREAKER HAD NO EFFECT. THIS LED MAINTENANCE TO THE K601 RELAY WHERE IT WAS FOUND THAT THE CONTACTS WERE STUCK. CONSEQUENTLY THE ONLY WAY TO SHUT THE PUMP OFF WAS WITH THE BATTERY MASTER SWITCH. AFTER REPLACEMENT OF THE RELAY, SYSTEM OPERATED NORMALLY. (TC NR 20070511004)                                                                                                          1L71 3T    RTA78EU                        
20070620000032007062000003GL  2007       6          20         CA070511005      220070502G732323007505        GOVERNOR                                BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              ENGINE          FAILED          W      D   RETURN TO BLOCK                                                                                 R  PARTIAL RPM/PWR LOSS                                                          TOTAKEOFF        1                      CA            1054                                                      (CAN) GOVERNOR DROOPED TO 95 PERCENT WOULD NOT RETURN TO 100 PERCENT. RETURNED TO BASE, TO CHANGE AIRCRAFT.  DRIVE FROM GOVERNOR WAS BINDING INTERMITTENTLY. WHEN THE GOVERNOR WAS MOVED IT SOUNDED LIKE THERE WAS SOME PARTS LOOSE INTERNALLY. GOVERNOR REPLACED, PROBLEM RECTIFIED. (TC NR 20070511005)                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3U3  U  H2SW    E4CE                 
20070620000042007062000004SW  2007       6          20         CA070511006      120070430G6410406016100119    BLADE                                   BELL  407   407         1182206SW  ALLSN 250C  250C47B          GL                              TAIL ROTOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1596                                                           (CAN) TAIL ROTOR BLADE WAS FOUND CRACKED AT THE TIP BLOCK. (TC NR 20070511006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3U3  UO H2SW    E1GL                 
20070620000052007062000005SW  2007       6          20         CA070511007      120070430G6220407310104105    SPRING          BELL        407010150105BELL  407   407         1182206SW  ALLSN 250C  250C47B          GL                              FRAHM ASSY      BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) 2 SPRINGS WERE FOUND BROKEN. (TC NR 20070511007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3U3  UO H2SW    E1GL                 
20070620000062007062000006SO  2007       6          20         CA070511008      220070502G8520                CRANKCASE       CONT        TSIO520AE3B CESSNA303   T303        2073820CE  CONT  O520  TSIO520AE   17040SO  MCAULY3AF32C3AF32C506   GL  ENGINE          CRACKED         W      K   NONE                                                                                            J  WARNING INDICATION                                                            CRCRUISE         1                      CA            1941  246135                                              (CAN) SUDDEN DROP OF OIL PRESSURE DURING FLIGHT TO THE BOTTOM OF THE GREEN ON OIL PRESSURE GAUGE. CONTINUED FLIGHT WITH SAFE LANDING. CRACK NOT FOUND BY NDT.  BOTTOM END REBEARINGED, BUT ENGINE OIL PRESSURE WOULD DROP ONCE WARMED UP (POST REPAIR). FURTHER NDT BY RTD QUALITY SERVICES FOUND POSITIVE CRACK INDICATION AT ROOF OF OIL PICKUP PASSAGE WHERE THE OIL PICKUP TUBE CONNECTS TO THE SOCKET MACHINED INTO THE CRANKCASE.  NDT TECHNICIAN MENTIONED A CASTING FLAW SEEMED TO BE THE CAUSE.  RTD MDT REPORT SUBMITTED AS SUPPORTING DOCUMENTATION TO THIS SDR. (TC NR 20070511008)                                                                                                                                                 1L72 3O3  O  A34CE   E8CE    5  CP57GL    
20070620000072007062000007NM  2007       6          20         CA070511009      120070511G32462601483         TIE BOLT        MESSIER     C20509000   BOEING767   767328      1385290NM  GE    CF6   CF680C2B6F  30025NE                              MLG WHEEL       SHEARED         W      K   NONE                                                                                            O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                  04207                                               (CAN) DURING ROUTINE WALKAROUND CHECK AFTER LANDING, A TIE BOLT FOR NR 2 MLG WHEEL WAS FOUND BROKEN.  BROKEN PARTS FOUND JAMMED IN THE BRAKE ASSY CAUSING DAMAGES TO BOTH WHEEL ASSY AND BRAKE ASSY. FURTHER INVESTIGATION ON GOING AS TO THE CAUSE OF BOLT FAILURE. (TC NR 20070511009)                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA1NM    E13NE                
             20081104     NE  2008       11         4          CA070511010      220070510G7414SB9RU3          GEAR            BOSCH                   DHAV  DHC1  DHC1        2801702GL  PWA   R985  R985AN14B   52008NE  HARTZLHCB3R HCB3R304    GL  MAGNETO         STRIPPED        W      O   OTHER                                                                                           Y  ENGINE STOPPAGE                                                               NRNOT REPORTED   1                      CA                                                                      (CAN) ON RUNUP BEFORE FLIGHT MAG CHECK CARRIED OUT. ENGINE WOULD NOT RUN WHEN SELECTED TO RT MAG. REMOVED RT MAG, FOUND 50 PERCENT OF TEETH ON MAIN TIMING GEAR TO BE STRIPPED OFF. RT MAG REPLACED WITH SERVICEABLE MAG. (TC NR 20070511010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  R  EXPA1L715E1     5  CP28EA    
20070620000082007062000008EA  2007       6          20         CA070511011      120070502G5210601R317621      HANDLE                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              PAX DOOR        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5941 5941                                                      (CAN) DURING ROUTINE MAIN CABIN DOOR INSPECTION FOUND MAIN CABIN PHASE IV DOOR HANDLE WITH (2) CRACKS. DOOR HANDLE REPLACED.  AIRCRAFT RETURNED TO SERVICE (TC NR 20070511011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA21EA   E15NE                
20070620000092007062000009NM  2007       6          20         CA070512001      120070510G5610NP15790213      WINDOW                                  DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  COCKPIT         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) UPON ARRIVAL AT THE GATE THE PILOT SET THE PARK BRAKE AND AND THE PILOT`S SIDE WINDOW OUTER LAYER SHATTERED.  THE WINDOW WAS REPLACED BY MAINTENANCE AND FUNCTION CHECKED SERVICEABLE.  (TC NR 20070512001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070620000102007062000010SO  2007       6          20         CA070514001      120070511G2550                UNKNOWN                                 LKHEED382   382G        526414USO  ALLSN 501D  501D22A     03006GL  HAMSTD54H   54H60117    NE  CARGO BAY       CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA       38990                                                          (CAN) AT FL220 APPROXIMATELY 20 MINUTES FROM DESTINATION THE AIRCRAFT EXPERIENCED A LOSS OF PRESSURIZATION. THE CREW DESCENDED TO 10,000 AND THE AIRCRAFT CONTINUED AND LANDED WITHOUT FURTHER PROBLEM. INVESTIGATION DETERMINED THE SOURCE OF THE PRESSURIZATION TO BE A CRACK MIDWAY IN THE RT EDGE OF THE UPPER CARGO. (TC NR 20070514001)                                                                                                                                                                                                                                                                                                                                                                                                   2H74 4T4  T  A1SO    E282    6  CP906     
20070711002882007071100288CE  2007       7          11         CA070514002      120070509G6120A1464           LINK            HARTZL      C23035L     MTSBSIMU2   MU2B60      5780460CE  GARRTTTPE331TPE33110    01514WP  HARTZLHCB4T HCB4TN5     GL  PISTON UNIT     TIGHT           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       291  291   M7489                                               (CAN) AT THE AIRCRAFT 100 HOUR INSPECTION AND DURING THE REMOVAL OF THE PROP PITCH LINKS, IT WAS FOUND THAT THE PIVOT PIN WAS DIFFICULT TO REMOVE.   AFTER REMOVAL, THE PISTON UNIT (THAT WAS REPLACED RECENTLY) WAS FOUND TO HAVE PAINT INSIDE THE PIVOT PIN HOLE CAUSING THE TIGHT FIT.  PAINT WAS REMOVED PIVOT PIN REPLACED AND CHECKED SERVICEABLE. (TC NR 20070514002)                                                                                                                                                                                                                                                                                                                                                                    1H72 3T4  TRTA10SW   E4WE    6  CP40EA    
20070618001252007061800125NE  2007       6          18         CA070514003      220070301G7261                SEAL                                    CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              ENGINE OIL SYS  LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE IN CLIMB AND DURING CRUISE THE LOW OIL PRESSURE WARNING ACTIVATED. THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED A LEAKING ACCESSORY GEARBOX LIP SEAL. (TC NR 20070514003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA22CE   E00059EN             
20070620000112007062000011NE  2007       6          20         CA070514004      220070502G7210                COVER                                   FOKKERF27   F27MK50            EU  PWA   PWA120PW125B           NE                              RGB             LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) THE ENGINE LOW OIL PRESSURE WARNING ACTIVATED ON APPROACH AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED LEAKING AT THE REDUCTION GEARBOX ACCESSORY COVER RELATED TO COATING LOSS. (TC NR 20070514004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA817    E20NE                
20070618001262007061800126CE  2007       6          18         CA070514005      120070228G2120                UNKNOWN                                 CESSNA500   500CESSNA   2076602CE  PWA   JD15  JT15D1A          NE                              CABIN           SMOKE           W      GA  O2 MASK DEPLOYED        UNSCHED LANDING                                                         B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                          77216                       (CAN) SMOKE WAS OBSERVED IN THE CABIN AIR FOLLOWING TAKE-OFF.  OXYGEN MASKS WERE DEPLOYED AND AN EMERGENCY DECLARED.   THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 4F4  F  A22CE   E25EA                
20070622000042007062200004EA  2007       6          22         CA070514006      220070303G7320304867607       FMU                                     AGUSTAAB139 AB139       0260110SW  PWA   PT6   PT6*        52043EA                                              UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          CRCRUISE         1                      CA                                                                      (CAN) ENGINE POWER REDUCED UNCOMMANDED IN CRUISE AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  THE FUEL MANAGEMENT MODULE (FMM) WAS SUBSEQUENTLY REPLACED. (TC NR 20070514006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2G72 4U3  T  R00002RDE2NE                 
20070618001272007061800127NE  2007       6          18         CA070514007      220070306G7532                BLEED VALVE                             AEROSPATR72 ATR72212    8680945EU  PWA   PW120 PW127            NE                              ENGINE          MALFUNCTIONED   W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                                                      (CAN) TAKEOFF WAS ABORTED DUE TO HIGH TURBINE TEMPERATURE INDICATION.  THE INTERCOMPRESSOR BLEED VALVE WAS SUBSEQUENTLY REPLACED. (TC NR 20070514007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA53EU   E20NE                
20070618001282007061800128NE  2007       6          18         CA070514008      220070307G732232448716        FUEL CONTROL                            AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              ENGINE          MALFUNCTIONED   W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                                                      (CAN) TAKEOFF WAS ABORTED DUE TO HIGH TURBINE TEMPERATURE INDICATIONS.  THE FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED. (TC NR 20070514008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRT        E20NE                
20070620000122007062000012CE  2007       6          20         CA070514009      120070426G8011                GEAR                                    CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA                              STARTER         IMPROPER PART   W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA            400                           L601976                     (CAN) THE GEARS ON THE STARTER DID NOT MESH WITH THE RING GEAR FROM THE ENGINE CAUSING THE TEETH TO RIDE UP AND HIT THE TOP OF THE OPPOSITE GEAR. THIS CAUSED THE ENGINE AND STARTER TO LOCK UP. (TC NR 20070514009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A12    E274                 
20070618001292007061800129NE  2007       6          18         CA070514010      220070223G7200                ENGINE                                  RAYTHN36    G36         7150061CE  PWA   PT6   PT6A68           NE                                              MAKING METAL    W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                          RA0363                      (CAN) ON A TRAINING MISSION, THE ENGINE EXPERIENCED A LOSS OF THRUST (DURING TRAFFIC PATTERN STALLS) ACCOMPANIED BY A NOISE AND A CHIP DETECTOR INDICATION.  THE PILOT DECLARED AN EMERGENCY AND ABORTED THE MISSION.   SUBSEQUENT INSPECTION REVEALED METAL PARTICLES IN THE ENGINE OIL. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514010)                                                                                                                                                                                                                                                                                                                                                         1L71 3O4  TRT3A15    E26NE                
20070618001302007061800130NE  2007       6          18         CA070514011      220070308G7313ST3367009       PACKING                                 AEROSPATR72 ATR72202    8680940EU  PWA   PW120 PW124B           NE                              FUEL NOZZLES    LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KRJFLUID LOSS                PARTIAL RPM/PWR LOSS      WARNING INDICATION        CLCLIMB          1                      CA                                                                      (CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION IN CLIMB AND WAS SHUTDOWN IN  FLIGHT.  SUBSEQUENT INSPECTION REVEALED A FUEL LEAK RESULTING FROM DAMAGED FUEL NOZZLE PACKINGS. (TC NR 20070514011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRTA53EU   E2ONE                
20070618001312007061800131EA  2007       6          18         CA070514012      220070305G7532                DIAPHRAGM                               SZD   48    SZD48       8821648EU  PWA   PT6   PT6A65B     52043EA                              BLEED VALVE     PUNCTURED       W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          CLCLIMB          1                      CA                                                                      (CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION IN CLIMB.  SUBSEQUENT INSPECTION REVEALED PUNCTURED COMPRESSOR BLEED VALVE DIAPHRAGM. (TC NR 20070514012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1K00   4  T  EXP1K00 E4EA                 
20070618001322007061800132CE  2007       6          18         CA070514013      120070309G7931                ENGINE                                  CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                                              LOW PRESSURE    W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          DB0676                      (CAN) THE ENGINE EXPERIENCED AN LOSS OF OIL PRESSURE DURING CRUISE AND WAS REMOVED FROM SERVICE FOR FURTHER INVESTIGATION.  MFG WILL INVESTIGATE AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA22CE   E00059EN             
20070618001332007061800133EA  2007       6          18         CA070514014      220070312G7314                SPLINE                                  BELL  412   412EP       1182205SW  PWA   PT6T  PT6T3       52045EA                              FUEL PUMP       WORN            W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                                                      (CAN) THE ENGINE SUFFERED AN IN-FLIGHT SHUTDOWN DUE TO FUEL STARVATION AS A RESULT OF WORN FUEL PUMP DRIVE SHAFT SPLINES. (TC NR 20070514014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G72 4U4  U  H4SW    E22EA                
20070618001342007061800134EU  2007       6          18         CA070514015      120070303G6123                AUTOFEATHER SYS                         AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                                              UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          APAPPROACH       1                      CA                  MM1347                                              (CAN) ON APPROACH, THE ENGINE EXPERIENCED UNCOMMANDED TORQUE REDUCTIONS ACCOMPANIED BY FEATHERING OF THE PROPELLER.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  THE ENGINE AUTO-FEATHER UNIT WAS SUBSEQUENTLY REPLACED. (TC NR 20070514015)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRT        E20NE                
20070618001352007061800135NE  2007       6          18         CA070514016      220070314G73218197354         FUEL CONTROL                            CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              ENGINE          FAULTY          W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             DEDESCENT        1                      CA       2599                                                           (CAN) DURING DESCENT, THE ENGINE WAS FOUND NOT TO RESPOND TO THROTTLE INPUT, ACCOMPANIED BY A FUEL BOOST PRESSURE WARNING INDICTATION.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED A FAULTY MECHANICAL FUEL CONTROL UNIT. (TC NR 20070514016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA22CE   E00053EN             
20070618001362007061800136EA  2007       6          18         CA070514017      220070316G7230                STATOR                                  BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA                              COMPRESSOR      DAMAGED         W      C   ABORTED TAKEOFF                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  TOTAKEOFF        1                      CA                                                                      (CAN) THE ENGINE EXPERIENCED COMPRESSOR STALLS ON TAKEOFF ROLL AND THE TAKEOFF WAS ABORTED.  SUBSEQUENT INSPECTION REVEALED A DAMAGED SECOND STAGE COMPRESSOR STATOR.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514017)                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E00062EN             
20070618001372007061800137NE  2007       6          18         CA070514018      220070309G7210                GEARBOX                                 CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                              ENGINE          MAKING METAL    W      O   OTHER                                                                                           J RWARNING INDICATION                                  PARTIAL RPM/PWR LOSS      CRCRUISE         1                      CA                                          PC0634                      (CAN) DURING CRUISE THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION ACCOMPANIED BY A NOISE AND SMOKE IN THE CABIN AIR.   SUBSEQUENT INSPECTION REVEALED OIL AT THE ENGINE INLET AND METALLIC DEBRIS ON THE REDUCTION GEARBOX CHIP DETECTOR.  MFG WILL MONITOR INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070514018)                                                                                                                                                                                                                                                                                                                                                                               1H71 3T3  T  A37CE   E4EA                 
20070618001382007061800138EU  2007       6          18         CA070514019      120070319G7931                ENGINE                                  AGUSTAA109  A119        0261102EU  PWA   PT6   PT6*        52043EA                                              LOW PRESSURE    W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 NRNOT REPORTED   1                      CA                                          UC0035                      (CAN) ENGINE OIL PRESSURE WAS SEEN TO INCREASE AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUE ONCE ESTABLISHED. (TC NR 20070514019)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G72 3U3  T  H7EU    E2NE                 
20070618001392007061800139NE  2007       6          18         CA070514020      220070202G7200                BEARING                                 BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                              NR 2            DAMAGED         W      O   OTHER                                                                                           A  FLAME/FIRE                                                                    NRNOT REPORTED   1                      CA                                                                      (CAN) THE ENGINE EXHIBITED FLAMES FROM THE EXHAUST IN FLIGHT.   SUBSEQUENT INSPECTION REVEALED A DAMAGED (NR 2) BEARING.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514020)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4T4  TRTA24CE   E26NE                
20070618001402007061800140CE  2007       6          18         CA070514021      120070318G7931                ENGINE                                  CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                                              LOW PRESSURE    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA                                          DD0343                      (CAN) THE ENGINE EXPERIENCED AN INCREASE IN OIL PRESSURE AND TEMPERATURE AND WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METALLIC DEBRIS IN THE ENGINE OIL.  MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514021)                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA22CE   E00059EN             
20070618001412007061800141EA  2007       6          18         CA070514022      220070222G7310                TUBE                                    AYRES S2    S2RHGT65    0970110SO  PWA   PT6   PT6A41      52043EA                              ENGINE          FRACTURED       W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      CA                                                                      (CAN) DURING SPRAYING OPERATIONS, THE ENGINE LOST POWER RESULTING IN A FORCED LANDING. SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL CONTROL P3 DELIVERY LINE. (TC NR 20070514022)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3T4  TNC        E4EA                 
20070618001422007061800142NE  2007       6          18         CA070514023      220070320G7310ST3367009       PACKING                                 AEROSPATR72 ATR72212    8680945EU  PWA   PW120 PW127            NE                              FUEL MANIFOLD   LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KR FLUID LOSS                PARTIAL RPM/PWR LOSS                                CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE EXHIBITED AN UNCOMMANDED POWER REDUCTION IN CRUISE AND WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED LEAKING FUEL MANIFOLD PACKINGS. (TC NR 20070514023)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA53EU   E20NE                
20070622000052007062200005SO  2007       6          22         CA070514024      220070514G8530637781          EXHAUST VALVE   CONT        639056      CESSNA421   421B        2076014CE  CONT  O520  GTSIO520H   17032SO                              ENGINE          FAILED          W      A   UNSCHED LANDING                                                                                 RE PARTIAL RPM/PWR LOSS      VIBRATION/BUFFET                                    CRCRUISE         1                      CA            847                                                       (CAN) EXHAUST VALVE HEAD SEPARATED, STRIKING THE INTAKE VALVE AND CAUSING THE INTAKE VALVE TO FAIL. THE HEAD OF THE EXHAUST VALVE LODGED INTO THE EXHAUST PORT. THE INTAKE VALVE HAD (2) PIECES SEPARATE AND ONE LODGED ITSELF INTO THE TOP OF THE NR 1 CYLINDER HEAD, THE OTHER PORTION MIGRATED TO AN ADJACENT CYLINDER. ALL CYLINDERS WILL BE REMOVED AS COMPRESSION IS LOW ON ALL. (TC NR 20070514024)                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A7CE    E7CE                 
20070618001432007061800143NE  2007       6          18         CA070514026      220070227G7310ST3367009       PACKING                                 AEROSPATR72 ATR72              EU  PWA   PW120 PW124B           NE                              FUEL MANIFOLD   LEAKING         W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) THE ENGINE FLAMED OUT ON APPROACH.  SUBSEQUENT INSPECTION REVEALED LEAKING FUEL NOZZLE MANIFOLD PACKINGS. (TC NR 20070514026)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRT        E2ONE                
20070622000062007062200006NE  2007       6          22         CA070514027      220070416G75320301037140      BLEED VALVE     TMECA       ARRIEL1D1   SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              ENGINE          BROKEN          W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                  9219                                                (CAN) PIPE FAILED/BROKEN AROUND COMPLETE CIRCUMFERENCE OF FLARE.  FOUND WHEN BLEED VALVE WOULD NOT PASS TEST FOR CORRECT OPERATION. (TC NR 20070514027)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  U  H9EU    E19EU                
20070618001442007061800144NE  2007       6          18         CA070514028      220070322G7250                TURBINE BLADES                          CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                              ENGINE          DAMAGED         W      O   OTHER                                                                                           A  FLAME/FIRE                                                                    TXTAXI/GRND HDL  1                      CA                                          PC0463                      (CAN) ON ENGINE SHUTDOWN FLAMES WERE SEEN EXITING THE EXHAUST.  SUBSEQUENT INSPECTION REVEALED DAMAGED COMPRESSOR TURBINE BLADES.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514028)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3T3  T  A37CE   E4EA                 
20070622000072007062200007EU  2007       6          22         CA070514029      120070422G5330                SKIN                                    SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) FOUND CRACK IN SKIN OF MAIN TRANSMISSION DECK DURING SCHEDULED 500 HOUR INSPECTION. DECK REPAIRED IAW MFG REPAIR INSTRUCTIONS FOR CRACKS DISCOVERED IN THIS AREA. (TC NR 20070514029)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  H9EU    E19EU                
20070618001452007061800145NE  2007       6          18         CA070514030      220070322G731033026779        LINE                                    BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE                              FUEL CONTROL    FRACTURED       W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                                                                      (CAN) A FUEL LEAK WAS NOTED DURING GROUND OPERATIONS.  SUBSEQUENT INSPECTION REVEALED A FRACTURE FUEL LINE AT THE FUEL CONTROL. (TC NR 20070514030)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 4T4  T  A24CE   E4EA                 
20070619000892007061900089NM  2007       6          19         CA070514031      120070512G2420                TRANSFORMER                 736664A     BOEING767   767233      1385113NM  PWA   JT9   JT9D7R4D    52054NE                              IDG             OPEN            W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       42599      D0161                                               (CAN) DURING CRUISE, THE LT AC BUS FAILED WITH THE LOSS OF ASSOCIATED SYSTEMS.  THE CONCERN WAS BEING ABLE TO START THE APU.  FLIGHT DECLARED A PAN-PAN WITH ATC AND BEGAN DIVERSION.  AT FL 350, 2 APU START ATTEMPTS, BUT START WAS ACHIEVED ONLY AT FL150.  IAW CHECKLIST, LT BUS TIE SWITCH WAS RESET, AND LT BUS RESTORED.  HOWEVER, APU GEN AND GEN FAILED LIGHTS WERE ON.  ACFT LANDED APPROX 3 TONS OVERWEIGHT.  MTC CARRIED OUT WIRING CHECKS IAW FIM 24-20-00-101, AND FOUND THE LT IDG CURRENT TRANSFORMER OPEN.  THEY REPLACED THE LT IDG AND LT GCU IAW AMM 24-11-01-401 AND 24-22-02.  NOTE:  GCU WAS CHANGED ALONG WITH THE IDG.  THE REMOVED GCU INFO IS:  P/N 734284D, S/N 1696, 73326 HOURS TOTAL TIME (TC NR 20070514031)    2L72 4F4  FRTA1NM    E3NE                 
20070618001462007061800146NE  2007       6          18         CA070514032      220070323G7250                TURBINE BLADES                          AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              ENGINE          DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 RA PARTIAL RPM/PWR LOSS      FLAME/FIRE                                          CLCLIMB          1                      CA                                          127007                      (CAN) THE ENGINE EXPEREINCED AN UNCOMMANDED POWER REDUCTION IN CLIMB, ACCOMPANIED BY NOISE AND FLAMES EXITING THE EXHAUST.  THE ENGINE WAS SHUT DOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED FRACTURED HIGH POWER TURBINE BLADES.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514032)                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRT        E20NE                
20070619000902007061900090SO  2007       6          19         CA070514033      120070429G2410LW18129         BELT                                    PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ALTERNATOR      LOOSE           W      A   UNSCHED LANDING                                                                                 H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA       25                                                             (CAN) PILOT NOTICED ALTERNATOR INOPERATIVE LIGHTS ILLUMINATE A FEW TIMES THEN STAYED ON, SO HE ELECTED TO LAND AT NEAREST AIRPORT. MAINTENANCE FOUND BOTH ALTERNATOR BELTS LOOSE, CAUSE WAS DETERMINED TO BE BELT STRETCH AND WEAR-IN DUE TO BOTH BELTS BEING REPLACED 25 HOURS PREVIOUSLY. (TC NR 20070514033)                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070618001472007061800147NE  2007       6          18         CA070514034      220070326G732132448094        FCU                                     PIPER PA31T PA31T       7103124SO  PWA   PT6   PT6A135     52043NE                              ENGINE          FAULTY          W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB, ENGINE POWER INCREASED UNCOMMANDED, RESULTING IN A TORQUE EXCEEDANCE.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED A FAULTY FUEL CONTROL UNIT. (TC NR 20070514034)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3T4  T  A8EA    E4EA                 
20070618001482007061800148EA  2007       6          18         CA070514035      220070326G73103011849         LINE                                    EMB   110   EMB110*            SO  PWA   PT6   PT6A34      52043EA                              FCU             FRACTURED       W      O   OTHER                                                                                           K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA                                                                      (CAN) A FUEL LEAK WAS DISCOVERED DURING GROUND HANDLING OPERATIONS. SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL TUBE. (TC NR 20070514035)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  TRTA21SO   E4EA                 
20070618001492007061800149NE  2007       6          18         CA070514036      220070328G7200                ENGINE                                  GULSTM200   200         4500308NM  PWC   PW306 PW306A      52165NE                                              NOISY           W      E   ENGINE SHUTDOWN                                                                                 EJ VIBRATION/BUFFET          WARNING INDICATION                                  CRCRUISE         1                      CA                                          CC0071                      (CAN) IN CRUISE THE ENGINE EMITTED A NOISE ACCOMPANIED BY VIBRATION, A FADEC FAULT INDICATION AND FIRE WARNING INDICATION.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514036)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA53NM   E35NE                
20070619000912007061900091NE  2007       6          19         CA070514037      220070321G7200                ENGINE                                                                     PWA   PT6   PT6A65AR    52043NE  HARTZLHCB5M HCB5MP3     GL                  NOISY           W      C   ABORTED TAKEOFF                                                                                 EJ VIBRATION/BUFFET          WARNING INDICATION                                  TOTAKEOFF        1                      CA                                          97047                       (CAN) THE ENGINE EMITTED A NOISE ON TAKEOFF ROLL ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN POWER.  TAKEOFF WAS ABORTED.  MFG WILL MONITOR INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514037)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              4  T          E4EA    6  CP44GL    
20070618001502007061800150EA  2007       6          18         CA070514038      220070328G7261                PACKING                                 BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA                              OIL PUMP        LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) ENGINE OIL PRESSURE FLUCTURATED DURING FLIGHT AND OIL WAS SEEN EXITING THE ENGINE COWLINGS.  SUBSEQUENT INSPECTION REVEALED A DAMAGED OIL PUMP O-RING PACKING. (TC NR 20070514038)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E00062EN             
20070618001512007061800151NE  2007       6          18         CA070514039      220070330G7313ST3367009       PACKING                                 AEROSPATR72 ATR72212    8680945EU  PWA   PW120 PW127            NE                              FUEL MANIFOLD   LEAKING         W      O   OTHER                                                                                           KXJFLUID LOSS                ENGINE FLAMEOUT           WARNING INDICATION        APAPPROACH       1                      CA                                                                      (CAN) THE ENGINE FLAMED OUT ON APPROACH.  SUBSEQUENT INSPECTION REVEALED DAMAGED FUEL NOZZLE MANIFOLD O-RING PACKINGS. (TC NR 20070514039)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA53EU   E20NE                
20070618001522007061800152NE  2007       6          18         CA070514040      220070331G7230                FAN BLADE                               LEAR  60    60LEAR      5170707CE  PWA   305   PW305A      52128NE                              ENGINE          FRACTURED       W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE, THE ENGINE EMITTED A LOUD NOISE AND HIGH VIBRATIONS AND SHUTDOWN.  SUBSEQUENT INSPECTION REVEALED A FRACTURED LOW PRESSURE COMPRESSOR FAN BLADE, DAMAGE TO THE ENGINE NACELLE INLET, MISSING ENGINES COWLS AND ASSOCIATED AIRFRAME IMPACT DAMAGE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514040)                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA10CE   E35NE                
20070618001532007061800153NE  2007       6          18         CA070514041      220070327G7321                DRIVE SHAFT                 9682011739  PILATSPC7   PC7         7090401EU  PWA   PT6   PT6A25      52043NE                              FCU             SHEARED         W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       4352       98034                                               (CAN) THE ENGINE WAS FOUND NOT TO RESPOND TO THROTTLE INPUT AND SUBSEQUENTLY ACCELERATED UNCOMMANDED.  THE ENGINE WAS SHUTDOWN ON APPROACH.  SUBSEQUENT INSPECTION REVEALED A SHEARED FUEL CONTROL UNIT DRIVE SHAFT. (TC NR 20070514041)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L71 3T3  TRTA50EU   E4EA                 
20070618001542007061800154NE  2007       6          18         CA070514042      220070403G7200                ENGINE                                  BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                                              MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                          114033                      (CAN) ENGINE TORQUE FLUCTUATED IN FLIGHT ACCOMPANIED BY HIGH INTER-TURBINE TEMPERATURE AND LOW OIL PRESSURE.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION FOUND THE POWER SECTION SEIZED AND THE EXHAUST DUCTS DENTED.  MFG WILL MONITOR THE INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514042)                                                                                                                                                                                                                                                                                                                                                                                            2L72 4T4  TRTA24CE   E26NE                
20070618001552007061800155NE  2007       6          18         CA070514043      220070404G7313ST3367009       PACKING                                 AEROSPATR72 ATR72212    8680945EU  PWA   PW120 PW127            NE                              FUEL NOZZLE     LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                                                                      (CAN) DURING BOARDING, FUEL WAS DISCOVERED LEAKING FROM THE ENGINE.  SUBSEQUENT INSPECTION REVEALED DAMAGED FUEL NOZZLE TRANSFER TUBE PACKINGS. (TC NR 20070514043)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA53EU   E20NE                
20070618001562007061800156NE  2007       6          18         CA070514044      220070403G732031B474707       FADEC                                   LEAR  60    60LEAR      5170707CE  PWA   305   PW305A      52128NE                              ENGINE          FAULTY          W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  DEDESCENT        1                      CA                                                                      (CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION DURING DESCENT AND WOULD NOT RESPOND TO THROTTLE INPUT.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  THE ELECTRONIC ENGINE CONTROL (FADEC) WAS SUBSEQUENTLY REPLACED. (TC NR 20070514044)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA10CE   E35NE                
20070618001572007061800157NE  2007       6          18         CA070514045      220070409G7250                TURBINE BLADES                          AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              ENGINE          FRACTURED       W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) SHORTLY AFTER TAKEOFF THE ENGINE EXHIBITED TORQUE FLUCTUATIONS AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE.  SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. (TC NR 20070514045)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRT        E20NE                
20070619000932007061900093NE  2007       6          19         CA070514046      220070411G7230                ROTOR                                   DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE                              ENGINE          SEIZED          W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CLCLIMB          1                      CA                                          AW0015                      (CAN) DURING CLIMB THE ENGINE EXHIBITED VIBRATION AND SHUTDOWN, UNCOMMANDED.  SUBSEQUENT INSPECTION REVEALED HIGH PRESSURE ROTOR SEIZURE AND METAL CONTAMINATION IN THE TURBO MACHINE OIL SYSTEM.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514046)                                                                                                                                                                                                                                                                                                                                                                                                                                                2H72 4T4  TRTA13NM   E20NE                
20070619000942007061900094NE  2007       6          19         CA070514047      220070411G7250                TURBINE BLADES                          PIAGIOP180  P180        6960204EU  PWA   PT6   PT6A66      52043NE                              TURBINE SECTION FRACTURED       W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB, THE ENGINE EMITTED A NOISE AND ENGINE PARAMETERS WERE SEEN TO FLUCTUATE.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. (TC NR 20070514047)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H72 3O4  TRTA59EU   E26NE                
20070619000952007061900095NE  2007       6          19         CA070514048      220070413G7313ST3367009       PACKING                                 DHAV  DHC8  DHC8201     2809001NM  PWA   PW120 PW123            NE                              FUEL NOZZLE     LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA                                                                      (CAN) DURING STARTING, FUEL WAS FOUND LEAKING FROM THE ENGINE. SUBSEQUENT INSPECTION REVEALED DAMAGED FUEL NOZZLE TRANSFER TUBE O-RING PACKINGS. (TC NR 20070514048)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E20NE                
20070622000522007062200052    2007       6          22         CA070514049      420070507G61226506715         GOVERNOR                                                                   ALLSN 501D  501D13D     03004GL  ALLSN A6441 A6441FN606  GL  RT PROPELLER    MALFUNCTIONED   W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) WHILE ON CLIMB OUT, AFTER THE CREW MADE A ROUTINE SELECTION OF PROP SYNC, THE RT PROP/ ENGINE BEGAN TO CYCLE UNCONTROLLABLY. THE CREW SHUT IT DOWN AND RETURNED TO STATION. MAINTENANCE REPLACED THE RT PROP GOVERNOR AND THE A/C RETURNED TO SERVICE.  (TC NR 20070514049)                                                                                                                                                                                                                                                                                                                                                                                                                                                                      4  T          E282    6  CP898     
20070622000532007062200053NE  2007       6          22         CA070514050      220070418G7200PT6A11AG        ENGINE                                  FLTCHR24    FU24AIRPTS  3530202WP  PWA   PT6   PT6A11AG    52043NE                                              MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) ENGINE POWER INCREASED UNCOMMANDED AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070514050)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  T  4A12    E4EA                 
20070622000542007062200054NE  2007       6          22         CA070514051      220070418G7200PT6A67A         ENGINE                                  AIRTRCAT802 AT802       0390305SW  PWA   PT6   PT6A67A     52043NE                                              FLAMED OUT      W      O   OTHER                                                                                           X  ENGINE FLAMEOUT                                                               CRCRUISE         1                      CA                                          RD0014                      (CAN) THE ENGINE FLAMED OUT IN FLIGHT.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514051)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L71 3T4  TNCA19SW   E26NE                
20070622000552007062200055EA  2007       6          22         CA070514052      220070413G7200PT6A28          ENGINE                                  BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA                                              SURGES          W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                          51225                       (CAN) THE ENGINE SURGED DURING CLIMB ACCOMPANIED BY AN INCREASE IN INTERTURBINE TEMPERATURE.  MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514052)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L72 3T4  T  A14CE   E4EA                 
20070622000562007062200056NE  2007       6          22         CA070514053      220070418G7250                TURBINE BLADES                          BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                              ENGINE          FRACTURED       W      C   ABORTED TAKEOFF                                                                                 R  PARTIAL RPM/PWR LOSS                                                          TOTAKEOFF        1                      CA                                                                      (CAN) ON ADVANCING POWER FOR TAKEOFF, THE ENGINE EMITTED A NOISE AND LOST POWER.  SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070514053)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4T4  TRTA24CE   E26NE                
20070622000572007062200057    2007       6          22         CA070514054      120070420G6123                AUTOFEATHER SYS                                                            PWA   PW120 PW123            NE                              ENGINE          MALFUNCTIONED   W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             ININSP/MAINT     1                      CA                                                                      (CAN) DURING WATER SCOOPING, THE ENGINE PROPELLER AUTO-FEATHERED.  THE ENGINE TORQUE SENSOR AND ELECTRICAL HARNESS WERE SUBSEQUENTLY REMOVED FOR INVESTIGATION. MFG WILL ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070514054)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     4  T          E20NE                
20070622000582007062200058NE  2007       6          22         CA070514055      220070422G7200PW120           ENGINE                                  DHAV  DHC8  DHC8*              NM  PWA   120   PW120            NE                                              FLAMED OUT      W      O   OTHER                                                                                           X  ENGINE FLAMEOUT                                                               CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE FLAMED OUT IN CRUISE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514055)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E20NE                
20070619000972007061900097NE  2007       6          19         CA070514056      220070420G7200PW121           ENGINE                                  AEROSPATR42 ATR42300    8680920EU  PWA   PW121 PW121       52124NE                                              FLAMED OUT      W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                          121328                      (CAN) THE ENGINE FLAMED OUT IN CRUISE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514056)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA53EU   E20NE                
20070618001582007061800158NE  2007       6          18         CA070514057      220070113G7230                BLADE                                   CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                              COMPRESSOR      DAMAGED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            DEDESCENT        1                      CA                                                                      (CAN) DURING DESCENT ENGINE OIL PRESSURE REDUCED ACCOMPANIED BY AN INCREASE IN INTER-TURBINE TEMPERATURE.  ENGINE POWER WAS REDUCED AND A LANDING ACCOMPLISHED AT LOW POWER.  SUBSEQUENT INSPECTION REVEALED COMPRESSOR TURBINE BLADE DAMAGE.  MFG WILL MONITOR INVESTIGATION AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514057)                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3T3  T  A37CE   E4EA                 
20070618001592007061800159EA  2007       6          18         CA070514058      220070227G7230                COMPRESSOR                              EMB   110   EMB110*            SO  PWA   PT6   PT6A34      52043EA                              ENGINE          DAMAGED         W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                          56418                       (CAN) DURING CRUISE THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A REDUCTION IN ALL PARAMERTERS TO ZERO.  SUBSEQUENT INSPECTION REVEALED COMPRESSOR AND POWER TURBINE DAMAGE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514058)                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 4T4  TRTA21SO   E4EA                 
20070619000982007061900098NE  2007       6          19         CA070514059      220070423G7313                PACKING                                 FOKKERF27   F27MK50            EU  PWA   PWA120PW125B           NE                              FUEL NOZZLE     DAMAGED         W      O   OTHER                                                                                           RXJPARTIAL RPM/PWR LOSS      ENGINE FLAMEOUT           WARNING INDICATION        CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE ENGINE POWER REDUCED UNCOMMANDED AND THE ENGINE SUBSEQUENTLY FLAMED OUT.  INSPECTION REVEALED A DAMAGED FUEL NOZZLE TRANSFER TUBE O-RING PACKING. (TC NR 20070514059)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA817    E20NE                
20070619000992007061900099NE  2007       6          19         CA070514061      220070423G7250                ENGINE                                  AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                                              MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) AT TOP OF CLIMB, ENGINE TORQUE REDUCED UNCOMMANDED ACCOMPANIED BY A POWER TURBINE OVER-SPEED CONDITION.  THE ENGINE WAS SHUTDOWN IN FLIGHT. MFG WILL MONITOR INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514061)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRT        E20NE                
20070619001012007061900101NE  2007       6          19         CA070514062      220070426G7250                TURBINE BLADES                          BELL  212   212         1181420SW  PWA   PT6T  PT6T3B      52045NE                              ENGINE          FRACTURED       W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                          TB0071                      (CAN) THE ENGINE CHIP DETECTOR WARNING ACTIVATED IN FLIGHT AND THE ENGINE SHUTDOWN UNCOMMANDED.  SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES.  MFG WILL MONITOR INVESTIGATION AND ADVISE OF ROOT CAUSE ONCE DETERMINED (TC NR 20070514062)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 4U4  U  H4SW    E22EA                
20070809000352007080900035CE  2007       8          9          CA070515001      120070514G2822MS2774317       RELAY                       2C68        CESSNA208   208         2073702CE  PWA   PT6   PT6A114     52043NE  MCAULY3AF34C3GFR34C703  GL  FUEL PUMP       INOPERATIVE     W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                                                      (CAN) A/C ABORTED TAKEOFF AUX PUMP LIGHT ON AT HIGH POWER.  RELAY REPLACED, A/C GROUND RUN AT HIGH POWER NO FAULT FOUND (TC NR 20070515001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3T3  TNTA37CE   E4EA    5  CP60GL    
20070619001022007061900102EA  2007       6          19         CA070515002      120070514G3250711619          COLLAR          DHAV        7110029     DHAV  DHC6  DHC6200     2802620EA  PWA   PT6   PT6A20      52043EA  HARTZLHCB3T HCB3TN3     GL  STEERING        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  226                                                 (CAN) DURING MAINTENACE TO REPAIR THE NOSE GEAR ASSEMBLY IT WAS NOTED THAT THE STEERING COLLAR WAS CRACKED. THE NOSE GEAR WAS THEN FULLY DISASSEMBLED TO REMOVE THE CRACKED STEERING COLLAR. THE NLG WAS THEN VISUALLY INSPECTED AND SOME OF THE ITEMS SENT FOR NDT. STEERING COLLAR CRACK CONFIRMED BY NDT. STEERING LIMITS OF ACTUATOR CHECKED FOR CORRECT TRAVEL AND VERIFIED WITHIN LIMITS. THIS COLLAR HAS BEEN IN SERVICE FOR SOME TIME.   (TC NR 20070515002)                                                                                                                                                                                                                                                                            1H72 3T3  TRTA9EA    E4EA    6  CP15EA    
20070619001032007061900103NM  2007       6          19         CA070515003      120070507G291065178444441     TUBE                                    BOEING727   727225      1384077NM  PWA   JT8   JT8D15      52051NE                              HYD SYSTEM      CHAFED          W      L   ABORTED APPROACH                                                                                KJ FLUID LOSS                WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) IB, HYDRAULIC A SYS PRESSURE WAS NORMAL ON APPROACH AND QUANTITY REPORTED APPROXIMATELY ZERO. UPON SELECTION OF FLAPS, QUANTITY READ ZERO AND LOW PRESSURE LIGHTS ILLUMINATED. FLIGHT CREW DECLARED AN EMERGENCY AND THE HYDRAULIC FAILURE CHECKLIST WAS CARRIED OUT AFTER MISSED APPROACH PROCEDURE. THE AIRCRAFT LANDED NORMALLY WITH NO FURTHER INCIDENT.  A HYD LEAK WAS FOUND INSIDE THE AFT AIRSTAIR AREA ON THE LT SIDE. THE HYDRAULIC A SYSTEM PRESSURE LINE FROM THE NR 1 ENGINE TO THE HYDRAULIC A SYSTEM MODULE WAS FOUND CHAFED WHERE THE LINE COMES INTO THE AFT AIRSTAIR AREA FROM THE NR 1 ENGINE PYLON. THE CHAFED LINE WAS CAUSED BY EXCESSIVE PLAY OF THE HYDRAULIC TUBING FIRE SEAL BETWEEN THE PYLON AND THE AFT AIRST2L73 4F4  F  A3WE    E2EA                 
20070619001112007061900111EA  2007       6          19         CA070515004      220070502G8530A4871           RETAINER                                ROBSINR22   R22BETA     7640110NM  LYC   O320  O320B2C     41508EA                              CYLINDER        BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING 25 HOUR INSPECTION, FOUND (NR 2), (A) CYLINDERS IB LOWER BAFFLE RETAINER HEAD BROKEN AND ITS SPRING MISSING, THUS AFT BAFFLE IN CONTACT WITH NR 2 CYLINDER OIL RETURN LINE CAUSED DEEP WEAR ON OIL LINE. NO LEAK FOUND AT THAT TIME. RETAINER, SPRING AND OIL RETURN LINE REPLACED. (TC NR 20070515004)                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3O3  O  H10WE   E274                 
20070619001122007061900112GL  2007       6          19         CA070515005      320070503G6114D2A34C580       HUB                                     CESSNA185   A185F       2072821CE  CONT  O520  IO520*      17032SO  MCAULY2A34C D2A34C58    GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3545 1052                                                      (CAN) EDDY CURRENT DETECTED INDICATION BEYOND ALLOWABLE LIMITS ON HUB SOCKET NR 1, 2 TO 3 THREADS DOWN. (TC NR 20070515005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  3A24    E5CE    5  CP3EA     
20070619001132007061900113SW  2007       6          19         CA070515006      120070501G2434LW10382         BRACKET                                 HUGHES269   269C1       8059504SW  LYC   O360  HO360C1A    41514EA                              ALTERNATOR      BROKEN          W      O   OTHER                                                                                           W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                          L3515336A                   (CAN) ALTERNATOR BRACKET BROKEN.  REPLACED BRACKET WITH NEW PART PN LW10382. (TC NR 20070515006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3O3  OO 4H12    E286                 
20070619001142007061900114EA  2007       6          19         CA070515007      220070513G7261                OIL SYSTEM                              DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE          MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA       262054436                          PCE41553                    (CAN) DURING CRUISE FLIGHT, THE FLIGHT CREW NOTICED A MOMENTARY FLUCTUATION AND THEN DECREASING OIL PRESSURE, THEN EVERYTHING RETURNED TO NORMAL.   MOMENTS LATER, THE ENGINE FAILED AND THE CREW CARRIED OUT THE SHUTDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT, ONCE ON THE GROUND, THE FLIGHT CREW ATTEMPTED TO TURN THE PROPELLER AND FOUND IT WAS SEIZED. MAINTENANCE ARRIVED AND CONFIRMED A CATASTROPHIC FAILURE OF THE POWER SECTION GEAR BOX. (TC NR 20070515007)                                                                                                                                                                                                                                                                      1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
             20081104         2008       11         4          CA070515008      420070515G61228210410         GOVERNOR                                BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  PROPELLER       OUT OF RIG      W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             LDLANDING        1                      CA            6508                                                      (CAN) ON NUMEROUS LANDINGS THE AC YAWED HARD TO THE LT. AFTER RIGGING THE SNAG WOULD GO AWAY FOR NUMEROUS LANDINGS THEN YAW AGAIN TO THE LT. MAINT REPLACED THE LT PROP GOVERNOR AND RETURNED THE ACFT TO SERVICE. TO DATE THE SNAG HAS NOT RE-OCCURED. (TC NR 20070515008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20080220000492008022000049SW  2008       2          20         CA070516001      120070515G5310712551          TUBE                                    BBAVIA7     7ECA        21101NNSW  LYC   O235  O235K2C     41505EA  SNSNCH72C   72CK        EA  FUSELAGE        BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3787                                                           (CAN) WHILE PREFLIGHTING THE AC, THE PILOT NOTED WRINKLED FABRIC AT THE LOWER AFT END OF THE FUSELAGE. OPENING THE FABRIC REVEALED THAT THE VERTICAL TUBE THAT FORMS THE FIN SPAR AND IS THE ATTACH POINT FOR THE RUDDER HINGES AND TAILWHEEL SPRING AFT ATTACH WAS BROKEN THROUGH ABOUT AN INCH AND A HALF UP FROM ITS LOWER END, JUST ABOVE THE WELDED SKID ATTACHMENT.    THERE IS NO EVIDENCE THAT THIS WAS CAUSED BY ANY FLIGHT LOADS OR HARD LANDINGS.  SUSPECT THAT TAILWHEEL SHIMMY FLEXED THE SKID PLATE ATTACHMENT IN A TORSIONAL MANNER AND CAUSED A FATIGUING OF THE TUBE AT THIS POINT, EVENTUALLY RESULTING IN ITS FAILURE. (TC NR 20070516001)                                                                                   1H71 3O3  O  A759    E223    5  NP9045    
20070809000362007080900036CE  2007       8          9          CA070516002      120070507G78102654008205      EXHAUST DUCT                            CESSNA208   208         2073702CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       837                                                            (CAN) SECONDARY EXHAUST DUCT CRACKED ALONG THE SEAM ON THE OUTER SIDE FROM ABOUT .2500 THE LENGTH DOWN TO .7500 THE LENGTH, CAUSING SEVERAL SMALLER CRACKS TO FORM ALONG INITIAL CRACK 90 DEGREES FROM THE ORIGINAL BOTH ON THE UPPER AND LOWER SIDES.  OTHER OPERATORS REPORTED THAT IT IS NOT UNCOMMON TO HAVE SOME CRACKING.  (TC NR 20070516002)                                                                                                                                                                                                                                                                                                                                                                                            1H71 3T3  TNTA37CE   E4EA    5  CP60GL    
20070622000762007062200076EU  2007       6          22         CA070516003      120070514G6123                SOLENOID                                PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  FEATHERING SYS  STUCK           W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          TXTAXI/GRND HDL  1                      CA            570                                                       (CAN) PILOT INITIATED START FOLLOWING TURNAROUND AND NOTICED PROP RPM FOLLOWING START WAS ONLY AT 500 RPM AND NOT AT THE NORMAL, ABOVE 1000 RPM AT ENGINE IDLE. ALSO HAD EIS FLASHING AMBER AND RED ON EIS AS PROP WAS OPERATING BELOW 950 RPM. PROP WAS NOT COMING OUT OF FEATHER POSITION. PILOT SHUTDOWN ENGINE. INVESTIGATION REVEALED A STUCK OPEN PROP FEATHERING SOLENOID WHICH DID NOT ALLOW UNFEATHERING OF PROP. ONCE SOLENOID COOLED DOWN SOLENOID FUNCTIONED NORMALLY. REPLACED OVERSPEED GOVERNOR WITH REPAIRED AND TESTED UNIT. (TC# 20070516003)                                                                                                                                                                                 1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080220000502008022000050SO  2008       2          20         CA070516004      120070505G2810                BLADDER                                 PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  FUEL TANK       INCORRECT       W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       7400                                                           (CAN) AC IN FOR MAINTENANCE AND FUEL DRAINED FROM AC. DID NOT GET ANY FUEL FROM THIS QUICK DRAIN SO ADDED FUEL TO TANK AND OBSERVED A FUEL LEAK AROUND THE COVER PLATE IN BOTTOM OF WING UNDER THE TANK AND LOCATION OF QUICK-DRAIN. MAINT REMOVED COVER AND FOUND THE QUICK DRAIN NOT CONNECTED TO FUEL BLADDER. FOUND THAT SOMEONE HAD THREADED A BOLT INTO THE BLADDER AND HAD REDUCED THE LENGTH OF CONNECTOR TO THE QUICK DRAIN SO THE COVER PLATE WOULD FIT BACK IN PLACE. NO SNAG ON AIRCRAFT ADDRESSING THIS AND NO WAY FUEL COULD HAVE BEEN SUMPED FROM THIS TANK. FUEL BLADDER TANK WAS REMOVED AND SERVICEABLE BLADDER INSTALLED. (TC NR 20070516004)                                                                                1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070619001152007061900115CE  2007       6          19         CA070517001      120070515G792077853           ADAPTER                                 CESSNA172   172N        2072434CE  LYC   O360  O360A4A     41514EA  SNSNCH76E   76EM8       EA  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                          L1859236A                   (CAN) DURING GROUND RUN AFTER OVERHAUL, AN OIL LEAK WAS NOTICED ORIGINATING FROM THE LOWER RT ATTACH POINT OF THE OIL FILTER ADAPTER.  UPON CLOSE VISUAL INSPECTION A CRACK WAS FOUND IN THE RADIUS OF THE LOWER RT FLANGE.  UNIT WAS REPLACED AND LEAK CHECKED. (TC NR 20070517001)                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A12    E286    5  NP4EA     
20070622000772007062200077EA  2007       6          22         CA070517002      220070418G7200O320D2J         ENGINE                                  CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA  MCAULY1C160 1C160DTM    GL                  FAILED          W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA            2280                          L1088539A                   (CAN) INTERMITTENT VIBRATION AFTER UNUSUAL FLIGHT ATTITUDES DURING TRAINING. (TC NR 20070517002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A12    E274    5  NP910     
20070622000782007062200078SW  2007       6          22         CA070517007      120070508G57309000351         WINGLET                                 GULSTM500   500S        0141107SW  LYC   O540  IO540E1B5   41532EA  HARTZLHCC3Y HCC3YR2     NE  WING            SEPARATED       W      K   NONE                                                                                            D  INFLIGHT SEPARATION                                                           ININSP/MAINT     1                      CA                                                                      (CAN) IT WAS FOUND THAT THE SHEET METAL SCREWS HOLDING THE TIP ON THE WING HAD ALL COME LOOSE. THE WING TIP THEN VIBRATED FOR A PERIOD OF TIME ,ELONGATING THE SCREW HOLES IN THE WING UNTIL ALL OF THE SCREWS FELL OUT AND THE WING TIP DEPARTED THE WING IN FLIGHT. THE PILOT DID NOT NOTICE ANYTHING ABNORMAL AND ONLY NOTICED IT WAS MISSING ON WALK AROUND. (TC NR 20070517007)                                                                                                                                                                                                                                                                                                                                                            1H72 3O3  O  6A1     1E4     5  CP25EA    
20070619001162007061900116EU  2007       6          19         CA070518001      120070514G7603355A57217007    LEVER                                   AEROSPAS355 AS355F2     8680812EU  ALLSN 25OC  250C20R          GL                              RT THROTTLE     BROKEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA       4995                                                           (CAN) PART BROKE IN (2) PIECES JUST ABOVE ATTACHMENT POINT DURING ENGINE PRE-START CHECK PROCEDURES. (TC NR 20070518001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G72 3U3  U  H11EU   E4CE                 
20070619001172007061900117NE  2007       6          19         CA070518002      220070516G8530LW13622         INTAKE VALVE                            ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          FRACTURED       W      C   ABORTED TAKEOFF                                                                                 E  VIBRATION/BUFFET                                                              TXTAXI/GRND HDL  1                      CA       567                                                            (CAN) PILOT LANDED TO CONDUCT TASK AT WELL SITE.  DURING ATTEMPTED START UP, THE AIRCRAFT WOULD NOT START. AFTER A SHORT TIME, THE PILOT ATTEMPTED AGAIN AND THE AIRCRAFT STARTED.   IT RAN VERY ROUGH AND EXCESSIVE VIBRATIONS. PILOT TOOK THE ENGINE POWER UP TO CHECK IF THE ISSUE WAS MAGNETO`S. HE THEN SHUT IT DOWN.   MAINTENANCE CONDUCTED FURTHER INVESTIGATIONS AND FOUND CYLINDER NR 3 INTAKE VALVE HAD SNAPPED OR FRACTURED IN 3 PIECES. PORTION OF THE VALVE WAS FOUND IN THE INTAKE INDUCTION BOX.  WILL NOTIFY WHEN FURTHER DETAILS ARE AVAILABLE. (TC NR 20070518002)                                                                                                                                                           1G71 3O3  O  H11NM   1E4                  
             20081104         2008       11         4          CA070518003      220070515G7322206061716003    LEVER                                                                                                                                   FCU             MISMANUFACTURED W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSP, ENGINEER ATTEMPTED TO REPLACE FCU LEVER ON FCU NOT YET INSTALLED ON ACFT. INSTALLING BOLT P/N AN173-5 COULD NOT BE INSERTED THROUGH HOLE BORE OF LEVER. BORE FOUND UNDERSIZE AND REMOVED FROM SERVICE. (TC NR 20070518003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             
20070618001622007061800162NE  2007       6          18         CA070518004      220070325G852048564           CASE                                    DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD22D   22D30       NE  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                          JP207649                    (CAN) ENGINE WAS OVERHAULED OCT 02,2005, ENGINE WAS REMOVED FROM STEEL SHIPPING CONTAINER FOR INSTALLATION MARCH 25, 2007. CRACKS WERE FOUND ON THE REAR CASE AT THE IB HOLES FOR MAGNETO MOUNTING. THE ENGINE WAS SENT TO APPROVED AMO AND REPAIRED. FOLLOWING REPAIR ENGINE WAS INSTALLED IN AIRCRAFT . GROUND RUN FOR 30 SECONDS AND ENGINE SHUTDOWN DUE TO OIL LEAK FROM REAR CASE.  VISUAL INSPECTION DISCOVERED THAT THE REAR CASE HAD (3) DISTINCT PIN HOLES THROUGH THE CASE IN THE AREA OF THE OIL SCREEN HOUSING. THE HOLES LOOKED LIKE CAUSED BY CORROSION. THE ENGINE WAS REMOVED AND IS TO BE SENT TO APPROVED AMO FOR FURTHER REPAIR OR REPLACEMENT OF REAR CASE/BLOWER ASSY.  (TC NR 20070518004)                                1H71 3R3  RRCA806    5E1     5  CP736     
20070619001182007061900118NM  2007       6          19         CA070518005      120070516G750069474753        DUCT                                    BOEING727   727260      138408KNM  PWA   JT8   JT8D17      52049NE                              BLEED AIR       RUPTURED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE PERFORMING THE DAILY INSPECTION, MAINTENANCE PERSONNEL HEARD A LOUD BANG, WHICH WAS FOLLOWED BY A DROP IN APU DUCT PRESSURE TO 0 PSI. UPON INSPECTION, 2 BLEED AIR DUCTS WERE FOUND RUPTURED, FORWARD OF THE APU LOAD CONTROL VALVE THAT CONNECT TO THE BLEED AIR BY-PASS VALVE. NO ADDITIONAL DAMAGE PROBLEMS WERE NOTED.  NOTE: INFORMATION LISTED ABOVE IN AREA 9, BLOCK(B) PN.  THE PN LISTED ARE FOR THE TWO DUCT ASSEMBLIES THAT WERE FOUND DAMAGED.  DUCT P/N 69-47475-3 AND 69-47474-3  (TC NR 20070518005)                                                                                                                                                                                                                 2L73 4F4  FRTA3WE    E2EA                 
20070620000132007062000013EA  2007       6          20         CA070518006      120070516G3260864808          PSEU                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              LANDING GEAR    MALFUNCTIONED   W      O   OTHER                                                                                           N  FALSE WARNING                                                                 CRCRUISE         1                      CA       2864                                                           (CAN) IN CRUISE FLIGHT CREW RECEIVED PROX SYS CHAN FAULT CAUTION MESSAGE AS WELL AS (3) RED GEAR INDICATIONS, IAW AFM HAD TO PERFORM ALTERNATE EXTENSION, FLIGHT LANDED WITHOUT INCIDENT.  AFTER MAINTENANCE TROUBLESHOOTING THE MDC IS POINTED TOWARDS THE PSEU ITSELF.  THE PSEU WAS REPLACED AND FUNCTION TESTS WERE CARRIED OUT AND GEAR SWINGS AND THE AIRCRAFT WAS RETURNED TO SERVICE.  PRESENT AC HRS:24426:01 AND CYCLES: 20077 (TC NR 20070518006)                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20070620000142007062000014SW  2007       6          20         CA070518007      120070517G6510MS150011        GREASE FITTING              407040303135BELL  407   407         1182206SW                                                               HANGAR BRGS     LOOSE           W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       200                                                            (CAN) WHILE THE SHAFT WAS REMOVED THE MECHANIC WENT TO WIPE THE HANGER BEARING GREASE FITTING AND THE FITTING CAME OFF IN HIS HAND.  ALL OTHER HANGER BEARING GREASE FITTINGS WERE THEN CHECKED AND 4 OUT OF THE 6 WERE FOUND TO BE VERY LOOSE. THE ONES WE FOUND LOOSE WERE AS FOLLOWS: BOTH FWD AND AFT OIL COOLER BLOWER HANGER BEARINGS AND THE 4TH AND 6TH HANGER BEARINGS. (TC NR 20070518007)                                                                                                                                                                                                                                                                                                                                            1G71 3U    O H2SW                         
20070620000152007062000015SW  2007       6          20         CA070518008      120070517G2810457370          FUEL CAP                                FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  LT WING         LEAKING         W      A   UNSCHED LANDING                                                                                 K  FLUID LOSS                                                                    CLCLIMB          1                      CA                                                                      (CAN) SHORTLY AFTER TAKEOFF, THE CREW NOTICED THAT FUEL WAS LEAKING FROM THE LT WING FUEL CAP. THE CREW RETURNED TO BASE WITHOUT INCIDENT.  THE AIRCRAFT WAS INSPECTED AND IT WAS DISCOVERED THAT THE FUEL CAP WAS DEFECTIVE.  THE LARGE PLASTIC NUT AT THE BASE OF THE CAP ASSEMBLY IS HELD AT THE CORRECT TORQUE WITH THE USE OF A PIN THAT PASSES THROUGH THE NUT INTO THE BASES OF THE ASSEMBLY.  THIS PIN WAS MISSING, WHICH ALLOWED THE NUT TO TURN WHEN THE FUEL CAP WAS OPENED AND CLOSED.  THE TORQUE ON THIS NUT SETS THE PROPER SEATING OF THE FUEL CAP.  BECAUSE THE NUT BACKED OFF, THE FUEL CAP BECAME LOSE AND ALLOWED FUEL TO LEAK PAST THE FUEL CAP. THE FUEL CAP WAS REPLACED WITH AN IMPROVED CAP THAT IS DESIGNED TO PREVENT2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20070620000162007062000016NM  2007       6          20         CA070518009      120070516G29159752753         RELIEF VALVE                            BOMBDRCL600 CL6002D15          NM  GE    CF34  CF34*            NE                              HYDRAULIC SYS   MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       3105 1230                                                      (CAN) ON PUSHBACK FROM GATE CREW RECEIVED NOSE STEERING INOP MESSAGE. AIRCRAFT STEERING MEL`D. AFTER TAKEOFF GEAR FAILED TO RETRACT. AIRCRAFT RETURNED TO ORIGINATING AIRPORT FOR NORMAL LANDING. MAINTENANCE TROUBLESHOOTING REPLACED HYD BALANCE RELIEF VALVE, NR 3 HYD SYSTEM BLED, GEAR SWINGS COMPLETED, AIRCRAFT RETURNED TO SERVICE. (NOTE: PART AT LAST REPAIR HAD BEEN RETURNED TO VENDOR AS CAUSING NOSE STEERING INOP (1875HR/853CY TSN)  (TC NR 20070518009)                                                                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20070620000172007062000017EA  2007       6          20         CA070520001      120070520G3230                LANDING GEAR                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                                              COLLAPSED       W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) UPON ARRIVAL CREW HAD A SUSPECTED HARD LANDING, STAB TRIM AURAL WARNING CLACKER SOUNDED AND BOTH MAIN GEAR COLLAPSED. THERE WAS MAJOR STRUCTURAL DAMAGE AND PRELIMINARY REVIEW OF PICTURES SHOWS EXCESSIVE ENGINE BLADE DAMAGE DUE TO DEBIS INGESTION, FURTHER UPDATE TO FOLLOW.  TSB HAS PULLED THE FDR AND CVR.  PRESENTLY INVESTIGATION IS UNDERWAY AND WILL UPDATE FURTHER WHEN COMPLETE.  (TC NR 20070520001)                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20070620000182007062000018EA  2007       6          20         CA070521001      120070520G3230                LANDING GEAR                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                                              COLLAPSED       W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) UPON ARRIVAL, CREW HAD A SUSPECTED HARD LANDING. STAB TRIM AURAL WARNING CLACKER SOUNDED AND BOTH MAIN GEAR COLLAPSED. THERE WAS MAJOR STRUCTURAL DAMAGE AND A PRELIMINARY REVIEW OF THE PICTURES SHOWS EXCESSIVE ENGINE BLADE DAMAGE DUE TO DEBRIS INGESTION. THE FDR AND CVR HAVE BEEN PULLED BY TSB AND AN INVESTIGATION IS UNDERWAY. NO PICTURES AVAILABLE TO THE FSR AS OF YET. (TC NR 20070521001)                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA21EA   E15NE                
20070620000192007062000019EA  2007       6          20         CA070521002      120070514G274070609           CONTROL UNIT                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              HORIZ STAB      MALFUNCTIONED   W      BHA EMER. DESCENT           DEACTIVATE SYST/CIRCUITSUNSCHED LANDING                                 FJ FLT CONT AFFECTED         WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) THERE WAS A STAB TRIM RUNAWAY EVENT THAT OCCURRED. AN EMERGENCY WAS DECLARED AND A RETURN TO BASE. FURTHER AC DAMAGE AFTER SUCCESSFUL LANDING. BASED ON THE ATTACHED CREW REPORT, IT WAS A STAB TRIM RUNAWAY NOSE DOWN EVENT.  PLEASE NOTE THAT A DFDR DOWNLOAD WAS CARRIED OUT ON THIS AC AND A COPY OF THIS DOWNLOAD WILL BE SENT TO THE APPROPRIATE PEOPLE WITHIN MFG AS SOON AS IT BECOMES AVAILABLE TO ME.  THE NTSB ADVISED THAT THE FAA HAS REPORTED THIS AIRCRAFT DECLARED AN EMERGENCY DUE TO A STABILIZER TRIM PROBLEM.  THE AIRCRAFT WAS ON A SCHEDULED FLIGHT WHEN THE STAB TRIM RUNAWAY FAULT OCCURRED.  THE NTSB ALSO REPORTED THAT THE CREW FOLLOWED THE QRH PROCEDURES AND AIRCRAFT REACHED A NOSE-DOWN ATTITUDE BY THE TI2L72 4F4  FRTA21EA   E15NE                
20070620000202007062000020EU  2007       6          20         CA070522001      120070518G7110V40GT3911AA     SPRING                      10562648    BOLKMS105   BO105S      5626006EU  ALLSN 250C  250C20B     03013GL                              ENGINE COWLING  BROKEN          W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) COMING OUT OF A MAJOR INSPECTION WHERE THE EJECTION SPRING ON ALL THE COWLS (P/N 105-62648, 105-62664, 105-62643 AND 105-62663) WERE REPLACED, SEVERAL EJECTION SPRING P/N V40GT39-1-1AA WERE BREAKING IN TWO PIECES.  THIS PROBLEM HAPPENED STATICALLY AND IN FLIGHT.  THESE EJECTION SPRINGS WERE ORDERED NEW FROM MFG AND RECEIVED ON DEC 22/06. BATCH NR S200602192. (TC NR 20070522001)                                                                                                                                                                                                                                                                                                                                              1G72 3U3  U  H3EU    E4CE                 
20070620000212007062000021WP  2007       6          20         CA070522002      120070519G3213369H60022       STRUT           HUGHES      369H600132  HUGHES369   369E        4470707WP  ALLSN 250C  250C20B     03013GL                              MLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING AN ANNUAL INSPECTION OF THE AIRCRAFT IT WAS NOTICED THAT THE LANDING GEAR HAD SOME PLAY IN IT.  UPON FURTHER INSPECTION THE ENGINEER FOUND THAT THE BRACE TO STRUT BOLT HAD SOME SLOP IN IT.  THE ENGINEER REMOVED THE BRACE BOLT AND FOUND 3 CRACKS EMMITTING FROM THE BLACE BOLT HOLE ON THE AFT RT LANDING GEAR STRUT.  ONE CRACK ON THE TOP OF THE STRUT AND 2 CRACKS ON THE BOTTOM OF THE STRUT. (TC NR 20070522002)                                                                                                                                                                                                                                                                                                          1G71 3U3  U  H3WE    E4CE                 
20070620000222007062000022SO  2007       6          20         CA070522003      220070507G8520653058          CAMSHAFT        CONT        IO520       CESSNA180   180K        2072624CE  CONT  O520  O520*            SO  MCAULYD3A34 D3A34C403   GL  ENGINE          SPALLED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1087       821995R                                             (CAN) IN REMOVING NR 1 CYLINDER TO BE CHANGED OUT THE LIFTERS WERE REMOVED TO BE BLEED DOWN, LIFTERS WERE SPAWLED. THE AME INSPECTED THE CAM AND THE EXHAUST LOBE WAS ALSO SPALLED. THE ENGINE WAS REMOVED AND PREPARED FOR SHIPMENT TO A REPAIR SHOP. UNDER FURTHER INVESTIGATION WE FOUND OTHER LOBES AND LIFTERS WITH SPALLING.  OUR HYPOTHESIS IS LACK OF ENGINE USE CAUSING INTERNAL CORROSION/RUST WICH LEAD TO FAILURE   (TC NRIN 20070522003)                                                                                                                                                                                                                                                                                           1H71 3O3  O  5A6     E5CE    5  CP47GL    
20080220000512008022000051SW  2008       2          20         CA070522004      120070522G6220407310101101    BEARING         BELL        407010100   BELL  407   407         1182206SW  ALLSN 250C  250C47B          GL                              MAIN ROTOR      SEPARATED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1493       LK37                                                (CAN) COMPLETE FAILURE/SEPARATION OF SHEAR BEARING ELASTOMERIC LAMINATIONS (4 OF 4). FOUND AT INSPECTION. SHEAR BEARING P/N 407-310-100-115. S/N 8345, 8325, 8109, 8113. (TC NR 20070522004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3U3  UO H2SW    E1GL                 
20070620000232007062000023EA  2007       6          20         CA070522005      220070521G7250                TURBINE WHEEL   PWC         PT6A65B     BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  ENGINE          UNKNOWN         W      D   RETURN TO BLOCK                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA            4137                                                      (CAN) ECTM TREND INDICATED ENGINE ITT WAS INCREASING WITH TIME. ENGINE SPLIT. CT WHEEL NOTED AS CONTACTING THE GUIDE VANE ASSY. ENGINE TO BE SENT TO MFG TO INVESTIGATE. (TC NR 20070522005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20080220000522008022000052CE  2008       2          20         CA070522006      120070520G273110552002221     CONTROL CABLE                           BEECH 76    76          1153005CE  LYC   O360  O360A1G6D        EA  HARTZLHCM2Y HCM2YR      GL  ELEVATOR TRIM   FRAYED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AIRCRAFT WAS IN THE HANGER FOR INSPECTION. AN INSPECTION WAS BEING STARTED IN THE AFT TAIL AREA. THE AME APPRENTICE NOTICED THE ELEVATOR TRIM CABLE SEVERELY FRAYED WHERE IT WRAPPED AROUND THE TRIM SERVO. THE CABLE WAS REMOVED AND REPLACED WITH A NEW PART (TC NR 20070522006)                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3O3  O  A29CE   E286    5  CP43GL    
20080220000532008022000053CE  2008       2          20         CA070523001      120070522G79203391000015      LINE                                    BEECH 33    F33A        1151425CE  CONT  O520  IO520BB     17032SO  MCAULY3A32C 3A32C406    GL  OIL SYSTEM      FRACTURED       W      A   UNSCHED LANDING                                                                                 KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            CRCRUISE         1                      CA       8334                                                           (CAN) OIL PRESSURE LINE FRACTURED AT FIREWALL CAUSING AN OIL LEAK ON THE INSIDE OF THE FIREWALL.   LINE APPEARS TO BE HARD FROM AGE.  AIRCRAFT LANDED WITHOUT ANY FURTHER PROBLEMS. (TC NR 20070523001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3O3  O  3A15    E5CE    5  CP21EA    
20080220000542008022000054CE  2008       2          20         CA070523002      120070518G2120EM6303          BLOWER                                  BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  CABIN           SEIZED          W      G   O2 MASK DEPLOYED                                                                                B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) WHILE ENROUTE, THE AC CABIN AND COCKPIT FILLED UP WITH SMOKE FROM WHAT SMELLED ELECTRICAL IN NATURE. OXYGEN WAS USED AND THE AC FINISHED ITS TRIP AND LANDED (DESTINATION WAS CLOSER THAN TO TURN AROUND). MAINT WAS CALLED AND AN AC WAS DISPATCHED TO CONTINUE THE DAY. SYSTEMS WERE CHECKED, NO FAULTS WERE FOUND. THE AC WAS RETURNED TO BASE WITH NO PASSENGERS ON BOARD. UPON FURTHER INSP AT THE BASE, IT WAS FOUND THAT ONE OF THE CABIN VENT BLOWERS WAS SEIZED AND THE (2) SPEED ADJUSTING RESISTORS INSTALLED ON THE BLOWER WERE WARPED AND MELTED FROM HEAT. THE VENT BLOWER WAS REPLACED AND THE AC WAS RETURNED TO SERVICE. (TC NR 20070523002)                                                                             2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070620000242007062000024EA  2007       6          20         CA070523003      120070523G2810                UNKNOWN                     21564075    CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  FUEL SYSTEM     CRACKED         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1850       546                                                 (CAN) LEAK AT (3) LOWER CORNERS NEAR INTERCONNECTS.  DROPS 9180 (TC NR 20070523003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20080319001392008031900139NM  2008       3          19         CA070523004      120070410G493069254518        SHUTOFF VALVE                           AMD   FALC50FALCON2000  2730170NM  PWC   PW308 PW308C      52182NE                              APU             OPEN            W      O   OTHER                                                                                           AB FLAME/FIRE                SMOKE/FUMES/ODORS/SPARKS                            TXTAXI/GRND HDL  1                      CA       118  118   P439                                                (CAN) WHILE PREPARING FOR A DEPARTURE. APU FAILED TO START. APU NEVER ACCEL`D PAST 13 PERCENT ON FIRST ATTEMPT AND LARGE AMOUNT OF FUEL VAPOR EMITTED FROM EXHAUST. NEAR THE END OF START ATTEMPT, BRIEF FLAME AND SMOKE EVIDENT AT EXHAUST PIPE EXIT. AFTER ALLOWING TIME FOR TRAPPED FUEL TO DRAIN, 2ND START ATTEMPTED. THIS TIME NO ACCEL PAST APPROX 10 PERCENT AND FIRE AND SMOKE EMITTING FROM TAILPIPE AND TAILCONE UPPER AIRSCOOPS. FIRE SELF EXTINGUISHED PRIOR TO DISCHARGE OF FIRE BOTTLES.  INITIAL INDICATIONS FALSELY LED US TO TROUBLESHOOT POSSIBLE A/C ELECTRICAL PROBLEM DUE TO ABNORMALLY HIGH START AMPERAGES AND VOLTAGE INDICATIONS. BOTH AIRFRAME AND APU MFG TECH REPS INVOLVED IN THE (4) DAY TROUBLESHOOTING PROCESS.2L72 4F4  FRTA50NM   E00065EN             
20070620000252007062000025EA  2007       6          20         CA070523005      120070523G2810215640022       FLUID                       215640022   CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  FULE SYSTEM     LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1849       540                                                 (CAN) LEAK AT LOWER CORNERS NEAR INTERCONNECTS.    (TC NR 20070523005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
             20081104     CE  2008       11         4          CA070523006      120070430G324608A01156027     GUSSET                                  CESSNA208   208         2073702CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  FLOAT ASSY      MISMANUFACTURED W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       15                                                             (CAN) AS THE RESULT OF BUMPING A DOCK, THE FWD BULKHEAD HAD TO BE REPLACED ON THE LT FLOAT ASSY ON THE ACFT.  AFTER GAINING ACCESS, IT WAS FOUND THAT THE AREA WHICH IS NOT NORMALLY ACCESSED HAD SEVERAL PARTS RIVETED AS PART OF THE STRUCTURE HAD NO PROPER EDGE DISTANCE ON THE RIVETS. FURTHER INVESTIGATION FOUND THE OTBD GUSSET WAS PAINTED OVER WITH PRC HIDING THE FACT THAT THE HOLES WERE DRILLED ONLY HALF ON THE GUSSET.  QC HAS BEEN ADVISED OF THE PROBLEM AND SUPPLIED REPLACEMENT PARTS, AND IS IN REVIEW OF QUALITY INSP PROCEDURES TO VERIFY WHY THIS HAPPEND SO IT WILL NOT HAPPEN AGAIN.  ADVISED OF A POSSIBLE ENGINEERING CHANGE ON THE PART TO INCREASE IT`S SIZE SLIGHTLY TO GET THE REQUIRED EDGE DISTANCE. THERE WER1H71 3T3  TNTA37CE   E4EA    5  CP60GL    
20080129000172008012900017WP  2008       1          29         CA070523007      120070521G6210                PIN             HUGHES                  HUGHES369   369A        4470503WP  ALLSN 250C  250C20B     03013GL                              M/R BLADE       BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3885       0098848293                                          (CAN) PIN FOUND BROKEN AT FIRST THREAD / SHANK. NUT WAS CAPTURED IN THE HANDLE CLIP.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3U3  U  H3WE    E4CE                 
20070622000792007062200079GL  2007       6          22         CA070523008      120070504G2720C2CF1777A       ARM                                     DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  RUDDER          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CRACK FOUND IN WELD RADIUS ON OB SIDE OF CABLE ATTACH ARM. (TC NR 20070523008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3R3  RRCA806    5E1     5  CP206     
20070620000262007062000026NE  2007       6          20         CA070524001      220070517G7314                PUMP                        TA7         BELL  205   205A1       1181414SW  LYC   T53   T5317A      41549NE                              FUEL SYSTEM     FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            DEDESCENT        1                      CA            1743  662AL3381                                           (CAN) DURING HELI-PORTABLE SEISMIC DRILLING OPERATIONS, UPON DESCENT WITH AN EXTERNAL LOAD: THE MASTER CAUTION WARNING INDICATION WAS ILLUMINATED. THE LOAD WAS SET AND RELEASED.  THE CAUTION PANEL OBSERVED TO REVEAL THAT THE ENGINE DRIVEN FUEL PUMP WARNING LIGHT WAS ON. THE P/C IMMEDIATELY ABORTED ANY FURTHER OPERATIONS AND RETURNED TO THE SERVICE LANDING WHICH WAS APPROXIMATELY ONE KILOMETER AWAY AND THE NEAREST SUITABLE LANDING SIGHT. A NORMAL LANDING AND ENGINE SHUTDOWN WAS CARRIED OUT. TROUBLESHOOTING BY THE AME AT SERVICE FOUND THAT IT WAS A POSITIVE INDICATION THAT ONE OF THE TWO PUMP ELEMENTS HAD FAILED TO DELIVER FUEL PRESSURE.  AD 2006-11-16, 1250 HOUR MAIN AND SECONDARY DRIVE SHAFT AND PUMP GEAR SPLIN1G71 4U4  U  H1SW    E17EA                
20070620000272007062000027EU  2007       6          20         CA070524002      120070522G2424243211          GCU                                     AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  NR 1            FAILED          W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA            157                                                       (CAN) DURING DEPARTURE THE NR 1 AC WILD SYSTEM WENT OFF LINE. WHEN THE CREW ATTEMPTED A RESET THE (BLUE) HYDRAULIC SYSTEM WENT OFF LINE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND CARRIED OUT A NORMAL LANDING. MAINTENANCE REPLACED THE NR 1 AC WILD GCU. AFTER WHICH THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070524002)                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20070620000282007062000028EA  2007       6          20         CA070524003      120070524G3246C3UF1085        STRUT           DHAV        557170      DHAV  DHC3  DHC3        2800202EA  PWA   PT6   PT6A34      52043EA  HARTZLHCB3T HCB3TN3     GL  FLOAT           CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING ANNUAL INSPECTION A (4 TO 5) CRACK WAS FOUND. THE CRACK PROPAGATED COMPLETELY THROUGH THE BOTTOM CENTER OF THE STRUT LEG BETWEEN THE LOWER ATTACH POINTS. THE STRUT LEG WAS REMOVED AND REPLACED. PICTURES ON FILE AT REPAIR STATION. (TC NR 20070524003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3R4  T  A815    E4EA    6  CP15EA    
20070620000292007062000029EA  2007       6          20         CA070524004      120070523G324010100199        SENSOR                                  CNDAIRCL600 CL600*      1900302EA  GE    CF34  CF34*            NE                              NR 1 BRAKE      CORRODED        W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CRCRUISE         1                      CA       5781 5781                                                      (CAN) DURING CRUISE CREW RECEIVED BRAKE OVERHEAT WARNING , LT OUTER BTMS SHOWING INCREASING BRAKE TEMP UP TO 20 UNITS, THEN STARTED TO DECREASE. AIRCRAFT DESCENDED TO LOWER ALTITUDE AND SPEED SLOWED. BRAKE TEMP STARTED TO RISE TO 18 UNITS. GEAR EXTENDED, BRAKE TEMPS RETURNED TO NORMAL GREEN INDICATION. RETURNED TO ORIGINATING AIRPORT, NORMAL LANDING. MAINTENANCE FOUND NR 1 BRAKE TEMP SENSOR HAD CORRODED PINS. BRAKE TEMP SENSOR REPLACED. AIRCRAFT RETURNED TO SERVICE. (NOTE: PART IS AN EXPENDABLE AND SYSTEM DOES NOT TRACK COMPONENT TIME. TIMES PROVIDED ARE AIRCRAFT TOTAL TIME.) (TC NR 20070524004)                                                                                                                      2L72 4F4  FRTA21EA   E15NE                
20070620000302007062000030    2007       6          20         CA070524005      120070519G271082740162001     LINK ASSY                                                                  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  RT AILERON      BROKEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             ININSP/MAINT     1                      CA       795                                                            (CAN) WHEN DOING WP8 INSPECTION TASK 000-057-640-500 GVI OF THE (RT) AILERON ASSY. MAINTENANCE FOUND LINK ASSY P/N 82740162-001 FROM THE RT AILERON LVDT BROKEN. (TC NR 20070524005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   4  T          E00062EN6  CP17BO    
20070622000802007062200080NE  2007       6          22         CA070524006      220070517G7200CT581402        ENGINE                                  SKRSKYS61   S61N        8142104NE  GE    CT58  CT581401    30011NE                              NR 1            FAILED          W      B   EMER. DESCENT                                                                                   X  ENGINE FLAMEOUT                                                               CRCRUISE         1                      CA       22313102                           295130C                     (CAN) REPORT NR 07-02204 (ON MAY 11, 2007) THE AC UNDERWENT AN ENGINE CHANGE ON NR 1 ENGINE AND REQUIRED A MAINTENANCE TEST FLIGHT. AFTER (2) GROUND RUNS INCLUDING LEAK CHECKS, DEPARTED TO THE TRAINING AREA TO PERFORM REQUIRED ENGINE TOPPING CHECK.  VERIFIED WEATHER CONDITIONS AT 2000 FT, PA AND DESCENDED TO 1000 FT PA TO BEGIN CHECK. WITH NR 2 ENGINE SSL PULLED BACK TO 94 PERCENT NF AND NR 1 ENGINE AT FULL THROTTLE WE NOTED ENGINE VALUES CLIMBING THROUGH 2000 PA. LEVELED AIRCRAFT OFF TO CHECK EMERGENCY FUEL LEVER RIGGING AND THE CO-PILOT INCREASED EMERGENCY FUEL LEVER TO MAXIMUM AFTER DECREASING  NR1 ENGINE SSL TO ABOVE GOVERNING RANGE. TOPPING VALUES WERE ON TARGET FOR NR 1 ENGINE AND THE CO-PILOT SLIGHTLY RE2G72 4U4  U  1H15    1E3                  
20070620000312007062000031EA  2007       6          20         CA070524007      120070520G2752735619C         COUPLING                                DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  T/E FLAP        TORN            W      K   NONE                                                                                            J  WARNING INDICATION                                                            LDLANDING        1                      CA                                                                      (CAN) CREW REPORTED (FLAP DRIVE) CAUTION LIGHT ILLUMINATED DURING FLAP EXTENSION , FLAPS CONTINUED TO MOVE. NORMAL LANDING. MAINTENANCE INSPECTION FOUND FLAP SECONDARY CENTER DRIVE COUPLING TORN FROM MOUNTING BRACKET AND LYING IN RT ARMPIT. FLAP SECONDARY CENTER DRIVE SECTION (CORE AND HOUSING) REPLACED, FLAP SECONDARY DRIVE CENTER COUPLING REPLACED. MOUNTING BRACKET REPLACED. FLAP SECONDARY DRIVES CLEANED AND LUBRICATED. AIRCRAFT RETURNED TO SERVICE.  NOTE: FLAP SECONDARY DRIVE INSPECTION AND LUBRICATION TASKS (1500HR INTERVAL) LAST COMPLETED 791HR / 949CY PREVIOUS. (TC NR 20070524007)                                                                                                                               2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
             20081104     WP  2008       11         4          CA070524008      120070523G6310V31001          SWITCH          ROBSIN      C0511       ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              CLUTCH ACTUATOR FAILED          W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA       349                                                            (CAN) DURING AN INSP, CLUTCH ACTUATOR FAILED TEST AND CLUTCH WOULD NOT ENGAGE DUE TO MICROSWITCH FAILURE. CLUTCH REPLACED AND CHECKED SERVICEABLE. (TC NR 20070524008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3O3  O  H11NM   E295                 
20070620000322007062000032EA  2007       6          20         CA070525001      120070525G32332158500116      ACTUATOR                    2158500116  CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  LANDING GEAR    FAILED          W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                  H213                                                (CAN) THE NEWLY OVERHAULED ACTUATOR FAIL THE FUNCTIONAL CHECK AFTER INSTALLATION, IT DOESNT STAY LOCKED WITH HYDRAULIC PRESSURE REMOVED.  (TC NR 20070525001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20070620000332007062000033NE  2007       6          20         CA070525002      220070511G7210MS949034        BOLT            PWC         311276701   PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE                              ENGINE          FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       946  946   83D248                                              (CAN) ENGINE WAS REMOVED AFTER THE PILOT REPORTED THAT A LOUD BANG AND SHUDDER WAS EXPERIENCED BY THE AIRCRAFT DURING CLIMB IN AUTOPILOT NEAR TAKEOFF POWER APPROXIMATELY 5 MINUTES AFTER TAKEOFF AT 6000 FT.  THE REDUCTION GEARBOX CHIP DETECTOR WAS ILLUMINATED AND THE AIRCRAFT RETURNED BACK TO BASE AT LOW POWER WITH NO OTHER ABNORMALITIES OBSERVED.  ALL GROUND OPERATIONS WERE NORMAL.  THE DATE OF THE INCIDENT WAS MAY 11, 2007.  DURING INVESTIGATION DISMANTLE OF THE POWER SECTION AND FIRST-STAGE REDUCTION CARRIER ASSEMBLY, OF (6) MACHINE HEX BOLTS (IPC P/N 3038338, CH. 72-11-00, FIGURE 4, ITEM 200, P/N MS9490-34) WAS FOUND WITHOUT THE BOLT HEAD ATTACHED.  NOTE THAT THE CARRIER HEX BOLTS SECURE THE FIRST-STAGE CARR1L71 3T4  TRTA78EU   E26NE                
20070622000812007062200081EU  2007       6          22         CA070525003      120070524G3230A1029E          BOLT                                    BAG   JETSTMJETSTM3101  1500215EU  GARRTTTPE331TPE33110U   01514WP  MCAULY4HFR344HFR34C652  NE  NLG             SHEARED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) NLG RETRACTION JACK MOUNT UPPER IB MOUNTING BOLT SHEARED. DISCOVERED DURING SCHEDULED NLG RETRACTION, JACK ATTACH BOLT INTEGRITY INSPECTION. ALL MOUNTING BOLTS REPLACED WITH NEW. (TC NR 20070525003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4T4  TRTA21EU   E4WE    6  C3PNE     
20070622000822007062200082NE  2007       6          22         CA070528001      220070521G7250                TURBINE         CFMINT      71200011    AIRBUSA319  A319112     3930323EU  CFMINTCFM56 CFM565A3         NE                              ENGINE          MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      CA                  733107                                              (CAN) WAITING FOR SHOP TEAR DOWN, SUSPECTED FAILURE CAUSES BUT NOT CONFRIMED ARE NR 4 BEARING OR HPT BLADE.  ENG TT 26462, CYC 12034, TSI 13977, CSI 6250. (TC NR 20070528001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA28NM   E29NE                
20070809000382007080900038EU  2007       8          9          CA070528002      120070511G32309740926112      RELAY                                   PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  MLG             FAULTY          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       3047                                                           (CAN) ON APPROACH THE LANDING GEAR WAS SELECTED DOWN. THE NOSE LANDING GEAR IN TRANSIT LIGHT WAS SLOW TO EXTINGUISH.  UPON MAINTENANCE TROUBLESHOOTING THE HYDRAULIC PUMP WAS FOUND TO BE INTERMIITTENTLY CUTTING OUT.  THE LANDING GEAR RELAY WAS REPLACED AND NO FURTHER ADNORMALITIES WERE REPORTED. (TC NR 20070528002)                                                                                                                                                                                                                                                                                                                                                                                                                     1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070622000832007062200083GL  2007       6          22         CA070528003      320070319G61144716            HUB             MCAULY      D2A34C58    CESSNA185   A185E       2072818CE  CONT  O520  IO520D      17032SO  MCAULY2A34C D2A34C58    GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3399 647   740488                                              (CAN) PROPELLER RECEIVED FOR OVERHAUL AT 10 YEARS CALENDAR TIME, FOUND HUB THREADS CRACKED, FOUND ONE BLADE THREAD CRACKED, FOUND ONE BLADE RETENTION NUT CRACKED.  FAA AD 91-15-04 APPLIED TO THIS PROPELLER FOR INITIAL INSPECTION AND MODIFICATION WHICH HAD BEEN ACCOMPLISHED (TC NR 20070528003)                                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O3  O  3A24    E5CE    5  CP3EA     
20070618001632007061800163NM  2007       6          18         CA070528004      120070307G3244                TIRE                                    AIRBUSA319  A319114     3930350NM  CFMINTCFM56 CFM565A3         NE                              NLG             DEFLATED        W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH AT 5000 FT CREW HEARD LOUD BANG, AIRCRAFT LANDED WITHOUT INCIDENT, FLIGHT CREW SUSPECTED A BIRD STRIKE. AT ARRIVAL GATE MAINTENANCE FOUND LT NOSE WHEEL TIRE DEFLATED AND OFF THE RIM. BOTH NOSE WHEEL ASSEMBLIES REPLACED, SHOP FOUND THAT THE LT NOSE WHEEL ASSEMBLY OVER INFLATION VALVE HAD BLOWN. NO EVIDENCE OF A BIRD STRIKE WAS FOUND. (TC NR 20070528004)                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA28NM   E29NE                
20070622000842007062200084GL  2007       6          22         CA070528005      320070319G61144716            HUB             MCAULY      D2A34C58    CESSNA185   A185F       2072821CE  CONT  O520  IO520D      17032SO  MCAULY2A34C D2A34C58    GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1563  690816                                              (CAN) PROPELLER RECEIVED FOR OVERHAUL AT 10 YEARS CALENDAR TIME, AT THAT TIME THE PROPELLER HAD BEEN INSPECTED IAW AIRWORTHINESS MANUAL PART VI APPENDIX C (4).  THE LAST OVERHAUL COMPLETED WAS JUNE 1987.  THE PROPELLER HAD EXCEEDED THE MFG HARD TIME OF 1,500 HOURS BETWEEN OVERHAULS. FOUND HUB THREADS CRACKED.  FAA AD 91-15-04 APPLIED TO THIS PROPELLER FOR INITIAL INSPECTION AND MODIFICATION WHICH HAD BEEN ACCOMPLISHED.   (TC NR 20070528005)                                                                                                                                                                                                                                                                                    1H71 3O3  O  3A24    E5CE    5  CP3EA     
20070622000852007062200085GL  2007       6          22         CA070528006      320070301G6111S90AT4          BLADE           MCAULY      D2A34C58    CESSNA185   A185E       2072818CE  CONT  O520  IO520D      17032SO  MCAULY2A34C D2A34C58    GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       890  890   736835                                              (CAN) PROPELLER RECEIVED FOR OVERHAUL AT 10 YEARS CALENDAR TIME, AT THAT TIME THE PROPELLER HAD BEEN INSPECTED PER AIRWORTHINESS MANUAL PART VI APPENDIX C (4).  THE LAST OVERHAUL COMPLETED WAS OCTOBER 1991. FOUND BOTH BLADE THREADS CRACKED.  FAA AD 91-15-04 APPLIED TO THIS PROPELLER FOR INITIAL INSPECTION AND MODIFICATION WHICH HAD BEEN ACCOMPLISHED. (TC NR 20070528006)                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  O  3A24    E5CE    5  CP3EA     
20070622001202007062200120EA  2007       6          22         CA070528007      120070526G3234750006000       SELECTOR VALVE                          CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              NLG WW          UNSERVICEABLE   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) CLIMBING THROUGHT 13000 FT AT 290 KIAS, THE NLG DOOR WARNING/UNSAFE MESSAGE WAS DISPLAYED AND CREW COULD HEAR A CLUNKING NOISE FROM THE NLG AREA.  ELECTED TO RETURN. MLG EXTENDED NORMALLY WITH (3) GREEN LIGHTS AND NO CAUTION/ADVISORY MESSAGES DISPLAYED.  AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER PROBLEM. TROUBLESHOOTING WAS IN PROGRESS AND FOUND THE LANDING GEAR SELECTOR VALVE WAS UNSERVICEABLE. PART WAS REPLACED, FUNCTION CHECK FOUND NO FURTHER DEFECT. AIRCRAFT RETURNED FOR SERVICE (TC NR 20070528007)                                                                                                                                                                                                  2L72 4F4  FRTA21EA   E15NE                
20070622001212007062200121EU  2007       6          22         CA070528008      120070413G7933RP22100         SENSOR          CFMINT      CFM565C4    AIRBUSA340  A340313            EU  CFMINTCFM56 CFM565C4    13802NE                              OIL SYSTEM      INOPERATIVE     W      E   ENGINE SHUTDOWN                                                                                 M  OVER TEMP                                                                     APAPPROACH       1                      CA       2790915670 741603                  741603                      (CAN) NR 2 ENGINE OIL TEMPERATURE HIGH, 30 MILES FROM AIRPORT, ENGINE SHUTDOWN IAW QRH PROCEDURES, AIRCRAFT LANDED WITHOUT INCIDENT. ENGINE OIL TEMP SENSOR AND FUEL RETURN VALVE REPLACED, NO SUBSEQUENT FAULTS AFTER PARTS CHANGED. (TC NR 20070528008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L74 4F4  FRTA197    E37NE                
20080131000342008013100034EA  2008       1          31         CA070528009      220070527G73103032791         LINE                                    BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  LT ENG FUEL     CHAFED          W      K   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      CA                                                                      (CAN) FUEL FLOW TRANSMITTER LINE P/N 3032791 FOUND CHAFED. NEW PART ON ORDER. (TC NR 20070528009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070622001222007062200122NM  2007       6          22         CA070528010      120070526G2530                UNKNOWN                                 BOEING767   767333      1385301NM  GE    CF6   CF680C2B6F  30025NE                              GALLEY          MALFUNCTIONED   W      H   DEACTIVATE SYST/CIRCUITS                                                                        O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) A FLIGHT ATTENDANT RECEIVED AN ELECTRIC SHOCK FROM THE WATER DISPENSER IN THE REAR GALLEY.  COFFEE MAKERS REMOVED, GALLEY WIRING INSPECTED AND CONTINUITY CHECK CARRIED OUT (L-4355954).  MORE IT TROUBLESHOOTING STEPS HAVE BEEN PROVIDED BUT NOT COMPLETED YET.  (TC NR 20070528010)                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA1NM    E13NE                
20080131000352008013100035CE  2008       1          31         CA070528011      120070528G5610PPG10138402522  WINDSHIELD                              BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  LT COCKPIT      CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) CO-PILOTS WINDSCREEN CRACKED UNDER PRESSURIZED CONDITION. AIRCRAFT RETURNED TO BASE FOR WINSHEILD REPLACEMENT. UNABLE TO INDICATE CORRECT MFG.  (NOT IN LIST)  (TC NR 20070528011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20080319001402008031900140CE  2008       3          19         CA070528012      120070524G2435300SGC12902     STARTER GEN                             CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              RIGHT           UNSERVICEABLE   W      A   UNSCHED LANDING                                                                                 HJ ELECT. POWER LOSS-50 PC   WARNING INDICATION                                  CLCLIMB          1                      CA            771                           DC0074                      (CAN) RT ENGINE GENERATOR FAILED WHICH ILLUMINATED THE GENERATOR FAIL LIGHT. AC RETURNED TO BASE. (TC NR 20070528012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA22CE   E00053EN             
20070809000392007080900039EU  2007       8          9          CA070528013      120070522G32511855A000003     MODULE                                  EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF3410E6    30015NE                              NLG STEERING    MALFUNCTIONED   W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA       2829                                                           (CAN) STEERING FAIL MESSAGE ON FINAL APPROACH, FLIGHT DID 2 MISSED APPROACHES FOR GEAR RECYCLING, LANDED ON THIRD CYCLING OF GEAR. FLIGHT HISTORY DATA BASE DOWNLOADED, MFG REP FOUND STEERING CONTROL MODULE AT FAULT. ACFT THR 3643, TCY 1663 (TC NR 20070528013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA57NM   E00070EN             
20080319001412008031900141EU  2008       3          19         CA070528014      120070527G71207254120511      MOUNT                                   SAAB  SF340 SF340A      7850100EU  GE    CT7TP CT75A       30030NE  ROTOL R389  R3894123F25 NE  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THE AFT ENGINE MOUNT BRACKET WAS DISCOVERED TO BE CRACKED DURING A SCHEDULED ENGINE CHANGE. THE AFFECTED BRACKET WAS REPLACED WITH A SERVICEABLE UNIT. NO FURTHER ACTION NOTED. (TC NR 20070528014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4T4  TRTA52EU   E8NE    6  CP30NE    
20070622001232007062200123WP  2007       6          22         CA070529001      220070529G725030606901        TURBINE BLADES  GARRTT      TFE73120R1B LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              RT ENGINE       MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2232 2232  P111221C                                            (CAN) DURING A DAILY INSPECTION, IT WAS NOTICED BY THE TECHNICIAN THAT A PIECE OF A BLADE FROM THE RT ENGINE TURBINE WAS MISSING. NO DIFFICULTIES HAD BEEN REPORTED BY THE FLIGHT CREW AND NO OTHER DAMAGE HAS BEEN NOTED ON THE ENGINE. THE ENGINE WILL BE REMOVED AND SENT FOR REPAIR TO AN OUTSIDE ENGINE SHOP. (TC NR 20070529001)                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTT00008WIE6WE                 
20080204001572008020400157EU  2008       2          4          CA070529002      120070528G6220704A3363320851  SPHERICAL STOP  SNIAS       AS350B2     SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              M/R HEAD        MISMANUFACTURED W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       13         2785                                                (CAN) ALL SPHERICAL STOPS WHERE REPLACED DURING A 500 HRS INSPECTION. PILOT REPORTED UNCONTROLLED STICK MOVEMENT DURING HYDRAULIC OFF TEST. WITH HYDRAULIC ON, NO PROBLEM WAS REPORTED. DURING TROBLESHOOTING THIS PROBLEM IT WAS FOUND THAT ONE OF THE SPHERICAL STOP BEARINGS PREVIOUSLY INSTALLED HAD A MFG DESIGN PROBLEM.  THE PRESET ANGLE ATTACH BOLT WHICH ATTACH TO THE STARFLEX WAS FOUND NOT IAW SPEC  WHICH INDUCED AN UNCONTROLLED STICK MOUVEMENT DURING HYDRAULIC OFF TEST. THIS PART WAS RETURNED TO MFG FOR EXCHANGE UNDER WARRANTY (TC NR 20070529002)                                                                                                                                                                        1G71 3U3  U  H9EU    E19EU                
20070622001242007062200124NE  2007       6          22         CA070529003      220070527G8500                ENGINE                                  DOUG  DC4   C54EDC      3021528WP  PWA   R2000 R20007M2    52023NE  HAMSTD23E   23E50       NE                  MAKING METAL    W      E   ENGINE SHUTDOWN                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) ENGINE REMOVED DUE TO METAL IN OIL SCREEN, TBO 750 HOURS.  ENGINE BEING SENT OUT FOR OVERHAUL. (TC NR 20070529003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L74 4R4  R  A762    5E5     6  CP603     
20070809000402007080900040NM  2007       8          9          CA070529004      120070507G301029S7D524007     BOOT                                    DORNERDO32  DO328100    2996000NM                                                               DE-ICE SYSTEM   LOOSE           W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       55                                                             (CAN) PILOTS REPORTED LT HORIZONTAL STAB DE-ICE BOOT APPEARS LOOSE. MAINTENANCE INSPECTED THE BOOT AND FOUND THE DE-ICER BOOT HAD COME LOOSE FROM THE AIRCRAFT AT THE AFT EDGES. THE ADHESIVE (3M 1300L) DID NOT SECURE THE DEICER BOOT TO STAB.  THE DEICER BOOT WAS RECENTLY REPLACED UNDER WORK ORDER 15249. TIME ON PART 54.6 HOURS AND 73 LANDINGS. DEICER BOOT REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070529004)                                                                                                                                                                                                                                                                                                             2H72 4T    RTA45NM                        
20070809000412007080900041CE  2007       8          9          CA070529005      120070511G553107310292        SPAR                                    CESSNA185   A185F       2072821CE  CONT  O520  IO520D      17032SO  HARTZLHCC3Y PHCC3YF1    GL  VERTICAL STAB   CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4534                                                           (CAN) DURING AN ANNUAL/100 HOUR INSPECTION FIN AFT SPAR WAS FOUND CRACKED. MFG SINGLE ENGINE CUSTOMER CARE SERVICE INFORMTION LETTER SE 80-85 ADDRESSES THIS PROBLEM. SERVICE KIT SK 185-25A INSTALLED THIS DATE. (TC NR 20070529005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O3  O  3A24    E5CE    5  CP25EA    
20070622001252007062200125SO  2007       6          22         CA070529006      220070507G8520646778          CONNECTING ROD  CONT        IO520D      CESSNA185   A185F       2072821CE  CONT  O520  IO520D      17032SO  MCAULY2A34C D2A34C58    GL  ENGINE          DESTROYED       W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA                  174942R                                             (CAN) DURING FLIGHT, THE ENGINE BEGAN TO RUN ROUGH. THE AIRCRAFT MADE AN UNSHEDULED LANDING FOR INSPECTION. THE CRANKCASE WAS FOUND CRACKED AT THE NR 2 CYLINDER.  THE ENGINE WAS REMOVED FROM THE AIRCRAFT. (TC NR 20070529006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  O  3A24    E5CE    5  CP3EA     
20070809000422007080900042CE  2007       8          9          CA070529007      120070529G27014527102070001   WASHER                                  LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              CONTROL COLLUMN FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2158                                                           (CAN) DURING A SCHEDULE INSPECTION THE PILOT CONTROL WHEEL WAS FOUND TO HAVE MORE FREE PLAY THAN THE CO-PILOT. UPON FURTHER INVESTIGATION IT WAS FOUND THAT THE TAB WASHER P/N 4527102070-001 WHICH IS SECURING THE NUT P/N NAS1423-20. HAD ONLY ONE TAB BENT, TO ADD TO THE PROBLEM THE TAB WAS IMPROPERLY BENT. AFTER A WHILE THE TAB PERMITTED THE NUT TO BACK OFF ONE FLAT GIVING THE FREE PLAY TO THE CONTROL WHEEL. IT WAS FOUND IN THE MM, CHAPTER 27-10-01 PAGE 202 SECTION B) 9.   BEND THE WASHER TABS TO THE NUT FLATS. ONLY ONE TAB WAS BENT, PERMITTING THE NUT TO BACK OFF, THE CO-PILOT CONTROL WHEEL WAS INSPECTED FOR PROPER INSTALLATION AND FOUND TO BE DONE CORRECTLY. THE TAB WASHER WILL BE REPLACED PRIOR TO RETURNING TH2L72 4F4  FRTT00008WIE6WE                 
20080220000552008022000055EU  2008       2          20         CA070529008      120070528G2932MA12401         PRESSURE SWITCH                         SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              HYDRAULIC SYSTEMDEFECTIVE       W      D   RETURN TO BLOCK                                                                                 P  NO WARNING INDICATION                                                         ININSP/MAINT     1                      CA                                                                      (CAN) SWITCH REMAINED OPEN AND WOULD NOT ACTIVATE THE HYDRAULIC PRESSURE WARNING HORN. (TC NR 20070529008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 3U3  U  H9EU    E19EU                
20070809000432007080900043    2007       8          9          CA070530001      420070529G342225863333        GYRO                                    CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              DIRECTIONAL     DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING THE COMPLETION OF AN UNASSOCIATED SB IT WAS NOTICED THAT THE C-12 GYRO HAD FREED ITSELF OF ITS MOUNTING. UNTIL NOW NO COMPARATOR ANNUNCIATIONS OR COMPASS RELATED SNAGS HAD BEEN REPORTED OR DETECTED. (TC NR 20070530001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 4F4  F  A22CE   E1NE                 
             20081104         2008       11         4          CA070530002      420070530G2562CIR112          ELT                                     BEECH 100   100BEECH    1152916CE  GARRTTTPE331TPE3316252B 01514WP  HARTZLHCB4T HCB4TN5     GL  CABIN           FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHEN TESTING ELT FOR THE REQUIREMENT OF CAR 571 APPENDIX G FOUND G SWITCH WOULD NOT ACTIVATE. (TC NR 20070530002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3T4  T  A14CE   E2WE    6  CP40EA    
20070618001662007061800166EA  2007       6          18         CA070530003      220070320G8520                CRANKSHAFT                              CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  ENGINE          FAILED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         ER VIBRATION/BUFFET          PARTIAL RPM/PWR LOSS                                NRNOT REPORTED   1                      CA                                                                      (CAN) ON THE WAY BACK TO THE AIRPORT THE ENGINE DEVELOPED ABNORMAL VIBRATIONS AND THE PILOT DECIDED TO CLIMB TO 2,400 FT, THEN THE ENGINE SUDDENLY STOPPED. THE PILOT DECIDED TO FORCE LAND ON THE AUTO ROUTE IN A WESTERLY DIRECTION. AFTER INSPECTION, IT WAS DETERMINED THAT THERE WAS NO LOSS OF OIL AND THAT THE PROP WAS UNABLE TO TURN. THE ENGINE CRANKSHAFT WAS THE CAUSE OF FAILURE. (TC NR 20070530003)                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A19    E223    5  NP50GL    
20070622001262007062200126NE  2007       6          22         CA070530004      220070528G726136022375        SEAL            PWA         PW121       AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE                              NR 1 ENGINE     LEAKING         W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                  PCE120714               PCE120714                   (CAN) WHILE CONDUCTING AN ACCEPTANCE CHECK FLIGHT, THE CREW OBSERVED A LOW OIL PRESSURE CONDITION ON THE NR 1 ENGINE. THE CREW CONDUCTED A PRECAUTIONARY SHUTDOWN OF THE ENGINE AND RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM.   MAINTENANCE DETERMINED THE NR 1 STARTER GENERATOR DRIVE SEAL WAS LEAKING. THE SEAL WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE AFTER SATISFACTORY GROUND RUN. (TC NR 20070530004)                                                                                                                                                                                                                                                                                                2H72 4T4  TRTA53EU   E20NE                
20070810000942007081000094CE  2007       8          10         CA070530005      120070520G3010SMR517515       BOOT                                    CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  HARTZLHCB3T HCB3TN3     GL  DE-ICE SYSTEM   WORN            W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       252                                                            (CAN) DE-ICE BOOT, FOUND WORN RUBBER THAT WAS MELTED FROM EXHAUST GASES. MINOR BLISTERING FOUND ON TOP RT OF BOOT. (TC NR 20070530005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3T3  T  A37CE   E4EA    6  CP15EA    
20070622001272007062200127NM  2007       6          22         CA070530006      120070530G2134                WARNING SYSTEM                          BOEING727   727225      1384077NM                                                               CABIN PRESSURE  ACTIVATED       W      JA  DUMP FUEL               UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER DEPARTURE, WHEN AT 13,000 FEET ALT WARNING HORN SOUNDED AND COULD NOT BE SILENCED WITH THE HORN CUTOUT. CREW TRIED SWITCHING TO STBY WITH NO RESULTS. HORN CONTINUED ON APPROACH. AT TIME OF INITIAL HORN, CABIN PRESSURE WAS 5000 FT AND 5PSI DIF. THE AIRCRAFT DUMPED FUEL FOR THE LANDING AND LANDED SUCCESSFULLY AND RETURNED TO THE RAMP. THE MAINTENANCE PERSON CARRIED OUT MM SYSTEM TESTS WITH NO FAULTS. AIRCRAFT WAS GROUND PRESSURIZED AND AGAIN NO FAULTS. THE CREW ATTEMPTED A SECOND DEPARTURE AND HAD THE WARNING COME ON AT 9000 FT. AIRCRAFT RETURNED TO DEPARTURE POINT AND IS AOG WHILE TROUBLESHOOTING IS IN PROGRESS. OPERATOR WILL ADVISE SDR REPORTING OF RECTIFICATION WHEN IT IS ESTABLISHED. (TC NR 2007052L73 4F      A3WE                         
             20081104         2008       11         4          CA070530007      420070530G2562AK450           ELT                                     AMTR  F1156 F1156C      5910310GL  LYC   O540  IO540*      41532EA                                              MALFUNCTIONED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHEN TESTING ELT FOR THE REQUIREMENT OF CAR 571 APPENDIX G FOUND LITTLE OR NO AUDIO MODULATION. UNIT WAS TRANSMITTING RF CARRIER ONLY. (TC NR 20070530007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONCEXPA1H711E4                  
20070620000342007062000034EA  2007       6          20         CA070531001      120070527G5610NP13932111      WINDSHIELD                              CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C1          NE                              COCKPIT         CRACKED         W      BA  EMER. DESCENT           UNSCHED LANDING                                                         O  OTHER                                                                         CRCRUISE         1                      CA       9395                                                           (CAN) CREW NOTED THAT LT W/S CRACKED IN CRUISE FLT (40,000FT) AND DIVERTED FOR MTX NO OTHER PROBLEMS NOTED.  C/A REMOVED AND REPLACED LT WINDSHIELD IAW MM 56-11-01. REF LGPG 2330059 ITEM 1, 2, AND 3 FOR OK TO INSTALL, FUNCTIONAL CHECK AND OPS CHECK.  END (TC NR 20070531001)                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA21EA   EOOO63EN             
20070620000352007062000035NE  2007       6          20         CA070531002      220070524G7200CF343A1         ENGINE                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              RIGHT           VIBRATION       W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         EDFVIBRATION/BUFFET          INFLIGHT SEPARATION       FLT CONT AFFECTED         CRCRUISE         1                      CA       5800                                                           (CAN) AIRCRAFT (FLT 4344) WAS ENROUTE WHEN CREW EXPERIENCED AN UNCONTROLLABLE VIBRATION FROM THE RT ENGINE. THE ENGINE WAS SHUTDOWN IN FLIGHT. THE AIRCRAFT WAS DIVERTED AND LANDED AT TRI.   IT WAS REPORTED BY THE CREW (TO MAINT CONTROL) THAT THE RT THROTTLE WAS BINDING NEAR FLIGHT IDLE BUT THEY WERE ABLE TO PERFORM A SHUTDOWN.  IN ADDITION, IT WAS REPORTED THAT PARTS OF THE COWL/NACELLE HAVE DEPARTED THE AIRCRAFT. (TC NR 20070531002)                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA21EA   E15NE                
20070620000362007062000036NM  2007       6          20         CA070531003      120070530G3411                PITOT SYSTEM                            BOEING727   727260      138408KNM  PWA   JT8   JT8D17      52049NE                              PITOT/STATIC SYSOBSTRUCTED      W      C   ABORTED TAKEOFF                                                                                 O  OTHER                                                                         TOTAKEOFF        1                      CA                                                                      (CAN) THE AIRCRAFT BEGAN THE TAKEOFF ROLL WHEN THE FLIGHT CREW NOTICED A LAG IN THE FIRST OFFICERS AIR SPEED INDICATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO ADDITIONAL PROBLEMS. UPON INSPECTION OF THE FIRST OFFICERS PITOT INSTALLATION AN OBSTRUCTION WAS FOUND (BUG/INSECT) AND WAS REMOVED. THE PITOT STATIC SYSTEM WAS TESTED IAW THE AIRPLANE MM WITH NO FURTHER FAULTS. THE AIRCRAFT WAS RETURNED TO SERVICE.  (TC NR 20070531003)                                                                                                                                                                                                                                                                   2L73 4F4  FRTA3WE    E2EA                 
20070622001282007062200128EU  2007       6          22         CA070531004      120070530G2120                UNKNOWN                                 AIRBUS330   A330243     3930330EU  RROYCERB211 RB211*      54555NE                              CABIN           ODOR            W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) DURING FLIGHT, A PAPER BURNING SMELL AT SEAT 26DE WAS REPORTED TO THE CABIN CREW. THE AUDIO SYSTEM WAS SHUTOFF IAW PRECAUTION AND SMELL DISAPPEARED AFTER 20 MINUTES. THE AUDIO SYSTEM WAS TESTED ON ARRIVAL AND THE AREA INSPECTED FOR BURNING MARKS. AUDIO SYSTEM AND AREA WAS FOUND NORMAL WITH NO DEFECT. AIRCRAFT WAS RETURN TO SERVICE WITH NO REPEAT.   (TC NR 20070531004)                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA46NM   A12EU                
20070622001292007062200129NE  2007       6          22         CA070531005      220070425G73133186100         VALVE                                   SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              ENGINE          MALFUNCTIONED   W      O   OTHER                                                                                           X  ENGINE FLAMEOUT                                                               ININSP/MAINT     1                      CA                                                                      (CAN) ASSEMBLY IS ON CONDITION.  AFTER CARRYING OUT A 100 HR AND 300 HR INSPECTION A FUNCTIONAL CHECK WITH THE INJECTOR ELECTRO VALVE (IEV) WAS ACCOMPLISHED. FOLLOWING A RUN-UP TO 100 PERCENT, THE ENGINE RPM WAS REDUCED AND STABILIZED AT JUST OVER FLIGHT IDLE FOR 30 SECONDS IAW COOL DOWN REQUIREMENTS. DEPRESSION OF THE STARTER BUTTON AT THIS POINT SHOULD NOT HAVE CAUSED ANY PROBLEM BUT IN THIS FUNCTIONAL CHECK A FLAME OUT OCCURRED. FOLLOWING THE FLAME OUT A BENCH TEST WAS CARRIED OUT AND IT WAS DETERMINED THAT IT`S OPERATION AT A PRE DETERMINED P2 PRESSURE WAS INTERMITTENT. SENT UNIT TO MFG FOR REPAIR OR OVERHAUL AND THE UNIT WAS SCRAPPED. (TC NR 20070531005)                                                     1G71 3U3  U  H9EU    E19EU                
20080220003192008022000319WP  2008       2          20         CA070531006      120070529G6310C0183           CLUTCH                                  ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              TRANSMISSION    SEIZED          W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         APAPPROACH       1                      CA       948  948                                                       (CAN) LOUD BANG DURING POWER CHANGE ON APPROACH.  INSPECTED AC AND FOUND CLUTCH ASSY ROUGH.  TURNED IT A FEW TIMES BY HAND AND SEIZED. NEW CLUTCH ASSY INSTALLED, DEFECT RECTIFIED. CLUTCH BEING SENT TO OUR IN HOUSE COMPONENT SHOP FOR INVESTIGATION.  WILL FWD THE PICTURES AND INFORMATION WHEN RECEIVED FROM THE COMPONENT SHOP. PICTURES ATTACHED AND CLUTCH ASSY BEING SENT TO MFG FOR WARRANTY AND INVESTIGATION. (TC NR 20070531006)                                                                                                                                                                                                                                                                                                   1G71 3O3  O  H11NM   1E4                  
20070622001302007062200130NE  2007       6          22         CA070531007      220070425G73133186100         VALVE                                   SNIAS 350   AS350B1     8680811EU  TMECA ARRIELARRIEL1D    60048NE                              ENGINE          MALFUNCTIONED   W      O   OTHER                                                                                           X  ENGINE FLAMEOUT                                                               ININSP/MAINT     1                      CA                                                                      (CAN) ASSEMBLY ON CONDITION. THIS UNIT WAS REMOVED SERVICEABLE FOR ANOTHER AIRCRAFT. A FUNCTIONAL CHECK WAS CARRIED OUT. FOLLOWING A RUN UP TO 100 PERCENT THE ENGINE RPM WAS REDUCED AND STABILIZED AT JUST OVER FLIGHT IDLE FOR 30 SECONDS IAW COOL DOWN REQUIREMENTS.  DEPRESSION OF THE STARTER BUTTON AT THIS POINT SHOULD NOT HAVE CAUSED ANY PROBLEM BUT IN THIS FUNCTIONAL CHECK A FLAME OUT OCCURED. A BENCH WAS CARRIED OUT WITH CONSISTENT FAILURES OCCURRED AT PRESCRIBED P2 PRESSURE. (TC NR 20070531007)                                                                                                                                                                                                                          1G71 3U3  U  H9EU    E19EU                
20070622001312007062200131SO  2007       6          22         CA070601001      120070528G5330                SKIN                                    LKHEED382   382G        526414USO  ALLSN 501D  501D22A     03006GL  HAMSTD54H   54H60117    NE  FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING PRE-FLIGHT CHECK PRIOR TO DEPARTING, CRACKING WAS OBSERVED IN THE AFT FUSELAGE SKIN IN THE AREA OF STATION 946. THE AIRCRAFT HAS BEEN FERRIED FOR REPAIR. (TC NR 20070601001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H74 4T4  T  A1SO    E282    6  CP906     
20070711002872007071100287EA  2007       7          11         CA070601002      120070531G2420820465          ADG                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                                              DEPLOYED        W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA       6118 6118                                                      (CAN) ADG DEPLOYED AS THE LANDING GEAR WAS SELECTED UP.  THE FLIGHT RETURNED WITHOUT INCIDENT.  MAINTENANCE TROUBLESHOOTING WAS CARRIED OUT AND THE ADG AUTO DEPLOY CONTROLLER WAS REPLACED AND TESTED SERVICEABLE. THE ADG WAS INSPECTED VISUALLY IAW MFG AND IS TO HAVE FLUORESCENT PENETRANT CARRIED OUT WITHIN 3 CALENDAR DAYS.  (TC NR 20070601002)                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20080220003202008022000320SW  2008       2          20         CA070601003      120070528G28102060636321      FUEL CELL                               BELL  206   206L1       1182107SW  ALLSN 250C  250C28      03013GL                                              LEAKING         W      O   OTHER                                                                                           KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            ININSP/MAINT     1                      CA                                                                      (CAN) FUEL SMELL NOTED. INSPECTION FOUND SMALL FUEL LEAK. FUEL CELL REMOVED SENT OUT FOR REPAIR, REINSTALLED. (TC NR 20070601003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3U3  U  H2SW    E1GL                 
20070711002862007071100286EA  2007       7          11         CA070601004      120070529G2797                WIRE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        BURNED          W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) FLAP FAIL MESSAGE COME ON DURING CRUISE AT ALT FL330 WITH NO FLAP SELECTION MADE.  AIRCRAFT RETURN TO  ORIGINATING STATION, MAINTENANCE REPLACED THE BPSU AND FECU BUT NO FIX. FURTHER INVESTIGATION REVEALED SOME BURNED WIRES AT LT BPSU CONNECTOR.  TEMPORARY REPAIRS CARRIED OUT AND AIRCRAFT FERRIED.  AIRCRAFT IS NOW UNDERGOING A HEAVY CHECK AND THE SNAG IS STILL BEING WORKED ON.  MORE SPECIFICS OF THE DEFECT RECTIFICATION TO FOLLOW. (TC NR 20070601004)                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20070622001322007062200132SW  2007       6          22         CA070604001      120070603G632023063393        GEARBOX         ALLSN       250C47B     BELL  407   407         1182206SW  ALLSN 250C  250C47B          GL                              MAIN ROTOR      SEIZED          W      R   AUTOROTATION                                                                                    JY WARNING INDICATION        ENGINE STOPPAGE                                     CRCRUISE         1                      CA       6077       CAE847124               CAE847124                   (CAN) ENGINE CHIP ILLUMINATED, APPROX 3-4 SECONDS LATER ENGINE FAILED. (TC NR 20070604001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 3U3  UO H2SW    E1GL                 
20070711002842007071100284GL  2007       7          11         CA070604002      220070518G7320                FADEC                                   BELL  407   407         1182206SW  ALLSN 250C  250C47B          GL                                              MALFUNCTIONED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A FLIGHT ON MAY 18 AT 6755.9 TAT, THE PILOT EXPERIENCED A CONTROLLED ENGINE OVERSPEED CONDITION.  THE PILOT WAS NOT GIVEN AT INDICATION IAW MFG FM CRITERIA.  LATER THE PILOT REPORTED THE CONDITION TO THE AME. THE AME DOWN LOADED THE FADEC INFORMATION AND THE FOLLOWING WERE NOTED.  38060 NP AND 53.3 PERCENT Q.  WHICH IS ACTUALLY 80 RPM BELOW THE POINT WHERE THE PILOT WOULD GET A LIGHT BUT OVER THE LIMITS IN MM 72-00-00 AND 77-50-00.  THE AIRCRAFT WAS REMOVED FROM SERVICE AND RETURNED TO THE MAIN MAINTENANCE BASE UNDER A TC FLIGHT PERMIT.  THE ENGINE HAS BEEN REMOVED AND SENT TO MFG FOR INSPECTION. (TC NR 20070604002)                                                                                    1G71 3U3  UO H2SW    E1GL                 
20080220003212008022000321WP  2008       2          20         CA070604003      120070526G243532991           LINK                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              STARTER GEN     CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING 100HR INSPECTION FOUND CRACKED STARTER GENERATOR LINK. (TC NR 20070604003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3O3  O  H11NM   1E4                  
20070711002822007071100282NE  2007       7          11         CA070605001      220070603G7321                FCU                                     AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  NR 2 ENGINE     INOPERATIVE     W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB AFTER DEPARTURE, THE CREW OBSERVED A SLOW DECREASE IN TORQUE ON THE NR 2 ENGINE AND WITH REDUCED FUEL FLOW.  THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM.   MAINTENANCE REPLACED THE NR 2 FUEL CONTROL UNIT (FCU) AND RETURNED THE AIRCRAFT TO SERVICE AFTER SATISFACTORY GROUND RUN. (TC NR 20070605001)                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20070711002812007071100281NE  2007       7          11         CA070605002      220070512G73203035381A        LINE                                    DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  HMU-P3          CRACKED         W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          CLCLIMB          1                      CA                                                                      (CAN) THE NR 2 ENGINE WAS SNAGGED AS NOT PRODUCING FULL POWER ON TAKEOFF AND IN FLIGHT. MAINTENANCE FOUND THAT THE P3 SENSE LINE WAS CRACKED AT THE HYDRO MECHANICAL UNIT.  UPON REMOVAL, THE LINE BROKE. THE SENSE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070605002)                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070712001272007071200127EA  2007       7          12         CA070605003      220070601G8520LW15328         MAIN BEARING    LYC         O360E1A6D   PIPER PA44  PA44180     7104402SO  LYC   O360  O360E1A6    41514EA  HARTZLHCC2Y HCC2YR2     GL  ENGINE          FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            3690  RL38277T                                            (CAN) MAIN BEARING FAILED DUE TO EXCESSIVE TSO. CRANKCASE DAMAGED BEYOND REPAIR. VERY CLOSE TO HAVING A COMPLETE ENGINE FAILURE. (TC NR 20070605003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  A19S0   E286    5  CP920     
             20081229     CE  2008       12         29         CA070605004      120070605G273005341221        BELLCRANK                               CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA                              ELEVATOR        MISINSTALLED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       8805                                                           (CAN) ELEVATOR UP TRAVEL FOUND TOO LOW. INVESTIGATION REVEALED UP CABLE ATTACH BOLT INSTALLED WRONG WAY. THIS RESULTED IN CONTACT WITH VERT STAB ATTACH BRACKET (WHERE CABLE PASSES THROUGH LIGHTENING HOLE)THUS LIMITING TRAVEL BY APPROX 3 DEG LESS THAN REQUIREMENT. BOLT INSTALLED PROPERLY AND SYSTEM RETURNED TO SERVICE.                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3O3  ONT3A12    E274                 
20070810000952007081000095SO  2007       8          10         CA070605005      120070605G53404178902         ATTACH BOLT                             PIPER PA42  PA42720     7104212SO  PWA   PT6   PT6A61      52043EA  HARTZLHCB3T HCB3TN3     GL  MLG ACTUATOR    BENT            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       202                                                            (CAN) CONTINUOUS PROBLEM OF PREMATURE WEAR AND INDICATIONS OF STRESS ON MAIN LANDING GEAR ACTUATOR ATTACH HARDWARE.  LOWER FORK BOLT PN 41789-02 AND UPPER ACTUATOR ATTACH BOLT 401-195 (AN5-17A) (BOTH LIFE LIMITED BY MFG INSPECTION PROGRAM) SHOW SIGNS OF BENDING AND/OR WEAR VIRTUALLY EACH DETAILED GEAR INSPECTION (TYPICALLY 200 AIRCRAFT HOURS). THESE PARTS ARE REMOVED AND CLOSELY INSPECTED EACH GEAR INSPECTION AND TYPICALLY REPLACED AT FAR LOWER INTERVALS THAN THE PUBLISHED LIFE LIMITS. (TC NR 20070605005)                                                                                                                                                                                                                  1L72 4T4  T  A23SO   E4EA    6  CP15EA    
20070810000962007081000096SW  2007       8          10         CA070606002      120070602G29102781032261      LINE                                    SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE33111U   01514WP  MCAULY4HFR344HFR34C652  NE  HYD SYSTEM      CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) HYD LEAK IN RT WHEEL WELL.  FOUND LINE CHAFED, LINE REPLACED AND AIRCRAFT RETURNED TO SERVICE AFTER SUCCESSFUL GEAR SWINGS CARRIED OUT. (TC NR 20070606002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4T4  TRTA8SW    E4WE    6  C3PNE     
20070712001282007071200128WP  2007       7          12         CA070606003      220070605G7250                TURBINE BLADES  GARRTT      TPE33112UHR FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  ENGINE          FAILED          W      E   ENGINE SHUTDOWN                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA       5510 5510  P70224                                              (CAN) THE AIRCRAFT WAS ON A SHORT REPOSITIONING FLIGHT.  AFTER AN UNEVENTFUL TAKEOFF AND CLIMB, THE CREW LEVELED AT 9,000 FT AND REDUCED POWER TO 30 PERCENT.  FIVE MINUTES LATER, THE RT ENGINE HAD A VIOLENT AND SUDDEN VIBRATION.  THE CREW SHUTDOWN THE ENGINE IMMEDIATELY AND DECLARED AN EMERGENCY.  THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE AND FOUND THAT THE NR 3 TURBINE WHEEL HAD (4) BLADES MISSING LARGE SECTIONS. THE OIL FEED LINE WAS SEVERED AND IMPACT DAMAGE WAS FOUND ON THE EXHAUST CONE AND TAIL PIPE. THE LAST MAJOR INSPECTION ON THIS ENGINE WAS A HSI/GBI AT 3499.2 HOURS.   (TC NR 20070606003)                                                                                    2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
             20081104     EA  2008       11         4          CA070606004      120070605G3233HF6G            ROD END                                 DHAV  DHC3  DHC3        2800202EA  WALTERM601  M601E11          EU                              ACTUATOR        BROKEN          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) PILOT COULD NOT GET GEAR DOWN INDICATION, BUT COULD GET GEAR UP AND LOCKED INDICATION. WATER LANDING CARRIED OUT. MAINT FOUND LT NOSE GEAR WOULD NOT EXTEND. ROD END FOUND BROKEN ON NOSE GEAR ACTUATOR, REPLACED AND ACFT RETURNED TO SERVICE. (TC NR 20070606004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3R3  T  A815    E00048EN             
20070712001292007071200129EA  2007       7          12         CA070606006      220070601G8530LW12966         CYLINDER        LYC         TIO540A2C   PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1636                                                           (CAN) LT ENGINE,  NR 5 CYLINDER WAS FOUND TO HAVE LOW COMPRESSION DURING THE INSPECTION PROCESS.  EXCESSIVE AIR WAS PASSING THE RINGS. CYLINDER WAS FOUND TO BE GLAZED. CYLINDER WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. WILL UPDATE WITH CYLINDER HOURS. (TC NR 20070606006)                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070810000972007081000097CE  2007       8          10         CA070607001      120070530G3230                BEARING                                 CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              UPLOCK ROLLER   WORN            W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA       7559 40                                                        (CAN) AC WAS UNABLE TO LOWER THE RT MAIN LANDING GEAR. THE EMERGENCY EXTENSION PROCEDURE DID NOT INITIALLY RELEASE THE LANDING GEAR UPLOCK. SUBSEQUENT MANIPULATION OF THE SYSTEM RELEASED THE GEAR TO A DOWN AND LOCKED CONDITION AND THE AIRCRAFT MADE A SAFE LANDING. MAINTENANCE INVESTIGATION REVEALED (2) CONDITIONS WHICH CONTRIBUTED TO THIS SITUATION. IT WAS NOTED DURING INSPECTION OF THE SYSTEM THAT THE EMERGENCY EXTENSION CABLE WAS CONTACTING THE BRAKE ASSY IN SUCH A WAY THAT THE CABLE WAS BEING DEFLECTED APPROXIMATELY .2500 INCH AND COULD PREMATURELY PULL THE HOOK OFF THE ROLLER.  THE CONCERN IS THAT THE CABLE MAY FRAY AND BREAK PREVENTING MANUAL EXTENSION OF THE GEAR. THIS WAS NOT A FACTOR IN THIS CASE.   INV1L72 4F4  F  A22CE   E1NE                 
20080319001422008031900142CE  2008       3          19         CA070607002      120070606G2410359553S8        RETAINING NUT   MOTORCRAFT              CESSNA210   210R        2073458CE  CONT  O520  IO520L      17032SO  MCAULYD3A34 D3A34C404   GL  ALTERNATOR SHAFTMISSING         W      O   OTHER                                                                                           BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CRCRUISE         1                      CA            1     97043226                                            (CAN) PILOT HAD CALLED AND REPORTED THAT THE ALTERNATOR THAT WE HAD REPLACED THE NIGHT BEFORE HAD GONE OFFLINE .7 HRS AND A SLIGHT ODOR OF BURNING RUBBER NOTED INTO HIS FIRST LEG OF FLIGHT. UPON LANDING INVESTIGATION HAD REVEALED THAT THE ALTERNATOR SHAFT FAN RETAINING NUT HAD COME LOOSE AND EXITED THE AC.  FAN HAD ROTATED ON SHAFT AND DRIVE BELT HAD COME OFF. NO DAMAGE TO ANYTHING IN ENG COMPARTMENT EXCEPT TO ALTERNATOR COMPONENTS. THIS ALTERNATOR HAD BEEN REPAIRED AND TESTED BY A COMPANY, WHICH I WILL NOT NAME THAT THIS HAS HAPPENED BEFORE. THE FAN HAD ALSO COME OFF THE SHAFT, POSSIBLY DUE TO INSUFFICENT TORQUE ON RETAINING NUT OR SELF LOCKING ABILITY OF NUT WAS NOT SUFFICENT. SERVICEABLE ALTERNATOR INSTALLED1H71 3O3  ORT3A21    E5CE    5  CP47GL    
20070711001552007071100155EA  2007       7          11         CA070607003      220070511G853005K21108        CYLINDER                                PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1279                               L896061A                    (CAN) DURING A VISUAL INSPECTION OF THE ENGINE, A CRACK WAS FOUND UNDERNEATH THE PUSHROD TUBE.  THE CRACK WAS RUNNING FROM THE BASE OF THE CYLINDER HEAD ALONG THE BOTTOM OF THE COOLING FINS TOWARDS THE HEAD. THE CRACK IS SIMILAR TO THAT FROM SDR 20070423005. (TC NR 20070607003)                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070711001562007071100156EA  2007       7          11         CA070607004      220070515G853005K21108        CYLINDER                                PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1744                               RL145668A                   (CAN) WHILE INSPECTING THE ENGINE, A CRACK WAS FOUND IN THE PUSHROD TUBE AREA OF THE NR 2 CYLINDER.  IT WAS AT THE BASE OF THE COOLING FINS AND RAN FROM THE BOTTOM OF THE CYLINDER HEAD TOWARDS THE TOP OF THE CYLINDER.  THE CRACK STARTS WHERE THE CYLINDER HEAD IS ATTACHED TO THE BARREL.  THIS IS SIMILAR TO THE EVENTS IN SDR`S 20070607003 AND 20070423005.   (TC NR 20070607004)                                                                                                                                                                                                                                                                                                                                                       1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070711001582007071100158GL  2007       7          11         CA070607005      120070528G8011AN33711         RELAY                                   DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985*       52008NE  HARTZLHCB3R HCB3R304    GL  STARTER         FAILED          W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                                                      (CAN) JUST AFTER TAKEOFF, PILOT NOTICED FAINT SMOKE ODOR BUT UNSURE OF SOURCE, CONTINUED.  DURING CLIMB WHITE SMOKE CAME IN AROUND RUDDER PEDALS SO PILOT SHUTDOWN ELECTRICS AND PROCEEDED TO LAND AIRCRAFT.  AFTER LANDING PILOT NOTICED SMOKE COMING FROM THE ACCESSORY SECTION BUT IT DIMINISHED RAPIDLY AND THERE WERE NO SIGNS OF FIRE. UPON FURTHER INSPECTION BY MAINTENANCE STAFF, THE STARTER (PN 756-21C) SHOWED SIGNS OF OVERHEATING AND WAS REPLACED.  THE STARTER RELAY (PN AN3371-1) WAS ALSO REPLACED.  UPON EVALUATION OF THE RELAY THE FOLLOWING WAS NOTED: CLOSE AT 5 VDC OPEN AT 0 VDC TESTED COIL RESISTANCE 9.1 OHMS OILY UNDER COVER, SCREWS AND GASKETS CONTACT A1 SHOWS SIGNS OF RECENT STICKING CONTACT SHOWS ARCING AR1H71 3R3  RRCA806    5E1     5  CP28EA    
20070810000982007081000098CE  2007       8          10         CA070607006      120070606G5100AE366372460330  HOSE                                    CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  UNKNOWN         LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      CA       1    1                                                         (CAN) HOSE PN-AE366372460330 REPLACED DUE TO SHEDULED MAINTENANCE AND LEAK CHECKED SERVICEABLE, AFTER 1.4 HRS AND 4 CYCLES FOUND LEAKING DURING GROUND HANDLING. HOSE REPLACED AND LEAK CHECKED SERVICEABLE (TC NR 20070607006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20070810000992007081000099CE  2007       8          10         CA070607008      120070607G3230MS2124010C40    UPLOCK ROLLER                           CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              MLG             WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CAMPAIGN NOTICE 851-32-40-040 AND 851-32-40-040R1 CARRIED OUT. ACTION WAS REQUIRED TO THE RT MAIN GEAR BEARING P/N MS21240-10C40. THE INSIDE BEARING MATERIAL WHEN INSPECTED WAS FOUND TO HAVE PIECES MISSING AND FURTHER INSPECTION REVEALED THE REMAINDER OF THE LINER WAS EASY TO REMOVE BY HAND. THERE WAS NO DAMAGE FOUND ON THE INNER SLEEVE OR ON THE BOLT. PRIOR TO DISASSEMBLY THE ROLLERS WERE INSPECTED IN SITU AND FOUND TO TURN WITH VERY LITTLE EFFORT REQUIRED. NEW BEARING WAS INSTALLED (TC NR 20070607008)                                                                                                                                                                                                              1L72 4F4  F  A22CE   E1NE                 
20070711001592007071100159NE  2007       7          11         CA070607009      320070604G6111E10950PK        BLADE           HARTZL                  BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       8796       HJ448                                               (CAN) DURING ROUTINE MAINTENANCE, THE LT PROPELLER BLADE NR 1 WAS FOUND CRACKED. THE CRACK RAN CHORD WISE APPROXIMATELY 2.3750 INCH FROM THE BLADE ROOT WITH A LENGTH OF APPROXIMATELY 1 INCH. THE PROPELLER HAS BEEN REPLACED AND WILL BE SENT FOR REPAIR AS WELL AS A STRIP REPORT. (TC NR20070607009)                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20070711001612007071100161NM  2007       7          11         CA070607010      120070607G2910012152130010    LINE                                    BOEING777   777*        UTILUSENM                                                               HYD SYSTEM      LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) ON TRAINING FLIGHT RT HYDRAULIC QUANTITY REDUCED. HYDRAULIC LEAK FOUND IN RIGHT ENGINE PYLON AREA. HYDRAULIC SUPPLY PIPE FOUND LEAKING AT FLEXIBLE AREA, THIS FLEXIBLE AREA IS COVERED BY A RUBBER SHEATH.  PEN INDICATES AREA FLUID WAS LEAKING FROM (TC NR 20070607010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F    RTT00001SE                     
20070810001002007081000100EA  2007       8          10         CA070607011      120070606G2750601R930507      FCU                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) (FLAPS FAIL) MESSAGE DISPLAYED ON APPROACH.  FLAPS FAILED WHEN SELECTING FROM FLAP 20 DEGREES TO FLAPS 30 DEGREES.  FLAPS REMAINED AT 20 DEGREES AT A SPEED OF 170 KIAS.  MAINTENANCE REPLACED FECU (FLAPS ELECTRONIC CONTROL UNIT) DUE TO UNABLE TO TEST AND THE LT BPSU (BRAKE POWER SENSOR UNIT) P/N 8550100-9, S/N 372. AIRFRAME HOURS: 24818:12 CYCLES: 20440. (TC NR 20070607011)                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA21EA   E15NE                
20070810001012007081000101CE  2007       8          10         CA070607012      120070517G27304527301000U1    DISCONNECT UNIT                         LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              ELEVATOR        WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2400 2400                                                      (CAN) WHEN AIRCRAFT WAS DOWN FOR A 2400 HR INSPECTION, IT WAS DISCOVERED THAT THERE WAS PLAY BETWEEN THE LT AND RT ELEVATOR (INSPECTION IRN D2730007).  AN ELEVATOR FREE-PLAY CHECK WAS C/W AND ELEVATORS WERE FOUND TO BE OUT OF LIMITS.  ELEVATOR CONTROL SYSTEM T/S AND FREE PLAY FOUND IN THE AFT ELEVATOR DISCONNECT.  PART REPLACED, FREE-PLAY RE-CHECKED AND FOUND TO BE WITHIN LIMITS. (TC NR 20070607012)                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTT00008WIE6WE                 
20080306000442008030600044CE  2008       3          6          CA070608001      120070606G5510115620010101    STRUCTURE                               BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  HORIZONTAL STAB CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       11730                                                          (CAN) CRACK FOUND IN STRUCTURE OF HORIZONTAL STAB. CRACK LOCATED AT TRAILING EDGE UPPER SURFACE AT CENTER OF HORIZONTAL STAB. CRACK LENGTH 0.600, CRACK REPAIRED IAW REPAIR DWG SUPPLIED BY MFG AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070608001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070810001022007081000102CE  2007       8          10         CA070608002      120070524G27204555401134011   TORQUE TUBE                             LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              RUDDER          CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2400 2400                                                      (CAN) DURING 2400 HR INSPECTION, SB 45-27-24/ DVI IAW 5-19-00-N2720030, CORROSION WAS FOUND INSIDE OF RUDDER TORQUE TUBE.  TORQUE TUBE WAS TO BE REPLACED IAW SB45-27-25.  WHEN TORQUE TUBE KIT ARRIVED, IT WAS DISCOVERED THAT THE REPLACEMENT TORQUE TUBE WAS MANUFACTURED INCORRECTLY.  A SECOND KIT WAS ORDERED AND IT TOO WAS INCORRECT.  ORIGINAL TORQUE TUBE CORROSION CLEANED AND REINSTALLED. (TC NR 20070608002)                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTT00008WIE6WE                 
20070810001032007081000103CE  2007       8          10         CA070608003      120070524G5741                ATTACH FITTING                          LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              WING TO BODY    WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2400 2400                                                      (CAN) DURING 2400 HR INSPECTION, IT WAS DISCOVERED THAT A NR OF THE WING TO FUSELAGE LINKS HAD WORN PAINT OFF THE ATTACH FITTINGS.  ALL AFFECTED FITTINGS AND LINKS INSPECTED.  NO DAMAGE FOUND.  MFG ADVISED OF FINDINGS.  MFG FOLLOWED UP WITH A LETTER OF APPROVAL TO INSTALL PHENOLIC SPACERS BETWEEN ALL LINKS AND FITTINGS. (TC NR 20070608003)                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTT00008WIE6WE                 
20070711001632007071100163CE  2007       7          11         CA070608004      120070524G6100                UNKNOWN         MCAULY      1A103       CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       8656 2793  SR774449                                            (CAN) PROPELLER RECEIVED FOR INSPECTION IAW AD 2003-12-05. INSPECTION FOUND CRACK INDICATIONS IN PREVIOUSLY REPAIRED AREAS.  PROPELLER HAS BEEN REMOVED FROM SERVICE IAW THIS AD AND ASB 221C. (TC NR 20070608004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A19    E223    5  NP50GL    
             20081104         2008       11         4          CA070608005      420070608G2562E01             ELT                                     CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA  MCAULY1C160 1C160DTM    GL                  INOPERATIVE     W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) WHEN TESTING ELT FOR THE REQUIREMENT OF CAR 571 APPENDIX G FOUND G SWITCH INOPERATIVE. UNIT BEING RETURNED TO MFG FOR REPAIR. (TC NR 20070608005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  ONT3A12    E274    5  NP910     
20070810001042007081000104EU  2007       8          10         CA070608006      120070606G6220350A31190700    STARFLEX        SNIAS                   SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              MAIN ROTOR HEAD DAMAGED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       2139       M1199                                               (CAN) WHILE WAITING FOR HIS CREW TO RETURN, THE PILOT NOTICED SOME BLACK SOOT AROUND ONE OF THE STARFLEX ARMS. FURTHER EXAMINATION REVEALED THAT THE STAINLESS STEEL BUSHING BONDED ON THE END OF THE STARFLEX ARM HAD COME LOOSE AND WAS FLOATING INSIDE THE SPHERICAL BEARING IN THE FREQUENCY ADAPTER. THE BUSHING WAS IN GOOD CONDITION THAT MORNING BEFORE THE FLIGHT AND NO UNUSUAL NOISES OR VIBRATIONS WERE DETECTED PRIOR TO DISCOVERING THE DAMAGED STARFLEX. THE PILOT AND CREW HAD TO BE FLOWN OUT OF THE BUSH WITH ANOTHER HELICOPTER. A NEW STARFLEX WAS INSTALLED ON SITE THE NEXT DAY WITH NO FURTHER ISSUES. (TC NR 20070608006)                                                                                               1G71 3U3  U  H9EU    E19EU                
20070711001672007071100167NM  2007       7          11         CA070608007      120070604G290010607102        BYPASS VALVE                            BOEING727   727233      138408ANM  PWA   JT8   JT8D15      52051NE                              HYD SYSTEM      FAILED          W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) ON ARRIVAL, THE IB FLAPS FAILED TO EXTEND WHEN LANDING, CONFIGURATION SELECTED. THE CREW ELECTED TO DIVERT. THE AIRCRAFT COMPLETED A NORMAL LANDING. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM AND INSPECTED THE SYSTEM FOR LEAKS AND ANOMALIES. THE FLAP POSITION INDICATOR WAS REPLACED AS PRECAUTION AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE AIRCRAFT SUBSEQUENTLY REPOSITIONED WITHOUT FURTHER PROBLEM. HOWEVER DURING DEPARTURE THE CREW OBSERVED LOW HYDRAULIC QUANTITY ON THE A SYSTEM AFTER SELECTING GEAR AND FLAPS UP. THE AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED A FAILED IB FLAP BYPASS VALVE.  BOTH A SYSTEM PUMPS AND THE RESPECTIVE CASE DRAIN FILTERS WERE REPLACED NO CON2L73 4F4  FRTA3WE    E2EA                 
20070711001692007071100169EU  2007       7          11         CA070608008      120070606G2730                CONTROL CABLE                           FOKKERF28   F28MK0100   4990807EU  RROYCETAY   TAYMK65015       EU                              ELEVATOR        BROKEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA                                                                      (CAN)  FLIGHT CREW REPORTED DURING HEAD START CHECKS THAT THE FLIGHT CONTROL LOCK WOULD NOT LOCK THE ELEVATOR CONTROLS AND WAS VERY STIFF WHEN MOVING CONTROL LOCK TO FREE POSITION.  RECERTIFICATION, FOUND THE FLIGHT CONTROL LOCK CABLE FCL1 SNAPPED AT AILERON FLIGHT CONTROL LOCK PULLEY.  CABLE REPLACED AND ADJUSTMENT COMPLETED.  OPERATIONAL TEST OF FLIGHT CONTROL LOCK SYSTEM COMPLETED.  FOLLOW UP ACTION THE CABLE BROKE AT AN IDLER PULLEY AND APPEARED TO HAVE BEEN POSSIBLE FRAYED. ENTIRE ELEVATOR CONTROL LOCK CABLE RUN INSPECTED AND FOUND SERVICEABLE.  IN FOLLOW UP A SPECIAL INSPECTION WILL BE ISSUED FOR AIRCRAFT TO INSPECT THE SAME AREA. (TC NR 20070608008)                                                        2L72 4F4  FRT                             
20070711001702007071100170NE  2007       7          11         CA070608009      220070607G7310D22AA1022       VALVE                                   AIRBUSA319  A319114     3930350NM  CFMINTCFM56 CFM565A1         NE                              FUEL RETURN     FAILED          W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  DEDESCENT        1                      CA       3007811851                         731901                      (CAN) DUE TO A LT ENGINE STALL MESSAGE ON ECAM, THE FLIGHT CREW SHUTDOWN THE NR 1 ENGINE AS A PRECAUTION.   MAINTENANCE FOUND FUEL RETURN VALVE AT FAULT DURING AN ENGINE MOTORING TEST, UNIT REPLACED IAW AMM 73-11-50. (TC NR 20070608009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA28NM   E29NE                
             20081104         2008       11         4          CA070608010      120070608G6320RG36343         SHAFT                                                                                                                                   GEARBOX PUMP    DAMAGED         W      K   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      CA       1556                                                           (CAN) S 76 MAIN GEARBOX REMOVED FOR GENERATING METAL. TSN 1556.5  THE METAL HAS BEEN SENT OUT FOR ANALYSIS TO ENSURE THAT IT IS THE TYPE CONSISTANT WITH THE DAMAGED PARTS. WE WILL ATTACH THE REPORT WHEN RECEIVED. (TC NR 20070608010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  
20070810001052007081000105EU  2007       8          10         CA070611001      120070608G28229638411403      PUMP                                    PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  FUEL BOOST      MALFUNCTIONED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            697                                                       (CAN) WHILE PERFORMING A DEFUEL OF AIRCRAFT TO PERFORM SCHEDULED MAINTENANCE, RT WING FUEL BOOST PUMP POPPED CIRCUIT BREAKER AFTER 3 MINUTES OF OPERATION DEFUELING AIRCRAFT.  PUMP WAS ALLOWED TO SIT FOR 10 MINUTES AND C/B RESET AND PUMP WOULD AGAIN WORK FOR 3 MINUTES. THIS HAPPENED 3 TIMES UNTIL DEFUEL WAS COMPLETE.  PUMP WAS REPLACED WITH O/H UNIT.  TESTED SATISFACTORY (TC NR 20070611001)                                                                                                                                                                                                                                                                                                                                        1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070711001742007071100174NM  2007       7          11         CA070611002      120070610G3244DR0231T         TIRE                                    BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NR 4            FAILED          W      C   ABORTED TAKEOFF                                                                                 E  VIBRATION/BUFFET                                                              TOTAKEOFF        1                      CA                                                                      (CAN) DURING A NORMAL AND SMOOTH TAKEOFF ROLL, CREW NOTICE A VIBRATION (120KNTS,V1=134KNTS).  AT VR ROTATED INTO SMOOTH CLIMB AND REQUESTED GEAR UP WITH POSITIVE CLIMB.  SHORTLY AFTERWARDS CABIN CREW CALLED TO SAY PASSENGERS REPORTED A WHEEL CAME OFF DURING TAKEOFF.  AIRCRAFT COMPLETED AN UNEVENTFUL LANDING.  NR 4 MAINWHEEL TIRE WAS FOUND SHREDDED WITH MAINWHEEL ASSY STILL IN PLACE. (TC NR 20070611002)                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070810001062007081000106EU  2007       8          10         CA070612001      120070529G3233                SWITCH                                  PILATSPC12  PC1245      7090551EU  GARRTTTPE331TPE33112UHR      WP  ROTOL R333  R333482F12  GL  MLG ACTUATOR    MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA                  0623E                                               (CAN) CREW REPORTED THE LT MAIN LANDING GEAR DOWN AND LOCK INDICATION WAS SHOWING (IN TRANSIT) WHEN SELECTED DOWN.  THE SYSTEM WAS TROUBLESHOT TO THE DOWNLOCK INDICATOR SWITCH IN THE GEAR ACTUATOR.  ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERVICE.  (TC NR 20070612001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3T4  TRTA78EU   E4WE    6  CP61GL    
20070711001752007071100175NM  2007       7          11         CA070612002      120070611G323282970014009     ACTUATOR                                DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  RT MLG DOOR     BYPASSING       W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA       4448044480                                                     (CAN) ON LANDING, GEAR DOWN SELECTION HEARD LOUD CLUNK, AND RT MAIN GEAR UNSAFE WARNING. CYCLED GEAR WITH SAME RESULT.  ALTERNATE GEAR EXTENSION ACTIVATED, ALL GEAR INDICATED DOWN, NORMAL LANDING.  MAINTENANCE INSPECTION FOUND RT AFT GEAR DOOR ACTUATOR SLOW TO OPEN DOORS DUE TO INTERNAL PRESSURE BYPASSING.  RT AFT GEAR DOOR ACTUATOR REPLACED, LEAK AND FUNCTION CHECKS COMPLETED.  AIRCRAFT RETURNED TO SERVICE. (TC NR 20070612002)                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070711001762007071100176NM  2007       7          11         CA070612003      120070601G2421                BRUSHES                                 ROBSINR22   R22BETA     7640110NM  LYC   O360  O360J2A     41514EA                              ALTERNATOR      LOOSE           W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       215                                                            (CAN) ON BACK OF ALTERNATOR, POWER-OUT STUD FOUND LOOSE AND NYLON BUSHING FOUND MELTED. WIRE TERMINAL WAS FOUND MELTED AND BROKEN.  PROBLEM HAS SINCE BEEN DETECTED ON TWO OTHER AIRCRAFT. (TC NR 20070612003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3O3  O  H10WE   E286                 
20070810001072007081000107SW  2007       8          10         CA070612004      120070612G6310269A5512        DRIVE BELT                              HUGHES269   269C1       8059504SW  LYC   O360  HO360C1A    41514EA                              MAIN ROTOR      SPLIT           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       59                                                             (CAN) DRIVE BELT AXIAL SPLIT OVER 50 PERCENT OF BELT CIRCUMFERENCE; SPLIT OCCURS UNDER OUTER LAYER OF BELT.   NOTE:  PLEASE ADVISE IF PHYSICAL VERIFICATION IS REQUIRED AS MUST RETURN BELTS TO MFR FOR WARRANTY CONSIDERATION. (TC NR 20070612004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3O3  OO 4H12    E286                 
20070712001302007071200130GL  2007       7          12         CA070612005      220070610G725023034787        BEARING                                 BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              ENGINE          FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       534  534                                                       (CAN) FOUND METAL ON BOTH CHIP PLUGS AND THEN FOUND THAT THE 2.5 BEARING HAD STARTED TO FAIL.  REPLACED BEARING AND INNER RACE OF SPUR ADAPTER. NO FURTHER PROBLEMS. (TC NR 20070612005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3U3  U  H2SW    E4CE                 
20070712001312007071200131EU  2007       7          12         CA070613001      220070612G7270JR21756A        DUCT                                                                       RROYCESPEY  SPEY55515P  54521EU                              ENGINE BYPASS   MISREPAIRED     W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       147162950                                                      (CAN) ENGINE FRONT BYPASS DUCT FOUND AT INSPECTION WITH NON STANDARD REPAIR OUTSIDE OEM LIMITATION. PATCH REPAIR ON OUTSIDE WALL 8 INCH LONG BY 2.5 INCH WIDE OUTSIDE SCOPE OF XRS3025. PART REJECTED AND REMOVED FROM ENGINE.  (TC NR 20070613001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    4  F          E2EU                 
20070711001772007071100177EA  2007       7          11         CA070613002      120070613G281021564002        FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  RT WING         LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    NRNOT REPORTED   1                      CA       1803                                                           (CAN) FUEL LEAK SUSPECTED ON RT WING.  RT FUEL CELL NR 6 HAS BEEN FOUND LEAKING AFTER INVESTIGATION AND REPLACED.  DROPS  9050 (TC NR 20070613002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
             20081104     CE  2008       11         4          CA070613003      120070612G8011MMU4001R        STARTER                                 CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  SNSNCH72C   72CK        EA                  SHORTED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            421                                                       (CAN) STUDENT TRIED TO START ENGINE THE STARTER WOULD NOT ENGAGE. AIRCRAFT BROUGHT INTO HANGAR AND COWLS REMOVED. AME TRIED TO ENGAGE STARTER IN THE SHOP BUT IT WOULD NOT ENGAGE. WHEN HE CHECKED THE STARTER IT WAS VERY HOT AND THERE WAS SOME SMOKE COMING OUT OF IT. STARTER REMOVED AND SENT BACK FOR WARRANTY REPLACMENT.                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A19    E223    5  NP9045    
             20081104     GL  2008       11         4          CA070613004      120070611G2497AN316010        CIRCUIT BREAKER                         DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN3     52008NE  HARTZLHCB3R HCB3R304    GL                  FAILED          W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) WHILE TROUBLESHOOTING A U/S TAIL NAV LIGHT AND REPLACING A CORRODED KNIFE CONNECTOR AT THE TAILCONE, POWER WIRE TO THE LIGHT ASSEMBLY OVERHEATED AND MELTED, FILLING THE CABIN WITH SMOKE. PWR WAS DISCONNECTED AND SMOKE DISSIPATED. FURTHER INVESTIGATION REVEALED THAT NAV LIGHT SOCKET HAD CORROSION BUILDUP ON THE WIRING TERMINALS THAT HAD SHORTED THE SOCKET TO GROUND. PWR LIRE MELTED FROM THE SOCKET BACK TO CIRCUIT BREAKER, AND FROM THERE TO MAIN BUS. INVESTIGATION WAS THEN CENTERED ON THE CIRCUIT BREAKER WHICH HAD NOT TRIPPED. BREAKER WAS FOUND TO BE A 10 AMP BREAKER AND NOT THE 5 AMP UNIT LISTED IN THE ACFT MANUAL. A FUNCTION CHECK OF THE BREAKER REVEALED THAT IT WOULD NOT TRIP AT ALL.  AN APPROPRIATELY RA1H71 3R3  RRCA806    5E1     5  CP28EA    
20070810001082007081000108SW  2007       8          10         CA070614001      120070608G6310269A5512        DRIVE BELT                              HUGHES269   269C1       8059504SW  LYC   O360  HIO360*     41514EA                              MAIN ROTOR      SPLIT           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       177                                                            (CAN) DRIVE BELT AXIAL SPLIT OVER 50 PERCENT OF BELT CIRCUMFERENCE; SPLIT OCCURS UNDER OUTER LAYER OF BELT. DEFECT HAS BEEN FOUND ON (2) OTHER AIRCRAFT OF THE SAME TYPE.  NOTE:  PLEASE ADVISE IF PHYSICAL INSPECTION IS REQUIRED AS MUST RETURN BELTS TO MANUFACTURER FOR WARRANTY CONSIDERATION. (TC NR 20070614001)                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3O3  OO 4H12    1E10                 
20080319001432008031900143SO  2008       3          19         CA070614002      120070604G7810LW15849         EXHAUST STACK                           PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  RT ENGINE       SEPARATED       W      D   RETURN TO BLOCK                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                                          L258765A                    (CAN) PRIOR TO DEPARTURE, ENGINE RUN-UP PILOT REPORTED THAT RT ENGINE RUNNING ROUGH. ENGINE ONLY PRODUCING 30" MP AND MAX 2250 RPM, AT GPH FF. RT MAG DROP WAS EXCESSIVE. MAINT INVESTIGATION FOUND ENGINE RT EXHAUST SEGMENT P/N LW-15849 SEPARATED FROM NR 5 EXHAUST STACK PIPE PN LW-10161 AT THE SLIP JOINT. NEW EXHAUST SEGMENTS INSTALLED AND ENGINE OPERATION CHECKED SERVICEABLE. NO VISIBLE HEAT DAMAGE NOTED TO AREA WIRING OR COMPONENTS. SLIGHT DISTORTION NOTED TO SOME AREA HOSE SUPPORT WRAPPING. NOTE: THIS ENG WAS RECENTLY INSTALLED AND HAD ACCUMULATED 2.2 HRS SINCE INSTALLATION. THE ORIGINAL EXHAUST SEGMENTS FROM THE REMOVED ENGINE WERE INSTALLED. NO DEFINITIVE CAUSE FOR THE SEPARATION HAS BEEN DETERMINED. SUSPECT1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070711001782007071100178SW  2007       7          11         CA070614003      120070613G29102781032682      LINE                                    SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  HYD SYSTEM      CRACKED         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  LDLANDING        1                      CA                                                                      (CAN) CREW NOTICED A LARGE PUDDLE OF HYDRAULIC FLUID COMING FROM THE NOSE WHEEL WELL AREA.  DETERMINED TO BE A CRACKED LINE ON A BEND RADIUS, WHICH WAS THE SUPPLY LINE TO THE NWS SYSTEM.  THE SYSTEM WAS DISABLED AND PLACED ON AN MEL DEFERRAL, CLEANED AND LEAK TESTED, SERVICEABLE.  AWAITING PARTS FOR REPAIR. (TC NR 20070614003)                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4T4  TRTA8SW    E4WE    5  CP10NE    
20070717000112007071700011NM  2007       7          17         CA070614004      120070511G2497                CONNECTOR                               DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  AC POWER MONITORBURNED          W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA                  552                                                 (CAN) UPON GETTING IN A/C DISCOVERED AC POWER C/B`S POPPED UPON  EXTERNAL PLUGGED INTO A/C ASSUME POPPED WHEN GSE PLUGGED IN PILOT ENTERED COCKPIT AND PUSHED ALL BREAKERS IN ON WALK AROUND  EXITING A/C AND DOING WALKAROUND WENT BACK TO COCKPIT AND DISCOVERED SMOKE REMOVED POWER FROM A/C AND CALL MAINTENANCE UPON REMOVAL OF AC POWER MONITOR DISCOVERED BURNED CONNECTOR ON INDICATOR AND CONNECTOR, CONNECTOR AND INDICATOR /MONITOR REPLACED WITH NO FURTHER ISSUES.                                                                                                                                                                                                                                                                 2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070711001792007071100179NE  2007       7          11         CA070614005      220070307G7250MS955608        BOLT                                    CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              GAS GENERATOR   LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4400                                                           (CAN) DURING SCHEDULED MAINTENANCE ACTIVITIES, 3 OF THE MS9556-08 BOLTS LOCATED AT THE ENGINE GAS GENERATOR TO INTERMEDIATE CASE FLANGE WERE DETERMINED TO BE LOOSE. AN ADDITIONAL BOLT WAS FOUND TO BE COMPLETELY MISSING.  MFG WILL INVESTIGATE AND ADVISE ON ROOT CAUSE AND REMEDIAL MAINTENANCE ACTIONS. (TC NR 20070614005)                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA22CE   E00059EN             
20070711002792007071100279NM  2007       7          11         CA070615001      120070612G243523088008        GENERATOR                               DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  NR 1            INTERMITTENT    W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA       2594                                                           (CAN) AFTER SEVERAL SECTORS WITH INTERMITTENT NR 1 DC GEN PROBLEMS, CREW REPORTED ILLUMINATION OF DC BUS CAUTION LIGHT PLUS SEVERAL OTHER CAUTIONS: AUX INV, NR 1 DC GEN, RUD FULL PRESS, NR 2 RUD HYD, EPWS.  THE QRH WAS ACTIONED BUT THEY WERE NOT ABLE TO RESTORE THE LOST BUSES. THE NR 1 DC GENERATOR WAS REPLACED AND THE SYSTEM TESTED NORMALLY. ON REMOVAL FROM THE A/C, THE DC GENERATOR WAS NOTED TO HAVE SIGNIFICANT DAMAGE WITH SEVERAL LARGE METALLIC (CHUNKS) DROPPING OUT. (TC NR 20070615001)                                                                                                                                                                                                                                  2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070810001092007081000109NM  2007       8          10         CA070615002      120070606G6310A1902           DRIVE BELT                              ROBSINR22   R22BETA     7640110NM  LYC   O360  O360J2A     41514EA                              MAIN ROTOR      SEPARATED       W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA       38                                                             (CAN) BELTS WERE REPLACED AT 2200HR OVERHAUL AND AFTER 38 HRS IN SERVICE WERE FOUND SEPARATED IN A SECTION ABOUT 2 INCHES LONG. (TC NR 20070615002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3O3  O  H10WE   E286                 
20070711002782007071100278    2007       7          11         CA070615003      120070613G3230622800200       SWITCH                                  BAG                                GARRTTTPE331TPE33110UG  01514WP  MCAULY4HFR344HFR34C652  NE  MLG             FAILED          W      O   OTHER                                                                                           L  NO TEST                                                                       APAPPROACH       1                      CA                                                                      (CAN) DURING APPROACH, THE CREW EXPERIENCED A LANDING GEAR FAILURE AND OBSERVED THE CIRCUIT BREAKER HAD POPPED. THEY PROCEEDED WITH AN EMERGENCY LANDING GEAR EXTENSION AND LANDED WITHOUT INCIDENT. THE FAULT WAS TRACED TO THE LT UPLOCK MICROSWITCH. WHEN THE MICROSWITCH WAS ACTIVATED THE FAULT DISAPPEARED AND WAS UNABLE TO BE RE-CREATED. THE SWITCH WAS REPLACED. (TC NR 20070615003)                                                                                                                                                                                                                                                                                                                                                         4  T          E4WE    6  C3PNE     
20070711002762007071100276EU  2007       7          11         CA070615004      120070613G3220A1026EAND9E     BOLT                                    BAG   JETSTMJETSTM3101  1500215EU  GARRTTTPE331TPE33110UG  01514WP  ROTOL R333  R333482F12  GL  NLG             FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) SCHEDULE INSPECTION AD UK 024-05-87 / SB53A-JA870510R1, WE NOTICE THE 2 UPPER BOLT OF THE NLG JACK MOUNTING BRACKET WERE SHEARED AND THE 2 LOWER ONES WERE LOOSE.  ACCOMPLISHED PART A OF THE SB C/OUT(ALL 4 BOLTS AND NUTS REPLACED), PARTS INSPECTED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070615004)                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4T4  TRTA21EU   E4WE    6  CP61GL    
20070810001102007081000110    2007       8          10         CA070615005      420070613G2350M1035CHKFJLJ2   AUDIO CONTROL                           SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE3311     01514WP  MCAULY4HFR344HFR34C652  NE                  STICKING        W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) BUTTONS HAVE TO BE PRESSED NUMEROUS TIMES BEFORE THEY ENGAGE, REPLACED UNIT.   (TC NR 20070615005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4T3  TRTA8SW    E3WE    6  C3PNE     
20080319001462008031900146    2008       3          19         CA070615006      420070613G2300M1035CHKFJLJ2   AUDIO CONTROL                           SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE331*     01514WP  MCAULY4HFR344HFR34C652  NE  COCKPIT         STICKING        W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) BUTTONS HAVE TO BE PRESSED NUMEROUS TIMES BEFORE THEY ENGAGE, REPLACED UNIT (TC NR 20070615006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4T3  TRTA8SW    E2WE    6  C3PNE     
20070711001802007071100180WP  2007       7          11         CA070616001      220070527G7200                ENGINE                                  RAYTHNDH125 HAWKER800XP 7150012CE  GARRTTTFE731TFE7315BR        WP                              LEFT            MAKING METAL    W      A   UNSCHED LANDING                                                                                 BE SMOKE/FUMES/ODORS/SPARKS  VIBRATION/BUFFET                                    CRCRUISE         1                      CA                                          P107188                     (CAN) DURING CRUISE, CREW NOTED ODOR IN CABIN AND VIBRATION, AND EXECUTED PRECAUTIONARY LANDING.  LT ENGINE HAD HIGH VIBRATION ON LOW POWER GROUND RUN, ENGINE OIL FILTER WAS HEAVILY CONTAMINATED WITH BOTH FERROUS AND NON-FERROUS MATERIAL, ENGINE WAS REMOVED FOR REPAIR, SUSPECT BEARING AND/OR CARBON SEAL FAILURE, TEARDOWN REPORT PENDING. (TC NR 20070616001)                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA3EU    E6WE                 
20070810001112007081000111CE  2007       8          10         CA070618001      120070617G3210MS2124010C40    BEARING                                 CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              MLG             WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THIS SDR IS BEING SUBMITTED TO SATISFY THE REQUIREMENT OF AIRCRAFT SERVICES DIRECTORATE CAMPAIGN NOTICE CN-1 851-32-40-040R1 THE INTERNAL TEFLON MATERIAL OF THE BEARING HAD DETERIORATED CAUSING THE BEARING TO BE DIFFICULT TO ROTATE. (TC NR 20070618001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 4F4  F  A22CE   E1NE                 
20070711001812007071100181EA  2007       7          11         CA070618002      220070606G8520                CRANKSHAFT                              PIPER PA28  PA28140     7102802SO  LYC   O320  O320E2A     41508EA  SNSNCH74D   74DM        EA  ENGINE          CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2746 2746                                                      (CAN) ENGINE CONVERTED TO 160 HP IAW STC SE367CH.  ENGINE NOW SIMILAR TO O-320-D2A.  CRANKSHAFT INSPECTED IAW AD 98-02-08.  PITTED FOUND, NO CRACKS. (TC NR 20070618002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L71 3O3  O  2A13    E274    5  NP88614   
20070810001122007081000112SW  2007       8          10         CA070618003      120070616G275220619502        ACTUATOR                                AIRTRCAT802 AT802A      0390308SW  PWA   PT6   PT6A67A     52043NE  HARTZLHCB5M HCB5MA3     GL  TE FLAP         FAILED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       616                                                            (CAN) DURING APPROACH FOR A SCOOPING OPERATION, THE FLAPS WOULD NOT EXTEND WITH AN AIR LOAD.  THE AIRCRAFT RETURNED TO BASE.  UPON INVESTIGATION BY MAINTENANCE STAFF,  FLAPS WOULD EXTEND THE FIRST 10 DEGREES WITH NO AIR LOAD AND THE ACTUATOR MADE A GRINDING NOISE.  THE FLAP ACTUATOR WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC 20070618003)                                                                                                                                                                                                                                                                                                                                                                             1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20070810001132007081000113EA  2007       8          10         CA070618004      120070613G2897MS312183P       CONNECTOR                               CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              AUX TANK        MISINSTALLED    W      O   OTHER                                                                                           W  INADEQUATE Q C                                                                NRNOT REPORTED   1                      CA                                                                      (CAN) ON PATS RT AUXILARY TANK FOUND THE PRESSURE DIFFERENTIAL SWITCH, THE SOCKET OF THE SWITCH AND THE ELECTRICAL HARNESS CONNECTOR HAVING BOTH PINS, THE CONNECTOR SHOULD BE A FEMALE TYPE. THE DIFFERENTIAL SWITCH IS WORKING ONLY ON GROUND DURING FUELING. FOUND ALSO THAT THE SYSTEM IS WORKING BECAUSE THAT THE PINS ARE CONTACTING EACH OTHER. PATS THE STC HOLDER ADVISED AND A SB IS ALREADY OUT (TC NR 20070618004)                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA21EA   E15NE                
20070810001142007081000114CE  2007       8          10         CA070618005      120070504G7603509440767       POWER LEVER                             BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  LT ENGINE       WORN            W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) FLIGHT SNAG REPORTED - (LT ENGINE REMAINS AT HIGH IDLE AT LOW IDLE SETTINGS).  MAINTENANCE FOUND THE AIRFRAME POWER LEVER ARM AT THE REVERSING CAM GROUND PIN HEAD JUMPED THE SPLINE, CAUSING THE SHOULDERED PIN TO HOLD THE FCU INTERCONNECT ARM FROM RESETTING TO GROUND IDLE.THE ARM WAS RE-ADJUSTED AND IS ASSUMED WORN OUT INTERNALLY. AS A PRECAUTION ALL THROTTLE ARMS WERE REPLACED. (TC NR 20070618005)                                                                                                                                                                                                                                                                                                                          1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070711001822007071100182EA  2007       7          11         CA070618007      220070618G7297311792401       WIRE HARNESS                                                               PWA   PT6   PT6A27      52043EA                              ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ACCESSORIES SERVICES PLANT 2.  DURING BENCH CHECKING ACTIVITIES THE PART WAS EXHIBITING AN UNKNOWN CONFIGURATION. UNABLE TO DETERMINE THE MANUFACTURING SOURCE.  THE PART WAS REPLACED WITH GENUINE PART. THIS PART WILL BE KEPT FOR 1 MONTH FOR EXAMINATION. (TC NR 20070618007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                4  T          E4EA                 
20070810001152007081000115EA  2007       8          10         CA070618008      120070617G3213492009          AXLE                                    CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF34*            NE                              LT MLG          BROKEN          W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       4513                                                           (CAN) REPORTED A FRACTURED LT IB MLG AXLE (NR 2) ON A/C, LT SHOCK STRUT ASSY HAS P/N 49200-9 WITH SPP0049 WITH CURRENTLY. EFFECTED SUBASSY PISTON/AXLE HAS P/N 49263-1 WITH S/N BA0066 AND IS ORIGINALLY INSTALLED ON A/C SINCE DELIVERY. RT SHOCK STRUT ASSY HAS P/N 49200-10 WITH S/N SPP0097 AND SUBASSY PISTON AXLE ASSY WITH P/N 49263-1 AND S/N BA0111 AND BOTH HAVE TAC=7763 (ORIGINALLY INSTALLED SINCE DELIVERY). (TC NR 20070618008)                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA21EA   E15NE                
20070810001162007081000116EA  2007       8          10         CA070618009      120070615G2820                O-RING                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              FUEL SYSTEM     LEAKING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) DURING FLIGHT, ENROUTE,  THE CREW OBSERVED A RT FUEL LOW PRESS MESSAGE ON EICAS FOLLOWED BY FUEL IMBALANCE.  AT 1000 LB FUEL DIFFERENTIAL BETWEEN TANKS, THE QRH PROCEDURE FOR FUEL IMBALANCE WAS INITIATED. AS A RESULT, THE RT ENGINE WAS SHUTDOWN.  THE AIRCRAFT DIVERTED.  AN EMERGENCY WAS DECLARED AND GROUND EMER EQUIP WAS ON STANDBY.  THE AIRCRAFT LANDED WITHOUT FURTHER EVENT.  MAINT FOUND A CLAMP FOR THE FUEL FEED LINE FROM THE RT COLLECTOR TANK WAS NOT PROPERLY ATTACHED.  THE CLAMP HAD SHIFTED SUFFICIENT TO ALLOW A MISALIGNMENT OF THE FUEL LINES RESULTING IN THE ESCAPE OF FUEL AT THAT LOCATION.  THE ROOT CAUSE FOR THIS IS NOT FULLY ESTABLISHED.  MAINT REPLACED THE COUPLING O-RINGS AND RECONNECTED THE WIG2L72 4F4  FRTA21EA   E15NE                
20070820000392007082000039EA  2007       8          20         CA070618010      120070613G3213492033          AXLE                                    CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF34*            NE                              MLG             SHEARED         W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       956                                                            (CAN) WHILE LOADING, THE PASSENGER AT SLC THE FLIGHT CREW FELT A CERTAIN JOLT . INVESTIGATING THE SOURCE , THE CREW FOUND MLG NR 4 AXLE COMPLETELY SHEARED OFF. MLG NR 4 MLG  AXLE COMPLETELY SHEARED OFF.  (TC NR 20070618010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
             20081104     CE  2008       11         4          CA070619001      120070617G273126616151        ACTUATOR                                CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  ELEVATOR TRIM   BINDING         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       3730 551                                                       (CAN) EXCESSIVE RESISTANCE IN ELEVATOR TRIM REPORTED. RT ELEVATOR TRIM ACTUATOR FOUND TO BE BINDING AND REPLACED WITH OVERHAULED UNIT. ACFT HAS FLOWN WITH NO REOCCURENCE OF THE DEFECT. THE SUBJECT ACTUATOR WAS OVERHAULED AND FITTED IAW THE MAINT SCHEDULE IN JULY 2006. (TC NR 20070619001)                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20070820000402007082000040CE  2007       8          20         CA070619002      120070618G5210504300401       STEP                                    BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  PAX DOOR        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING AN INSP IT WAS NOTICED THAT THE STEP ON THE AIRSTAIR DOOR WAS CRACKED AT THE PIVOT STUD.  THE STEP WAS REMOVED AND A SERVICEABLE STEP WAS INSTALLED. (TC NR 20070619002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070820000412007082000041CE  2007       8          20         CA070619006      120070618G3297                WIRE                                    CESSNA340   340A        2076405CE  CONT  O520  TSIO520NB   17040SO  HARTZLHCC3Y PHCC3YF2    GL  MLG             CUT             W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       2738                                                           (CAN) LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO A FAULTY WIRE TERMINAL CONNECTION BETWEEN THE (GEAR-UP LIMIT SWITCH) AND THE (GEAR MOTOR RELAY). (TC NR 20070619006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3O3  O  3A25    E8CE    5  CP25EA    
20070820000422007082000042NE  2007       8          20         CA070619007      220070611G7321                BOLT                                    SKRSKYS61   S61N        8142104NE  GE    CT58  CT581401    30011NE                              FCU CONNECTION  LOOSE           W      A   UNSCHED LANDING                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) OCCURRENCE WHERE THE ENGINE SPEED CONTROL DISENGAGED FROM THE FUEL CONTROL UNIT, RESULTING IN AN IN-FLIGHT SHUTDOWN OF THE ENGINE. SUSPECTED CAUSE WAS A LOOSE SELF LOCKING BOLT, P/N NK4-4A, AND OR A WORN NON METALLIC LOCKING INSERT ON THE NK4-4A BOLT. IN ORDER TO PREVENT THIS FROM HAPPENING AGAIN, THE MAINTENANCE CREW HAVE BEEN REMINDED TO TAKE CARE WHEN INSTALLING THE SPEED CONTROL WHEN RE-USING THE NK4-4A BOLT TO ENSURE THAT THERE IS THREAD INTERFERENCE.  MM, SA 4045-80, SECTION 20-00, PAGE 5, PARAGRAPH 9 (REUSE OF SELF LOCKING NUTS), SUB-PARAGRAPH C. STATES THAT ALL NUTS MUST BE CHECKED BEFORE RE-USE. THERE MUST BE THREAD INTERFERENCE, SUCH INTERFERENCE INDICATES THAT THE SELF LOCKING FEATURE IS WORKIN2G72 4U4  U  1H15    1E3                  
20070820000432007082000043    2007       8          20         CA070620002      420070322G6122321524          SOLENOID        HAMSTD      4U1827      CNDAIRCL215 CL2151A10   1900320EA  PWA   R2800 CA3         52026NE  HAMSTD43E   43E60       NE  PROP GOVERNOR   INOPERATIVE     W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                  CSP0059                                             (CAN) DURING A TEST FLIGHT, THE NR 1 PROP WAS FEATHERED TO VERIFY CORRECT FUNCTION OF THE SYSTEM. THE FLIGHT CREW WAS UNABLE TO UNFEATHER THE PROPELLER AND RETURNED TO THE AIRPORT.  MAINTENANCE CREWS FUNCTION TESTED THE SYSTEM ON THE GROUND AND THE SYSTEM FUNCTIONED CORRECTLY. THE PROP FEATHERING SOLENOID WAS SUSPECT AND WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070620002)                                                                                                                                                                                                                                                                                                                                          2H72 4R4  RRTA14EA   E231    6  CP871     
20070711001832007071100183NM  2007       7          11         CA070620003      120070607G3150                UNKNOWN                                 BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU                  UNKNOWN         W      H   DEACTIVATE SYST/CIRCUITS                                                                        N  FALSE WARNING                                                                 TXTAXI/GRND HDL  1                      CA       946                                                            (CAN) WHEN REFUELING AIRCRAFT GROUND CREW NOTICED THAT WHEN THE REFUEL PANEL DOOR WAS OPEN THAT THEY HAD LIGHTS ON THE PANEL THAT SHOULD NOT HAVE BEEN ON. (TC NR 20070620003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070820000442007082000044EU  2007       8          20         CA070621001      120070621G6220                BUSHING         UROCOP                  UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              SCISSOR LINK    FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       98                                                             (CAN) FACTORY NON- FIELD REPLACEABLE BUSHING BOND FAILED IN THE SCISSOR LINK, BROKE FREE AND WORE INTO THE SISSOR LINK. EXCESSIVE PLAY AND "SMOKE" WAS EVIDENT. (TC NR 20070621001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G72 3U3  UNCR0001RD E34NE                
20070820000452007082000045CE  2007       8          20         CA070621002      120070616G2910                MOTOR                                   BEECH 76    76          1153005CE  LYC   O360  O360A1G6D        EA  HARTZLHCM2Y HCM2YR      GL  HYD SYSTEM      CONTAMINATED    W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA                                                                      (CAN) DURING APPROACH, PILOTS SELECTED LANDING GEAR DOWN, GEAR MOTOR CIRCUIT BREAKER POPPED AND GEAR WOULD NOT EXTEND. AN EMERGENCY EXTENSION WAS CARRIED OUT SATISFACTORILY.  AFTER RETURN TO BASE MECHANICS FOUND THAT THE HYDRAULIC MOTOR WAS CONTAMINATED WITH HYDRAULIC FLUID WHICH LED TO AN ELECTRICAL SHORT.  FURTHER INSPECTION FOUND THAT THE O-RING WHICH SEPARATES THE RESERVOIR AND THE MOTOR WAS DETERIORATED. MECHANICS FOUND THAT SPARE POWER PACKS IN STORES HAD SIMILAR CONTAMINATION DUE TO FAULTY O-RINGS. THESE SPARE POWER PACKS ARE LAID ON THEIR SIDES WHICH WOULD ALLOW FLUID TO PASS TO THE MOTOR. A FLEET WIDE INSPECTION OF POWER PACKS IN SERVICE IS BEING CARRIED OUT BY THE AMO TO PREVENT FURTHER OCCURRENCES. A1L72 3O3  O  A29CE   E286    5  CP43GL    
20070820000462007082000046CE  2007       8          20         CA070621003      120070620G57111058100237      FRAME                                   BEECH 76    76          1153005CE  LYC   O360  O360A1G6D        EA  HARTZLHCM2Y HCM2YR      GL  RT WING         SEPARATED       W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) DURING TAXI PILOTS FELT THE RT WING DROP SUDDENLY AND HEARD A TIRE SKIDDING SOUND. THEY IMMEDIATELY STOPPED THE AIRCRAFT.  MECHANICS FOUND THE LANDING GEAR A-FRAME HAD BROKEN FREE FROM THE MAIN LANDING GEAR TRUNNION. THE LANDING GEAR DID NOT COLLAPSE BUT ROTATED OB AND CONTACTED THE WING WHEEL WELL SKIN CUTOUT, AFTER THE A-FRAME BECAME DISCONNECTED. THE A-FRAME THAT FAILED HAD BEEN REPLACED WITH AN IMPROVED DESIGN AS REQUIRED BY AD 97-06-10. A FLEET WIDE INSPECTION OF A-FRAMES IN SERVICE ON COMPANY OPERATED AIRCRAFT IS BEING CONDUCTED BY THE AMO TO DETECT EVIDENCE OF CRACKS AT THE WELD BETWEEN THE UPPER ATTACH FITTING (SQUARE SHAPE) AND THE ROUND TUBULAR STRUCTURE. (TC NR 20070621003)                     1L72 3O3  O  A29CE   E286    5  CP43GL    
20070820000472007082000047SO  2007       8          20         CA070621004      120070611G27314173478         CABLE                                   PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ELEVATOR TRIM   SEPARATED       W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA       14256                                                          (CAN) PILOT REPORTED ELEVATOR TRIM VERY STIFF WHILE IN FLIGHT, THEN FREE AFTER SEVERAL ATTEMPTS. MAINT INVESTIGATION REVEALED TRIM CABLE P/N 41734-78 SEPARATED AT THE TRIM SERVO P/N 1C469-6-498. CABLE WAS REPLACED AND SYSTEM RIGGED IAW MM 5-32. CABLE INSPECTION DID NOT REVEAL ANY UNUSUAL WEAR OR FRAYING AT THE SEPARATED ENDS. CABLE WAS SHREDDED AND APPEARED TO BE TORN APART. FURTHER INVESTIGATION BY AVIONICS REPAIR STATION REVEALED THAT THE ELEVATOR ELECTRIC/AP TRIM SERVO CLUTCH RELEASE MECHANISM WAS INTERMITTENT. SERVO WAS REPAIRED AND OPERATION CHECKED SERVICEABLE.  (TC NR 20070621004)                                                                                                                              1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070820000482007082000048EA  2007       8          20         CA070622002      220070620G8550O320H2AD        ENGINE                                  CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA  MCAULY1C160 1C160DTM    GL  LEFT            LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       6383 2085                          RL567576T                   (CAN) OIL LEAKING FROM FRONT LT AREA OF ENGINE. (TC NR 20070622002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A12    E274    5  NP910     
20070820000492007082000049WP  2007       8          20         CA070622003      120070619G6310                SHAFT                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              CLUTCH          WORN            W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       563                                                            (CAN) LOUD (BANG) HEARD DURING FLIGHT. CLUTCH SUSPECTED. REMOVED TO INSPECT. CLUTCH WAS TORN DOWN IN THE COMPONENT SHOP AND SHAFT WAS FOUND WORN BEYOND LIMITS.  SPRAG WAS MOST LIKELY DRAGGING ON THE SHAFT. CLUTCH AND SHAFT ASSY BEING SENT BACK FOR WARRANTY. (TC NR 20070622003)                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3O3  O  H11NM   1E4                  
20070820000502007082000050EU  2007       8          20         CA070622004      120070619G21219599022154      BLOWER                                  PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  RIGHT           INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       6594                                                           (CAN) RT VENTILATION BLOWER WOULD NOT OPERATE WHEN SWITCHED ON. REPLACED WITH NEW. (TC NR 20070622004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070820000512007082000051SW  2007       8          20         CA070622005      120070621G2841EA4703587       INDICATOR                               BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              FUEL QTY        DEFECTIVE       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) FUEL QUANTITY INDICATOR WAS REMOVED DUE TO INDICATION PROBLEMS.  WHEN REMOVED IT WAS FOUND THAT THE FLOAT WAS FULL OF FUEL AND ONE OF THE DECALS FROM PHP WAS GONE AND WAS IN THE FUEL SYSTEM.  DECAL WAS LOCATED AND SENDER IS BEING REPLACED WITH A NEW UNIT. (TC NR 20070622005)                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3U3  U  H2SW    E4CE                 
20070711001842007071100184CE  2007       7          11         CA070622006      120070619G2822025323150       PUMP                                    CESSNA425   425         2076018CE  PWA   PT6   PT6A112     52043NE  MCAULY3G34C73GFR34C701  GL  FUEL SYSTEM     CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1453                                                      (CAN) DURING AN INSPECTION THE INLET FILTER WAS REMOVED. THE FILTER COVER (CAP) WAS FOUND CRACKED UNDER THE O-RING LOCATION ALL THE WAY AROUND.  IT APPEARS TO HAVE BEEN OVER TORQUED.  IT WAS NOT LEAKING AT THIS TIME.  THE INLET FILTER ASSEMBLY WAS REPLACED. (TC NR 20070622006)                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 3T3  TRTA7CE    E4EA    5  CP60GL    
20070820000522007082000052EU  2007       8          20         CA070622007      120070619G6220C623A2005103    SCISSOR LINK                            UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              MAIN ROTOR      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       98                                                             (CAN) (1) OF (4) BONDED BUSHINGS FAILED, RESULTING EXCESSIVE PLAY/SMOKING. BUSHING CONTINUED TO WEAR INTO SCISSOR LINK UNTIL CAUGHT AT FIRST 100 HOUR INSPECTION (SINCE NEW). (TC NR 20070622007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G72 3U3  UNCR0001RD E34NE                
20070820000532007082000053CE  2007       8          20         CA070622008      120070612G27301016100190014   TORQUE TUBE                             BEECH 200   B200        1152922CE  PWA   PT6   PT6A42      52043NE  HARTZLHCD4N3HCD4N3A     GL  ELEVATOR CONTROLMISMANUFACTURED W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) DURING RIGGING CHECK, DUE TO REPLACEMENT OF THE ELEVATOR TORQUE TUBE, DISCOVERED THE ARM LOCATION WAS INCORRECT IN RELATION TO THE MOUNTING PLATE.  THIS RESULTED IN NOT BEING ABLE TO ACHIEVE FULL TRAVEL OF THE ELEVATOR.  THIS WAS CONFIRMED WHEN COMPARED TO THE REMOVED TORQUE TUBE AND THE SECOND REPLACEMENT.  THE CONCLUSION IS INCORRECT ASSEMBLY AT MFG.  (TC NR 20070622008)                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070711001852007071100185EA  2007       7          11         CA070625001      220070606G8530O320H2AD        CYLINDER                                CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA  MCAULY1C160 1C160DTM    GL  ENGINE          CRACKED         W      A   UNSCHED LANDING                                                                                 RE PARTIAL RPM/PWR LOSS      VIBRATION/BUFFET                                    CLCLIMB          1                      CA            1400                          L518276T                    (CAN) INSTRUCTOR RETURNED FROM A FLIGHT WHERE HE EXPERIENCED A ROUGH ENGINE AND LOSS OF POWER FOR A FEW MOMENTS, AFTER WHICH THE ENGINE RAN NORMALLY AGAIN.  WHEN MAINTENANCE REMOVED THE COWLING TO CHECK OVER THE ENGINE, A LOT OF OIL WAS NOTICED IN THE COWL, FURTHER INSPECTION AND CLEANING FOUND A 2 INCH LONG CRACK IN THE CRANKCASE FROM CYLINDER NR 2 MOUNTING PAD AND FORWARD. (TC NR 20070625001)                                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A12    E274    5  NP910     
20070820000542007082000054NE  2007       8          20         CA070625004      220070624G8560                SUPERCHARGER                            DOUG  DC6   DC6B        3021712WP  PWA   R1340 BWASP       52016NE  HAMSTD43E   43E60       NE  ENGINE          FAILED          W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA            1906                                                      (CAN) AT TOP OF CLIMB ENGINE POWER DECREASED TO 20 INCH MANIFOLD PRESSURE AND 80 BMEP.  ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO AIRPORT.  SUSPECT ENGINE SUPERCHARGER BLOWER FAILED. (TC NR 20070625004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L74 4R3  R  6A4     ATC14   6  CP871     
20070820000552007082000055EU  2007       8          20         CA070625005      120070613G672021863753        PUSH-PULL ROD                           SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              T/R GEARBOX     CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1000                                                           (CAN) HEAT SHRINK WHICH PROTECTS THE TAIL ROTOR PUSH PULL TUBE AS IT GOES THRU BEARING P/N 359A27-1191-20 IS CHAFING PREMATURLY AT THE AFT MOST BEARING LOCATION ON THE TAILBOOM.  IPC 67.20.10.00006.00 FIG. 3 (TC# NR 20070625005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3U3  U  H9EU    E19EU                
20070820000562007082000056SW  2007       8          20         CA070626001      120070622G2820206063607101    HOSE                                    BELL  206   206L4       1182110SW                                                               FUEL SYSTEM     DEBONDED        W      K   NONE                                                                                            KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            ININSP/MAINT     1                      CA                                                                      (CAN) FUEL HOSE ASSY DEBONDED CAUSING FUEL LEAK FROM FWD TANKS. THE RUBBER BELLOW PART OF THE TUBE ASSEMBLY DEBONDED FROM THE ALUMINUM TUBING. THIS HOSE ASSEMBLY IS LOCATED ON THE LT SIDE FWD FUEL TANK. REFER TO HELICOPTER IPB FIGURE 28-3 ITEM NR 57.  (TC NR 20070626001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3U    NCH2SW                         
20070820000572007082000057CE  2007       8          20         CA070627001      120070622G32601013646281      DOWNLOCK SWITCH                         BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  LT MLG          UNSERVICEABLE   W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) THE AIRCRAFT WAS ON A RETURN LEG, WHEN THE CREW LOWERED THE LANDING GEAR THEY NOTICE AN UNSAFE INDICATION ON THE LT MAIN. THEY ABORTED THE LANDING AND INITIATED A (GO-AROUND) PROCEDURE. THE LANDING GEAR WAS CYCLED TWICE MORE AND ON THE SECOND TRY A SAFE INDICATION WAS OBSERVED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LT MAIN LANDING GEAR DOWNLOCK SWITCH ASSY (P/N 101-364628-1) WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT. THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070627001)                                                                                                                                                                                                                                 2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070820000582007082000058NE  2007       8          20         CA070627002      220070624G72614138T09P03      CARBON SEAL                 CF343B1     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              NR 2 ENGINE     DAMAGED         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                          872403                      (CAN) ON CLIMB OUT, CREW REPORTED NR 2 OIL PRESSURE WAS LOW AND FLUCTUATING BETWEEN 30-41 PSI.  INTERMITTENTLY TRIGGERING THE LOW OIL WARNING. THE AIRCRAFT WAS DIVERTED AND LANDED NORMALLY. AT LOCATION, CONTRACT MAINTENANCE ADDED (4) QUARTS OF OIL AND A/C WAS CHECKED SERVICEABLE.  THE A/C THEN RETURNED TO ORIGINATING BASE WHERE FURTHER TROUBLESHOOTING WAS TO BE CARRIED OUT.  MAINTENANCE FOUND NR 2 ENGINE IDG CARBON SEAL DAMAGED.  THE CARBON SEAL WAS REPLACED AND LEAK CHECKS AND RUNS CARRIED OUT AND CHECKED SERVICEABLE.  A/C HRS.:17552:25, CYCLES:13370  (TC NR 20070627002)                                                                                                                                              2L72 4F4  FRTA21EA   E15NE                
20070820000592007082000059CE  2007       8          20         CA070627003      120070626G26213090385659      SQUIB           PACIFICSCIEN            LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              FIRE BOTTLE     INOPERATIVE     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2172       39925B1                                             (CAN) WHILE PERFORMING ANOTHER MAINTENANCE TASK IT WAS DISCOVERED THAT THE LOWER (FWD) FIRE BOTTLE SQUIBS WERE NOT INSTALLED IN THE CORRECT POSITION.  BOTH FIRE BOTTLES CONTAIN A SQUIB FOR THE LT AND RT ENGINES, THE LOWER NR 1 BOTTLE IS FOR THE FIRST SHOT AND THE UPPER NR 2 BOTTLE IS FOR THE SECOND SHOT.  THE LT AND RT SQUIBS ON EACH BOTTLE HAVE A DIFFERENT PN WITH A DIFFERENT CONNECTOR PLUG RECEPTACLE IN ORDER NOT TO ACCIDENTALLY SWAP LT AND RT ENGINES EXTINGUISHING CAPABILITIES.  HOWEVER, SINCE THE SQUIBS WERE INSTALLED INCORRECTLY THE FIRST EXTINGUISHING SHOT WOULD HAVE BEEN DIRECTED TO THE WRONG ENGINE.  UPON INVESTIGATION IT WAS DISCOVERED THAT THE SQUIBS MAY HAVE BEEN INSTALLED INCORRECTLY AT THE LAST 10-2L72 4F4  FRTT00008WIE6WE                 
20070711001872007071100187NE  2007       7          11         CA070628001      320070625G61147826691         BOLT                                    DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  PROPELLER HUB   SHEARED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       190048360                                                      (CAN) DURING REINSTALLATION OF PROPELLER ASSEMBLY AFTER NR 2 ENGINE CHANGE, ONE OF THE MOUNTING BOLTS (P/N 782669-1) SHEARED. A DIFFERENT PROPELLER ASSEMBLY WAS INSTALLED. AFFECTED SHEARED BOLT TO BE REMOVED AND REPLACED IAW CMM P/N 802325-1, CH 61-13-06, HUB  REPAIR 7-5, PAGES 601-602. TIMES AND CYCLES ARE FOR HUB ASSEMBLY. (TC NR 20070628001)                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070820000602007082000060NE  2007       8          20         CA070628003      220070516G7260MS949034        BOLT                                    MRCHTIS205  S20522R     8120412EU  PWA   PT6   PT6A65AR    52043NE                              FIRST STAGE     FAILED          W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA       175                                PCE97543                    (CAN) ENGINE S/N PCE 97543 WAS REMOVED SUBSEQUENT TO IN-FLIGHT SHUTDOWN AFTER THE ENGINE OIL PRESSURE DROPPED TO (0) IN FLIGHT.  METAL WAS FOUND IN THE OIL FILTER AND RGB DURING GROUND CHECKS PRIOR TO ENGINE REMOVAL.  DURING INVESTIGATION DISMANTLE OF THE POWER SECTION, (2) OF (6) FIRST-STAGE REDUCTION CARRIER ASSEMBLY MACHINE HEX BOLTS (IPC P/N 3032844, CH. 72-11-00, FIGURE 4, ITEM 200, P/N MS9490-34) WERE FOUND WITHOUT THE BOLT HEADS ATTACHED (REFERENCE FIGURE 1).  NOTE THAT THE CARRIER HEX BOLTS SECURE THE FIRST-STAGE CARRIER AND THE FIRST-STAGE REDUCTION SPLINED ADAPTER.  THERE ARE A QUANTITY OF SIX HEX BOLTS INSTALLED WITH KEYWASHERS AND ARE TORQUED 75 TO 85 IN.LB.  ENGINE OVERHAUL RECORDS INDICATED THAT Q1L71 3O4  T  A9EU    E4EA                 
20070820000612007082000061WP  2007       8          20         CA070629001      220070625G72108941241         SHAFT                                                                      GARRTTTPE331TPE33110    01514WP                              SPLINES         WORN            W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA            2321                                                      (CAN) AIRCRAFT EXPERIENCED A NTS EVENT DURING LANDING PHASE, WITH POWER LEVER REDUCED TO FLIGHT IDLE, AC CONFIGURED FOR LANDING, WITH NORMAL ATTITUDE FOR LANDING. AIRCRAFT LANDED AND TAXIED WITH NO OTHER PROBLEMS REPORTED. AIRCRAFT INSPECTED, FLIGHT IDLE BLADE ANGLES ADJUSTED AND RETURNED TO SERVICE.  DUE TO SOAP RESULTS AND NTS GROUND CHECK RESULTS, THE ENGINE WAS SUBSEQUENTLY REMOVED FROM SERVICE. NTS ACTION IS POTENTIALLY DUE TO (SUSPECTED) COMBINATION OF WEAR OF THE QUILL SHAFT AND BALL LOCK WHICH WOULD HAVE IN EFFECT, CAUSED A REDUCTION IN THE PRELOAD OF THE NTS SYSTEM, THEREBY ALLOWING THE NTS TO ACTIVATE AT A LOWER THRESHOLD THAN SET CALIBRATION.  CODE (TC NR20070629001)                                         4  T          E4WE                 
             20081105         2008       11         5          CA070629002      120070629G2910                PACKING                                                                                                                                 HYD ACTUATOR    DEFECTIVE       W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) WHILE REPLACING O-RINGS AND BACK-UP SEALS IN SOME HYDRAULIC ACTUATORS, FOUND SOME OF NEW BACK-UP SEALS DEFECTIVE. THE CHAMFERED EDGE OF THE SEAL IS TO SHORT WHICH IN TURN CAUSED THE EDGE TO DAMAGE THE O-RING. IT SEEMS TO ACT AS A KNIFE EDGE. ALL SEALS IN A BATCH WERE NOT FOUND LIKE THIS, ONLY A FEW.  THAT IS WHY SOME OF OUR ACTUATORS HAVE BEEN LEAKING DUE TO THE BACK-UP SEAL CUTTING THE O-RING.  WILL BE SENDING A REPORT AND PICTURES TO THE VENDOR.                                                                                                                                                                                                                                                                                                                 
20070820000622007082000062WP  2007       8          20         CA070629003      120070525G2916D2112           RESERVOIR                               ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              HYD SYSTEM      LEAKING         W      K   NONE                                                                                            KJ FLUID LOSS                WARNING INDICATION                                  ININSP/MAINT     1                      CA       196                                                            (CAN) DURING POST INSPECTION RUN UPS, IT WAS WITNESSED THE HYDRAULIC RESERVIOR WAS VENTING HYDRAULIC FLUID OUT OF THE VENT. NO DETERMINING FACTOR COULD BE FOUND, SO THE RESERVIOR WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20070629003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3O3  O  H11NM   1E4                  
20080220003222008022000322SO  2008       2          20         CA070703001      120070628G32114032700         TRUNNION                                PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  LT MLG          CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       19470                  317405228                               (CAN) DURING A SCHEDULED LAYOVER, ON POST FLIGHT WALK AROUND THE PILOTS NOTICED THAT THE LT GEAR STRUT WAS DEFLATED. EXAMINATION BY MAINT SHOWED THAT THE TRUNNION HAD CRACKED ALONG THE WELD THAT HOLDS THE (2) HALVES OF THE TRUNNION TOGETHER. IT HAD CRACKED UP PAST THE ORINGS INTO THE SEALED AREA OF THE STRUT.  IT IS UNKNOWN IF THIS STRUT IS THE ORIGINAL AIRCRAFT ONE. (TC NR 20070703001)                                                                                                                                                                                                                                                                                                                                           1L72 3O3  O  A20SO   E14EA   5  CP33EA    
             20081104     EA  2008       11         4          CA070703002      220070509G7414M3548           ROTOR SHAFT     SLICK       4370        ZLIN  242   Z242L       9970204EU  LYC   O360  AEIO360A1B6 41514EA                              MAGNETO         SHEARED         W      C   ABORTED TAKEOFF                                                                                 R  PARTIAL RPM/PWR LOSS                                                          TXTAXI/GRND HDL  1                      CA       1272                                                           (CAN) A STUDENT PILOT NOTICED THAT THE ENGINE WOULD NOT RUN WHEN THE RT MAGNETO WAS SELECTED. MAINT WAS CALLED AND THE RT MAGNETO WAS REMOVED FROM THE ENGINE AND DISSASSEMBLED. THE ROTOR WAS FOUND SHEARED AT THE CAM ROTOR SLOT. (TC NR  20070703002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L71 3O3  O0 A76EU   1E10                 
20080131000712008013100071SW  2008       1          31         CA070703003      120070701G28221C27            CARTRIDGE       AIRBORNE                BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              BOOST PUMP      UNSERVICEABLE   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) CAUTION LIGHT ILLUMINATED DURING FLIGHT INDICATING A BOOST PUMP FAILURE. FUEL SYSTEM INSPECTED FWD BOOST FOUND TO BE NOT OPERATING. CARTRIDGE CHANGED OUT WITH AN OVERHAULED UNIT.FUEL SYSTEM SERVICABLE. (TC NR 20070703003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U3  U  H2SW    E4CE                 
20070820000632007082000063SO  2007       8          20         CA070703004      220070613G8530AEC631397       CYLINDER                                CESSNA185   A185E       2072818CE  CONT  O520  IO520D      17032SO  HARTZLHCC3Y HCC3YF1     GL  NR 2            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       484  454                           547388                      (CAN) CYLINDER CRACKED FROM FUEL INJECTOR TO SPARK PLUG HOLE, CRACK FOUND DURING 100 HR INSPECTION (TC NR 20070703004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3O3  O  3A24    E5CE    5  CP25EA    
20070820000642007082000064SO  2007       8          20         CA070703005      220070608G7414662             MAGNETO                                 CESSNA206   U206G       2073356CE  CONT  O520  IO520F      17032SO  MCAULYD3A34 D3A34C401   GL  ENGINE          UNSERVICEABLE   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            300                                                       (CAN) SHEARED MOUNTING FLANGE HOUSING. (TC NR 20070703005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  O  A4CE    E5CE    5  CP47GL    
20070820000652007082000065NM  2007       8          20         CA070703006      120070702G26124739551         CONTROL PANEL                           BOEING737   737*               NM  GE    CFM56 CFM567B24        NE                              FIRE CONTROL    DAMAGED         W      K   NONE                                                                                            N  FALSE WARNING                                                                 ININSP/MAINT     1                      CA       1046010460                                                     (CAN) ON JULY 2/07 IN PREPARATION FOR THE DAYS FLYING THE CREW REPORTED THE CARGO FIRE BELL SOUNDING.  THE FORWARD CARGO FIRE C/BS WERE FOUND POPPED AND SMOKE WAS COMING FROM THE FLIGHT DECK CARGO FIRE DETECTOR PANEL.  THIS RESULTED IN THE FWD CARGO PIT EXTINGUISHER DISCHARGING ITSELF. THE FIRE PANEL MODULE AND THE DEPLETED FIRE BOTTLE WERE REPLACED.  THE OEM TO WHICH THE DAMAGED PANEL WAS SENT HAS BEEN REQUESTED TO INVESTIGATE, PROVIDE A DETAIL STRIP REPORT AND PHOTOS.  FURTHER INFORMATION WILL BE SUBMITTED AT THE CONCLUSION OF THIS INVESTIGATION. (TC NR 20070703006)                                                                                                                                                  2L72 4F4  FRTA16WE   E00055EN             
20070820000662007082000066    2007       8          20         CA070704001      120070703G781031015827        EXHAUST DUCT                                                               GARRTTTPE331TPE33110UA  01514WP                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) UPON ROUTINE INSPECTION, THE MAINTENENCE CREW FOUND THE EXHAUST DUCT CRACKED. THE ENGINE WAS REMOVED AND THE EXHAUST DUCT WAS REPLACED WITH A OVERHAULED ONE. NO OTHER PROBLEMS WERE DETECTED AT THIS INSPECTION. (TC NR 20070704001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            4  T          E4WE                 
20070820000672007082000067EA  2007       8          20         CA070704002      120070703G2750C6CF14681       ROD                                     DHAV  DHC6  DHC6300     2802606EA                                                               TE FLAPS        MISMANUFACTURED W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION OF THE FLAP RODS IAW S/B 6/502 AND 6/388 IT WAS NOTICED THAT THE SWAGED END OF THE FLAP ROD WAS NOT COMPRESSED.  UPON INSPECTION OF THE ROD IT WAS NOTED THAT THE COLLAR WAS NOT IN THE CORRECT POSITION AND HAD NOT BEEN COMPRESSED ENOUGH.  THE SWAGED END MEASURES 0.9880OF AN INCH AND THE END IN QUESTION MEASURES 1.0055 OF AN INCH. THERE IS NORMALLY A BUMP IN THE SWAGED END, BUT THE END IN QUESTION DOES NOT HAVE ANY BUMP ON IT.  (TC NR 20070704002)                                                                                                                                                                                                                                                       1H72 3T    RTA9EA                         
20070820000682007082000068NM  2007       8          20         CA070704003      120070704G521085210276101     BOLT                                    DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  HANDRAIL SUPPORTLOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CREW REPORTED THAT MAIN CABIN DOOR WOULD STOP OPENING SOMETIMES. FLIGHT ATTENDANT HAD TO PUSH THE HANDRAIL TO GET THE DOOR FULLY OPEN. LINE MAINTENANCE FOUND REAR HANDRAIL SUPPORT STRUT BOLT (REF IPC 52-10-00-35-50) UNSCREWED AND CONTACTING WITH HANDRAIL LOWER NEWEL STRUT (REF IPC 52-10-00-40-90). THE BOLT HAS NO LOCKING FEATURE. THE BOLT WAS TIGHTENED, SYSTEM CHECKED SERVICEABLE AND THE AIRCRAFT RELEASED INTO SERVICE (TC NR 20070704003)                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
             20081104     CE  2008       11         4          CA070704004      120070703G2435                BRUSHES                                 CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  STARTER GEN     WORN            W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA       1005                                                           (CAN) PILOT ATTEMPTED TO START AIRCRAFT. AIRCRAFT FAILED TO START. FURTHER INVESTIGATION REVEALED A STARTER BRUSH HAD FRACTURED AND SEPARATED INTO A FEW PIECES. DAMAGE TO THE COMMUNTATOR WAS FOUND. IT WAS APPROXIMATELY 240 HRS SINCE THE LAST BRUSH INSPECTION AND NO ISSUE WERE NOTED.  (TC NR 20070704004)                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20070820000692007082000069NM  2007       8          20         CA070704005      120070627G5210R2210151        DOOR FRAME                              ROBSINR22   R22BETA     7640110NM  LYC   O320  O320B2C     41508EA                              PAX DOOR        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING VISUAL INSPECTION TO COMPLY WITH AWD 2005-16-05 LT DOOR ASSY WAS FOUND CRACKED.  FUTHER INSPECTION OF THE TECH-TOOL DOOR AND FRAME REVEALED ADDITIONAL CRACKS. DOOR FOUND TO BE U/S AND REMOVED FROM A/C. (TC NR 20070704005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 3O3  O  H10WE   E274                 
20080131000372008013100037NM  2008       1          31         CA070704006      120070627G5210R2210152        FRAME                                   ROBSINR22   R22BETA     7640110NM  LYC   O320  O320B2C     41508EA                              RT DOOR         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING VISUAL INPECTION TO COMPLY WITH AWD 2005-16-05 RT DOOR ASSY WAS FOUND CRACKED. FUTHER INPECTION OF THE TECH-TOOL DOOR AND FRAME ASSY REVEALED ADDITIONAL CRACKS. DOOR FOUND TO BE UNSERVICEABLE AND REMOVED FROM A/C. (TC NR 20070704006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3O3  O  H10WE   E274                 
20070820000702007082000070    2007       8          20         CA070704007      420070704G611305503214        BULKHEAD                                CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA  MCAULY1C160 1C160DTM    GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       652                                                            (CAN) BULKHEAD IS CRACKED AROUND SEVERAL OF THE PROP THROUGH BOLT HOLES. (TC NR 20070704007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  ONT3A12    E274    5  NP910     
20070820000712007082000071    2007       8          20         CA070704008      420070517G611305503214        BULKHEAD                                CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA                              SPINNER         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       320                                                            (CAN) CRACKED AROUND SEVERAL OF THE PROP BOLT THROUGH HOLES. (TC NR 20070704008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A12    E274                 
20070820000722007082000072NE  2007       8          20         CA070704009      220070509G7313ST3367009       PACKING                                 AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              FUEL MANIFOLD   DEFECTIVE       W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) SHORTLY AFTER TAKE-OFF PASSENGERS REPORTED FLUID ESCAPING FROM THE ENGINE.  THE PILOT REDUCED ENGINE POWER AND DIVERTED TO POINT OF DEPARTURE.  SUBSEQUENT INSPECTION REVEALED LEAKING FUEL NOZZLE MANIFOLD PACKINGS.  MFG HAS DETERMINED THE PACKINGS TO BE ASSOCIATED WITH A MANUFACTURER`S QUALITY ESCAPE (REFERENCE: MFG SERVICE BULETIN SB21740) (TC NR 20070704009)                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRT        E20NE                
20070820000732007082000073EA  2007       8          20         CA070704010      220070505G7532                BLEED VALVE                             BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA                              COMPRESSOR      FAULTED         W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      CA       4107                                                           (CAN) ON APPROACH, AN ENGINE FADEC CAUTION LIGHT ILLUMINATED AND THE PILOT ELECTED TO SHUTDOWN THE ENGINE (PRECAUTIONARY).  SUBSEQUENT INSPECTION REVEALED A FAULTY INTERCOMPRESSOR BLEED VALVE. (TC NR 20070704010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E00062EN             
20070820000742007082000074NE  2007       8          20         CA070704011      220070514G7261                OIL SYSTEM                              PIAGIOP180  P180        6960204EU  PWA   PT6   PT6A66      52043NE                              ENGINE          OVERTEMP        W      E   ENGINE SHUTDOWN                                                                                 MJ OVER TEMP                 WARNING INDICATION                                  CRCRUISE         1                      CA                                          104058                      (CAN) IN FLIGHT, THE ENGINE OIL TEMPERATURE WAS SEEN TO INCREASE AND THE ENGINE WAS SHUTDOWN.  POST-FLIGHT INSPECTION REVEALED OIL LEAKAGE AT THE ENGINE (C) FLANGE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070704011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H72 3O4  TRTA59EU   E26NE                
20070820000752007082000075EU  2007       8          20         CA070704012      120070511G29133022375         SEAL                                    REIMS 406   F406        7535723EU  PWA   PT6   PT6A112     52043NE                              HYDRAULIC PUMP  FRACTURED       W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND SUBESQUENTLY DECREASE.  OIL WAS SEEN ESCAPING FROM THE ENGINE NACELLE.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INVESTIGATION REVEALED A FRACTURED HYDRAULIC PUMP PAD OIL SEAL. (TC NR 20070704012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3T3  TRTA54EU   E4EA                 
20070820000762007082000076NE  2007       8          20         CA070704014      220070519G7310ST3367009       PACKING                                 AEROSPATR72 ATR72212    8680945EU  PWA   PW120 PW127            NE                              FUEL MANIFOLD   FRACTURED       W      D   RETURN TO BLOCK                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                                                                      (CAN) FUEL WAS FOUND LEAKING FROM THE FUEL MANIFOLD DRAIN DURING TAXI.  SUBSEQUENT INSPECTION REVEALED LEAKING FUEL MANIFOLD PACKINGS.  MFG HAS DETERMINED THE PACKINGS TO BE ASSOCIATED WITH A MANUFACTURER`S QUALITY ISSUE (REFERENCE MFG SB21740). (TC NR 20070704014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA53EU   E20NE                
20070820000772007082000077NE  2007       8          20         CA070704015      220070511G7261                ENGINE                                                                     PWA   PT6   PT6A65AR    52043NE  HARTZLHCB5M HCB5MP3     GL                  SEIZED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         BR SMOKE/FUMES/ODORS/SPARKS  PARTIAL RPM/PWR LOSS                                CRCRUISE         1                      CA                                          97048                       (CAN) IN CRUISE, SMOKE WAS OBSERVED IN THE CABIN AND ENGINE POWER REDUCED UNCOMMANDED.  THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE.  SUBSEQUENT INSPECTION REVEALED SEIZURE OF THE ENGINE AND OIL LEAKAGE.  MFG WILL MONITOR THE INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070704015)                                                                                                                                                                                                                                                                                                                                                                                 4  T          E4EA    6  CP44GL    
20070820000782007082000078EA  2007       8          20         CA070704016      220070513G7210                GEARBOX                                 DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE          DISTRESSED      W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                          41553                       (CAN) PRIOR TO START OF DESCENT, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE. DURING THE DESCENT THE ENGINE FLAMED OUT.  SUBSEQUENT INSPECTION REVEALED REDUCTION GEARBOX DISTRESS.  MFG WILL INVESTIGATE THE EVENT AND ADVICE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070704016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070820000792007082000079NE  2007       8          20         CA070704017      220070523G7200                ENGINE                                  BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE                                              OVERTEMP        W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         AJ FLAME/FIRE                WARNING INDICATION                                  CRCRUISE         1                      CA                                          PJ0243                      (CAN) IN CRUISE, THE ENGINE INTER-TURBINE TEMPERATURE WAS SEEN TO INCREASE AND FLAMES AND SPARKS WERE SEEN EXITING THE EXHAUST.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070704017)                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 4T4  T  A24CE   E4EA                 
             20081104         2008       11         4          CA070704018      120070702G324095214071        LINER           LORAL       95409761                                                                                                    BRAKE ASSY      SEPARATED       W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         LDLANDING        1                      CA            2                                                         (CAN) DURING THE ROLLOUT AFTER LANDING, THE FLIGHT CREW NOTICED THE LT BRAKE PEDAL TRAVEL WAS MORE THAN NORMAL. UPON INSP IT WAS NOTED THAT THE FIXED LININGS P/N 9521407-1 (2 OF THE 3) HAD SEPARATED FROM THE BRAKE ASSY. THE LININGS WERE LATER LOCATED ON THE RUNWAY THAT THE ACFT HAD LANDED ON. THERE WAS NO VISIBLE EVIDENCE AS TO WHY THE LININGS SEPARATED. ONE THEORY IS THAT A FOREIGN OBJECT SUCH AS A ROCK WAS THROWN INTO THE BRAKE ASSY AT THE TIME OF LANDING. THE ACFT WAS INSPECTED, THE BRAKE ASSY WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE. (TC NR 20070704018)                                                                                                                                                                                              
20070820000802007082000080    2007       8          20         CA070705001      220070528G7320                FADEC                                   CESSNA680   680CE       2076811CE                                                                               MALFUNCTIONED   W      O   OTHER                                                                                           RF PARTIAL RPM/PWR LOSS      FLT CONT AFFECTED                                   LDLANDING        1                      CA                                                                      (CAN) THE ENGINES FAILED TO RESPOND TO THROTTLE INPUT FOLLOWING TOUCHDOWN. PRELIMINARY INVESTIGATION REVEALED THE ISSUE RELATED TO THE FADEC`S RESPONSE TO ARMING THE THRUST REVERSERS ON APPROACH (NOT AN AFM PROCEDURE), COUPLED WITH A BOUNCE FOLLOWING INITIAL TOUCHDOWN.  P&WC WILL INVESTIGATE AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC# 20070705001)                                                                                                                                                                                                                                                                                                                                                                               2L72 4F    RCT00012WI                     
20070820000812007082000081CE  2007       8          20         CA070705002      120070530G2435                SEAL                                    BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE                              STARTER GEN     LEAKING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) ENGINE OIL PRESSURE WAS SEEN TO REDUCE AND FLUCTUATE IN CRUISE AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED A FAULTY LIP SEAL (RECENTLY REPLACED) ON THE STARTER GENERATOR DRIVE SHAFT. (TC NR 20070705002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 4T4  T  A24CE   E4EA                 
20070820000822007082000082EU  2007       8          20         CA070705003      120070528G24353022383         SEAL                                    AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF5       NE  STARTER GEN     LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) ON A MAINTENANCE FLIGHT, THE ENGINE LOW OIL PRESSURE WARNING ACTIVATED AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED A LEAKING STARTER GENERATOR GARLOCK LIP SEAL. (TC NR 20070705003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20070820000832007082000083NE  2007       8          20         CA070705004      220070519G7200                ENGINE                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              POWER LOSS      W      A   UNSCHED LANDING                                                                                 ERJVIBRATION/BUFFET          PARTIAL RPM/PWR LOSS      WARNING INDICATION        CRCRUISE         1                      CA                                          PC0810                      (CAN) IN CRUISE FLIGHT, THE ENGINE EMITTED A LOUD NOISE AND LOST POWER, RESULTING IN A FORCED LANDING.  MFG WILL MONITOR INVESTIGATION OF THE INCIDENT AND REPORT ROOT CAUSE ONCE DETERMINED. (TC NR 20070705004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3T3  T  A37CE   E4EA                 
20070820000842007082000084NE  2007       8          20         CA070705005      220070303G73213244768         FCU                                     BEECH 1900  1900C       1154161CE  PWA   PT6   PT642A           NE                              ENGINE          DEFECTIVE       W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) IN FLIGHT THE ENGINE EXPERIENCED AN UNCOMMANDED ACCELERATION RESULTING IN AN OVER-TORQUE CONDITION.  SUBSEQUENT INSPECTION REVEALED A FAULTY FCU.  (TC NR 20070705005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4T4  TRTA24CE   E4EA                 
20070820000852007082000085EA  2007       8          20         CA070705006      120070618G5330215300174       SKIN                                    CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  BS 584.5        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1308                                                           (CAN) A 3 INCH CRACK WAS DISCOVERED IN THE SKIN.  CAUSE AT HIS TIME IS UNKKOWN AIND IS UNDER FURTHER INVESTIGATRION (TC NR 20070705006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20070820000862007082000086EA  2007       8          20         CA070705007      120070618G5330215300174       SKIN                                    CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  BS 584.5        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1308                                                           (CAN) A (5) INCH CRACK WAS DISCOVERED IN THE SKIN AT APPROX F/S 584.50 AND W/L100. CAUSE AT THE TIME IS NOT KNOWN AND IS UNDER FURTHER INVESTIGATION. (TC NR 20070705007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
             20081104         2008       11         4          CA070705008      220070705G741410160858        HOUSING                                                                                                                                 MAGNETO         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       499                                                            (CAN) MAG SENT IN FOR 500 HR INSP. FOUND MOUNTING EAR CRACKED WHERE HOLD-DOWN NUT AND WASHER CONTACT EAR. THIS IS A NEW STYLE OF CASTING FROM MFG WITH THE NAME "EMPIRE" CAST INTO THE INTERIOR OF THE HSG AND JUST THE LETTERS "TCM" CAST ON THE OUSIDE OF THE HSG. THE OLD STYLE OF HSG HAD EITHER "TCM" OR "BENDIX" AND THE MAGNETO INFORMATION BLOCK CAST INTO THE OUTSIDE OF THE HSG. THE OLD STYLE OF HSG WOULD CRACK IF OVERTORQUED OR IF THE WRONG GASKET WAS USED IN APPROXIMATELY 1 OUT OF 30 MAGS RECEIVED FOR INSP. IN THIS CASE 4 OF 6 MAGS WITH THE NEW CASTING HAVE CRACKS IN THIS LOCATION. SEPERATE SDR`S WILL BE FILED FOR EACH MAGNETO. (TC NR 20070705008)                                                                                                            
             20081105         2008       11         5          CA070705011      220070705G741410160858        HOUSING         BENDIX                                                                                                                  MAGNETO         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       2000                                                           (CAN) MAGNETO SENT IN AS A CORE, BUT HAS SAME CRACK AS 3 OTHER MAGNETOS RECEIVED FOR REPAIR. THIS CRACK IS IN A NEW STYLE OF CASTING PUT INTO PRODUCTION BY MFG.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          
20070820000872007082000087SW  2007       8          20         CA070705012      120070705G2434ALU8521LS       ALTERNATOR                              HUGHES269   269C1       8059504SW  LYC   O360  HIO360*     41514EA                                              FAILED          W      E   ENGINE SHUTDOWN                                                                                 H  ELECT. POWER LOSS-50 PC                                                       TXTAXI/GRND HDL  1                      CA       400                                                            (CAN) ALTERNATOR FAILED ON STARTUP.  FOUND ROTOR JAMMING AND PULLEY HAD OVERHEATED.  LOOSE PARTS HEARD INSIDE ALTERNATOR.  NO PREVIOUS INDICATIONS OF IMPENDING FAILURE. (TC NR 20070705012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3O3  OO 4H12    1E10                 
             20081104     SW  2008       11         4          CA070705013      120070702G7810                GASKET                                  HUGHES269   269C1       8059504SW  LYC   O360  HIO360G1A   41898EA                              EXHAUST         CRACKED         W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA       210                                                            (CAN) DURING ROUTINE INSP, IT WAS NOTICED THAT NEARLY ALL OF THE GASKET BETWEEN THE FWD FLANGE AND THE EXHAUST MUFF HAD CRACKED AND FALLEN AWAY, LEAVING THE POSSIBILITY OF A CABIN EXHAUST LEAK. (TC NR 20070705013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3O3  OO 4H12    1E10                 
20080220003232008022000323CE  2008       2          20         CA070706001      120070706G3230AN33701         RELAY                                   BEECH 90    C90         1152913CE  PWA   PT6   PT6A21      52043EA  HARTZLHCB3T HCB3TN3     GL  LANDING GEAR    CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING ANNUAL INSPECTION OF THE HYD LANDING GEAR INSTALLATION THE LANDING GEAR RELAY EXHIBITED SIGNS OF HEAVY PITTING AND METAL TRANSFER. THE LANDING GEAR RELAY WAS REPLACED. (TC NR 20070706001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T4  T  3A20    E4EA    6  CP15EA    
20070820000882007082000088GL  2007       8          20         CA070706002      220070705G723023056109        SCROLL          RROYCE                  BELL  206   206L1       1182107SW  ALLSN 250C  250C28      03013GL                              COMPRESSOR      WARPED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7120       CAC70614                                            (CAN) DURING A GROUND RUN AN AIR LEAK WAS FOUND AT THE SCROLL DIFFUSER SPLIT LINE.  COMPRESSOR ASSY WAS CHANGED OUT. (TC NR 20070706002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3U3  U  H2SW    E1GL                 
20070820000892007082000089EU  2007       8          20         CA070706003      120070703G3240                BRAKE ASSY                              EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF34*            NE                              MLG             OVERHEATED      W      O   OTHER                                                                                           MJ OVER TEMP                 WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                                                                      (CAN) HOT BRAKE INDICATION ON TAXI IN OF 460 CELSIUS.  BRAKE OVERTEMP INSPECTION CARRIED OUT WITH NO FAULTS.  CMC MESSAGE BRAKE TEMP SENSOR OVERHEAT.  IAW FIM, REPLACE TEMP SENSOR.  PLACED ON MEL DUE NO STOCK. FOLLOWING DAY, RT IB/OB BRAKE TEMPERATURES CREPT UP TO 110/ 195 CELSIUS. THERE IS A HISTORY OF HYDRAULIC CONTROL PROBLEMS, POSSIBLE CAUSE IN THIS CASE MAY BE THE BRAKE CONTROL VALVE. (TC NR 20070706003)                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA57NM   E15NE                
20070820000902007082000090GL  2007       8          20         CA070706004      220070705G732023065144        FUEL CONTROL                            BELL  206   206L1       1182107SW  ALLSN 250C  250C28      03013GL                              ENGINE          UNSERVICEABLE   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       144671070                                                      (CAN) FUEL CONTROL WAS INTERMITTENT ON ENGINE LIGHT-OFF DURING A START.  FUEL CONTROL CHANGED OUT. (TC NR 20070706004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3U3  U  H2SW    E1GL                 
20080220003242008022000324NM  2008       2          20         CA070706005      120070703G5280450530501       SHEAR PIN                               PIPER PA60  PA60600     7106001NM  LYC   O540  IO540K1J5   41532EA  HARTZLHCC3Y HCC3YR2     NE  LG DOOR         SHEARED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF THE PILOT SELECTED GEAR UP, THE GEAR UP LIGHT FAILED TO ILLUMINATE. THE LANDING GEAR WAS EXTENDED AND THE AIRCRAFT LANDED AT AIRPORT. UPON INVESTIGATION THE LANDING GEAR DOOR SHEAR PIN WAS FOUND SHEARED. THE PIN WAS REPLACED, THE AIRCRAFT WAS PLACED ON JACKS AND A FUNCTION CHECK OF THE LANDING GEAR AND INDICATING SYSTEM WAS COMPLETED WITH NO FAULTS. THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070706005)                                                                                                                                                                                                                                                                                                   1M72 3O3  ORTA17WE   1E4     5  CP25EA    
20070820000912007082000091EA  2007       8          20         CA070707001      120070706G29100860163002      ACCUMULATOR                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              HYD SYSTEM      SEPARATED       W      D   RETURN TO BLOCK                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       25942                                                          (CAN) DURING TAXI-OUT, HYD 1 LO PRESS MESSAGE CAME ON.  THE CREW REPORTED LOUD BANG FROM AFT PART OF CABIN.  CREW EXECUTED RELEVANT ABNORMAL CHECKLISTS AND RETURNED TO RAMP.  AFTER VERIFICATION BY THE MTCE CREW, THEY FOUND OUT THAT THE NR 2 HYDRAULIC ACCUMULATOR SEPARATED. (TC NR 20070707001)                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA21EA   E15NE                
             20081104         2008       11         4          CA070708001      420070421G2562ELT10           ELT                                     CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA                              CABIN           MALFUNCTIONED   W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) ELT FOUND DEFECTIVE DURING ROUTINE INSP. ELT WAS FOUND MAKING SQUELCHING SOUND THROUGH RADIO, ON FURTHER INVESTIGATION IT WAS FOUND THAT ELT WAS ACTIVATED WHICH COULD NOT BE SWITCHED-OFF EVEN AFTER DISCONNECTING THE CONNECTOR/POWER. ELT WAS REMOVED FROM ACFT AND BATTERY WAS DISCONNECTED TO DEACTIVATE THE ELT.  ELT WAS SENT  FOR REPAIR. (TC NR20070708001)                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    E274                 
20070820000922007082000092WP  2007       8          20         CA070709001      120070706G270024031404021     SHAFT                                   CVAC  30    30          2423202WP  ALLSN 501D  501D13H     03004GL  ALLSN A6441 A6441FN606  GL  ROLL FORCE      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THE ROLL FORCE MODIFICATION WAS BEING INSTALLED IN THE  AIRCRAFT IAW STC SA05-49.  UPON TORQUING THE PILOT`S YOKE ASSEMBLY SHAFT IAW THE INSTRUCTIONS CONTAINED IN DOCUMENT K130-102-001-012, THE FLANGE ON THE SHAFT P/N 240-3140402-1 CRACKED.  THE REMAINING AIRCRAFT IN THE FLEET WERE INSPECTED FOR SIGNS OF PLAY WITH NO DEFECTS NOTED. THE AIRCRAFT ARE ALSO BEING INSPECTED FOR EXCESSIVE BREAK AWAY TORQUE OF CONTROL YOKE SHAFT NUT. ANY ADDITIONAL FINDINGS WILL BE FORWARDED UPON COMPLETION OF THE INSPECTIONS. (TC NR 20070709001)                                                                                                                                                                                          2L74 4J4  T  4A30    E282    6  CP898     
20070820000932007082000093NM  2007       8          20         CA070709002      120070707G2420HCAIN022        GENERATOR                               DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  NR 2            INOPERATIVE     W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AT THE END OF EXTENSIVE POST BLOCK CHECK GROUND RUNS; THE NR 2 ENG GEN FELL OFF LINE AND NR 1 TRU AND AC BUS FELL OFF LINE; TRIED TO POWER BACK AND RESET IT WAS NOTICED THAT THE AC GEN CAUTION LIGHT WAS NOT SHOWING. SO THE AIRCRAFT WAS SHUTDOWN AND AFTER SOME INVESTIGATION IT WAS FOUND THAT THE AC GEN CONTACTOR HC-AIN-022 HAD FAILED INTERNALLY MELTING THE RELAY AND ASSOCIATED WIRING. (TC NR 20070709002)                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080319001472008031900147NE  2008       3          19         CA070709003      220070705G73205018T64G02      MANIFOLD                                SKRSKYS61   S61N        8142104NE  GE    CT58  CT581401    30011NE                              LT FUEL         FRACTURED       W      FE  ACTIVATE FIRE EXT.      ENGINE SHUTDOWN                                                         BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CRCRUISE         1                      CA       10521209                           280140MA                    (CAN) THE PILOTS NOTICED A WARM SEMI SMOKE SMELL, AND OBSERVED A T5 RISE IN NR 1 ENGINE. THE FIRE LIGHT ACTIVATED ON NR 1 ENGINE. THE ENGINE WAS SHUT DOWN AS WELL AS A THE FIRE BOTTLES WERE ACTIVATED. THE AC LANDED WITH ONE ENGINE WITH NO INCIDENT. THE ENGINE WAS REPLACED. ENGINE TSN 23764.8, TSO 2373.5, (TC NR 20070709003)                                                                                                                                                                                                                                                                                                                                                                                                           2G72 4U4  U  1H15    1E3                  
20070820000942007082000094NM  2007       8          20         CA070709004      120070706G3244DR7622T         TIRE                                    BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  MLG             FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) LT INNER TIRE BLOWN AFTER TAKEOFF. UNSCHEDULED LANDING CARRIED OUT. A/C TOWED TO HANGER.  INSPECTION AND NR 1 AND NR 2 MAINWHEELS REPLACED.  TIRE WAS A RETREAD R2. (TC NR 20070709004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
             20081104     CE  2008       11         4          CA070710001      120070705G2434DOFF10300JR     ALTERNATOR                              CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA                              ENGINE          INOPERATIVE     W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       NRNOT REPORTED   1                      CA            351                                                       (CAN) ALTERNATOR NOT CHARGING . (TC NR 20070710001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A12    E274                 
20070820000952007082000095NM  2007       8          20         CA070710002      120070615G351017426008        OXYGEN MASK                             BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  COCKPIT         INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) F/O`S OXYGEN MASK WHEN DONED, WEARER COULD NOT EXHALE WHEN BREATHING. ENGINEERING INVESTIGATION INDICATES THAT THE MASK EXHALE VALVE IS DEFECTIVE. MASK REPLACED. AIRCRAFT RETURNED TO SERVICE SATISFACTORY. MASK HAS BEEN RETURNED TO THE MANUFACTURER FOR REPAIR AND WITH A REQUEST FOR A STRIP REPORT. (TC NR 20070710002)                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070820000962007082000096NM  2007       8          20         CA070710003      120070531G3150301450301       PSEU                                    BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  PROXIMITY SENSORINOPERATIVE     W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) ON DEPARTURE CLIMBING THROUGH 9000 FT, THE ENGINE DISPLAY POWERPLANT ADVISORY ILLUMINATED. FOLLOWING DISCUSSIONS WITH BASE ENGINEERING THE CREW DECIDED TO RETURN THE AIRCRAFT TO BASE WHERE AN APPROACH AND LANDING WAS CARRIED OUT WITHOUT INCIDENT. THE POWERPLANT ADVISORY FAULT CODE 338 IS THE 3RD OCCURRANCE ON THIS AIRCRAFT. FOLLOWING ADVICE FROM THE MFG AND DETAILED TROUBLESHOOTING THE AIRCRAFT`S PSEU WAS REPLACED. AIRCRAFT WAS RELEASED BACK TO SERVICE WHERE IT HAS OPERATED SINCE WITHOUT INCIDENT. (TC NR 20070710003)                                                                                                                                                                                                2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070820000972007082000097EA  2007       8          20         CA070710004      220070426G72303034051         GUIDE VANE                              DHAV  DHC7  DHC7102     2802708EA  PWA   PT6   PT6A50      52043EA  HAMSTD24PF  24PF305     GL  ENGINE          FAILED          W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA            73                            86123                       (CAN) DURING FLIGHT, THE TURBINE TEMPERATURE ROSE SUDDENLY FROM 738 TO 785 DEGREES CELSIUS. A BORESCOPE INSPECTION REVEALED DAMAGE TO THE CT GUIDE VANE. THE ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THE HOT SECTION WAS REMOVED FROM THE ENGINE AND FURTHER INSPECTED. ONE OF THE CT GUIDE VANES AIRFOIL-COOLING DUCT SURFACE HAD BEEN PREVIOUSLY REPAIRED. THE VANE CRACKED/FAILED AROUND THE WELDS ALLOWING THE COOLING DUCT TO OPEN UP AND BREAK AWAY.  WITHOUT THE PROPER COOLING THE VANE BURNED THROUGH. THE HOLE IN THE VANE CHANGED THE AIRFLOW ALLOWING DIRECT FLOW TO THE CT BLADES IN TURN CAUSING THEM TO OVERHEAT. GUIDE VANE CSO 48.  THIS IS THE SECOND FAILURE OF THIS NATURE AS  THE OTHER FAILURE OCCURRED2H74 4T4  T  A20EA   E4EA    6  CP1NE     
20070820000982007082000098CE  2007       8          20         CA070711001      120070605G7120                TUBE                                    CESSNA185   A185F       2072821CE  CONT  O520  IO520D      17032SO  HARTZLHCC3Y HCC3YF1     GL  RT NACELLE      CRACKED         W      K   NONE                                                                                            E  VIBRATION/BUFFET                                                              ININSP/MAINT     1                      CA       2590                                                           (CAN) ONE TUBE CRACKED NEAR RT REAR ENGINE LOAD MOUNT.  NEW MOUNT INSTALLED. (TC NR 20070711001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  O  3A24    E5CE    5  CP25EA    
20080220003252008022000325CE  2008       2          20         CA070711002      120070708G30201013800019      BOOT                                    BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  HORIZ STAB      DAMAGED         W      A   UNSCHED LANDING                                                                                 FE FLT CONT AFFECTED         VIBRATION/BUFFET                                    CLCLIMB          1                      CA                                                                      (CAN) THE AIRCRAFT DEPARTED AND BEGAN TO CLIMB TO CLEARED ALTITUDE. AS THE AIRCRAFT PASSED 5500 FEET THERE WAS A VIBRATION OR BUFFETING FELT THROUGH THE CONTROL COLUMN. THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. A THROUGH INSPECTION WAS CARRIED OUT WHICH REVEALED A DAMAGED LT HORIZONTAL DE-ICE BOOT. SEVERAL HOLES WERE FOUND AND REPAIRED IAW APPROVED PROCEDURES. THE AIRCRAFT WAS RETURNED TO SERVICE AND OPERATED WITHOUT ANY FURTHER PROBLEMS. (TC NR 20070711002)                                                                                                                                                                                                                                                            2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20070820000992007082000099EA  2007       8          20         CA070711003      120070711G2810215640024       FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE                  LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1924                                                           (CAN) FUEL CELL NR 7 RT, LEAKING BY THE LOWER INTERCONNECT CORNER.   A/C HOURS: 1924 CYCLES: 1236 DROPS: 9808  (TC NR 20070711003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20070820001002007082000100EA  2007       8          20         CA070711004      120070711G2810K215T6400212    FUEL CELL                               CNDAIRCL215 CL2156B11215       EA                                                                               LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) TESTED BEFORE INSTALLATION, THE CELL HAS BEEN FOUND WITH LOOSE LOWER PROBED ADAPTOR AND LEAKING BY THE TOP CORNER REPAIR PATCH . THE CELL HAS BEEN REJECTED. (TC NR 20070711004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T    RTA14EA                        
20070820001012007082000101CE  2007       8          20         CA070711005      120070711G251005142031        SEAT                                    CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA                              COCKPIT         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DEFECT REPORTED IN THE JOURNEY LOG BOOK THAT RT SEAT WOULD NOT ADJUST.  REMOVED SEAT, INSPECTED, AND FOUND THE SEAT BOTTOM FRAME CRACKED COMPLETELY IN (2) PIECES.  AREA IS DIFFICULT TO INSPECT BECAUSE OF UPHOLSTERY INSTALLATION.  LOWEST TIME IN THE FLEET. (TC NR 20070711005)                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  ONT3A12    E274                 
20070820001022007082000102EA  2007       8          20         CA070711006      120070711G2810K215T6400212    FUEL CELL                               CNDAIRCL215 CL2156B11215       EA                                                                               LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) TESTED BEFORE INSTALLATION, THE CELL HAS BEEN FOUND LEAKING BY A PIN HOLE NEAR UPPER PROBE ADAPTOR AND REJECTED. (TC NR 20070711006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T    RTA14EA                        
20070820001032007082000103GL  2007       8          20         CA070711007      120070710G2823TC17300         SELECTOR                                DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  FUEL            STIFF           W      K   NONE                                                                                            O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) REMOVED CABLE DRUM FROM FUEL SELECTOR, LUBRICATED SELECTOR WITH YIELD AND REINSTALLED CABLE DRUM. (TC NR 20070711007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3R3  RRCA806    5E1     5  CP206     
20070820001042007082000104NM  2007       8          20         CA070712001      120070709G6120699018002       CONTROLLER                              BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NR1 ENGINE      MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 FYJFLT CONT AFFECTED         ENGINE STOPPAGE           WARNING INDICATION        CRCRUISE         1                      CA       3109                                                           (CAN) DURING CRUISE AT 25,000 FT, THE NR 1 POWERPLANT AND NR 1 PEC (PROP ELECTRONIC CONTROLLER) CAUTION LIGHTS ILLUMINATED. THE NR 1 ENGINE WENT INTO THE AMBER.  PILOTS CARRIED OUT AN IN-FLIGHT SHUTDOWN, DECLARED AN EMERGENCY AND RETURNED TO BASE.  FAULT CODES 161 AND 157 WERE LOGGED IN THE CDS. PROPELLER ELECTRONIC CONTROL UNIT REPLACED, OVERSPEED GOVERNOR (OSG) FAULTS HAVE BEEN SINCE BEEN CLEARED AND FUNCTIONAL CHECKS HAVE BEEN COMPLETED. (TC NR 20070712001)                                                                                                                                                                                                                                                                2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070820001052007082000105EU  2007       8          20         CA070712002      120070710G2910TC2500065500    LINE                                    BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  HYDRAULIC SYS   PERFORATED      W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) AFTER DEPARTING, THE CREW OBSERVED BOTH THE LT AND RT HYDRAULIC PRESSURE LOSS INDICATION LIGHTS WERE ILLUMINATED. THE AIRCRAFT DIVERTED  AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NR 2 HYDRAULIC PRESSURE RETURN LINE TO THE HP FILTER IN THE WHEEL WELL PERFORATED DUE TO CONTACT WITH A BROKEN CLAMP WHICH SUPPORTS THE GENERATOR COOLING BLEED AIR LINE. BOTH ITEMS WERE REPLACED AFTER WHICH THE AIRCRAFT WAS SATISFACTORILY GROUNDED AND RETURNED TO SERVICE. FIRST AIR CONDUCTED A CHECK OF THE REMAINING SAME TYPE AIRCRAFT OPERATED AND FOUND NO SIMILAR CONDITION PRESENT. (TC NR 20070712002)                                                                                                                  2L72 3T4  T  A24EU   A196    6  CP899     
             20081104         2008       11         4          CA070712003      420070712G2562ELT97A256       ELT                                                                                                                                                     ACTIVATED       W      D   RETURN TO BLOCK                                                                                 N  FALSE WARNING                                                                 NRNOT REPORTED   1                      CA                                                                      (CAN) ELT ACTIVATED ON FIRST ENGINE START. DIDN`T LEAVE THE GROUND.  (TC NR 20070712003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  
20070820001062007082000106EA  2007       8          20         CA070713001      120070710G301014463108        PICCOLO TUBE                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                                              RUPTURED        W      H   DEACTIVATE SYST/CIRCUITS                                                                        J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) THE FLIGHT CREW RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE DURING FLIGHT. THE APPLICABLE SYNOPTIC PAGE SHOWED THE RT WING LEADING EDGE BEING AT FAULT. WING ANTI-ICE SWITCH WAS SELECTED FROM NORMAL TO STAND-BY WITHOUT SUCCESS. DURING TROUBLESHOOTING, MAINTENANCE DISCOVERED THE RT WING OB ANTI-ICE DUCT (PICCOLO TUBE) REF IPC 30-11-00-10-240C END CAP MISSING. THE WELDED PICCOLO TUBE END CAP HAS RUPTURED FROM THE ASSY. THE ANTI-ICE DUCT ASSY WAS REPLACED IAW AMM 30-11-41 AND THE AIRCRAFT RELEASED INTO SERVICE. (TC NR 20070713001)                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20080220003262008022000326EU  2008       2          20         CA070713002      120070712G6510350A34021006    DRIVE SHAFT                             SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              TAIL ROTOR      OUT OF ROUND    W      K   NONE                                                                                            E  VIBRATION/BUFFET                                                              ININSP/MAINT     1                      CA       2473                                                           (CAN) UNABLE TO BALANCE SHORT SHAFT, RUNOUT CHECK OF FWD END OF SHAFT WAS .017 INCH. PREVIOUS T-CHECK REVEALED A RUNOUT OF .009 INCH WITH TROUBLES OF SAME NATURE AND SHORT SHAFT WAS INSPECTED AND FOUND TO BE BENT, AND REPLACED WITH BALANCE OBTAINED. (TC NR 20070713002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H9EU    E19EU                
20070820001072007082000107EA  2007       8          20         CA070713003      220070706G7313252416314       SERVO                                   PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  FUEL INJECTOR   LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1225                          L653661A                    (CAN) FUEL INJECTOR SERVO ON LT ENGINE FOUND TO HAVE AN INTERNAL LEAK AND WOULD NOT SHUTDOWN PROPERLY.  SERVO WAS REMOVED AN OVERHAULED UNIT INSTALLED ENGINE GROUND RUN. (TC NR 20070713003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070820001082007082000108GL  2007       8          20         CA070715001      220070714G7261                FITTING                                 LKHEED188   188C        5262604SO  ALLSN 501D  501D13      03004GL  ALLSN A6441 A6441FN606  GL  OIL SYSTEM      LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) THE CREW NOTICED A LOSS OF OIL QUANTITY ON THE NR 3 ENGINE. THIS LOSS WAS FOLLOWED BY A FLUCTUATION IN THE REDUCTION GEARBOX PRESSURE. THE ENGINE WAS SHUTDOWN PRIOR TO LANDING. IT WAS DETERMININED THAT A FITTING ON THE TURBINE SECTION WAS LEAKING. THERE WAS 3-4 GALLONS OF OIL REMAINING IN THE RESEVOIR, THE AIRCRAFT WAS FERRIED FOR AN ENGINE CHANGE. (TC NR 20070715001)                                                                                                                                                                                                                                                                                                                                                        2L74 4T4  T  4A22    E282    6  CP898     
20070820001092007082000109EA  2007       8          20         CA070716001      120070714G5343215340711       MOUNT                                   CNDAIRCL215 CL2151A10   1900320EA  PWA   R2800 R2800CA3    52026NE  HAMSTD43E   43E60       NE  LANDING GEAR    DAMAGED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED AND THE RT/MAIN GEAR DID NOT INDICATE UP AND LOCKED. THE GEAR WAS SELECTED DOWN AND ALL (3) GEAR INDICTED DOWN AND LOCKED. MAINTENANCE HAS FOUND THE RT MAIN GEAR ACTUATOR MOUNTING DAMAGED. PARTS 215-34071-1,215-34071,215-34014-3,215-34014-2 ON ORDER. (TC NR 20070716001)                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4R4  RRTA14EA   5E8     6  CP871     
20070820001102007082000110EU  2007       8          20         CA070716002      120070713G3150                WARNING MESSAGE                         AIRBUS320   A320211     3930320EU  CFMINTCFM56 CFM565A1         NE                              STAB TRIM       ACTIVATED       W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       5151937472                                                     (CAN) AFTER DEPARTURE, AN ECAM MSG INDICATED STAB TRIM FAILURE.  NEITHER OF THE AUTOPILOTS COULD BE RE-ENGAGED.  AN EMERGENCY WAS DECLARED WITH ATC AND THE FLIGHT LANDED APPROX 7.5 TONS OVERWEIGHT. (TC NR 20070716002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA28NM   E29NE                
20070820001122007082000112NM  2007       8          20         CA070717001      120070626G2497                WIRE                                    BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  EDU             DAMAGED         W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       APAPPROACH       1                      CA                                                                      (CAN) LATE IN THE AIRCRAFT`S LANDING SEQUENCE, THE FLIGHT DECK ENGINE DISPLAY SUFFERED A FAILURE CAUSING THE DISPLAY TO GO BLANK. THE LANDING WAS COMPLETED WITHOUT INCIDENT. ONCE SHUTDOWN ON THE RAMP, THE CREW IDENTIFIED THAT ONE OF THE ESID CIRCUIT BREAKERS WAS (POPPED).  FOLLOWING ADVICE FROM ENGINEERING, ATTEMPTS TO RESET THE CIRCUIT BREAKER WERE UNSUCCESSFUL. ON SITE ENGINEERING INVESTIGATION IDENTIFIED THAT BOTH POWER WIRES TO THE EDU WERE DAMAGED DUE CHAFING RESULTING IN A SHORT CIRCUIT TO GROUND. DAMAGED WIRES WERE REPAIRED IAW MM PROCEDURES. IT WAS ESTABLISHED THAT THE WIRE CHAFING WAS DUE TO INCORRECT FACTORY INSTALLATION OF THE WIRING LOOM EDU CONNECTOR BACKSHELL WHICH IN TURN ALLOWS THE LOOM WIRES TO2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070820001132007082000113NE  2007       8          20         CA070717002      220070704G73214120T01P02      FMU                                     CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF34*            NE                              NR 1 ENGINE     UNSERVICEABLE   W      C   ABORTED TAKEOFF                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  TOTAKEOFF        1                      CA                                                                      (CAN) STARTING T/O, NR 1 ENGINE DID NOT RESPOND TO THROTTLE IN TOGA POSTION.  ENGINE REMAINED AT IDLE. AFTER 10 SECONDS L ENGINE FLAMEOUT CAUTION MSG. T/O ABORTED AT 40 KNOTS.  MDC (MAINTENANCE DIAGNOSTICS COMPUTER) INTERROGATED BY MAINTENANCE. FAULT CODE 353 BIT 29 SET, FMU CMD/POS DISAGREE (WF METERING VALVE ACTUAL POSITION DOES NOT MATCH EXPECTED POSITION BASED ON COMMAND).   SUSPECT WF METERING VALVE TORQUE MOTOR. SUSPECT FAULTY COMPONENT: FMU 4120T01P02).  FMU P/N4120T01P02  S/N12391265 REMOVED AND CHANGED IAW AMM 73-21-02-400-801-A01. ENGINE LEAK CHECKED AND FUNCTIONED SATISFIED. AIRCRAFT RETURNED TO SERVICE. (TC NR 20070717002)                                                                              2L72 4F4  FRTA21EA   E15NE                
20080220003272008022000327SW  2008       2          20         CA070717003      120070629G52102050314352      BRACKET                                 BELL  212   212         1181420SW  PWA   PT6T  PT6T3       52045EA                              PAX DOOR        BROKEN          W      O   OTHER                                                                                           N  FALSE WARNING                                                                 APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH TO THE LANDING AREA, THE (DOOR LOCK) LIGHT ON CAUTION PANEL ILLUMINATED. AIRCRAFT LANDED SAFELY WITHOUT ANY FURTHER INCIDENT. UPON LANDING THE ENGINEER EXITED THE AIRCRAFT AND PHYSICALY CHECKED ALL DOORS AND PANELS TO ENSURE THAT THEY WERE CORRECTLY SECURED. NO DOORS OR PANELS WERE FOUND OPEN.  UPON INVESTIGATION OF THE RT PASSENGER/CARGO DOOR, IT WAS FOUND TO BE LOOSE IN THE DOOR TRACK. FURTHER INVESTIGATION REVEALED THAT THE UPPER FWD ROLLER BRACKET HAD FAILED. THIS ALLOWING THE MICRO-SWITCH TO BE DEACTIVATED, AND THE LIGHT COMING ON.   THE BRACKET WAS REPLACED AND NO FURTHER PROBLEMS EXISTED. (TC NR 20070717003)                                                                                1G71 4U4  U  H4SW    E22EA                
20070820001142007082000114EA  2007       8          20         CA070717004      120070628G521085210240055     ROD                                     DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  PAX DOOR        FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) PASSENGER DOOR AFT SUPPORT STRUT BROKE MAKING IT DIFFICULT TO OPEN THE MAIN CABIN DOOR.  EXPLANATION CODES: 7(A) SPECIAL OPS- AIRCRAFT HAD ALREADY LANDED AND PASSENGERS WERE ABOUT TO DISEMBARK. 7(B)  DOOR WAS DIFFICULT TO OPEN. 7(C) DOOR WAS OPENED BY (2) CREW MEMBERS. (TC NR 20070717004)                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070820001152007082000115NE  2007       8          20         CA070717005      220070619G7310021578201       FILTER                                  CESSNA425   425         2076018CE  PWA   PT6   PT6A112     52043NE  MCAULY3G34C73GFR34C701  GL  FUEL PUMP       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING AN INSPECTION THE INLET FILTER WAS REMOVED. THE FILTER COVER (CAP) WAS FOUND CRACKED UNDER THE O-RING LOCATION ALL THE WAY AROUND. IT APPEARS TO HAVE BEEN OVER TORQUED. IT WAS NOT LEAKING AT THIS TIME. THE INLET FILTER ASSEMBLY WAS REPLACED. (TC NR 20070717005)                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 3T3  TRTA7CE    E4EA    5  CP60GL    
20080306000462008030600046    2008       3          6          CA070717006      420070705G3197                WIRE HARNESS                            UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                                              BURNED          W      O   OTHER                                                                                           N  FALSE WARNING                                                                 CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE FLIGHT, PILOT NOTED THE V/A INDICATION ON THE VEMD WAS OSCILLATING INTERMITTENTLY BETWEEN PARAMETERS, AS WELL, THE LOW ROTOR AURAL WARNING WAS INTERMITTENTLY SOUNDING AND AT TIMES WAS ON STEADY. AT NO TIME WERE ANY ANOMOLIES NOTICED IN THE COCKPIT ENGINE INDICATIONS OR ENGINE PERFORMANCE. UPON LANDING, THE PILOT NOTED THE VEMD CIRCUIT BREAKER ON THE COCKPIT PANEL WAS TRIPPED. AFTER SUBSEQUENT TROUBLESHOOTING, IT WAS FOUND THAT THE WIRE HARNESS LEADING UP TO THE VEMD WAS PINCHED BETWEEN THE TOP AFT LT CORNER OF THE VEMD (VIEWED LOOKING FORWARD WITH VEMD INSTALLED AND GLARESHIELD REMOVED) AND THE GLARESHIELD ITSELF. SEVERAL WIRES WERE FOUND CHAFED THROUGH AND/OR BURNED THROUGH ALTOGETHER. UPON1G72 3U3  UNCR0001RD E34NE                
20070820001162007082000116CE  2007       8          20         CA070717007      120070623G3230NAS464P6A16     BOLT                                    CESSNA177   177RG       2073709CE                                                               MLG             SHEARED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       3940                                                           (CAN) MAIN GEAR JAMMED ON RETRACTION FROM TAKEOFF. LANDED WITH MAIN GEAR PARTIALLY EXTENDED. (TC NR 20070717007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O      A20CE                        
20070820001172007082000117    2007       8          20         CA070717009      420070512G6113                BRACKET                                 CESSNA120   120         2071402CE  CONT  C85   C8512F      17008SO  MCAULY1B90  1B90CM      GL  SPINNER         BROKEN          W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA                                                                      (CAN) V-BRACKET OF SPINNER BROKE ON ONE SIDE, THAT CAUSED OFFSET OF SPINNER WHICH CAUSED VIBRATION AND DECIDED TO CONDUCT A PRECAUTIONARY LANDING ON A FARMERS FIELD. NO FURTHER DAMAGE. (TC NR 20070717009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  O  A768    E233    5  NP842     
20070820001182007082000118NM  2007       8          20         CA070717010      120070703G2797BACC63BV22F55PN CONNECTOR                               BOEING737   737800*            NM  CFMINTCFM56 CFM567B26US      NE                              TE FLAPS        CORRODED        W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       19956                                                          (CAN) AFTER FLAP 25 TAKEOFF, WHEN FLAP RETRACTION INITIATED, FLAP ASYMMETRY INDICATED AND TE FLAP SKEW SENSOR CB POPPED. AIRCRAFT RETURNED TO JTR. SFCC BITE TEST CARRIED OUT, MSG 27-51407 INTERMITTENT. FIM TASK 27-51-00-810-848 CARRIED OUT WITH NO FINDINGS. VISUAL CHECK OF SLAT/FLAP SYSTEM CARRIED OUT WITH NO FINDINGS. OVERWEIGHT LANDING INSP CARRIED OUT WITH NO FINDINGS. AC DEPARTED TO DUB. ON APPROACH TO DUB, MACH TRIM LIGHT CAME ON MOMENTARY, FOLLOWED BY NO PITCH COMMANDS ON CAPTAIN`S FD, NO AP A AND MAGENTA IAS INDICATION ON CAPTAIN`S DU. WHEN FLAP SELECTED TO 1, FLAP ASYMMETRY INDICATION OBSERVED AND TE FLAP SKEW SENSOR CB WAS FOUND POPPED. AFTER EXTENSIVE TROUBLESHOOTING A SHORT WAS FOUND IN THE LT TE FLA2L72 4F4  FRTA16WE   E00055EN             
20070820001192007082000119CE  2007       8          20         CA070717011      120070621G321321A05000016     ARM                                     CESSNA172   172N        2072434CE  LYC   O360  O360A1F6    41514EA  MCAULY1A200 1A200FA     GL  FLOATS          BENT            W      E   ENGINE SHUTDOWN                                                                                 O  OTHER                                                                         LDLANDING        1                      CA       244        23076                                               (CAN) ON ROLL OUT AFTER LANDING THE RT MAIN LANDING GEAR COLLAPSED. INVESTIGATION FOUND THAT THE ACTUATING CYLINDER BENT (P/N D68194-A-4). FURTHER INVESTIGATION FOUND THE RETRACT ARM P/N 21A05000-016 HAD WORN ELONGATED BOLT HOLES NOT ALLOWING A DOWN LOCK OVER CENTRE POSITION. (TC NR 20070717011)                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A12    E286    5  NP874     
20070820001202007082000120NE  2007       8          20         CA070717012      220070611G8510288935          THRUST BEARING                          DHAV  DHC3  DHC3        2800202EA  PWA   R1340 R134059     52016NE  HAMSTD23D   23D40       NE  PROPELLER       BROKEN          W      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              TXTAXI/GRND HDL  1                      CA       851                                                            (CAN) WHILE TAXIING FROM DOCK, THE AIRCRAFT ENGINE STARTED SHAKING AND THE PILOT SHUT THE ENGINE DOWN. AIRCRAFT TOWED BACK TO DOCK. AFTER RE-STARTING, STRANGE NOISES FROM NOSE CASE, AND PROPELLER LOOKED (OUT OF TRACK).  PROPELLER REMOVED FROM COVER ON NOSE CASE REMOVED. BEARING SEPARATOR HAD STARTED TO BREAK UP. (TC NR 20070717012)                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3R3  R  A815    5E2     6  CP719     
20070820001212007082000121EA  2007       8          20         CA070717014      220070711G7261061040M0240180  LINE                                    DHAV  DHC6  DHC6100     2802610EA  PWA   PT6   PT6*        52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE OIL      FAILED          W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) THE CREW OF FLOATPLANE EXPERIENCED A 10 LB LOSS OF TORQUE IN CRUISE ALONG WITH LOWERED OIL PRESSURE AND AN INCREASE IN OIL TEMP.  THE PILOT CONTINUED THE FLIGHT TO A MAINTENANCE BASE USING REDUCED POWER ON THE AFFECTED ENGINE.  AN UNEVENTFUL LANDING AND DOCKING WAS MADE.  MAINTENANCE INVESTIGATION REVEALED THAT THE MAJORITY OF THE ENGINE OIL SUPPLY HAD BEEN EJECTED THROUGH THE ENGINE BREATHER SYSTEM.  INSPECTION OF THE ENGINE OVERBOARD BREATHER LINE INTERNALLY REVEALED THAT IT HAD BROKEN DOWN AND PARTIALLY PLUGGED THE ACCESSORY CASE VENTING SYSTEM.  THIS CAUSED THE ACCESSORY CASE TO PRESSURIZE AND THE ENGINE OIL TO VENT OVERBOARD.  THE BREAKDOWN OF THE LINE RESULTED FROM THE LINE BEING POORLY ROUTED DURIN1H72 3T3  TRTA9EA    E2NE    6  CP15EA    
20070820001222007082000122NE  2007       8          20         CA070717015      220070711G7321806304101A      FUEL CONTROL                            PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  ENGINE          MALFUNCTIONED   W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA       590  63                                                        (CAN) ON TAKEOFF, THE FULL ENGINE POWER (43 PSI) WAS NOT ACHIEVABLE, 35 PSI WAS ALL THE ENGINE WOULD PRODUCE. THE PILOT REPORTED ENGINE WAS NOT CONTROLABLE WITH POWER LEVER WHEN PULLED TO IDLE (ENGINE AT 35 PSI TORQUE). ADVISED NOT TO TRY AND START THE ENGINE AND TO REPLACE THE FCU. FCU WAS REPLACED AND ALL ENGINE RUNS CHECKED SERVICEABLE. (TC NR 20070717015)                                                                                                                                                                                                                                                                                                                                                                       1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20070820001232007082000123    2007       8          20         CA070717016      420070705G2562C5895120103     ELT                                     CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA                              CABIN           INTERMITTENT    W      O   OTHER                                                                                           N  FALSE WARNING                                                                 LDLANDING        1                      CA            91                                                        (CAN) EARLY ACTIVATION. SELF-ACTIVATION REPORTED TWICE. (TC NR 20070717016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  ONT3A12    E274                 
20070820001242007082000124NM  2007       8          20         CA070717017      120070703G5753NAS679A3W       NUT                                     BOEING727   727225      1384077NM  PWA   JT8   JT8D15      52051NE                              TE FLAPS        LOOSE           W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH, CREW SELECTED FLAPS FROM 2 TO 5 AND HAD AN AMBER LIGHT INDICATION FOR THE NR 1 KRUGER FLAP INDICATING STILL RETRACTED. FELT MODERATE VIBRATION AND DECLARED AN EMERGENCY.  UNEVENTFUL LANDING.  MAINTENANCE CYCLED SYSTEM AND COULD NOT FAULT. FURTHER INSPECTION FOUND THE NR 1 KRUGER FLAP SWITCH LINK BOLT/NUT LOOSE.  (TC NR 20070717017)                                                                                                                                                                                                                                                                                                                                                                                2L73 4F4  F  A3WE    E2EA                 
20070820001252007082000125GL  2007       8          20         CA070717019      120070717G5270SAL2D864        PLUNGER                                 DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  DOOR SWITCH     SEIZED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1090                                                           (CAN) AT INSPECTION OBSERVED THE FRONT DOOR HANDLE IN OPEN POSITION BUT STILL ABLE TO START ENGINE.   UPON INSPECTION, FOUND WITH DOOR OPEN MANUALLY OPERATING PLUNGER ON FORWARD DOOR LOCK OUT SWITCH ON LOWER DOOR SILL, FOUND SWITCH PLUNGER SEIZED IN CLOSED POSITION. THIS CAN ALLOW AIRCRAFT TO BE STARTED WITH FORWARD DOOR NOT LATCHED PROPERLY. RECTIFICATION IS TO REPLACE SEIZED SWITCH PLUNGER AND LUBRICATE SWITCHES ON A REGULAR BASIS. (TC NR 20070717019)                                                                                                                                                                                                                                                                       1H71 3R3  RRCA806    5E1     5  CP206     
20070820001262007082000126NM  2007       8          20         CA070718001      120070708G7931310573501A      REGULATOR                               DHAV  DHC8  DHC8101     2809002NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  ENGINE OIL      FLUCTUATES      W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CRCRUISE         1                      CA            8278                          121242                      (CAN) DURING FLIGHT, THE OIL PRESS INDICATOR NR 1 ENGINE, DROPPED TO 50 PSI. QRH DRILL COMPLETED, UNSCHEDULED LANDING COMPLETED. OIL PRESSURE REGULATOR ASSEMBLY REPLACED IAW AMM 71-01-50, SYSTEM TESTED SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070718001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070820001272007082000127CE  2007       8          20         CA070718002      120070717G32302317100016      ACTUATOR                                LEAR  60    60LEAR      5170707CE  PWA   305   PW305A      52128NE                              NLG             FAULTY          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA       4538 4538                                                      (CAN) DURING ARRIVAL, NOSE LANDING GEAR WOULD NOT INDICATE DOWN AND LOCK.  ALTERNATE GEAR EXTENSION WAS PERFORMED.  AIRCRAFT WAS FERRIED, FUNCTIONAL CHECK OF THE EMERGENCY GEAR EXTENSION WAS CHECKED, NOSE GEAR STAYED IN WHEEL WELL.  FREE FALL PRESSURE TESTED AND FOUND TO BE BETWEEN 85 TO 90 LBS (MAX LIMIT 20 LBS).  GEAR DOOR AND GEAR ACTUATOR WAS DISCONNECTED AND GEAR FREE FALL WAS CHECKED AND FOUND TO BE WITHIN LIMITS.  SUSPECT FAULTY INTERNAL GEAR ACTUATOR LOCKING SLEEVE.  NOSE GEAR ACTUATOR REPLACED.  FUNCTIONAL CHECK CARRIED OUT-SERVICEABLE. (TC NR 20070718002)                                                                                                                                                     2L72 4F4  FRTA10CE   E35NE                
20070820001282007082000128    2007       8          20         CA070718003      420070717G3418906100004       COMPUTER                                DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  STALL WARNING   FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA       8277                                                           (CAN) DURING CRUISE, THE NR 2 STALL SYSTEM FAIL AND PUSHER SYSTEM FAIL CAUTION LIGHTS ILLUMINATED.  QRH CHECKLIST WAS PERFORMED.  UNSCHEDULED LANDING COMPLETED. DUAL STALL WARNING COMPUTER DETERMINED TO BE THE CAUSE OF THE REPORTED DEFECT.  DUAL STALL WARNING COMPUTER REPLACED IAW AIRCRAFT MM CHAPTER 27-33-00 AND SYSTEM TESTED SERVICEABLE.  AIRCRAFT RETURNED TO SERVICE. (TC NR 20070718003)                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070820001292007082000129CE  2007       8          20         CA070718004      120070714G6120022A431113      LEVER                                   MTSBSIMU2   MU2B36      5780412CE  GARRTTTPE331TPE33110    01514WP  HARTZLHCB3T HCB3TN5     GL  PROP PITCH      LOOSE           W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             DEDESCENT        1                      CA       4539 4539                                                      (CAN) THE PPC LEVER WAS FOUND SEPARATED FROM THE PPC INPUT SHAFT.  THE BOLT WAS OF THE CORRECT P/N, YET WAS THREAD BOUND WITHOUT PRODUCING ENOUGH TENSION TO HOLD THE PPC ARM ONTO THE PPC SHAFT.  THE PPC ARM WAS REINSTALLED AND A WASHER WAS PLACED UNDER THE HEAD OF THE BOLT TO PROVIDE A BETTER GRIP ON THE SPLINED SHAFT.    THE PPC INPUT SHAFT HAS A THREADED BORE WHICH WOULD ALLOW THE USE OF AN ADDITIONAL BOLT AND WASHER AS A BACKUP RETAINER FOR THE PPC ARM IN THE EVENT THAT THE ARM WERE TO LOOSEN OFF.  THE AIRFRAME IPC DOES NOT SHOW A BOLT FOR THIS PURPOSE.  (TC NR 20070718004)                                                                                                                                         1H72 3T4  TRTA10SW   E4WE    6  CP15EA    
20070820001302007082000130GL  2007       8          20         CA070718005      220070715G72406899081         COMBUSTION LINER                        BELL  206   206L1       1182107SW  ALLSN 250C  250C30P     03013GL                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1008                                                      (CAN) COMBUSTION LINER REMOVED AND INSPECTED DURING UN-RELATED ENGINE MAINTENANCE. FOUND CRACKED AND WARPED BEYOND LIMITS. (TC NR 20070718005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3U3  U  H2SW    E1GL                 
20070820001312007082000131CE  2007       8          20         CA070718006      120070627G531205120151        BULKHEAD                                CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160DTM    GL  FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2884                                                           (CAN) DURING THE 200 HOUR INSPECTION, A ONE-INCH CRACK WAS NOTED RUNNING HORIZONTALLY ACROSS THE FLANGE BEND RADIUS AT THE LOWER LT CORNER OF THE BULKHEAD.  A SMALL DENT WAS NOTED AT THIS POINT, PROBABLY EXISTING SINCE MFG, STRESSING THE ALUMINUM AND TIGHTENING THE BEND RADIUS SOMEWHAT.  THIS AREA CAN BE FELT TO FLEX SLIGHTLY WHEN THE TAIL IS MANUALLY MOVED SIDEWAYS. (TC NR 20070718006)                                                                                                                                                                                                                                                                                                                                           1H71 3O3  ONT3A12    E274    5  NP910     
20080306000472008030600047SW  2008       3          6          CA070719001      120070716G7603212060722001    MOUNT                                   BELL  412   412EP       1182205SW                                                               THROTTLE        INTERFERENCE    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       284                                                            (CAN) DURING A SCHEDULED INSPECTION, AN AREA OF INTERFERENCE BETWEEN THE A THROTTLE JACKSHAFT MOUNT ASSY AND THE LT AIR INLET DUCT WAS IDENTIFIED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1G72 4U      H4SW                         
             20081104         2008       11         4          CA070719007      420070718G2330178661101       ELECTRICAL BOX                          BOEING777   777*        UTILUSENM                                                               SEAT            BURNED          W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                                                                      (CAN) THE VIDEO ENTERTAINMENT SYS ON 3 SEATS WAS NOT WORKING. WHEN THE SEAT ELECTRONICS BOX WAS ACCESSED AND REPLACED DAMAGE WAS NOTED ON THE REMOVED UNIT. SOOT ASSOCIATED WITH WHAT APPEARED TO BE BURNED CIRCUIT CARD IN THE SEU WAS OBSERVED. AN ELECTRICAL BURNING TYPE ODOR WAS PRESENT IN THE AREA. (TC NR 20070719007)                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F    RTT00001SE                     
20080306000482008030600048SW  2008       3          6          CA070719008      120070719G6320206040581001    TUBE                                    BELL  206   206L1       1182107SW  ALLSN 250C  250C30P     03013GL                              XMSN OIL        CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) OIL LINE CRACKED IN BEND JUST FWD TO FLARED FITTING. SUSPECT FATIGUE FROM IMPROPER TIGHTENING AT SOME POINT THROUGHOUT THE LIFE OF THE LINE. SUSPECT THIS TUBE WAS ORIGINAL EQUIPMENT. UNABLE TO DETECT LEAK ON GROUNG RUN LEAK CHECK AS THE MAINROTOR TRANSMISSION WOULDN`T BE WARM ENOUGH TO BE SENDING OIL TO THE OIL COOLER. (TC NR 20070719008)                                                                                                                                                                                                                                                                                                                                                                                      1G71 3U3  U  H2SW    E1GL                 
20070820001322007082000132NM  2007       8          20         CA070719009      120070628G2750745583A         FLEX DRIVE                              DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  TE FLAPS        SEIZED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) FLIGHT CREW REPORTED (FLAP DRIVE) CAUTION LIGHT ILLUMINATED FROM 2-3 SECONDS WHEN FLAPS SELECTED. MAINTENANCE INSPECTION FOUND FLAP SECONDARY DRIVE, IN WING CENTER SECTION, CORE HAD UNWOUND AND SEIZED CAUSING THE CASING TO ROTATE AND DAMAGED SUPPORT BRACKET AND TORQUE SENSOR.  FLAP CORE APPEARED TO LACK LUBRICATION AND RUST WAS EVIDENT. FLAP SECONDARY FLEX SHAFT REPLACED. ALL OTHER FLAP SECONDARY DRIVES LUBRICATED.  BRACKET AND TORQUE SENSOR DAMAGE REPAIRED. AIRCRAFT RETURNED TO SERVICE. FLAP SECONDARY DRIVE IS CLASSIFIED AS AN EXPENDABLE PART AND TIME ON PART NOT TRACKED. (TC NR 20070719009)                                                                                                                   2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070820001332007082000133NM  2007       8          20         CA070720003      120070717G2910AE7128852       HOSE                                    BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NLG ACTUATOR    RUPTURED        W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) DURING SELECTING GEAR UP, THE CAUTION WARNING AND NOSE GEAR INDICATED NOT UP, MAIN GEAR UP.  SUBSEQUENTLY NOTED (NR 2 HYDRAULIC SYSTEM ZERO QUANTITY.  FLUID LOSS DUE TO DAMAGED HYDRAULIC PIPE IN NLG WELL. REPAIRS COMPLETED, AC RTS. (TC NR 20070720003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070820001342007082000134CE  2007       8          20         CA070720004      120070718G2730EM21542         CURRENT LIMITER                         LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              ELEVATOR        FAILED          W      K   NONE                                                                                            N  FALSE WARNING                                                                 ININSP/MAINT     1                      CA       2312                                                           (CAN) WHEN COMPLETING POST FLIGHT INSPECTION (DI), AN AMBER CAS MESSAGE, ELEVATOR DISCONNECT WAS NOTICED ON THE EICAS DISPLAY.  ELEVATOR DISCONNECT WAS NOT ACTUATED AT THIS TIME (THIS INDICATES THE ELEVATORS ARE DISCONNECTED ON THE GROUND).  ELEVATOR DISCONNECT FUNCTION CHECKED AND IT WAS DISCOVERED THAT THE ELEVATORS WOULD NOT DISCONNECT.  SYSTEM TROUBLESHOT AND FOUND THAT CURRENT LIMITER HAD FAILED.  A NEW LIMITER WAS ORDERED AND INSTALLED.  ELEVATOR DISCONNECT SYSTEM FUNCTION CHECKED SERVICEABLE.  MFG NOTIFIED OF FAILURE. (TC NR 20070720004)                                                                                                                                                                          2L72 4F4  FRTT00008WIE6WE                 
20070820001352007082000135SW  2007       8          20         CA070720005      120070719G2742                ACTUATOR                                SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  PITCH TRIM      MALFUNCTIONED   W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA            898                                                       (CAN) AFTER FLAP RETRACTION, FLIGHT CREW DISCOVERED THAT THEY HAD NO CONTROL OF PITCH TRIM USING PRIMARY OR SECONDARY CIRCUITS. AFTER DISCUSSION WITH MAINTENANCE, FLIGHT CONTINUED TO MAINTENANCE BASE WHERE MAINTENANCE REPLACED TRIM ACTUATOR. (TC NR 20070720005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4T4  TRTA8SW    E4WE    5  CP10NE    
20070820001362007082000136EU  2007       8          20         CA070720006      120070707G324003024400        BRAKE ASSY                              PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  MLG             FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA            825                                                       (CAN) WHILE AIRCRAFT WAS BEING PUSHED BACK USING A TOWING DEVICE PART OF THE BRAKE ROTORS CAME LOOSE ON THE RT MLG AND PUNCTURED THE RIM ASSEMBLY.  CAUSED THE TIRE TO GO FLAT. BRAKE DISC AND WHEEL.  REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.  WAS INFORMED BY THE LOCAL DEALER THAT THE ROTORS USED IN THIS BRAKE DISC WERE SUPPOSED TO BE NEW AND IMPROVED JUST FOR THIS SITUATION. (TC NR 20070720006)                                                                                                                                                                                                                                                                                                                           1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080306000492008030600049SW  2008       3          6          CA070720007      120070710G6230212040136001    BEARING         BELL                    BELL  205   205A1       1181414SW  LYC   T53   T5317BLYC   41616NE                              MAST            SPALLED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            2210  A1212568                                            (CAN) THIS PN BEARING IS A (ON CONDITION) PART. THE MAST WAS LAST OVERHAULED 2210.4 HOURS AGO. THE ENGINEER FOUND FERROUS METAL IN THE TRANSMISSION INTERNAL AND EXTERNAL FILTERS. A POWDER OR PASTE WAS FOUND ON THE TRANSMISSION CHIP DETECTOR, NOT ENOUGH TO ACTIVATE A CHIP LIGHT. (TC NR 20070720007)                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 4U4  U  H1SW    E17EA                
20070820001372007082000137GL  2007       8          20         CA070720008      220070718G7230                COMPRESSOR                              LKHEED382   382G        526414USO  ALLSN 501D  501D22A     03006GL  HAMSTD54H   54H60117    NE  ENGINE          ERODED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA            6233                          550195                      (CAN) DEPARTING DESTINATION, THE CREW NOTED A COMPRESSOR STALL CONDITION ASSOCIATED WITH HIGH TGT ON NR 1 ENGINE. THE CREW CARRIED OUT A PRECAUTIONARY SHUTDOWN, RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM.   MAINTENANCE FOUND SIGNIFICANT EROSION IN THE COMPRESSOR 5TH AND 10TH STAGE BY VISUAL INSPECTION AND ELECTED TO REPLACE THE ENGINE. (TC NR 20070720008)                                                                                                                                                                                                                                                                                                                                                    2H74 4T4  T  A1SO    E282    6  CP906     
20070820001392007082000139EU  2007       8          20         CA070720010      120070718G215015310000        A/C PACK                                BAG   JETSTMJETSTM3212  1500217EU                                                               RIGHT           SEIZED          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA            328                                                       (CAN) PILOT REPORTED OVER TEMP LIGHT, AND CONTINUED FLIGHT IAW J-31 MEL.  UPON TROUBLESHOOTING IT WAS FOUND THAT THE RT CAU WAS SEIZED.  CAU WAS REPLACED WITH OVERHAULED UNIT AND AIRCRAFT RETURNED TO SERVICE.  THIS UNIT HAS A 6000 HOUR LIFE BETWEEN OVERHAULS, AND FAILED AFTER 327.5 HOURS IN SERVICE. SEIZED UNIT WILL BE SENT FOR WARANTY OVERHAUL. (TC# 20070720010)                                                                                                                                                                                                                                                                                                                                                                   2L72 4T    RTBA15CAA                      
20080306000502008030600050SW  2008       3          6          CA070720011      120070710G6220206011260103    BOLT                                    BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              MAIN ROTOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1141 1141                                                      (CAN) MAIN ROTOR PARTS SENT TO NDT FOR INSPECTION AND ON MAGNAFLUX INSPECTIION FOUND STRAP BOLT CRACKED ON SHANK ABOUT ONE QUARTER WAY AROUND. PART SENT TO BELL HELICOPTER LAB FOR FURTHER INVESTIGATION. BOLT WAS PURCHASED NEW ON MARCH 14,2005 (TC NR 20070720011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3U3  U  H2SW    E4CE                 
20070820001402007082000140EA  2007       8          20         CA070721001      120070718G3297                WIRE HARNESS                            CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              MLG             FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                                                      (CAN) THE A/C ARRIVED AND WAS TAXIING TO THE GATE WHEN IT WAS NOTED THAT NR 3 BTMS WAS ON THE RISE AND SUSPECTED DRAGGING BRAKES.  THE FLIGHT CREW NOTICED THAT THE BRAKE TEMP MONITOR DROPPED TO ZERO.  THE CAPTAIN GOT OUT OF THE A/C TO CHECK THE RT GEAR WHEN HE SAW THAT IT WAS ON FIRE, AT THIS TIME THE RAMP CREW EXTINGUISHED THE FIRE WITH A FIRE EXTINGUISHER.  MAINTENANCE ON THE SCENE REPLACED NR3 MAIN WHEEL AND FOUND THAT THE DISCONNECT ON NR3 BRAKE LINE WAS LOOSE AND ONLY TOOK TWO TURNS TO REMOVE. IT IS SUSPECTED THAT THE QUICK DISCONNECT CONNECTOR MAY HAVE BACKED OFF CAUSING THE DRAGGING BRAKE CONDITION LEADING TO OVERHEAT AND FLUID LOSS CAUSING THE FIRE.  NR 3 AND NR 4 BRAKES WERE REPLACED THE NIGHT BEFORE F2L72 4F4  FRTA21EA   E15NE                
20080320000032008032000003CE  2008       3          20         CA070723001      120070719G325050820035        ROD                                     BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  MCAULY4HFR344HFR34C762  NE  NLG STEERING    CORRODED        W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       20586                                                          (CAN) DURING THE REPLACEMENT OF RODEND P/N F4-19 ON THE NOSE LANDING GEAR STEERING BARREL ASSY. P/N 50820042-601 WAS DISASSEMBLED TO FACILITATE THE REMOVAL OF THE RODEND FROM THE ROD ASSY P/N 50-820035 (ITEM 21). AFTER DISASSY IT WAS NOTICED THAT THE ROD ASSY WAS HEAVILY CORRODED. THE CORROSION SEEMED TO START FROM INSIDE THE ROD ASSEMBLY AND WORKED ITS WAY OUT, CAUSING THE HARD CHROME TO FLAKE OFF IN 4 SPOTS ALL NEAR THE CARTER OF THE HOLLOW TUBE REVEALING A HOLES IN THE PARENT METAL COMPLETELY THROUGH THE WALL OF THE TUBE. THE ROD ASSEMBLY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.  THERE IS NO CURRENT REQUIREMENT TO DISASSEMBLE THIS PART FOR INSPECTION AND THE CORRODED AREA IS NOT VISIBLE WITH THE PA1L72 3T4  T  A14CE   E4EA    6  C3PNE     
20070917000752007091700075SW  2007       9          17         CA070724001      120070718G3233                O-RING                                  GULSTM690TP 690         0141720SW  GARRTTTPE331TPE3315251K      NM  HARTZLHCB3T HCB3TN5     GL  GEAR ACTUATOR   LEAKING         W      K   NONE                                                                                            J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) INCIDENT/HAZARD DESCRIPTION: UNSAFE GEAR WARNING LIGHT ILLUMINATED. HYDRAULIC PRESSURE WAS DOWN TO 500 PSI.  ONCE ON GROUND, FOUND HYDRAULIC FLUID HAD LEAKED OUT IN THE RT WHEEL WELL, DETERMINED THE RT GEAR ACTUATOR FOR BRINGING GEAR UP HAD A O-RING FAIL (SPLIT)  AIRCRAFT SLOWED TO BELOW 200KTS, GEAR SELECTED DOWN AND (3) GEAR CONFIRMED AND GEAR VISUALLY DOWN AND LOCKED. ONCE GEAR WAS DOWN HYDRAULIC PRESSURE WAS BACK UP TO 1000 PSI, AND LANDING MADE . BRAKES WORKED FINE, AIRCRAFT REPAIRED FOR ALERTS ON THE 19TH OF JULY. TEST FLIGHT COMPLETED (TC NR 20070724001)                                                                                                                                                   1H72 3T4  T  2A4     E2WE    6  CP15EA    
20070820001412007082000141EA  2007       8          20         CA070724002      120070711G2731C3CF3487        CABLE                                   DHAV  DHC3  DHC3        2800202EA  GARRTTTPE331TPE33110R   0517 WP  HARTZLHCB4T HCB4TN5     GL  ELEV TRIM       FRAYED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A 100/150 HOURS INSPECTION, THE ELEVATOR, LOWER TRIM CABLE (P/N: C3CF348-7) WAS FOUND FRAYED IN (2) LOCATIONS. THE FIRST LOCATION WAS IN THE PEDESTAL AREA WHERE THE TRIM CABLE ATTACHES TO THE ELEVATOR TRIM DRUM ASSEMBLY (P/N: C3CF222-3). IT APPEARS THAT THE CABLE WAS WEARING ON THE FWD AND REAR GUARDS P/N: C3CF310-3 AND C3CF309-3. THE SECOND AREA FOUND FRAYING WAS LOCATED IN THE UPPER CABIN AREA WHERE THE TRIM CABLE PASSES THROUGH FAIRLEAD BETWEEN FS 171.8 TO FS 194.8.  CABLE REPLACED, AIRCRAFT RETURNED TO SERVICE.  (TC NR 20070724002)                                                                                                                                                                      1H71 3R4  T  A815    E4WE    6  CP40EA    
             20081104         2008       11         4          CA070724003      420070724G2562AK450           ELT                                     CESSNA180   180K        2072624CE  CONT  O470  O470U       17026SO  MCAULY2A34C C2A34C204   GL                  CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) BATTERY CONNECTIONS HAD EXCESSIVE CORROSION AND EVEN THOUGH THE INDICATOR LAMP INDICATED THAT UNIT WAS WORKING THE UNIT HAD NO SWEEP OUTPUT (TC NR 20070724003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O3  O  5A6     E273    5  CP3EA     
20070820001422007082000142EA  2007       8          20         CA070724004      120070721G2797CF61A22WHT      WIRE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        DAMAGED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE GEAR/FLAPS/BTMS INDICATIONS APPEARED WITH FLAP INDICATION SHOWING BOTH SIDES. FLAPLESS LANDING WAS SAFELY PERFORMED. MAINTENANCE FOUND WIRE CF61A22WHT AT CONNECTOR P2CF OF RT FLAP POSITION TRANSDUCER WITH DAMAGED INSULATION AND TOUCHING THE SHIELD OF THE HARNESS. WIRE REPAIRED (REO601R-20-12-001 AND REO601R-20-12-048); CONNECTOR P2CF (P/N D38999-26WB355N) AND HARNESS (P/N HET-A-02B) REPLACED. (TC NR 20070724004)                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
20070820001432007082000143NE  2007       8          20         CA070724005      220070723G7323204060765007    CONTROL LEVER                           BELL  205   205A1       1181414SW  LYC   T53   T5317A      41549NE                              ENGINE          BROKEN          W      A   UNSCHED LANDING                                                                                 RFJPARTIAL RPM/PWR LOSS      FLT CONT AFFECTED         WARNING INDICATION        DEDESCENT        1                      CA                                                                      (CAN) THIS IS THE INITIAL REPORT. INFORMATION NOT HERE YET. THE PILOT COULD ONLY GET 92 PERCENT NR RP, LANDED THE AIRCRAFT NO INCIDENT, AFTER SHUTDOWN THE ENGINEER OPENED THE GOVERNOR SIDE ENGINE COWLING AND FOUND THE THE GOVERNOR LEVER BROKEN BOTH ENDS OF THE LEVER OR ARM WERE SECURE AND SAFETY.  WE ARE STILL INVESTIGATING. (TC NR 20070724005)                                                                                                                                                                                                                                                                                                                                                                                      1G71 4U4  U  H1SW    E17EA                
20070820001442007082000144GL  2007       8          20         CA070724006      220070723G7200                ENGINE                                  BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                                              OVERHEATED      W      E   ENGINE SHUTDOWN                                                                                 M  OVER TEMP                                                                     TXTAXI/GRND HDL  1                      CA                                          821948                      (CAN) THE PILOT HAD JUST TAKEN HIS FINGER OFF THE THE STARTER ON STARTUP AND WAS REVIEWING HIS COMPANY PILOT MINI LOG WHEN HE NOTED A DIFFERENT ENGINE SOUND AS THOUGH IT HAD INCREASED. WHILE CHECKING THE THROTTLE AND SCANNING THE GAUGES THE PILOT NOTICED THAT THE TOT WAS AT 1000 DEGREES. THE ENGINE ASSEMBLY WAS REPLACED. (TC NR 20070724006)                                                                                                                                                                                                                                                                                                                                                                                          1G71 3U3  U  H2SW    E4CE                 
20071213001972007121300197SW  2007       12         13         CA070724007      120070721G7931                ENGINE                                  KAMOV KA32  KA32A1             SW  KLIMOVTB3117TB3117BMA        EU                                              MAKING METAL    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA       638  346                                                       (CAN) THE LT ENG OIL PRESSURE CAUTION LIGHT WAS FLICKERING WHILE SLINGING A LOAD. THE OIL PRESSURE GAUGE WAS CROSSCHECKED AND INDICATED 2.5 KG/CM2 (THE CAUTION RANGE) AND THE OIL TEMPERATURE WAS NORMAL. THE LOAD WAS DROPPED OFF. AFTER THE LOAD WAS DELIVERED AIRCRAFT BACK IN LEVEL FLIGHT, THE CREW REVIEWED THE CHECKLIST AND FLIGHT MANUAL. AS A PRECAUTIONARY MEASURE THE ENGINE WAS BROUGHT BACK TO IDLE. AT IDLE THE LT ENGINE WAS STILL BEING MONITORED, A FEW MILES FROM SERVICE THE FLIGHT CREW ADVANCED THE THROTTLE TOWARDS AUTO TO CHECK THE OIL PRESSURE. THE LT OIL PRESSURE LIGHT ILLUMINATED STEADILY AND THE OIL PRESSURE REMAINED AT IDLE OIL PRESSURE (2 KG/CM2 MINIMUM ALLOWABLE AT IDLE) THE AIRCRAFT WAS AT A WEIGHT 1G72 4U4  UNC        EXPE4U               
20070820001452007082000145WP  2007       8          20         CA070724008      120070724G7410AH720           RELAY                                   CVAC  340   34030       2422702WP  ALLSN 501D  501D13D     03004GL  HAMSTD54H   54H60       NE  IGNITION POWER  DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) NR 1 ENGINE FAILED TO START DUE TO NO IGNITION.  FOUND IGNITION RELAY P/N AH720 S/N CN-90127 FOUND CONNECTOR SEPARATED FROM BODY OF RELAY.    RELAY REPLACED AND ENGINE GROUND RUN SERVICEABLE. (TC NR 20070724008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4R4  T  6A6     E282    6  CP906     
20070912000572007091200057CE  2007       9          12         CA070725001      120070712G2752995240257       ACTUATOR                                BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  TE FLAP         NOISY           W      D   RETURN TO BLOCK                                                                                 F  FLT CONT AFFECTED                                                             LDLANDING        1                      CA            2963                                                      (CAN) UPON LANDING AN ATTEMPT TO RETRACT THE FLAPS FROM APPROACH TO ZERO RESULTED IN THE MOVEMENT OF THE RT IB FLAP ONLY. THE REMAINING (3) FLAPS DID NOT MOVE. A FLIGHT PERMIT WAS GRANTED AND THE A/C WAS FLOWN WITH THE FLAPS LOCKED IN THE ZERO POSITION. THE GEARBOX OPERATION WAS NOISY AND WAS REPLACED.  THE SYSTEM WAS RIGGED AND OPERATIONALLY CHECKED IAW MFG INSTRUCTIONS.  NO OTHER PROBLEMS WERE NOTED.  (TC NR 20070725001)                                                                                                                                                                                                                                                                                                      1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070820001462007082000146NM  2007       8          20         CA070725002      120070322G38106BS10011        DRAIN VALVE                             AMD   FALC50FALCON2000  2730170NM  CFE         CFE73811B        NE                                              DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3626 3626                                                      (CAN) THE AIRCRAFT POTABLE WATER SYSTEM WAS DAMAGED DUE TO HAVING THE WATER SYSTEM FULL OF WATER. THEN PARKING THE AIRCRAFT ON THE RAMP FOR 8 HRS AT -14 DEGREES C. WITH NO ADDITIONAL HEAT TO KEEP THE WATER SYSTEM FROM FREEZING.  UPON ARRIVING, THE PILOTS REPORTED (WATER APPEARS TO LEAKING FROM THE BELLY) THE MAINTENANCE PERSONAL INVESTIGATED THE PROBLEM AND FOUND THE WATER SYSTEM DRAIN VALVE WAS DAMAGED DUE TO THE SEVERE FREEZING OF THE WATER SYSTEM. THE DRAIN VALVE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.  A REMINDER TO ALL PILOTS TO MONITOR THE POTABLE WATER SYSTEM AND THE OAT IN THE WINTER. (TC NR 20070725002)                                                                                          2K72 4F4  FRTA50NM   E44NE                
20080306000512008030600051CE  2008       3          6          CA070725003      120070717G27503X5K8563A44172  FLEX DRIVE                              BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  TE FLAP CONTROL DAMAGED         W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) AN ATTEMPT TO LOWER THE FLAPS TO APPROACH SETTING FROM ZERO DEGREES RESULTED IN THE RT IB FLAP NOT MOVING AND THE (3) OTHERS MOVING TO FULL DOWN. THE PILOT LANDED WITHOUT INCIDENT AND A FERRY PERMIT WAS GRANTED FOR A FLIGHT WITH THE FLAPS UP AND LOCKED. UPON DISASSEMBLY OF THE SYSTEM IT WAS FOUND THAT THE RT FLAP FLEX DRIVE WAS DAMAGED AND BINDING UP OPERATION OF THE ACTUATOR. (TC NR 20070725003)                                                                                                                                                                                                                                                                                                                           1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070820001472007082000147NM  2007       8          20         CA070725004      120070504G301029S7D524007     BOOT                                    DORNERDO32  DO328100    2996000NM  PWA   119   PW119C           NE  HARTZLHDE6C HDE6C3B     NE  HORIZONTAL STAB LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       55                                                             (CAN) PILOTS REPORTED LT HORIZONTAL STAB. DE-ICER BOOT APPEARS LOOSE.  MAINTENANCE INSPECTED THE DE-ICER BOOT AND FOUND THE BOOT HAD COME LOOSE FROM THE AIRCRAFT AT THE AFT EDGES. THE ADHESIVE (3M 1300L) DID NOT SECURE THE DE-ICER BOOT TO THE STAB. THE BOOT WAS RECENTLY REPLACED BY AC SERVICES, UNDER WO 15249.  TIME ON PART WAS 54.6 HOURS AND 73 LANDINGS THE DE-ICER BOOT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC 20070725004)                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA45NM   E20NE   6  CP34NE    
20080319001492008031900149EA  2008       3          19         CA070725005      220070711G72303027301         BLADE                                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  COMPRESSOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A ROUTINE COMPRESSOR TURBINE BLADE (STRETCH) INSP, ONE CT BLADE WAS FOUND CRACKED DURING THE NDT PROCESS. THE CRACK WAS ACROSS THE BLADE FACE AND BACK. THIS TYPE OF CRACK SCRAPS THE BLADE AND THE SET IT WAS INSTALLED WITH. THIS SET OF BLADES HAD A TSN OF 9299.1 HOURS. THE BLADES WERE REPLACED AND THE AC RETURNED TO SERVICE. (TC NR 20070725005)                                                                                                                                                                                                                                                                                                                                                                          1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070820001482007082000148EA  2007       8          20         CA070725006      220070725G85200360A3A         CRANKCASE                                                                  LYC   O360  O360A3A     41514EA                              ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1800                                                      (CAN) OVERHAULED CYLINDER ASSY`S WERE INSTALLED APPROX 500 HRS AGO ONTO A FRETTED CRANKCASE.  THE CENTER MAIN BEARING THEN SPUN IN THE BEARING SADDLE.  METAL WAS DETECTED IN THE OIL SCREEN AND THE ENGINE WAS SUBSEQUENTLY TORN DOWN FOR OVERHAUL.  THE CRANKCASE IS UNSERVICEABLE. (TC NR 20070725006)                                                                                                                                                                                                                                                                                                                                                                                                                                              3  O          E286                 
20071102000032007110200003GL  2007       11         2          CA070726003      220070709G73212542102         SLEEVE          HONEYWELL               BELL  206   206L        1181522SW  ALLSN 250C  250C20R2         GL                              FUEL CONTROL    CRACKED         W      O   OTHER                                                                                           BK SMOKE/FUMES/ODORS/SPARKS  FLUID LOSS                                          TXTAXI/GRND HDL  1                      CA            30    333104                                              (CAN) PILOT STARTING A/C, THROTTLE OPENED, NO ENGINE LIGHT OFF OCCURED. OPENED ENGINE COWL TO INVESTIGATE, NOTICED FUEL DRIPPING FROM AROUND START DE-RICHMENT ADJUSTMENT OF FCU, ONTO THE STARTER GENERATOR. CONTACTED MAINTENANCE PERSONNEL TO INVESTIGATE. FUEL CONTROL UNIT WAS REMOVED, AND O/H`D UNIT INSTALLED - NO FURTHER DEFECT NOTED ON START-UP. OVERHAUL SHOP WORK ORDER DETAILS REVEALED A CRACKED SLEEVE ASSY P/N 2542102, AND CRACKED SCREWS P/N 334S606 (TC NR 20070726003)                                                                                                                                                                                                                                                    1G71 3U3  U  H2SW    E4CE                 
20070820001492007082000149NE  2007       8          20         CA070726004      220070726G72304017T37P02      SEAL                                                                       GE    CT58  CT581402    30011NE                              COMPRESSOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                          280122KL                    (CAN) MULTIPLE CRACKS THROUGH KNIFE EDGE SEALS. THIS REPORT WILL ALSO BE SUBMITTED TO MFG IAW SEI-183 SECTION 72-32-7 PAGE 302.  (TC NR 20070726004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   4  U          1E3                  
20070820001502007082000150NE  2007       8          20         CA070727001      220070727G7310AN81510         FITTING                                 DHAV  DHC8  DHC8202     2809007NM  PWA   120   PW123D      52152NE  HAMSTD14SF  14SF23      NE  FUEL MANIFOLD   BROKEN          W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) ENGINE DRIVEN PUMP NR 1, INLET PRESSURE MANIFOLD FITTING AN 815-10 BROKEN IN FLIGHT.  FITTING HAS BEEN REPLACED AND A/C RETURNED TO SERVICE.  (TC NR 20070727001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070820001512007082000151SO  2007       8          20         CA070727002      220070725G853065354A10        CYLINDER HEAD                           CESSNA402   402C        207590RCE  CONT  O520  TSIO520VB   17040SO  MCAULY3AF32C3AF32C505   GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CYLINDER ASSY FOUND CRACKED DURING INSPECTION. LEAK COULD BE HEARD FROM CRACK DURING DIFF COMPRESSION TEST. CYLINDER REMOVED AND LARGE CRACK OBSERVED IN HEAD CASTING (INTERIOR VIEW). THE S/N OF CYLINDER REMOVED IS E41375-4 (TC NR 20070727002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3O3  O  A7CE    E8CE    5  CP22EA    
20080306001322008030600132SW  2008       3          6          CA070727003      120070725G2911MS28775212      O-RING          BELL                    BELL  205   205A1       1181414SW  LYC   T53   T5313B      41549NE                              ACCUMULATOR     FAILED          W      B   EMER. DESCENT                                                                                   F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) LOST OF HYDRAULIC IN FLIGHT, EMERGENCY LANDING, FAULT FOUND IN THE ACCUMULATOR, O-RING P/N MS28775-212 REPLACED A/C GROUND RUN AND LEAK CHECK COMPLETED AND RELEASED TO SERVICE. (TC NR 20070727003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 4U4  U  H1SW    E17EA                
20070820001522007082000152NM  2007       8          20         CA070727004      120070725G7920                FITTING                                 BOEING727   727243      138408DNM  PWA   JT8   JT8D9A      52048NE                              GEARBOX OIL     DAMAGED         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  DEDESCENT        1                      CA                                                                      (CAN) TOP OF DESCENT, THE NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED, QTY AT ZERO.  PRECAUTIONARY ENGINE SHUTDOWN CARRIED OUT.   GEARBOX FITTING (OIL PRESSURE DIFFERENTIAL SWITCH) THREAD REPAIRED AND FITTING REPLACED. ENGINE INSPECTEED IAW MM AND RETURNED TO SERVICE.  (TC NR 20070727004)                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L73 4F4  FRTA3WE    E2EA                 
20070820001532007082000153NE  2007       8          20         CA070727005      220070726G8550                SEAL                                    DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  IMPELLER        FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA            255                                                       (CAN) ENGINE REMOVED DUE TO EXCESSIVE OIL CONSUMPTION.  UPON REMOVING NR 7 CYLINDER INTAKE TUBE, OIL WAS NOTED. THIS INDICATES POSSIBLE IMPELLER SEAL FAILURE. ENGINE WAS REMOVED FROM SERVICE. (TC NR 20070727005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3R3  RRCA806    5E1     5  CP206     
20070820001542007082000154CE  2007       8          20         CA070727006      120070723G7120                WEB                                     CESSNA172   172K        2072430CE  LYC   O320  O320E2D     41508EA  MCAULY1A175 1A175ATM    GL  ENGINE MOUNT    CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            536                                                       (CAN) CRACK FOUND AT LOWER WELD WEB LT SIDE. (TC NR 20070727006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A12    E274    5  NP857     
20070820001552007082000155SW  2007       8          20         CA070727008      120070717G3243VI151000        MASTER CYLINDER                         SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  BRAKES          FAULTED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA            7753                                                      (CAN) AIRCRAFT ABORTED TAKEOFF DUE TO A DRAGGING BRAKE. UPON MAINTENANCE INSPECTION THE RT BRAKE MASTER CYLINDERS WERE FOUND AT FAULT.  BRAKE PRESSURE COULD NOT BE RELEASED BY THE AFFECTED MASTER CYLINDERS.  BOTH NR 2 AND NR 4 BRAKE MASTER CYLINDERS WERE REPLACED.   NR 2 CYLINDER P/N V-1000 S/N 3187 TSO - 4382.9,  NR 4 CYLINDER P/N VI-15-1000 S/N 13008 TSO- 7753.3. (TC NR 20070727008)                                                                                                                                                                                                                                                                                                                                             2L72 4T4  TRTA8SW    E4WE    5  CP10NE    
20070820001562007082000156WP  2007       8          20         CA070727009      120070723G3234340315061627    LEVER                                   CVAC  440   440         2422902WP  ALLSN 501D  501D22      03005GL  HAMSTD54H   54H60       NE  LANDING GEAR    DISTORTED       W      O   OTHER                                                                                           O  OTHER                                                                         DEDESCENT        1                      CA       1086910869                                                     (CAN) UPON SELECTION OF (GEAR DOWN), THE LOCKING ARM OF THE LANDING GEAR SELECTOR HANDLE STUCK IN THE EXTENDED POSITION, PREVENTING ASSOCIATED FUNCTION OF DEPRESSING THE GEAR WARNING LIGHT SWITCH.  THE RESULT WAS NO GEAR DOWN INDICATING LIGHTS ON THE ANNUNCIATOR PANEL.  EMERGENCY PROCEDURES FOLLOWED AND AC LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND LANDING GEAR ACTUATING LEVER LOCKPIN JAMMED AND CONTROL HANDLE BEYOND THE 90 DEGREE POSITION. LEVER DISASSEMBLED, DAMAGE FOUND WAS A DISTORTED (CUPPED) INTERNAL ALUMINUM 960D10L WASHER. CUPPED WASHER REMOVED. NEW WASHER AND ONE EXTRA WASHER INSTALLED FOR SUPPORT DURING RE-RIG OF HANDLE WITHOUT COMPROMISING TRAVELS PER CONVAIR MAINTENANCE MANUAL LANDING GEAR MECHANIC2L72 4R4  T  6A6     E282    6  CP906     
20070912000582007091200058GL  2007       9          12         CA070729001      120070717G3220203220080       FORK                                    DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  NOSE GEAR       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3109                                                           (CAN) DURING ROUTING INSPECTION, A CRACK SIMILAR TO THE ONE IN THE ATTACHMENT WAS FOUND.  FORK WAS REPLACED.  FLEET INSPECTION REVEALED (3) OTHER AIRCRAFT WITH VARYING CRACK PROGRESSION ALL FORKS WERE REPLACED. (TC NR 20070729001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20070820001572007082000157NE  2007       8          20         CA070729002      220070712G852039892           COUNTERWEIGHT                           BEECH 18    D18S        1151004CE  PWA   R985  R985AN14B   52008NE  HAMSTD22D   22D30       NE  ENGINE          SEPARATED       W      A   UNSCHED LANDING                                                                                 EY VIBRATION/BUFFET          ENGINE STOPPAGE                                     CRCRUISE         1                      CA            251                           42121964                    (CAN) AIRCRAFT WAS IN CRUISE, ALL SYSTEMS NORMAL WHEN A VIOLENT VIBRATION HAPPENED IN THE LT ENGINE.  ENGINE SEIZED DURING SHUTDOWN/FEATHER PROCESS AND FEATHERING WAS UNAVAILABLE. A SAFE LANDING WAS MADE ON A LAKE. INVESTIGATION REVEALED NR 1 CYLINDER COMPLETELY REMOVED FROM THE ENGINE AND NR 9 PARTIALLY REMOVED.  FORWARD COUNTERWEIGHT HAD SEPARATED COMPLETELY FROM ITS ARM AND WAS FOUND LODGED IN THE TOP PART OF THE ENGINE AFTER BLOWING OUT A SECTION OF THE NOSE SIDE OF THE CRANKCASE COVER.  AN ENGINE CHANGE WAS CONDUCTED ON SITE AND AIRCRAFT RETURNED TO RED LAKE WITH A LOANER PROP INSTALLED. (TC NR 20070729002)                                                                                                     1L72 3R3  R  A765    5E1     5  CP736     
20070820001582007082000158EA  2007       8          20         CA070729003      120070728G5210601R319119      STRUT                                   CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              PAX DOOR        DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ON ARRIVAL IT WAS DISCOVERED THAT THE PAX AIRSTAIR HAD BEEN DAMAGED WHEN CLOSED.  MAINTENANCE FOUND A SMALL PUNCTURE IN THE MAIN CABIN DOOR INNER SKIN BESIDE UPPER STEP.  MAINTENANCE DISCOVERED THE GAS STRUT ON THE MCD FAILED CAUSING THE SKIN PUCTURE BY CABLE ATTACHMENT ON THE DOOR BRACKET NOT RETRACTING.  NDT C/O NO CRACKS FOUND, STRUT AND COUNTER BALANCE REPLACED AND REO 601R-52-11-1295 C/O WITH A RE-INSPECT OF THE SPEED TAPE EVERY 50 HRS.  PRESENT A/C HOURS 25062:54 AND CYCLES 20668. (TC NR 20070729003)                                                                                                                                                                                                           2L72 4F4  FRTA21EA   E15NE                
             20081104         2008       11         4          CA070730001      420070730G2562                G SWITCH                                                                                                                                ELT             MALFUNCTIONED   W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) DURING ANNUAL INSP IT WAS FOUND THAT THE G-SWITCH OPERATION WAS OVERSENSITIVE. UNIT REJECTED AND RETURNED TO MFG FOR REPAIR (TC NR 20070730001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     
20070820001592007082000159EU  2007       8          20         CA070730002      120070723G324030244           BRAKE DISC                              PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  MLG             BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1848                                                           (CAN) AT THE TIME OF TAKEOFF THE WHEEL OF BLOCKED LT A AND A CAUSED THE EXIT OF TRACK OF THE APPARATUS. APPARATUS A DOES NOT SUFFER ANY DAMAGE AND AT SUMMER MOVED TO THE AIR OF PARKING. A TEAM OF MAINTENANCE OF THE COMPANY EAST GONE ON THE SPOT AND A FOUND THAT A DISC OF THE LT BRAKE WAS BROKEN. REPLACED BRAKE. (TC NR 20070730002)                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
             20081104     EU  2008       11         4          CA070730003      120070716G5610                WINDSCREEN                              BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33110    01514WP  ROTOL R333  R333482F12  GL  COCKPIT         CRACKED         W      B   EMER. DESCENT                                                                                   O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) AFTER LEVELLING OFF AT 20000 FT, THE RT PILOTS WINDSCREEN CRACKED.  A/C BEGAN A DESCENT TO 5500 FT AND RETURNED TO BASE UNPRESSURIZED WITH NO FURTHER INCIDENT. WINDSHIELD HEAT WAS IN USE WITH NO OVERHEAT CAPTIONS.A NEW WINDSCREEN WAS INSTALLED WITH NO ABNORMALITIES IN ITS REMOVED AND REPLACED. (TC NR 20070730003)                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T4  TRTBA15CAA E4WE    6  CP61GL    
             20081104         2008       11         4          CA070730004      120070102G24216431041         ROTOR           HONEYWELL                                                                                                               GENERATOR       FAILED          W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       NRNOT REPORTED   1                      CA                                                                      (CAN) RECENT DASH 8 400 AC GENERTOR (P/N1152218-3,-4,-5) FAILURE INVESTIGATIONS AT MFG HAVE IDENTIFIED THE MAIN ROTOR BANDS AS THE INITIAL FAILURE LOCATIONS FOR FIVE GENERATORS INVESTIGATED (S/N 062C-0420, 062C-0421, 1152218-00026, 1152218-00062, 1152218-00064). FIELDED AC GENERATORS MAY HAVE A WELD JOINT NONCONFORMANCE ASSOCIATED WITH INTERNAL ROTOR BANDS (QTY 2 IAW GENERATOR). THE NONCONFORMANCE IDENTIFIED IS AN INCOMPLETE FUSION OF THE WELD JOINT. THIS CONDITION WAS INITIALLY IDENTIFIED IN EARLY JAN 2007 ON GENERATOR S/N 1152218-00064 ORIGINALLY SHIPPED ON FEB 20, 2006. (TC NR 20070730004)                                                                                                                                                                   
20070820001602007082000160SO  2007       8          20         CA070730005      120070728G5753                STRUCTURE                               LKHEED188   188C        5262604SO  ALLSN 501D  501D13      03004GL  ALLSN A6441 A6441FN606  GL  TE FLAPS        SEPARATED       W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) FIRE SUPPRESSION OPERATIONS IN RUGGED MOUNTAINOUS TERRAIN. FINISHED LAST OF 4 DROPS. APPLIED MAX POWER AND FLAPS TO 78 PERCENT AND PROCEEDED WITH CLEAN UP CHECKLIST.  NOTICED ABNORMAL OF CONTROL COLUMN ( MORE AILERON).  ADJUSTED TRIMS AND POWER SETTINGS.   PNF WENT TO THE BACK NOTICED DAMAGE TO RT OB PORTION OF FLAP. PILOT SLOWED AIRCRAFT.   ADVISED FSS OF PROBLEM. PILOT RAN FLAPLESS CHECKLIST AND REQUESTED EMERGENCY VEHICLES. PILOT SLOWED AIRCRAFT TO DETERMINE CONTROLLABILITY. REVIEWED BRAKE FIRE PROCEDURES PRIOR TO LANDING AND THEN FLEW APPROACH AT MARKED BUG TO RUNWAY AND LANDED WITHOUT INCIDENT.  MAINTENANCE FOUND 5 FT OF THE RT FLAP PANEL SEPARATED FROM THE ASSEMBLY AND TRAILING ON THE FLAP RAIL. MAI2L74 4T4  T  4A22    E282    6  CP898     
             20081104     CE  2008       11         4          CA070730006      120070730G24971013841069      METER                                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  ELECTRICAL LOAD DISCONNECTED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            100                                                       (CAN) DURING START UP FOR SERVICE CHECK THE VOLTAGE WAS CHECKED BUT THERE WAS NO INDICATION ON THE METER.  METER WAS REMOVED AND THE PUSH TO TEST SWITCH WAS FOUND DISCONNECTED FROM THE BODY OF THE METER. THE METER WAS REPLACED WITH REPAIRED UNIT. THIS METER WAS JUST INSTALLED AFTER A REPAIR. UNIT HAD ABOUT 100 HOURS ON IT, NUT THAT HOLDS SWITCH IN PLACE HAS STRIPPED OR BACKED OFF. UNIT SENT BACK FOR REPAIR. (TC NR 20070730006)                                                                                                                                                                                                                                                                                                  1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070820001612007082000161NE  2007       8          20         CA070731001      220070727G7320                SEAL                                    AIRBUS310   A310300     3930305EU  GE    CF6   CF680C2A5        NE                              HMU             LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       2538                                                           (CAN) DURING TAXI-IN AT THE GATE, A LARGE FUEL LEAKAGE WAS OBSERVED COMING FROM THE HMU FUEL DRAIN BELOW NR 2 ENGINE. ENGINE WAS SHUTDOWN, BUT LEAKAGE CONTINUED.  NR 2 ENGINE FIRE HANDLE WAS PULLED AND LEAKAGE STOPPED.   FOUND LEAKAGE WAS FOM THE MEC SHAFT SEAL. MEC WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070731001)                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA35EU   E13NE                
20070912000592007091200059SO  2007       9          12         CA070731002      120070727G2750486597          FLEX COUPLING                           PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  FLAP MOTOR      SEIZED          W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                  6059                                                (CAN) ON CLIMB OUT PILOT FOUND HIS FLAP CIRCUIT BREAKER HAD POPPED AND HIS FLAPS WOULD NOT RETRACT.  HE MADE AN UNEVENTFUL LANDING.  UPON TROUBLE SHOOTING, IT WAS FOUND THAT THE R/H FLAP FLEX SHAFT (MOTOR TO TRANSMISSION) WAS SEIZED.  AS A RESULT OF THE SEIZED SHAFT, THE MOTOR WAS ALSO DAMAGED.  THE MOTOR AND SHAFT HAVE BOTH BEEN REPLACED AND THE AIRCRAFT RELEASED FOR SERVICE. (TC NR 20070731002)                                                                                                                                                                                                                                                                                                                                 1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080324004162008032400416CE  2008       3          24         CA070801001      120070727G2810369200157       FUEL CELL                               BEECH 95    95B55       1152729CE  CONT  O470  IO470L      17026SO  HARTZLHCC3Y PHCC3YF2    GL  RT WING         DETERIORATED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THE RT WING LEADING EDGE FUEL CELL WAS REMOVED BECAUSE OF A FUEL LEAK. A REPLACEMENT FUEL CELL WAS ORDERED. PRIOR TO INSTALLATION OF THE NEW (OVERHAULED) CELL, IT WAS INSPECTED AND FOUND TO CONTAIN A LARGE QUANTITY OF SAWDUST-LIKE PARTICLES. ON FURTHER INSPECTION, THE FUEL CELL STILL HAD THE FOAM FILLED FUEL RESERVOIR INSIDE. THIS FOAM WAS BREAKING DOWN. AFTER DISCUSSIONS WITH MFG TECH SUPPORT IT WAS CONCLUDED THAT AD68-26-06 HAD BEEN COMPLIED WITH AT SOME POINT OF TIME WHICH REQUIRED THE INSTALLATION OF FUEL RESERVOIRS TO PREVENT ENGINE POWER LOSS DURING STEEP TURNS ON TAKEOFF. THESE RESERVOIRS HAD A FOAM INSERT WHICH WAS COMPATIBLE WITH 100/130 FUEL. THE USE OF 100LL HOWEVER CAUSES THE FOAM TO BREAK DOW1L72 3O3  ORT3A16    3E1     5  CP25EA    
20070821000812007082100081    2007       8          21         CA070801002      420070731G23303088510101      ENTERTAIN SYS                           BOEING737   737*               NM  CFMINTCFM567CFM567B22   13802NE                              CABIN           SMOKE           W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA                                                                      (CAN) WHILE LOADING THE AFT BAGGAGE PIT, A BURNING ELECTRICAL ODOR AND SMOKE WERE NOTICED AND TRACED TO THE LIVE-TV ELECTRICAL RACK COMPONENT WIRELESS AIRCRAFT UNIT.  POWER WAS REMOVED FROM THE AIRCRAFT AND THE WIRELESS AIRCRAFT UNIT WAS REMOVED.  THIS COMPONENT WILL BE RETURNED TO THE MFG AND A COMPLETE TEARDOWN REPORT WILL BE REQUESTED. THIS SDR WILL BE UPDATED ONCE THAT INFORMATION IS AVAILABLE.   (TC NR 20070801002)                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA16WE   E00055EN             
20070821000832007082100083SO  2007       8          21         CA070801003      220070725G8550635616          PAN                                     CESSNA206   U206G       2073356CE  CONT  O520  IO520F      17032SO  MCAULYD3A34 D3A34C401   GL  ENGINE OIL      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) OIL PAN FOUND CRACKED DURING INSPECTION. (TC NR 20070801003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  O  A4CE    E5CE    5  CP47GL    
20070821000842007082100084SO  2007       8          21         CA070801004      220070720G8530AEC65385        CYLINDER                                CESSNA185   A185E       2072818CE  CONT  O520  IO520D      17032SO  HARTZLHCC3Y HCC3YF1     GL  NR 6            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION FOUND 6 CYLINDER CRACKED AT SPARK PLUG HOLE. (TC NR 20070801004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  O  3A24    E5CE    5  CP25EA    
20070821000852007082100085SO  2007       8          21         CA070801005      220070720G8530AEC65385        CYLINDER                                CESSNA185   A185E       2072818CE  CONT  O520  IO520D      17032SO  HARTZLHCC3Y HCC3YF1     GL  NR 5            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION FOUND NR 5 CYLINDER CRACKED AT SPARK PLUG HOLE. (TC NR 20070801005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  3A24    E5CE    5  CP25EA    
20070821000862007082100086EU  2007       8          21         CA070801006      120070729G3320BR6303121       LIGHT                                   SAAB  SF340 340B        7860101EU  GE    CT7TP CT75A2      30030NE  ROTOL R389  R3894123F25 NE  CABIN           OVERHEATED      W      A   UNSCHED LANDING                                                                                 MB OVER TEMP                 SMOKE/FUMES/ODORS/SPARKS                            CRCRUISE         1                      CA                                                                      (CAN) CABIN OVERHEAD FLOURESCENT LIGHTING FIXTURE OVERHEATED.  BURNED OUT BULB FOUND AND CONTACTS IN FIXTURE THAT CONDUCT ELECTRICITY TO BULB FOUND LOOSE AND OVERHEATED, CAUSING PLASTIC PART OF ASSY TO OVERHEAT. PARTS REPLACED AND A/C RELEASED TO SERVICE WITHOUT ANY FURTHER INCIDENT. (TC NR 20070801006)                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T4  TRTA52EU   E8NE6   6  CP30NE    
20070912000602007091200060SW  2007       9          12         CA070801007      120070731G6510476205561       BEARING                                 BELL  47    47G2        1181008SW  LYC   O435  VO435A1E    41516EA                              DRIVE ASSY      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            889                                                       (CAN) ON WALK AROUND TAIL ROTOR OUTPUT SHAFT AT TRANSMISSION WAS NOTED TO HAVE LOTS OF PLAY, FWD DRIVESHAFT WAS REMOVED TO CHECK FOR COUPLING SPLINE WEAR WHICH WAS GOOD SO THE DRIVE ASSY WAS REMOVED FOR FURTHER INVESTIGATION. IT WAS DETERMINED THAT ONE OF THE DUPLEX BEARINGS WAS ROUGH AND THE ROLLER BEARING P/N 47-620-929-1 WAS WORN AND THE DRIVE GEAR WAS SHOWING SIGNS OF UNEVEN WEAR CAUSED BY THE DUPLEX BEARING STARTING TO FAIL WHICH IN TURN MADE THE SHAFT MOVE IN AN UNEVEN PATTERN DAMAGING THE GEAR AND ROLLER BEARING. THE ROUGH FEELING DUPLEX BEARING WAS TAKEN APART AND FOUND THAT THE INNER RACE WAS STARTING TO SPALL ABOUT A THIRD OF THE WAY AROUND, NO METAL OR FLAKES HAD BEEN FOUND AND THE SCREEN WAS PULLED 1G71 3O3  O  H1      E279                 
20070821000872007082100087NE  2007       8          21         CA070801008      220070720G8530327626          CYLINDER HEAD                           CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 CWASP       52016NE  HAMSTD43E   43E60       NE  ENGINE          CRACKED         W      E   ENGINE SHUTDOWN                                                                                 RB PARTIAL RPM/PWR LOSS      SMOKE/FUMES/ODORS/SPARKS                            FFFIRE FIGHTING  1                      CA            76                            P35411                      (CAN) DURING A NORMAL WATER PICKUP FOR FIRE FIGHTING OPERATIONS, THERE WAS A NOTICEABLE LOSS OF MANIFOLD PRESSURE(MP) AND BMEP INDICATIONS. ON NR 1 POWER REDUCTION THERE WAS A SMALL BACKFIRE AND FURTHER LOSS OF MP AND BMEP.  WATERLOAD WAS JETTISONED AND FLIGHTCREW REDUCED POWER TO CLIMB. THEY CLIMBED TO CRUISE ALTITUDE AND NOTICED A SMALL OIL LEAK AND SMOKE TRAIL. ALL OTHER INDICATIONS WERE NORMAL EXCEPT FOR A COLD CYLINDER HEAD TEMP. AFTER APPROX.: 45 WITH A SMOKE TRAIL AND OIL LEAK APPARENTLY GETTING WORSE, THE FLIGHTCREW SHUT DOWN AND SECURED THE RT ENGINE.  AME FOUND CRACKED NR 2 CYCLINDER AND BROKEN PUSHROD AND HOUSING. CYLINDER WAS REPLACED, SCREEN CHECKED OK. ENGINE GROUND RUN AND FOUND SERVICEABLE.  (TC2H72 4R3  RRTA14EA   ATC14   6  CP871     
20070821000882007082100088EA  2007       8          21         CA070801009      120070722G261241493           ELBOW                                   CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 CWASP       52016NE  HAMSTD43E   43E60       NE  FIRE DETECTION  CRACKED         W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 CRCRUISE         1                      CA       4816 4816  1003                                                (CAN) DURING BOMBING OPERATIONS, FLIGHTCREW HAD AN INTERMITTENT RT, ZONE 1 FIRE INDICATION.  THEY LEFT THE FIRE CIRCUIT, CLIMBED TO ALTITUDE, AND SECURED RT ENGINE IAW CHECKLIST.  SHORTLY AFTERWARD (APPROX 5 MINUTES)THE LT GENERATOR FAILED. UPON ENTERING THE ZONE, ELECTRICAL POWER LOST TO RADIOS,   MADE A LANDING WITHOUT INCIDENT.  AMES FOUND CRACKED CERAMIC ELBOW ON FIRE DETECTION SYSTEM THE FOLLOWING DAY AFTER ANOTHER FALSE INDICATION. ELECTRICAL POWER CHARGING SYSTEM LOST WHEN LT ENGINE GENERATOR FAILED ON OPERATING ENGINE DURING SINGLE ENGINE OPERATIONS. GENERATOR REPLACED. SYSTEM CHECKED, FOUND SERVICEABLE. (TC NR 20070801009)                                                                                 2H72 4R3  RRTA14EA   ATC14   6  CP871     
20070912000612007091200061CE  2007       9          12         CA070802001      120070214G531111543008435     FRAME                                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       19854                                                          (CAN) ON INSPECTION WE NOTICED THE FRAME WAS CRACKED ON THE LT AND THE RT SIDE.  A NEW FRAME WAS INSTALLED. (TC NR 20070802001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070912000622007091200062CE  2007       9          12         CA070802002      120070213G5210504300431397    CABLE                                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  DOOR STEP       FRAYED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ON INSPECTION IT WAS NOTICED THAT THE UPPER AND THE LOWER CABLES WERE FRAYED. THEY WERE REPLACED AND ADJUSTED. (TC NR 20070802002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070912000632007091200063CE  2007       9          12         CA070802003      120070312G5344                HINGE                                   BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  LT DOOR         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ON INSPECTION THE LT DOOR WAS FOUND CRACKED ALONG THE FRONT HINGE. (TC NR 20070802003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070912000642007091200064CE  2007       9          12         CA070802004      120070723G28101019200931      FUEL TANK                               BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  PURGE TANK      CRACKED         W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      NRNOT REPORTED   1                      CA                                                                      (CAN) IT WAS NOTICED THAT ON SHUTDOWN THE LT ENGINE SMOKED.  NOTICE THAT THE COLLECTOR TANK WAS CRACKED ALONG THE WELD. (TC NR 20070802004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20070821000932007082100093    2007       8          21         CA070802005      420070726G611305503214        BULKHEAD                                CESSNA172   172N        2072434CE  LYC   O320  O320D2J     41508EA  MCAULY1C160 1C160DTM    GL  SPINNER         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       380                                                            (CAN) THIS AIRCRAFT HAS HAD ALL THE AFT BULKHEAD AND HEAVIER SPINNER UPGRADES AND HAS HAD IT ALL ASSEMBLED IAW THE LATEST SB. CRACKS WERE FOUND FORMING PARALLEL FROM THE PROP BOLT HEAD CONTACT SURFACE ON (3) OF THE (6) HOLES. HAVE TO LOOK VERY CAREFULLY AS THE CRACKS RADIATING FROM THE PROP BOLT HOLES ARE VERY FINE AND HIDE UNDER THE FACTORY PRIMER. THE TORQUE OF THE PROP BOLTS IS SHEAR STRESSING THE BULKHEAD. A COVER PLATE IS NEEDED TO OFFSET THE BOLTS FROM THE THIN ALUMINUM SHEET METAL BULKHEAD. THIS PROBLEM IS CONSTANTLY RE-OCCURRING WITH THIS SPINNER ASSY. (TC NR 20070802005)                                                                                                                                      1H71 3O3  ONT3A12    E274    5  NP910     
20070821000952007082100095EA  2007       8          21         CA070802006      220070724G8530LW12416         CYLINDER                                CESSNA172   172N        2072434CE  LYC   O320  O320D2J     41508EA                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2019                                                           (CAN) (2) CRACKS FOUND DURING ENGINE ON-CONDITION INSPECTION. CRACKS START FROM BOTTOM SPARK PLUG HOLE AND EACH CRACK GOES TO A VALVE SEAT. THESE CRACKS WERE NOT DETECTED DURING DIFFERENTIAL PRESSURE INSPECTION OR LEAK TEST. INTERNAL BORESCOPE INSP WAS DETECTION METHOD IAW LATEST B041. (TC NR 20070802006)                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O3  ONT3A12    E274                 
20070912000022007091200002SO  2007       9          12         CA070802007      120070722G781065442003        CLAMP                                   PIPER PA28  PA28140     7102802SO  LYC   O320  O320E3D     41508EA  SNSNCH74D   74DM        EA  EXHAUST PIPE    WORN            W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) PIN THAT PROTRUDES THROUGH THE MUFFLER AND EXHAUST PIPE WAS WORE ALLOWING THE THEM TO SEPARATE. OTHER AIRCRAFT IN THE FLEET WERE CHECKED AND FOUND OK.  (TC NR 20070802007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O3  O  2A13    E274    5  NP88614   
20070821000972007082100097GL  2007       8          21         CA070802008      320070727G6197MS3126E1419S    CONNECTOR                               DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  WIRE HARNESS    UNSERVICEABLE   W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) ON CLIMB OUT SHORTLY AFTER TAKEOFF, THE BETA WARNING LIGHTS (BOTH) CAME ON AND THE NR 2 PROPELLER STARTED TO FEATHER.  THE PILOT PULLED THE BETA SYSTEM CIRCUIT BREAKER BUT THE LIGHTS DID NOT GO OFF, BUT THE PROPELLER STOPPED GOING TO FEATHER.  THE PILOT LANDED AND CONTACTED MAINTENANCE.  WHEN MAINTENANCE DID A GROUND RUN THE NR 2 PROPELLER WOULD NOT COME OUT OF FEATHER.  TROUBLESHOOTING THE SYSTEM FOUND THAT THE CONNECTOR ON THE BETA SYSTEM CONTROL BOX WAS SHORTED OUT INTERNALLY, WHICH CAUSED FAULTS IN THE BETA CONTROL AND CAUTION LIGHT DIMMING CIRCUITS.  THE BETA SYSTEM WAS CAUSED TO (THINK) THE NR 2 PROPELLER WAS GOING INTO BETA, WHEN ACTUALLY IT WAS NOT, AND THEREFORE STARTED TO FEATHER THE PROPELLER. 1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20070821000992007082100099NM  2007       8          21         CA070802009      120070702G612330005000056     TSCU                                    DHAV  DHC8  DHC8201     2809001NM  PWA   120   PW123D      52152NE  HAMSTD14SF  14SF23      NE  NR 2            MALFUNCTIONED   W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                                                      (CAN) AUTOFEATHER ARM LIGHT FAILED TO ILLUMINATE DURING TAKEOFF ROLL (AUTO FEATHER SYSTEM INOP).  REPLACED THE NR 2 TSCU IAW P/W MM 72-01-10, PAGE 420-424, PARAGRAPH 7. GROUND RUNS COMPLIED WITH.  OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (TC NR 20070802009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070821001012007082100101EA  2007       8          21         CA070802010      120070801G5270SAL2D864        PLUNGER                                 DHAV  DHC2  DHC2MK3     2800107EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  CARGO DOOR      SEIZED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION, FOWARD CARGO DOOR SWITCH PLUNGER WAS FOUND SEIZED. (TC NR 20070802010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3T4  T  A806    E4EA    6  CP15EA    
20070912000042007091200004CE  2007       9          12         CA070803001      120070420G5753052323113       FLAP TRACK                              CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA  MCAULY1C160 1C160DTM    GL  LT TE FLAP      SEPARATED       W      A   UNSCHED LANDING                                                                                 EF VIBRATION/BUFFET          FLT CONT AFFECTED                                   DEDESCENT        1                      CA                                                                      (CAN) DURING HARD MANEUVERING WITH FLAPS DOWN, A LOUD BANG WAS HEARD BY THE PILOTS WHO NOTICED THE LT FLAP BEING PUSHED BACK AT A STRANGE ANGLE.  THE FLAPS WERE LEFT IN THE DOWN POSITION AND THE AIRCRAFT WAS RETURNED WITHOUT INCIDENT.  UPON INVESTIGATION THE LT IB FLAP TRACK WAS FOUND SEPARATED AND CRACKED FROM THE AIRFRAME AT THE LOWER FLANGE.  THE CAUSE APPEARS TO BE THE CHERRYMAX RIVETS ATTACHING THE LOWER FLANGE OF THE WING RIB FRETTING, BECOMING WORN, AND WEARING THE RIVET HOLES IN THE WING SPAR UNTIL THE HIGHER STRESSES OF MANEUVERING TORE THEM FREE.   THE FLAPS AND TRACKS WERE REMOVED, SPAR INSPECTED WITH NO DAMAGE NOTED.  THE FLAP TRACK RIB ASSY`S WERE REPLACED, USING STRUCTURAL SCREWS AND NUTS TO ATTAC1H71 3O3  ONT3A12    E274    5  NP910     
20070821001022007082100102EA  2007       8          21         CA070803002      120070802G61233014403         TSCU                                    DHAV  DHC6  DHC6300     2802606EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  RIGHT           INOPERATIVE     W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA       667                                                            (CAN) AUTOFEATHER DID NOT ARM DURING THE TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AN AUTOFEATHER TEST PERFORMED ON THE TAXIWAY WHICH ALSO DID NOT ARM THE AUTOFEATHER. RETURNED TO BLOCK WHERE MAINTENANCE PERFORMED TROUBLESHOOTING AND REPLACED THE RT TSCU.   (TC NR 20070803002)                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H72 3T4  TRTA9EA    E20NE   6  CP7NE     
20070821001042007082100104EU  2007       8          21         CA070803003      120070601G61233004800001      AUTOFEATHER SYS                         AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              PROP CONTROL    DEFECTIVE       W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE WAS REPORTED TO HAVE EXPERIENCED AN INFLIGHT SHUTDOWN.  AUTOFEATHER CONTROL UNIT WAS SUBSEQUENTLY REPLACED. (TC NR 20070803003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2H72 4T4  TRT        E20NE                
20070821001072007082100107EA  2007       8          21         CA070803004      220070601G7261                OIL SYSTEM                              SKRSKYS76   S76B        8143007NE  PWA   PT6   PT6B36      52043EA                              ENGINE          LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                          PT0001                      (CAN) ENGINE OIL TEMPERATURE WAS OBSERVED TO INCREASE IN FLIGHT AND THE PILOT ELECTED TO SHUT THE ENGINE DOWN.  OIL WAS SUBSEQUENTLY SEEN LEAKING FROM THE ENGINE EXHAUST.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070803004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G72 4U4  U  H1NE    E4EA                 
20070821001102007082100110NE  2007       8          21         CA070803005      220070530G7250                TURBINE BLADES                          AIRTRCAT802 AT802A      0390308SW  PWA   PT6   PT6A67A     52043NE                              ENGINE          FRACTURED       W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA                                          RD0007                      (CAN) THE ENGINE LOST POWER ON TAKEOFF ROLL AND THE TAKEOFF WAS ABORTED.  SUBSEQUENT INSPECTION REVEALED FRACTUED POWER TURBINE BLADES AND A DISCONNECTION BETWEEN THE POWER TURBINE AND PROP.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070803005)                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3T4  TNCA19SW   E26NE                
20070912000052007091200005CE  2007       9          12         CA070803006      120070803G32440213500         TIRE                                    RAYTHNC90   C90GT       7150062CE  PWA   PT6   PT6A135     52043NE  HARTZLHCE4N HCE4N3      NE  MLG             DELAMINATED     W      C   ABORTED TAKEOFF                                                                                 E  VIBRATION/BUFFET                                                              TOTAKEOFF        1                      CA       223                                                            (CAN) VIBRATION REPORTED ON TAKEOFF AND LANDING STARTING/ENDING AT 60-70 KNOTS, VIBRATION INCREASED AT HIGH SPEEDS ON GROUND AND DISAPPEARED AFTER LANDING GEAR WAS RETRACTED.  LT AND RT MAIN WHEEL TIRE BALANCE PATCHES WERE FOUND DELAMINATED AND FLOATING INSIDE WHEEL ASSEMBLIES.  RT TIRE P/N 021-350-0 S/N 6121W00482 REPLACED WITH TIRE P/N 850T06-3, LT TIRE P/N 021-350-0 S/N 6200W00106 ALSO REPLACED WITH NEW TIRE P/N 850T06-3  2) HIGH SPEED TAXI CHECKS COMPLETED WITH PILOTS UP TO 100 KNOTS, NO VIBRATIONS NOTED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070803006)                                                                                                                                                         1L72 3T4  TRT3A20    E4EA    5  CP10NE    
20070912000062007091200006NE  2007       9          12         CA070803007      220070617G7200PT6A67R         ENGINE                                  STBROSSD3   SD360       8100606EU  PWA   PT6   PT6A67R     52043NE                                              DAMAGED         W      O   OTHER                                                                                           BRJSMOKE/FUMES/ODORS/SPARKS  PARTIAL RPM/PWR LOSS      WARNING INDICATION        APAPPROACH       1                      CA                                                                      (CAN) ON SHORT FINAL, THE ENGINE LOST POWER AND SMOKE WAS SEEN EXITING THE ENGINE EXHAUST.  POST-FLIGHT INSPECTION REVEALED INTERNAL ENGINE DAMAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE COMPLETED. (TC NR 20070803007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  T  A41EU   E26NE                
20070912000072007091200007NE  2007       9          12         CA070803008      220070618G7210                TOWERSHAFT                              DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE                              REDUCTION GB    SEIZED          W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE WAS REPORTED TO HAVE EXPERIENCED AN INFLIGHT SHUTDOWN.  SUBSEQUENT INSPECTION REVEALED A SEIZED TOWER SHAFT AND DEBRIS IN THE ENGINE OIL.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070803008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA13NM   E20NE                
20070912000082007091200008CE  2007       9          12         CA070803009      120070803G32440763670         TIRE                                    RAYTHNC90   C90GT       7150062CE  PWA   PT6   PT6A135     52043NE  HARTZLHCE4N HCE4N3      NE  NLG             OUT OF ROUND    W      C   ABORTED TAKEOFF                                                                                 E  VIBRATION/BUFFET                                                              TOTAKEOFF        1                      CA       187                                                            (CAN) NOSE WHEEL SHIMMY TIRE PN 076-367-0 SN 4190W00091 FOUND OUT OF ROUND .5 INCH. TIRE REPLACED AND REBALANCED.  NOSE WHEEL STEERING DAMAGE CAUSED BY SHIMMY REPAIRED AS REQUIRED ALL WORN BOLTS, BUSHINGS, BEARINGS AND NOSE STEERING IDLER ASSY. REPLACED NEW.  (TC NR 20070803009)                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3T4  TRT3A20    E4EA    5  CP10NE    
20070912000092007091200009GL  2007       9          12         CA070803010      120070227G79312279300004      TRANSMITTER                             DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  ENGINE OIL PRESSDEFECTIVE       W      O   OTHER                                                                                           N  FALSE WARNING                                                                 DEDESCENT        1                      CA                                                                      (CAN) OIL PRESSURE REPORTED LOW WHEN ENGINE BROUGHT BACK TO IDLE FOR LANDING. INSTALLED NEW OIL PRESSURE SENDER AND AIRFRAME GAUGE CALIBRATION CHECK COMPLETED.  LOGBOOK NOT AT CURRENTLY CLOSE AT HAND, FOR TOTAL TIME ON OIL SENDER, OPERATOR HAS REPLACED THEM IN THE PAST DUE TO SIMILAR TROUBLE.  (TC NR 20070803010)                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20070912000102007091200010NE  2007       9          12         CA070803011      220070615G7210MS949034        BOLT                                    STBROSSD3   SD360       8100606EU  PWA   PT6   PT6A67R     52043NE                              REDUCTION GEAR  SHEARED         W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) ON CLIMB, ENGINE OIL PRESSURE WAS SEEN TO FALL TO ZERO AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INVESTIGATION REVEALED A SHEARED 1ST STAGE REDUCTION GEAR CARRIER BOLT. (TC NR 20070803011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  T  A41EU   E26NE                
20070912000112007091200011SO  2007       9          12         CA070803012      120070728G272063420006        TORQUE TUBE                             PIPER PA34  PA34200     7103405SO  LYC   O360  LIO360C1E6  41515EA  HARTZLHCC2Y HCC2YK2     GL  LT RUDDER       BROKEN          W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA       11513                                                          (CAN) THE LT RUDDER CABLE TORQUE TUBE CONNECTION BROKE OFF FROM THE TUBE.  RUDDER CONTROL WAS LIMITED TO THE TRIM. (TC NR 20070803012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3O3  O  A7SO    1E10    5  CP920     
20070912000122007091200012NE  2007       9          12         CA070803013      220070625G7250                TURBINE BLADES                          UROCOPEC135 EC135P1     8680990EU  PWA   PW206 PW206B      0    NE                              ENGINE          DAMAGED         W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                          BB0113                      (CAN) THE ENGINE WAS REPORTED TO HAVE SHUTDOWN IN CRUISE.  SUBSEQUENT INSPECTION REVEALED POWER TURBINE BLADE DAMAGE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070803013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G72 3U3  UO H88EU   E42NE                
20070912000132007091200013NE  2007       9          12         CA070803014      220070627G7200                ENGINE                                  FOKKERF27   F27MK50            EU  PWA   PWA120PW125B           NE                                              POWER LOSS      W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                          124152                      (CAN) THE ENGINE LOST POWER IN FLIGHT AND WAS SHUTDOWN BY THE CREW.  MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070803014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA817    E20NE                
20070912000142007091200014GL  2007       9          12         CA070803015      120070730G79312279300004      TRANSMITTER                             DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  ENGINE OIL PRESSDEFECTIVE       W      O   OTHER                                                                                           N  FALSE WARNING                                                                 DEDESCENT        1                      CA       194                                                            (CAN) PILOT REPORTED LOW OIL PRESSURE DURING DESCENT WITH ENGINE RPM REDUCED TO IDLE.  COMPLEATED OIL PRESSURE GUAUGE CALIBRATION CHART USING CABIBRATED GAUGE. INDICATED 30PSI -> ACTUAL 38PSI, INDICATED 20 -> ACTUAL 27PSI, INDICATED 15PSI -> ACTUAL 20PSI, INDICATED TOP OF RED LINE 12PSI -> ACTUAL 18PSI, MIDDLE OR REDLINE 10PSI -> ACTUAL 16PSI.  (TC NR 20070803015)                                                                                                                                                                                                                                                                                                                                                                  1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20070912000152007091200015NE  2007       9          12         CA070803016      220070626G7230                COMPRESSOR                              BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                              ENGINE          SEIZED          W      E   ENGINE SHUTDOWN                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  APAPPROACH       1                      CA                                          114113                      (CAN) ON APPROACH, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A LOSS OF OIL PRESSURE AND AN INCREASE IN INTER-TURBINE TEMPERATURE.  THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED COMPRESSOR SEIZURE AND INTERNAL OIL LEAKAGE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070803016)                                                                                                                                                                                                                                                                                                                                                                                          2L72 4T4  TRTA24CE   E26NE                
20070912000172007091200017CE  2007       9          12         CA070804001      120070801G2840AG112           SIGHT GLASS                             BOEING75    A75N1       1380134CE  CONT  R670  R670*       17016SO                              FUEL TANK       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       351                                                            (CAN) AD CF61-7 CALLS FOR AN ANNUAL REPLACEMENT OF THIS TUBE, HOWEVER THIS OPERATOR HAS OBTAINED AN AMOC TO ALLOW OPERATING UNTIL FAILURE.  IT HAS BEEN FOUND THAT THIS TUBE WILL FAIL AT ANY TIME, REGARDLESS OF REPLACEMENT OR TIME IN SERVICE.  IT WILL FAIL AT THE BASE WHERE IT IS INSERTED INTO THE TANK FITTING, AND WILL MANIFEST ITSELF AS A MINOR (WEEP).  THE DANGER OF COURSE IS IF IT BREAKS OFF ENTIRELY.  THEREFORE, CONTINUED VIGILENCE IS PARAMOUNT. (TC NR 20070804001)                                                                                                                                                                                                                                                       1Q71 3R3  R  A743    E162                 
20070917000412007091700041SO  2007       9          17         CA070805001      120070803G324017766110        HOSE                                    PIPER PA31T PA31T       7103124SO  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  RT MLG BRAKE    FAILED          W      E   ENGINE SHUTDOWN                                                                                 BA SMOKE/FUMES/ODORS/SPARKS  FLAME/FIRE                                          TXTAXI/GRND HDL  1                      CA       2564                                                           (CAN) WHILE THE PILOTS WHERE TAXIING THE AIRCRAFT, IT WAS NOTED THAT THE RT BRAKES WHERE U/S.  AS THEY WHERE TAXIING BACK TO THE FBO ANOTHER AIRCRAFT REPORTED SMOKE COMING FROM THE RT BRAKE AREA.  THE FIRE WAS PUT OUT BY THE AIRPORT FIRE DEPARTMENT QUICKLY.  AFTER THE INITIAL INSPECTION WAS CARRIED OUT, IT WAS FOUND THAT THE RT LOWER FLEXIBLE BRAKE LINE WAS U/S THAT ATTACHES TO THE CALIPER.  THE RT TIRE WAS U/S DUE TO THE FIRE.  THE WHEEL ASSY WAS REPLACED AND THE AIRCRAFT WAS TOWED TO THE FBO`S HANGER WHERE IT WAS JACKED AND A DETAILED INSPECTION WAS CARRIED OUT.  AFTER THE INSPECTION WAS CARRIED OUT, THERE WAS NO DAMAGE TO THE RT MLG, SURROUNDING PARTS AND STRUCTURE OTHER THAN THE FLEXIBLE BRAKE LINE, CALIPER1L72 3T4  T  A8EA    E4EA    6  CP15EA    
20070912000182007091200018NM  2007       9          12         CA070807001      120070727G3230651781914       LOCK ACTUATOR                           BOEING737   73735B      13844BMNM  GE    CFM56 CFM563B1    13802NE                              NLG             FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) DURING APPROACH, THE NOSE LANDING GEAR DID NOT RECEIVE A DOWNLOCK INDICATION IN THE COCKPIT. IT WAS BELIEVED BY THE CREW THAT THE GEAR FAILED TO EXTEND. A SECOND ATTEMPT WAS MADE AND THE NOSE GEAR EXTENDED AND LOCKED AS NORMAL.  NOTE: THE EMERGENCY EXTENSION WAS NOT USED.  WITH THE LANDING GEAR EXTENDED, THE AIRCRAFT WAS REMOVED FROM SERVICE AND FERRIED TO DESTINATION.  MAINTENANCE INSPECTED THE SYSTEM AND CONDUCTED TROUBLESHOOTING IAW THE AMM. AFTER CONSULTATION WITH MFG, THEY REPLACED THE LOCK ACTUATOR AS IT IS RESPONSIBLE FOR LOCKING THE LANDING GEAR IN THE UP AND DOWN POSITIONS. ITS REPLACEMENT WAS RECOMMENDED BY MFG. AS A PRECAUTION, THE NOSE GEAR ACTUATOR WAS ALSO REPLACED. THE LANDING GEAR UNDERWEN2L72 4F4  FRTA16WE   E2GL                 
20070912000192007091200019NM  2007       9          12         CA070807002      120070803G2611CGAB140000      SMOKE DETECTOR                          BOEING737   737522      138449FNM  CFMINTCFM56 CFM563C1    13802EU                              FWD CARGO BAY   MALFUNCTIONED   W      FA  ACTIVATE FIRE EXT.      UNSCHED LANDING                                                         N  FALSE WARNING                                                                 CRCRUISE         1                      CA                                                                      (CAN) ENROUTE, IT WAS LESS THEN AN HOUR INTO THE FLIGHT WHEN AN ORANGE DETECT LIGHT FOR THE FORWARD CARGO SMOKE DETECTION SYSTEM CAME ON. THE EXTINGUISHER SYSTEM WAS ACTIVATED AND THE FLIGHT DIVERTED TO CLOSEST AIRPORT AND LANDED SAFELY.  AN INSPECTION OF THE FORWARD CARGO COMPARTMENT FOUND NO EVIDENCE OF FIRE OR SMOKE. AN OVERWEIGHT LANDING INSPECTION WAS CARRIED OUT.  THE AIRCRAFT WAS FERRIED BACK TO BASE WHERE THE SYSTEM WAS EXAMINED.  NO SYSTEM FAULTS WERE FOUND, BOTH FORWARD SMOKE DETECTORS WERE REPLACED AS A PRECAUTION AND THE DIVERTER VALVE AND METERING VALVE WERE REPLACED DUE TO THE SYSTEM BEING ACTIVATED.  THE CARGO SMOKE AND FIRE EXTINGUISHER SYSTEM INSTALLED ON THIS AIRCRAFT IS AN AAE STC ST01674AT. 2L72 4F4  FRTA16WE   E21EU                
20070912000202007091200020EU  2007       9          12         CA070807003      320070804G6111697071003       BLADE                                   BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  PROPELLER       DAMAGED         W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA       3425 360                                                       (CAN) DURING APPROACH, AN AIRCRAFT EXPERIENCED IMPACT STRUCTURE DAMAGE DUE TO LOSS OF THE PROPELLER BLADE EROSION STRIP. THE PROPELLER COMPONENT CAME OFF AND STRUCK THE FUSELAGE ICE SHIELD AND DAMAGED THE FUSELAGE.   INSPECTION FOUND THAT THE COMPLETE EROSION STRIP (LEADING EDGE GUARD) WAS MISSING, FROM THE NR 5 BLADE ON LT PROPELLER. THIS BLADE HAD 308 FLIGHT HOURS AND 36O CYCLES SINCE IT WAS REPAIRED DUE TO A BLADE TIP CRACK.  (TC NR 20070807003)                                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070912000212007091200021SO  2007       9          12         CA070807004      120070801G324017700200        PIN                                     PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  PARKING BRAKE   SHEARED         W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) PARKING BRAKE VALVE STOP PIN IN THE OFF POSITION WAS SHEARED OFF CAUSING THE BRAKE LEVER TO GO PAST THE STOP POSITION. THIS CAUSE THE BRAKE TO BE IN A ON POSITION. ON LANDING THE PILOT TESTED HIS BRAKES BY PUMPING THE BRAKES AND BECAUSE THE LEVER WAS PAST THE STOP POSITION IT CAUSE THE BRAKES TO LOCK ON.  WHEN THE PILOT LANDED, THE BRAKES WHERE BOTH LOCKED ON CAUSING THE TIRES TO BURST INTO FLAMES. (TC NR 20070807004)                                                                                                                                                                                                                                                                                                     1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070912000222007091200022    2007       9          12         CA070807005      420070717G2397MS3126E1419P    CONNECTOR                               BELL  205   205A1       1181414SW  LYC   T53   T5317A      41549NE                              NR 2 VHF RADIO  BURNED          W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      DEDESCENT        1                      CA                                                                      (CAN) TRAINING FLIGHT, NOTICED SMOKE COMING UP FROM CENTER CONSOLE BEHIND VHF NR 2 RADIO.  PUT DOWN, A/C ON GROUND. CO-PILOT JUMPED OUT TO CHECK IN BATT COMPARTMENT.  NO ANOMALIES FOUND. FORCE TRIM CB POPPED. CARGO RELEASE LIGHT CAME ON AND STAYED ON. VHF RADIO INOPERATIVE TO TRANSMIT AND RECEIVE, BUT WAS ALWAYS LIVE. CONNECTOR AT BASE OF PILOT CYCLIC STICK, FOUND BURNED/SHORTING OUT, AFFECTING ALL 3 CIRCUITS. (TC NR 20070807005)                                                                                                                                                                                                                                                                                               1G71 4U4  U  H1SW    E17EA                
20070912000232007091200023EU  2007       9          12         CA070807006      120070714G6320332A38101521    PIN                                     SNIAS AS332 AS332C      8680808EU  TMECA MAKILAMAKILA1A    60040EU                              M/R GEARBOX     WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ON MAIN ROTOR GEARBOX REMOVAL SMALL PIN P/N 332A38-1015-21 FOUND INSTALLED IN LIEU OF LARGE PIN P/N 332A38-1019-21 IN LOWER POSITION OF FORWARD SUSPENSION BAR.  RESULTANT, RADIAL PLAY 6 MM APPROXIMATELY.  MFG CONTACTED TO DETERMINE FURTHER ACTION.  RECORDS INDICATE PIN INSTALLED FOR 40 FLIGHT HOURS.  (TC NR 20070807006)                                                                                                                                                                                                                                                                                                                                                                                                         2G72 4U4  U  H4EU    E12NE                
20070912000242007091200024EA  2007       9          12         CA070807007      220070715G7322                CONTROL CABLE                           CESSNA172   172N        2072434CE  LYC   O320  O320H2AD    41508EA                              CARBURETOR      WORN            W      BA  EMER. DESCENT           UNSCHED LANDING                                                         RF PARTIAL RPM/PWR LOSS      FLT CONT AFFECTED                                   CLCLIMB          1                      CA                                                                      (CAN) ONCE AIRCRAFT REACHED 5000 FT THE PILOT COMMENCED CRUISE CHECKLIST, LEANED THE MIXTURE OF THE ENGINE WHEN THE POWER REDUCED TO IDLE. PILOT COULD NOT REGAIN ENGINE POWER AND MADE THE DECISION TO LAND IN A FIELD APPROX 3 MILES NE OF AIRPORT.  UPON LANDING THERE WAS NO APPARENT DAMAGE TO THE AIRCRAFT OR THE PEOPLE ON BOARD. UPON INSPECTION, THE AIRCRAFT WAS NOT DAMAGED AND IT WAS FOUND THAT THE HARDWARE ATTACHING THE MIXTURE CABLE TO THE CARBURETOR WAS WORN, ALLOWING THE CABLE TO SLIDE IN THE CARBURETOR MIXTURE ARM. (TC NR 20070807007)                                                                                                                                                                                1H71 3O3  ONT3A12    E274                 
20070912000252007091200025SW  2007       9          12         CA070807008      120070805G2913                DRIVE SHAFT     ROMEC                   BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              HYD PUMP        SHEARED         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA       2074 2074  00010494                                            (CAN) APPROX 1 HR INTO FLIGHT, COCKPIT NR WARNING HORN CAME ON INTERMITTENTLY.  NR GAUGE BEGAN GIVING ERRATIC INDICATIONS, BEFORE PROGRESSIVELY DECAYING DOWN TO A STABILIZED READING OF 30 PERCENT.  AFTER LANDING, A VISUAL INSP REVEALED A LARGE AMOUNT OF HYDRAULIC FLUID ON THE XMSN DECK, AND A SHEARED OFF INTERNALLY WRENCHING SOCKET HEAD FROM THE UPPER LT CORNER OF MOUNTING PLATE OF THE NR TACH DRIVE ASSY TO THE HYDRAULIC PUMP.  PILOT OPENED UP HYDRAULIC RESERVOIR AND FOUND APPROX 20 PERCENT OF FLUID REMAINING.  ENGINEER WAS CALLED AND REMOVED THE NR TACH GENERATOR, REVEALING A SHEARED SHAFT AT THE DRIVE ADAPTER FOR THE TACH GENERATOR.  HYDRAULIC PUMP AND RESERVOIR ASSEMBLY WAS REPLACED, AND AIRCRAFT DEPARTED FO1G71 3U3  U  H2SW    E4CE                 
20070912000262007091200026WP  2007       9          12         CA070808001      120070807G7820C16932          MUFFLER                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              TAILPIPE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       609                                                            (CAN) DURING SCHEDULED INSPECTION.  AD CF90-03R2 BEING ACCOMPLISHED, A LARGE CRACK WAS FOUND AT THE TAILPIPE ATTACHMENT POINT, IN THE MUFFLER SUB-ASSY.  IT WAS DIFFICULT TO DETERMINE ROOT CAUSE OF CRACK ORIGINATION, BUT POSSIBLE CAUSE WAS IMPACT WITH FOREIGN OBJECT WHEN AIRCRAFT LANDED IN AN UNPREPARED LANDING AREA.  MUFFLER SUB-ASSEMBLY P/N C169-32 REPLACED WITH NEW ASSY, SAME P/N, A/C RELEASED FOR CONTINUED OPERATION (TC# 20070808001)                                                                                                                                                                                                                                                                                        1G71 3O3  O  H11NM   1E4                  
             20081104     CE  2008       11         4          CA070808002      120070807G324410X3504         TIRE                                    CESSNA185   A185F       2072821CE  CONT  O550  IO550D      17042SO  MCAULYD3A34 D3A34C401   GL  MLG             BULGED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) TIRE CORDS DELAMINATING FROM THE INSIDE ALL AROUND THE TIRE.  NO EXTERNAL FAULTS COULD BE DETECTED VISUALLY UNTIL TIRE BEGAN TO BULDGE. (TC NR 20070808002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  O  3A24    E3SO    5  CP47GL    
20070917000422007091700042CE  2007       9          17         CA070808003      120070807G561010138402523     WINDSCREEN                              BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) ON CLIMBOUT, PILOTS WINDSCREEN SHATTERED/CRACKED.  DEVIATED TO ANOTHER AND DEPLANED PASSENGERS.  THE PILOTS INSPECTED THE WINDSCREENS AND DECIDED, BASED ON INFORMATION PROVIDED BY MAINTENANCE, OUT OF MM CHAPTER 5, THAT IT WOULD BE ACCEPTABLE TO FERRY FOR WINDSCREEN REPLACEMENT.  MAINTENANCE PERSONNEL DETERMINED THAT THE COPILOTS WINDSCREEN WAS DELAMINATED AND HAD SMALL CRACKS IN THE LOWER INSIDE CORNER.  IT HAS BEEN CONCLUDED THAT AT SOME POINT IN TIME THE WINDSCREEN HEAT HAD BEEN LT ON AND HAD DELAMINATED THE RT WINDSCREEN,  IT WAS UNDETERMINED WHAT HAD OCCURRED TO THE LT WINDSCREEN TO CAUSE IT TO SHATTER. (TC NR 20070808003)                                                                                2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
             20081112         2008       11         12         CA070808004      220070808G741410400576        CAPACITOR                                                                                                                               MAGNETO         MISMANUFACTURED W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) WHEN REMOVED FROM PACKAGE (NEW) THE FLAG TERMINAL THAT CONNECTS TO THE POINTS IN THE MAGNETO DID NOT HAVE ANY WIRE VISIBLE OUTSIDE THE CRIMP AREA OF THE TERMINAL. ACCORDING TO MFG, THE WIRE MUST BE FLUSH OR EXTENDED SLIGHTLY BEYOND THE CRIMP AREA. ALL 54 CAPACITORS IN STOCK WERE CHECKED AND FOUND TO HAVE THE SAME DEFECT. THESE CAPACITORS WILL BE SENT BACK TO TCM FOR WARRANTY EVALUATION.                                                                                                                                                                                                                                                                                                                                                                               
20070917000432007091700043    2007       9          17         CA070809001      420070806G3442                CDU                                     BOEING737   737210C     1384459NM  PWA   JT8   JT8D9A      52048NE                              WX RADAR        FAILED          W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE AFTER DEPARTURE, THE CREW OBSERVED A FAILURE WITH THE WEATHER RADAR.  DUE TO FORECAST CONDITIONS THE CREW ELECTED TO RETURN TO POINT OF DEPARTURE.  MAINTENANCE REPLACED THE DISPLAY UNIT AND THE SYSTEM TESTED SERVICEABLE.  THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEM REPORTED. (TC NR 20070809001)                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  F  A16WE   E2EA                 
             20081105     CE  2008       11         5          CA070809002      120070809G3233ADI79990021A    ACTUATOR                                BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  MLG             DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) NOSE GEAR ACTUATOR SENT IN TO HAVE SEALS REPLACE DO TO UNIT BECAUSE IT WAS SITTING ON SHELF FOR 6 YEARS. ACTUATOR WAS OVERHAULED AND HAD NEVER BEEN USED. UNIT WAS DISASSEMBLED TO REPLACE SEALS AND INTERIOR OF CYLINDER WAS SCORED AND A SPRING BROKEN. ACTUATOR HAS BEEN SENT BACK FOR OVERHAUL.                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20070917000442007091700044NM  2007       9          17         CA070809003      120070805G2622898052          EXTINGUISHER                            BOEING737   737*               NM  CFMINTCFM567CFM567B22   13802NE                              COCKPIT         LEAKING         W      G   O2 MASK DEPLOYED                                                                                K  FLUID LOSS                                                                    CRCRUISE         1                      CA       12530                                                          (CAN) FLIGHT DECK FIRE EXTINGUISHER LEAKED IN CRUISE.  CAPTAIN AND F/O HEARD A HISSING SOUND COMING FROM THE FIRE EXTINGUISHER BEHIND AND LEFT OF THE F/O. CAPTAIN AND F/O DONNED O2 AND ASSESSED THE SITUATION IE; FEELING THE LEAK NEAR THE EXTINGUISHER`S NECK.  CAPTAIN THEN RELEASED FIRE EXTINGUISHER FROM ITS HOLDER AND STOWED THE UNIT IN THE FORWARD LAVATORY FOR THE REMAINDER OF THE FLIGHT.  CAPTAIN OPENED VENTS AND PUT PACKS ON HIGH AND ENQUIRED AS TO HOW THE FO WAS FEELING. FO SEEMED FINE AND LATER COMMENTED THAT HE MAY HAVE BEEN A BIT DIZZY.  A DETAILED REPORT HAS BEEN REQUESTED FROM THE REPAIR FACILITY AND DETAILS WILL BE UPDATED TO THIS REPORT AS THEY ARE OBTAINED. (TC NR 20070809003)                      2L72 4F4  FRTA16WE   E00055EN             
             20081104     NM  2008       11         4          CA070809004      120070610G2622898052          EXTINGUISHER                            BOEING737   737*               NM  CFMINTCFM567CFM567B22   13802NE                              COCKPIT         FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       10279                                                          (CAN) FOUND A FLIGHT DECK FIRE EXTINGUISHER THAT WAS REMOVED FROM THE AIRPLANE FOR LOSS OF PRESSURE. BOTTLE WAS FOUND COMPLETELY EMPTY AND THE TOP WAS LOOSE. YOU COULD SPIN THE TOP RIGHT OFF. STRIP REPORT REQUESTED FROM REPAIR FACILITY FOR INFORMATION. THIS REPORT WILL BE UPDATED AS INFORMATION BECOMES AVAILABLE. (TC NR 20070809004)                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA16WE   E00055EN             
             20081105     EA  2008       11         5          CA070810001      120070809G32126A05158019      COVER                                   DHAV  DHC2  DHC2MK3     2800107EA  PWA   PT6   PT6A34      52043EA  HARTZLHCB3T HCB3TN3     GL  MLG FLOATS      DAMAGED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            LDLANDING        1                      CA       220                                                            (CAN) THIS TURBO OPERATING AMPH FLOATS WAS ON DESCENT TO LAND AT ITS HOME AIRPORT WHEN THERE WAS NO GEAR DOWN INDICATION ON RT MAIN WHEEL. PILOT ASKED PASSENGER IN THE RT SEAT TO LOOK AT THE TOP OF FLOATS TO CHECK TIE-DOWN ROPES, AND IT WAS NOTICED THAT THE END OF THE FLOAT ROPE WAS IN INSP HOLE ABOVE MAIN GEAR LOCKING MECHANISM. PILOT RETRACTED THE LANDING GEAR TO UP POSTION AND WHEN THERE WAS ALL 4 GEAR UP INDICATION, HE LANDED SAFELY IN THE WATER. ACFT WAS THAN TRANSPORTED TO ITS MAINT BASE WHERE PROBLEM WAS IDENTIFIED AS A DAMAGED UP LOCK CARRAIGE COVER, IT WAS THAN REPLACED WITH A NEW UNIT. THE SYSTEM WAS FUNCTION TESTED SERVICEABLE AND ACFT WAS RETURNED TO SERVICE. NOTE: THE PILOT IN COMMAND WILL BE MORE 1H71 3T4  T  A806    E4EA    6  CP15EA    
20070912000272007091200027EA  2007       9          12         CA070812001      120070809G32304622            PRIORITY VALVE                          CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              NLG             FAULTY          W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA       123203214                                                      (CAN) ON APPROACH, GEAR WAS SELECTED DOWN AND THE NOSE GEAR DID NOT COME DOWN.  THE CREW THEN CYCLED THE GEAR, BUT THE NOSE GEAR STILL DID NOT COME DOWN.  THE CREW SWITCHED 3B HYDRAULIC PUMP FROM AUTO TO ON AND 30 SECONDS LATER THE NOSE GEAR CAME DOWN.  THE LANDING GEAR WAS DEFERRED FOR THE A/C TO RETURN FOR REPAIR.  MAINTENANCE T/S DISCOVERED NLG PRIORITY VALVE TO BE AT FAULT.  PRIORITY VALVE WAS REPLACED AND GEAR SWINGS C/O AND A/C WAS CHECKED SERVICEABLE. (TC NR 20070812001)                                                                                                                                                                                                                                              2L72 4F4  FRTA21EA   E15NE                
20070912000282007091200028NE  2007       9          12         CA070813001      220070727G852027056CA1        PISTON                                  DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  ENGINE          CRACKED         W      O   OTHER                                                                                           KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            NRNOT REPORTED   1                      CA                                                                      (CAN) THE PILOT MADE A PRECAUTIONARY LANDING WHEN HE NOTICED OIL DROPS ON THE WINDSHIELD AND SAW SOME SMOKE COMING OUT FROM THE REAR OF THE COWLING. THE ENGINE WAS INSPECTED TO DETERMINE THE CAUSE OF THE OIL LEAK. A DIFFERENTIAL COMPRESSION SHOWED THAT THE NR 2 CYLINDER WAS FLAT. THE CYLINDER ASSEMBLY WAS REMOVED AND REVEALED THAT THE PISTON WAS CRACKED FROM HALFWAY ACROSS THE TOP, DOWN TO THE PISTON PIN HOLE AND THAT THERE WAS ALSO A .3750 INCH RAGGED HOLE THROUGH THE PISTON ON THE TOP EDGE OF IT ALLOWING THE PRESSURIZATION OF THE CRANKCASE AND PUSHING OIL OUT THE FRONT CASE AROUND THE PROPELLER SHAFT. A COMPLETE CYLINDER AND PISTON ASSEMBLY WERE INSTALLED.  THE PART IS AVAILABLE IF REQUESTED. (TC NR 2007081301H71 3R3  RRCA806    5E1     5  CP206     
20070912000292007091200029NM  2007       9          12         CA070813002      120070730G3411                PITOT TUBE                              BOEING727   727223      1384074NM  PWA   JT8   JT8D15A     52051NE                                              BLOCKED         W      C   ABORTED TAKEOFF                                                                                 P  NO WARNING INDICATION                                                         TOTAKEOFF        1                      CA                                                                      (CAN) THE AIRCRAFT BEGAN TO DEPART ON THE TAKE-OFF ROLL WHEN THE FLIGHT CREW OBSERVED THAT THE CAPTAINS AIRSPEED INDICATION HAD FAILED. THE TAKE-OFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO ADDITIONAL PROBLEMS. UPON INSPECTION OF THE CAPTAINS PITOT-TUBE A PARTIAL BLOCKAGE WAS NOTICED. AN INSECT AND SOME DEBRIS WAS REMOVED FROM THE PITOT-TUBE AND A LEAK TEST WAS CARRIED OUT ON THE CAPTAINS PITOT-STATIC SYSTEM, IAW THE AIRPLANE MM, AND NO FAULTS WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070813002)                                                                                                                                                                                          2L73 4F4  F  A3WE    E2EA                 
20070912000302007091200030SO  2007       9          12         CA070813003      220070719G85200200            PISTON                                  CESSNA150   150H        2071818CE  CONT  O200  O200A       17020SO                              NR 2 CYLINDER   WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1314                                                           (CAN) TOP RING BROKEN.  ALL CYLINDERS REPLACED WITH NEW CYLINDER, PISTONS RINGS VALVES.  COMPRESSION TEST AT INSPECTION ON MIN - 60 OVER 80. (TC NR 20070813003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  O  3A19    E252                 
20070912000312007091200031CE  2007       9          12         CA070813004      120070615G31106227876011      DISPLAY                                 BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  COCKPIT         LOOSE           W      O   OTHER                                                                                           O  OTHER                                                                         TOTAKEOFF        1                      CA                                                                      (CAN) DURING TAKEOFF ROTATION THE MFD SLID OUT OF ITS RACK. THE DISPLAY WAS LIMITED IN MOVEMENT AFT BY THE F/O. THE UNIT WAS PUSHED BACK INTO PLACE AND THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. THE MFD HAD RECENTLY BEEN REPLACED. UPON INVESTIGATION THE LOCKING CLIPS THAT RETAIN THE MFD WERE FOUND IN THE LATCHED POSITION, HOWEVER, THEY HAD FAILED TO ENGAGE THE RACK. THE MFD IS FLUSH ROUTED. THAT IS TO SAY ONCE INSTALLED THERE IS LITTLE TO NO EDGE UPON WHICH TO PULL THE UNIT IN ORDER TO CHECK ITS SECURITY. NORMAL OPERATION OF THE LOCKING FEATURE IS FOR THE LOCKING TAB TO ROTATE DUE TO THREAD FRICTION IN A CLOCKWISE MOTION AS THE LOCKING SCREW IS TURNED. WHEN THIS LOCK FAILS, IT IS NORMALLY DUE TO MISALIGNMEN2L72 4T4  T  A24CE   E4EA    6  CP56GL    
             20081104         2008       11         4          CA070813005      420070803G3420LUN1241E8G8R    INDICATOR                               GROB  120   G120A       1660208EU  LYC   O540  AEIO540D4D5      EA  HARTZLHCC3Y HCC3YR      GL  ATTITUDE        UNRELIABLE      W      O   OTHER                                                                                           N  FALSE WARNING                                                                 CRCRUISE         1                      CA       225  120                                                       (CAN) MFG INSTALLED MICROTECHNA ELECTRIC ATTITUDE INDICATORS IN A FLEET OF 9 AIRCRAFT USED FOR FLIGHT TRAINING. AFTER 18 MONTHS, ONE ORIGINAL ATTITUDE INDICATOR IS STILL FUNCTIONING AFTER 500 HOURS (9) INSTRUMENTS AVERAGED 225 HOURS BEFORE FAILING THE FIRST TIME. (6) HAVE FAILED WITH AN AVERAGE OF 120 HOURS TSO. (3) AIRCRAFT HAVE BEEN GROUNDED WAITING FOR REPLACEMENT INTSTRUMENTS.                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  ORTA49CE   1E4     5  CP25EA    
20070912000322007091200032SW  2007       9          12         CA070814002      120070710G6210206015001107    BLADE                                   BELL  206   206L        1181522SW  ALLSN 25OC  250C20R          GL                              MAIN ROTOR      DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 C  F.O.D.                                                                        LDLANDING        1                      CA       3143                                                           (CAN) UPON LANDING IN A BRUSH AREA, THE PILOT LOWERED THE COLLECTIVE, WHICH IN TURN RAISED (2) TREES THAT WERE SITUATED ON THE LEFT AND THEN HIT THE ROTOR DISK. THE PILOT THEN DISPLACED THE  AIRCRAFT TO THE RT. AN ENGINE SHUTDOWN WAS PERFORMED AND VISUAL INSPECTION CARRIED OUT.  THE ROTOR RPM DID NOT DECREASE UPON IMPACT WITH THE TREES, ONLY A COLLISION SOUND WAS NOTED. PRIOR TO ENGINE SHUTDOWN, ALL ENGINE PARAMETERS WERE NORMAL. THE VISUAL INSPECTION REVEALED THAT THE BLADE WEIGHTS WERE MISSING AT THE BLADE TIPS (3.5 - 4 INCHES). (TC NR 20070814002)                                                                                                                                                                    1G71 3U3  U  H2SW    E4CE                 
20070912000332007091200033SO  2007       9          12         CA070814003      120070707G3230487312          SPRING                                  PIPER PA23  PA23250     7102308SO  LYC   O540  IO540C4B5   41532EA  HARTZLHCE2Y HCE2YR2     GL  DOWNLOCK HOOK   BROKEN          W      EL  ENGINE SHUTDOWN         ABORTED APPROACH                                                        O  OTHER                                                                         APAPPROACH       1                      CA                                                                      (CAN) RT LANDING GEAR DOWN LOCK SPRING (P/N 487-312) BROKE AND LODGED ITSELF BETWEEN THE HOOK AND THE LOCK OF THE UPLOCK BOX.  THE GEAR COULD NOT MOVE AND THEN THE GEAR LIGHT DID NOT COME ON. (TC NR 20070814003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 3O3  O  1A10    1E4     5  CP9EA     
20070912000342007091200034SO  2007       9          12         CA070814004      120070718G2910460635          BOWL                                    PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  HYD FILTER      LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    CRCRUISE         1                      CA                                                                      (CAN) THE RT POWERPACK FILTER BOWL HAD A HYDRAULIC LEAK IN FLIGHT, THE POWERPACK WAS PARTIALLY EMPTY. THE LANDING GEAR WAS MANUALLY DESCENDED AND THE PILOT DECLARED AN EMERGENCY.   MECHANIC REPLACED FILTER ASSY (460635) WITH O-RING (MS 28778-16) THE POWER PACK WAS SERVICED, GEAR SWING CARRIED OUT, LEAK CHECKED SERVICEABLE. (TC NR 20070814004)                                                                                                                                                                                                                                                                                                                                                                                        1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070912000352007091200035    2007       9          12         CA070814005      120070812G781089P11985        CLAMP                                                                      WRIGHTR1820 982C9HE2    67020EA  HAMSTD43D   43D51       NE  EXHAUST PIPE    BROKEN          W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CRCRUISE         1                      CA                                          PC10184C                    (CAN) AIRCRAFT WAS ENROUTE TO A FIRE, DURING CRUISE, THE NR 2 ENGINE FIRE WARNING SYSTEM ACTIVATED. THE ENGINE POWER WAS REDUCED AND THE FIRE WARNING WENT OUT. WHEN POWER WAS RE-APPLIED THE FIRE WARNING CAME ON AGAIN. THE RETARDANT LOAD WAS JETTISONED AND THE AIRCRAFT RETURNED TO BASE. UPON INVESTIGATION BY MAINTENANCE CREW, AN EXHAUST CLAMP HAD BROKEN, ALLOWING THE EXHAUST STACK TO SEPARATE FROM THE CYLINDER CAUSING A FALSE FIRE WARNING INDICATION. A SECOND EXHAUST CLAMP WAS FOUND BROKEN ON THE NR 1 ENGINE WHICH HAD ALSO CAUSED A FIRE WARNING. ALL REMAINING AIRCRAFT IN THE FLEET WILL BE INSPECTED FOR EXHAUST CLAMP CONDITION. (TC NR 20070814005)                                                                          4  R          E259    6  CP8879    
20070912000362007091200036GL  2007       9          12         CA070814006      120070810G5511C2TP160A        BRACKET                                 DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HARTZLHCB3R HCB3R304    GL  HORIZONTAL STAB CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CORROSION ON FRONT TAILPLANE PICKUP BRACKET, FOUND AT INSPECTION WHILE DOING CF-1991-42R1.   (TC NR 20070814006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3R3  RRCA806    5E1     5  CP28EA    
20070912000372007091200037CE  2007       9          12         CA070814007      120070813G78103022406         EXHAUST DUCT                            BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            390                                                       (CAN) DURING ROUTINE MAINTENANCE ON THE ENGINE, AN INSPECTION OF THE POWER TURBINE BLADES INDICATED LARGE CRACKS AND MISSING SECTIONS OF THE EXHAUST DUCT. THIS ENGINE WAS INSTALLED ON APRIL 02, 2007 AFTER OVERHAUL. THE CAUSE OF THE CRACKS ARE UNDER INVESTIGATION. (TC NR 20070814007)                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070912000382007091200038GL  2007       9          12         CA070814008      120070809G3250C2UT473         POST                                    DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  TILLER          SHEARED         W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) TILLER POST FOUND SHEARED AT TOP, UNDER CABLE ATTACH FLANGE. (TC NR 20070814008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1H71 3R3  RRCA806    5E1     5  CP206     
20070912000392007091200039CE  2007       9          12         CA070814009      120070813G2560                SEAT BELT                               CESSNA172   172K        2072430CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160DTM    GL  COCKPIT         FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) SEAT BELT LOOPS THAT SECURE THE FRONT SEAT LAP BELTS TO THE SEAT FAILED.  THIS ALLOWED THE SEAT BELT, WHILE BEING SECURED, TO LOOP OVER THE SEAT BACK ADJUSTMENT LEVER.  WHEN THE PILOT ADJUSTED HIS SEAT PRIOR TO TAXI, THE SEAT BACK ADJUST LEVER WAS ACTIVATED AND THE SEAT BACK RECLINED TO ITS FULL BACK POSITION. (TC NR 20070814009)                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  ONT3A12    E274    5  NP910     
20070912000402007091200040NE  2007       9          12         CA070814010      220070807G7200                ENGINE                                  SKRSKYS61   S61N        8142104NE  GE    CT58  CT581401    30011NE                                              MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  HOHOVERING       1                      CA                                          295178                      (CAN) ROTORCRAFT WAS LOGGING AT THE TIME OF THE ENGINE SHUTDOWN.  THE AIRCRAFT WAS HOVERING ABOVE A LOG GETTING READY TO PULL THE LOG FROM THE SETTING.  NR 1 ENGINE INDICATIONS DROPPED OFF (IE OIL PRESSURE, FUEL PRESSURE, NG). THE AIRCRAFT RELEASED ITS LONGLINE AND BEGAN AN UNSCHEDULED LANDING.  THE AIRCRAFT LANDED WITHOUT INCIDENT AND THE ENGINE WAS REMOVED FOR INSPECTION. (TC NR 20070814010)                                                                                                                                                                                                                                                                                                                                    2G72 4U4  U  1H15    1E3                  
20071102000042007110200004SO  2007       11         2          CA070815001      120070813G3230487495          SPRING          PIPER       7872322     PIPER PA44  PA44180     7104402SO  LYC   O360  O360A1H     41514EA  HARTZLHCC2Y HCC2YR2     GL  DOWNLOCK SPRING BROKEN          W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) ON A LANDING APPROACH, THE PILOT NOTICED THAT THE LT (GREEN) GEAR DOWN AND LOCKED LIGHT WAS NOT ILLUMINATED. AS THE AIRCRAFT WAS SLOWED DOWN ON FINAL THE (GEAR) UNSAFE LIGHT CAME ON. THE PILOTS ELECTED TO GO AROUND AND INFORMED FLIGHT SERVICES ABOUT THEIR CIRCUMSTANCES AND THE LOCAL FIRE DEPARTMENT WAS INFORMED ALSO. MAINTENANCE WAS NOTIFIED AND SPOKE DIRECTLY TO THE PILOTS. IT WAS LEARNED THAT AN EMERGENCY EXTENSION WAS CARRIED OUT AND THE RESULT WAS THE SAME. IT WAS ALSO ESTABLISHED THAT THE LT MAIN GEAR WAS GOING FULL TRAVEL AND JUST NOT LOCKING DOWN. IT WAS DECIDED TO HAVE THE EMERGENCY EXTENSION KNOB PUSHED BACK INTO ITS NORMAL POSITION AND THE GEAR RETRACTED AND EXTENDED HYDRAULICALLY. IT WAS AT THI1L72 3O3  O  A19S0   E286    5  CP920     
20070912000412007091200041GL  2007       9          12         CA070815002      320070813G6110B1843           SEAL            HARTZL      HCB3TN3                                                                         HARTZLHCB3T HCB3TN3     GL  PROPELLER       MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  BUA24432                                            (CAN) PROPELLER WAS RECEIVED BY SHOP BECAUSE OF GREASE LEAKAGE AROUND BLADE CLAMPS. UPON DISASSEMBLY TO PERFORM REPAIRS IT WAS NOTICED THAT THE DUST SEAL WAS MISSING FROM THE PROPELLER PISTON ASSEMBLY. SINCE THIS ITEM CAN`T PHYSICALLY FALL OUT IT IS ASSUMED THAT IT WAS INADVERTENTLY LEFT OUT AT A PREVIOUS REPAIR. (TC NR 20070815002)                                                                                                                                                                                                                                                                                                                                                                                                                               6  CP15EA    
20070917000452007091700045EA  2007       9          17         CA070815003      220070809G7200                ENGINE                                  BEECH 99    99          1154002CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL                  DAMAGED         W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  NRNOT REPORTED   1                      CA       126763595                          PCE51741                    (CAN) DURING TAKEOFF ROLL, (JUST PRIOR TO VR) A LOUD POP WAS HEARD. THE AC CONTINUED WITH THE TAKEOFF AND ONCE AIRBORNE THE CREW DIVERTED BACK TO DEPARTURE AIRPORT FOR LANDING. AS THEY WERE COMING AROUND, THE PROP RPM, TORQUE, AND FUEL FLOW ON THE RT ENGINE BEGAN TO FLUCTUATE BUT REMAINED WITHIN LIMITS. POWER WAS REDUCED AND AN UNEVENTFUL LANDING CARRIED OUT. FLIGHT CREW CONTACTED MAINTENANCE AND WERE INSTRUCTED TO CARRY OUT A GROUND RUN. THE ENGINES WERE RUN UP AND ALL PARAMETERS WERE WITHIN LIMITS, WHEN POWER WAS ADVANCED BEYOND 85 PERCENT NG ON THE RT ENGINE, TORQUE AND FUEL FLOW BEGAN TO FLUCTUATE. AS THIS SEEMED TO INDICATE IT WAS A FUEL SCHEDULING PROBLEM, IT WAS DECIDED, IN CONSULTATION BETWEEN THE FLIGH1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20070912000422007091200042    2007       9          12         CA070816001      320070810G6110                CONNECTOR                               CVAC  440   440         2422902WP  ALLSN 501D  501D13D     03004GL  ALLSN STC   STCA6441        OIL PROP FILLER UNSECURE        W      A   UNSCHED LANDING                                                                                 K  FLUID LOSS                                                                    CRCRUISE         1                      CA                                                                      (CAN) ENGINE NR 1 RPM UNSTABLE, REDUCED RPM TO 13,600.  AIRCRAFT DIVERTED TO NEAREST AIRPORT. ENGINE WAS SHUTDOWN IN FINAL APPROACH, DUE TO RPM REDUCTION TO 13500 RPM.  MAINTENANCE WAS SENT ON SITE AND FOUND THAT OIL PROPELLER FILLER PLUG WAS NOT SECURED PROPERLY AND ONE GALLON OF OIL HAD LEAKED OUT.   PROPELLER REFILLED AND ENGINE RUN C/O (SERVICEABLE). AIRCRAFT RETURN TO SERVICE.  (TC NR 20070816001)                                                                                                                                                                                                                                                                                                                           2L72 4R4  T  6A6     E282    6  CP898     
20070912000432007091200043EA  2007       9          12         CA070816002      120070816G2730215T9250446     CONTROL CABLE                           CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  ELEVATOR        WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A VISUAL INSPECTION ( 50 HRS),  A TECH FOUND AN ELEVATOR CABLE BADLY WORN, ALMOST CUT AT FUS STN 726 ZONE 310 FRONT OF THE PULLEY (TC NR 20070816002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20070912000442007091200044EA  2007       9          12         CA070816003      120070815G27216018610017      POTENTIOMETER                           CNDAIRCL604 CL604       1900301EA                                                               RUDDER TAB CONTRINOPERATIVE     W      C   ABORTED TAKEOFF                                                                                 O  OTHER                                                                         TOTAKEOFF        1                      CA       7                                                              (CAN) ON TAKEOFF ROLL, AS THE AC WAS ACCELERATING AND PRIOR TO 80 KTS. FULL RUDDER INPUT WAS APPLIED TO MAINTAIN CENTERLINE. CENTERLINE WAS UNABLE TO BE MAINTAINED AND THE TAKEOFF WAS ABORTED. THE AIRCRAFT TAXIED WITHOUT INCIDENT BACK TO BASE.  AIRCRAFT IS OPERATED BY MFG. MARKING N605JP (TC NR 20070816003)                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F    RTA21EA                        
20080129000192008012900019    2008       1          29         CA070817001      420070718G3197E321A           CONNECTOR                               PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  CONTROL PANEL   BURNED          W      HD  DEACTIVATE SYST/CIRCUITSRETURN TO BLOCK                                                         B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA       15304                  317952033                               (CAN) SMOKE WAS REPORTED FROM THE OVERHEAD SWITCH PANEL WHEN TAXIING FOR TAKEOFF. THE CONNECTOR BEHIND THE PANEL WAS FOUND IN A BURNED CONDITION. THE CONNECTOR WAS REPLACED BY REMOVING THE BURNED WIRING AND SPLICING IN A NEW CONNECTOR. (TC NR 20070817001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070917000472007091700047NM  2007       9          17         CA070817002      120070813G575385780009011     FLAP TRACK                              DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  RT WING         CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       40546                                                          (CAN) EXCESSIVE CORROSION FOUND ON FLAP TRACKS NR 4 AND NR 5 ON BOTH LT AND RT WINGS DURING 60K REPLACEMENT OF FLAP TRACKS. SUPPORT BRACKETS REMOVED FOR TRANSFER TO NEW BEAMS, CORROSION FOUND IN RECESSES OF TRACKS BEHIND BRACKETS. LT NR 4 TRACK FOUND FULL OF WATER, BOTH SIDES OF BRACKET APPEARS TO BE NEWER BRACKET. RUST STARTING TO FORM BELOW PAINT.  NR 4 LT: P/N 85780009-011; NR 4 RT: P/N 85780009-112; NR 5 LT: P/N 85780010-007;  NR 5 RT: P/N 85780010-008.   RECTIFICATION: FLAP TRACKS REPLACED AS PART OF THE 60K WORK PACKAGE REQUIREMENT. FURTHER INSPECTION OF CORROSION AND CAUSE SHOULD BE CARRIED OUT.  (TC NR 20070817002)                                                                                          2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080324004182008032400418GL  2008       3          24         CA070817003      120070816G32468834040         PIN                                     NAMER T6    HARVARDMK4  1922828GL  PWA   R1340 R1340*      52016NE  HAMSTD12D   12D40       NE  TAIL WHEEL      SHEARED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4917                                                           (CAN) DURING 50 HOUR INSP, EXCESSIVE ROTATIONAL MOVEMENT WAS NOTED ON THE TAIL WHEEL KNUCKLE (FORK), WITH THE TAIL WHEEL CONTROL LOCK ON. TAIL WHEEL MAST WAS DISMANTLED AND PIN HOLDING THE UPPER AND LOWER EXTENSION PIECES TOGETHER WAS FOUND SHEARED. THIS COULD HAVE RESULTED IN THE LOSS OF THE ENTIRE TAIL WHEEL, OR POTENTIALLY IN THE LOSS OF CONTROL ON THE GROUND. UNIT WAS REPAIRED AND RETURNED TO SERVICE. THIS PIN COULD HAVE BEEN DAMAGED BY IMPROPER GROUND HANDLING OF THE AIRCRAFT IE: PUSHING AC IN REVERSE WITH THE CONTROL LOCKS OFF. (TC NR 20070817003)                                                                                                                                                                 1L71 3R3  R  EXPA1L715E2     5  CP257     
20070912000452007091200045WP  2007       9          12         CA070817005      120070816G3246CON1194515      WHEEL                                   GRUMANTS2   TS2ACALFORST3951102WP  WRIGHTR1820 982C9HE2    67020EA  HAMSTD43D   43D51       NE  MLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING AN (A) INSPECTION, A 6 INCH LONG CRACK WAS NOTED ON THE MAIN WHEEL OUTER HALF. THE CRACK WAS RUNNING AROUND THE CIRCUMFERENCE OF THE WHEEL. THE WHEEL ASSEMBLY WAS REMOVED AND A SERVICEABLE WHEEL ASSEMBLY WAS INSTALLED. THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070817005)                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4R4  R  A25WE   E259    6  CP8879    
20070912000462007091200046WP  2007       9          12         CA070817006      120070814G2620                MANIFOLD                                CVAC  340   340CVAC     242270AWP  ALLSN 501D  501D13D     03004GL  ALLSN A6441 A6441FN606  GL  EXTINGUISHER    MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE, AT APPROXIMATELY 7000 FEET AND THE RETARDANT SYSTEM DE-ARMED, THE RETARDANT TANK CONTENTS EXITED THE TANK. THE CREW RETURNED TO BASE.  MAINTENANCE TROUBLESHOT THE SYSTEM AND THE HYDRAULIC MANIFOLD FOR THE RETARDANT TANK WAS REPLACED. THE TANK DOOR OVER CENTERS WERE CHECKED. THE RETARDANT TANK SYSTEM WAS FUNCTION CHECKED, THE AIRCRAFT WAS TEST FLOWN AND RETURNED TO SERVICE. (TC NR 20070817006)                                                                                                                                                                                                                                                                                                                2L72 4R4  T  6A6     E282    6  CP898     
20070912000472007091200047EA  2007       9          12         CA070817007      120070814G5280                DOOR                                    CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF34*            NE                              LT MLG          MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THE LT MAIN GEAR DOOR WAS MISSING AND HAD CAUSED DAMAGE TO THE LT IB FLAP WHEN IT EXITED THE AIRCRAFT. (TC NR 20070817007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20080221000132008022100013    2008       2          21         CA070819001      420070817G34216224565001      VERTICAL GYRO                           BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCE4N HCE4N3      NE  EFIS            FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) PILOT`S EFIS DISPLAYED ATT AND FD FLAGS, CO-PILOT FINISHED FLIGHT. REPLACED GYRO, PROBLEM SOLVED. (TC NR 20070819001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 4T4  T  A24CE   E4EA    5  CP10NE    
20070912000482007091200048NM  2007       9          12         CA070820001      120070801G3231483023          SEQUENCE VALVE                          BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  RT MLG DOOR     INOPERATIVE     W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF, RT GEAR DOOR LIGHT REMAINED ON. LOWERED GEAR, RT MAIN GEAR DID NOT EXTEND.  ACCOMPLISHED ALTERNATE GEAR EXTENSION.  MAINTENANCE REPLACED RT MLG DOOR SOLENOID SEQUENCING VALVE AND SECONDARY MLG SELECTOR VALVE FITTING. BLEED NR 2 HYD SYSTEM.  A/C RETURNED TO SERVICE. (TC NR 20070820001)                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070912000492007091200049CE  2007       9          12         CA070821001      120070820G323312810016        HOUSING                                 CESSNA172   172RG       2072438CE  LYC   O360  O360F1A6    41514EA  MCAULY2D34C B2D34C220   GL  ACTUATOR        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5458                                                           (CAN) 500 HOUR LIQUID PENETRANT INSPECTION IAW MFG SEB 01-2 REVEALED, CRACK AT INDICATED AREA (TC NR 20070821001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  O  3A17    E286    5  CP7EA     
20070912000502007091200050NM  2007       9          12         CA070821002      120070815G271082740162101     LINK ASSY                               BOMBDRDHC8  DHC8402     1390042NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  LT AILERON      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1753                                                           (CAN) WHILE MAINTENANCE WAS DOING A OVERNIGHT CHECK TO THE AIRCRAFT, THEY OBSERVED THE LINK-ASSY AILERON LVDT WAS HANGING DOWN.  THE ROD LINK HAD BROKEN AT THE AILERON END. (TC NR 20070821002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20070912000512007091200051EA  2007       9          12         CA070821003      320070608G611176EM8S5060      BLADE           SNSNCH      76EM8S5060  PIPER PA28  PA28181     7102807SO  LYC   O360  O360A4M     41514EA  SNSNCH76E   76EM8S5     EA  PROPELLER       DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  16514K                                              (CAN) WELDED PROPELLER, AIRCRAFT IMPORTED, NO LOG FOR FIXED-PITCH PROP.  PROP REMOVED FOR 5 YR CORROSION INSPECTION AS A PRECAUTIONARY MEASURE - SINCE PROP WAS ONLY ALODINED, PROP WAS ANODIZED DURING INSPECTION AT HOPE AERO, TIP FOUND STAINED AFTER ANODIZING.  CONFIRMED WELDING OF PROP BY EDDY CURRENT. (TC NR 20070821003)                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  O  2A13    E286    5  NP4EA     
20070912000522007091200052EA  2007       9          12         CA070821004      120070821G3246215850026       WHEEL                                   CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  NLG             DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       140                                                            (CAN) THE (6) DOWEL PINS ON NOSE WHEEL HAS BEEN FOUND PROTRUDED FROM HUB AND THE RETAINING WASHER DEFORMED OR BENDED.   (TC NR 20070821004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20080319001522008031900152SW  2008       3          19         CA070821005      120070820G7500                B-NUT                                   BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              BLEED AIR       LOOSE           W      R   AUTOROTATION                                                                                    R  PARTIAL RPM/PWR LOSS                                                          DEDESCENT        1                      CA                                                                      (CAN) THE ROTORCRAFT DEPARTED AT LANDING AREA AT APPROX 4500 FT WITH ALL NORMAL PARAMETERS. AT APPROX 4300 FT THE PILOT NOTICED A DIFFERENCE IN ENGINE NOISE LEVELS. THE DIFFERENCE IN NOISE LEVELS WERE ACCOMPANIED BY ACTIVATION OF THE ENGINE AUTO RE-LIGHT SYS AND A DROP IN NG TO GROUND IDLE. THE PILOT ELECTED TO ENTER INTO AUTOROTATION AND LANDED WITH NO DAMAGE TO THE AC.  THE CAUSE WAS DETERMINED TO BE AN AIR LEAK TO THE GOVERNOR FROM A LOOSE B-NUT. (TC NR 20070821005)                                                                                                                                                                                                                                                       1G71 3U3  U  H2SW    E4CE                 
20080306001332008030600133CE  2008       3          6          CA070821006      120070820G7110101910016651    INTAKE          BEECH                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL  COWL            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) COWL ASSY LOWER FWD P/N 101-910024-1 WAS ONCE MODIFIED. (TC NR 20070821006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 4T4  T  A24CE   E4EA    5  CSTC      
20070912000532007091200053EA  2007       9          12         CA070822001      120070822G2810215640026       FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  NR 5            LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) FUEL LEAK ON CELL, RT, NR 5.  DROPS 9963 (TC NR 20070822001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20070912000542007091200054EA  2007       9          12         CA070822002      120070822G2810215640011       FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE                  LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       834                                                            (CAN) FUEL LEAKING FROM PATCH ON BOTTOM SURFACE OF CELL.  A/C HOURS 1889 CYCLES 1142 DROPS 9727  (TC NR 20070822002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20071102000052007110200005NM  2007       11         2          CA070822003      120070805G2910AS11510K0324    HOSE                                    BOEING767   767306      1385148NM                                                               HYDRAULIC SYS   DAMAGED         W      A   UNSCHED LANDING                                                                                 JFJWARNING INDICATION        FLT CONT AFFECTED         WARNING INDICATION        CRCRUISE         1                      CA                                                                      (CAN) AIRCRAFT WAS ONE HOUR OUT OF DEPARTURE PLACE AND ON ROUTE TO ENGLAND WHEN EICAS ILLUMINATED WITH THE FOLLOWING MESSAGES: C HYD SYS FLUID LOSS - C HYD SYS PRESS AIRCRAFT DIVERTED TO NEAREST AIRPORT WHERE IT WAS FOUND THAT THE LT MAIN LANDING GEAR TRUCK TILT ACTUATOR RETURN FLEX HOSE WAS DAMAGED. THE FOLLOWING MAINTENANCE ACTIONS WERE PERFORMED: - DAMAGED HYDRAULIC HOSE REPLACED (TC NR 20070822003)                                                                                                                                                                                                                                                                                                                           2L72 4F    RTA1NM                         
20070912000552007091200055NE  2007       9          12         CA070822004      220070822G7210311294501       CASE                                                                       PWA   PT6   PT6A67D          NE                              RGB             CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) THIS PART WAS DECLARED UNSERVICEABLE DURING A TENTATIVE REPAIR AT MFG,  HOWEVER, IT WAS REINSTALLED INTO THE ENGINE BY MISTAKE AND DELIVERED TO THE CUSTOMER.  THE PART WAS CORRODED ON THE EXTERNAL WALL AND FURTHER PROGRESSION OF THIS DAMAGE COULD HAVE RESULTED IN A SUBSTANTIAL OIL LEAK FROM THE REDUCTION GEARBOX.  MFG DISCOVERED ITS MISTAKE PRIOR ENGINE USE AND THE ENGINE WAS IMMEDIATELY RECALLED FOR PART REPLACEMENT.  MFG IS CURRENTLY EXAMINING THE MAINTENANCE RECORDS OF SPECIFIC ENGINES TO MAKE SURE THAT A SIMILAR MISTAKE DID NOT HAPPEN ELSEWHERE.  (TC NR 20070822004)                                                                                                                                                 4  T          E26NE                
20071102000062007110200006CE  2007       11         2          CA070822005      120070816G579765280042        WIRE HARNESS                            CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              WING            CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9022                                                           (CAN) WHILE DOING SKIN REPAIRS ON RT WING WE FOUND WIRES CHAFED IN THE FLAP BAY AREA WHERE THE BUNDLE WAS TY WRAPPED TO A NYLON ANCHOR. THE TY WRAP WAS ONLY PUT THROUGH ON LEG OF THE ANCHOR NOT BOTH. THE CONDITION WAS FOUND AT 4 ANCHORS. THE LT WING WAS INSPECTED. THE WIRE BUNDLE THERE WAS TY WRAPPED THROUGH BOTH LEGS OF THE ANCHOR AND NO DEFECT WAS FOUND. THE P/N OF THE ANCHOR IS S1471-4. THE TY WRAPS ANCHORING THE WIRE BUNDLES SHOULD BE REMOVED TO REALLY INSPECT FOR DAMAGE AS THE AREA IS DIFFICULT TO INSPECT AND THE DAMAGE IS AT THE BOTTOM OF THE WIRE BUNDLE. (TC NR 20070822005)                                                                                                                                     2L72 4F4  FRTA22CE   E25EA                
20080306001342008030600134SW  2008       3          6          CA070822006      120070820G6320206040004       TRANSMISSION                            BELL  206   206L1       1182107SW  ALLSN 250C  250C28B     03013GL                              MAIN ROTOR      MAKING METAL    W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA       6670 2778                                                      (CAN) SHORTLY AFTER TAKEOFF THE PILOT RECEIVED A CHIP LIGHT ON THE TRANSMISSION.  LANDED THE AIRCRAFT.  METAL WAS DISCOVERED ON THE SENSOR. THE AIRCRAFT WAS REMOVED FROM SERVICE AND THE TRANSMISSION WAS REPLACED WITH A SERVICEABLE UNIT. AIRCRAFT RETURNED TO SERVICE (TC NR 20070822006)                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H2SW    E1GL                 
20071102000072007110200007CE  2007       11         2          CA070822007      120070816G801187818           RELAY                                   CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  SNSNCH72C   72CK        EA  STARTER         BURNED          W      HA  DEACTIVATE SYST/CIRCUITSUNSCHED LANDING                                                         B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) STARTER RELAY STUCK CLOSED AFTER ENGINE START. SUBSEQUENT DAMAGE WAS NOTED ON STARTER AS WELL. (TC NR 20070822007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A19    E223    5  NP9045    
20080306001362008030600136SO  2008       3          6          CA070822008      120070821G2912AN62341         FILTER HOUSING                          PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  HYD SYSTEM      CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) ON THE 21ST OF AUGUST 2007, MAINTENANCE RECEIVED A CALL THAT AN AC HAD A HYDR FLUID LEAK. A RESCUE MISSION WAS DISPATCHED TO THE AC. UPON INVESTIGATION ONCE MAINT ARRIVED AT LOCATION IT WAS FOUND THAT THE NR 1 ENG HYDR FILTER HSG WAS LEAKING. AFTER DISASSEMBLY, IT WAS NOTED THAT THERE WAS A CRACK IN THE TREADS RUNNING .5 AROUND THE DIAMETER. THE HYDR FILTER WAS ISOLATED FROM THE SYS, THE SYS TOPPED UP WITH FLUID, AND A LEAK RUN PERFORMED BEFORE RETURNING TO DEPARTURE WITHOUT PASSENGERS. IT HAS BEEN DETERMINED THROUGH AN INVESTIGATION THAT THE FAILURE WAS A DIRECT RESULT OF THE USAGE OF THE WRONG PN O-RING. THE O-RING THAT WAS FOUND INSTALLED ON THE FILTER HOUSING IS OF THE SAME OUTER DIAMETER AS THE PROPE1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20070912000562007091200056EU  2007       9          12         CA070823001      120070816G275059128437        SENSOR                                  EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF3410E6    30015NE                              TE FLAP         DEFECTIVE       W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH, FLIGHT EXPERIENCED A FLAP FAIL MESSAGE.  SLAT WENT TO 3 GREEN, FLAP INDICATION BECAME YELLOW, AND SHOWED BELOW THE 2 MARKER.  FLIGHT DID GO AROUND, AND DECLARED EMERGENCY WITH TOWER.  CFR WAS AVAILABLE, AND FLIGHT LANDED AT HIGHER THAN NORMAL SPEED.  INFLIGHT PERFORMED ABNORMAL LANDING PROCEDURE AFTER THEY WERE BRIEFED BY FLIGHT CREW THAT THEY WERE GOING TO LAND AT HIGHER THAN NORMAL SPEED.  PRIOR TO TAXI, CFR INSPECTED AIRCRAFT. ON INVESTIGATION, FOUND RT OB FLAP SKEW SENSOR AT FAULT, SENSOR REPLACED IAW AMM 27-53-06-400.  MOC REQUESTED THAT NR 4 AND NR 3 RT FLAP ACTUATORS BE REPLACED AS WELL.  (TC NR 20070823001)                                                                               2L72 4F4  FRTA57NM   E00070EN             
20080306001372008030600137    2008       3          6          CA070823002      420070821G2564                JETTISON SYSTEM                         SKRSKYS76   S76C        8143008NE  TMECA ARRIELARRIEL2S2   60036NE                              LIFE RAFT       FAILED          W      C   ABORTED TAKEOFF                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) EXTERNAL LIFERAFT JETTISON SYS FAILED TO OPERATE. WHEN LEVER ACTUATED, CABLE BROKE AND PULLEY BRACKET ON LT SIDE OF CENTER PEDESTAL DETACHED. (2) BRACKETS UNDER FLOOR FOUND TO BE LOCATED INCORRECTLY.  INSTALLATION WAS CARRIED OUT IAW ASI-500-100 REV.G. (TC NR 20070823002)                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G72 3U4  UNCH1NE    E00054EN             
20071102000082007110200008CE  2007       11         2          CA070823003      120070821G2510SPL19251        LOCK                                    CESSNA206   T206H       2073303CE  LYC   O540  TIO540AJ1A       EA  MCAULY3D36C B3D36C432   GL  SEAT            BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       366                                                            (CAN) RT SEAT LOCKING PIN SHEATH FOUND BROKEN AT THE SEAT LEG ATTACH POINT. THE LOCKING PIN WOULD RETRACT BUT NOT ENGAGE ON THAT SIDE. THE SEAT LOCK MECHANISM COMPRISES OF A SPRING LOADED HANDLE , WITH TWO CABLES ATTACHED AND TWO SHEATHS SECURED TO THE SEAT LEG WHICH SURROUND THE LOCKING PINS. PART REPLACED. (TC NR 20070823003)                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  ORTA4CE    E14EA   5  CP58GL    
20070917000492007091700049SW  2007       9          17         CA070823004      120070821G6310M2742630150     RETAINER                                BELL  407   407         1182206SW                                                               FREEWHEEL UNIT  MISINSTALLED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  A6724                                               (CAN) UPON QUALIFYING A FREEWHEELING UNIT, IT WAS DISCOVERED THAT THE WRONG RETAINING RINGS WERE USED IN (2) PLACES.  SUSPECT RETAINING RINGS M27642/3-0152C WERE INSTALLED IN ASSEMBLIES INSTEAD OF M27426/3-0150C RETAINING RINGS.  THIS OCCURRED DURING APRIL 07. (TC NR 20070823004)                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3U    O H2SW                         
20070917000502007091700050NE  2007       9          17         CA070823005      220070819G7261                IMPELLER                                DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  ENGINE          LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KBJFLUID LOSS                SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION        TXTAXI/GRND HDL  1                      CA       1075810758                         TM120329                    (CAN) ON TAXI, THE F/O NOTICED SMOKE IN THE FLIGHT DECK AND F/A CONFIRMED HAZE IN CABIN. BLEEDS WERE TURNED OFF. AS AIRCRAFT TURNED ONTO GATE LAV SMOKE DETECTOR WENT OFF. CREW STOPPED 10 FEET SHORT OF THE GATE SHUT DOWN AIRCRAFT AND DEPLANED PASSENGERS.   IT WAS NOT A RAPID DEPLANEMENT AS THERE WAS NO PANIC AMONG PASSENGERS BUT CONCERN AS THEY COULD SEE SMOKE. FIRE FIGHTERS BOARDED AIRCRAFT AFTER PASSENGERS DEPLANED AND REPORTED NO VISIBLE SMOKE OR OIL SMELL. A LITTLE LATER MAINTENANCE WENT ON BOARD AND NO SMOKE ODOR WAS EVIDENT. A VERY SLIGHT OIL/HYDRAULIC ODOR WAS NOTICED AROUND THE CENTER CABIN AREA. MAINTENANCE TROUBLE SHOOTING CONSISTED OF A SERIES OF ENGINE RUNS WHICH ISOLATED PROBLEM TO NR 2 ENGINE. REPL2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070917000512007091700051GL  2007       9          17         CA070823006      120070713G51002224121400      BRACKET                                 DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  ALTERNATOR      BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       95                                                             (CAN) ALTERNATOR BRACKET IS BREAKING ON THESE AIRCRAFT AROUND 100 HOURS T/S.  THE FACTORY HAS RUN OUT OF STOCK AND IS ROBBING THE PART FROM NEW PRODUCTION AIRCRAFT.  SUGGEST RE ENGINEERING AND POSSIBLE AD. (TC NR 20070823006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20071102000092007110200009CE  2007       11         2          CA070823007      120070821G2822A10055B         PUMP                                    CESSNA206   T206H       2073303CE  LYC   O540  TIO540AJ1A       EA  MCAULY3D36C B3D36C432   GL  FUEL BOOST      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       366                                                            (CAN) FUEL DYE RESIDUE NOTED ON ELECTRIC FUEL BOOST PUMP HOUSING, FOUND TO BE FROM AN AUX PORT PLUG. PLUG RESEALED, FURTHER CHECK FOR SEEPING SATISFACTORY. (TC NR 20070823007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3O3  ORTA4CE    E14EA   5  CP58GL    
20080306001382008030600138SW  2008       3          6          CA070823008      120070818G2810EA4703587       TANK                                    BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              FUEL SYSTEM     FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) TANK UNIT WAS INSTALLED FOR AN INACCURATE FUEL INDICATION. AFTER INSTALLATION OF THE REPAIRED TANK UNIT WE APPLIED GROUND POWER FOR THE FUEL CALIBRATION AND FOUND THE GAUGE TO BE INOPERATIVE. AFTER TROUBLESHOOTING IT WAS DETERMINED THAT THE TANK UNIT WAS FAULTY.  THE TANK UNIT WAS REMOVED AND A RESISTANCE CHECK WAS PERFORMED IAW THE MM, THE TANK UNIT FAILED THE TEST. (TC NR 20070823008)                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  H2SW    E4CE                 
20070917000522007091700052CE  2007       9          17         CA070823009      120070724G7931IO360G          ENGINE                                  CESSNA337   337G        2075730CE  CONT  O360  IO360G      17025SO  MCAULY2AF34CD2AF34C306  GL                  FAILED          W      AE  UNSCHED LANDING         ENGINE SHUTDOWN                                                         J  WARNING INDICATION                                                            CRCRUISE         1                      CA            1990                                                      (CAN) REAR ENGINE EXPERIENCED A LOSS OF OIL PRESSURE DURING FLIGHT. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. ENGINE WAS REPLACED.  UNABLE TO DETERMINE OIL PRESSURE PROBLEM WITH FAILED OIL PRESSURE ON ENGINE. ENGINE WAS SHIPPED TO ENGINE SHOP. (TC NR 20070823009)                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H72 3O3  O  A6CE    E1CE    5  CP5EA     
20071102000102007110200010CE  2007       11         2          CA070823010      120070725G552007341102        TORQUE TUBE     CESSNA                  CESSNA182   182G        2072716CE  CONT  O470  O470R       17026SO  MCAULY2A36C 2A36C29     GL  ELEVATOR        LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3830                                                           (CAN) MINOR PLAY (UP AND DOWN) ON THE RT ELEVATOR CAUSE BY LOOSE RIVETS ON THE TORQUE TUBE (TC NR 20070823010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A13    E273    5  CP880     
20070917000532007091700053NM  2007       9          17         CA070823011      120070822G5610001A561A0000218 WINDOW                                  DORNERDO32  DO328100    2996000NM                                                               COCKPIT         CRACKED         W      B   EMER. DESCENT                                                                                   O  OTHER                                                                         CRCRUISE         1                      CA       6521 6088                                                      (CAN) ENROUTE AT FLIGHT LEVEL 27,000 THE PILOTS LT SIDE WINDOW CRACKED WITH A LOUD POP.  INITIATED DESCENT TO 8,000 FEET AND MANUALLY RAISED CABIN PRESSURE TO ZERO DIFFERENTIAL PRESSURE AND CONTINUED.  ADVISED COMPANY OF THE FAILURE PRIOR TO ARRIVAL.  AN ENGINEER INSPECTED THE WINDOW AND FOUND IT WITHIN LIMITS FOR A FERRY FLIGHT. AUGUST 23,2007  FOR REPLACEMENT OF THE WINDOW. (TC NR 20070823011)                                                                                                                                                                                                                                                                                                                                  2H72 4T    RTA45NM                        
20071102000112007110200011EA  2007       11         2          CA070823012      120070821G261214034012        SWITCH                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              RT FIRE DETECT  FAILED          W      O   OTHER                                                                                           N  FALSE WARNING                                                                 TXTAXI/GRND HDL  1                      CA       9156 9156                                                      (CAN) DURING LANDING ROLLOUT CREW RECEIVED MOMENTARY ILLUMINATION OF (BOTTLE ARMED PUSH TO DISCH) FOR RT ENG. CREW WAS CHECKING FOR TRAFFIC AS HAD BEEN CLEARED ACROSS ANOTHER RUNWAY. WHEN ACROSS THIS RUNWAY NOTICED RED (R ENG OIL PX) AND RT ENG N1 AND N2 (ZERO). CREW CARRIED OUT RT ENG SHUTDOWN PROCEDURE. MAINTENANCE INSPECTION FOUND RT ENG FIRE PUSH SWITCH FAULTY. SWITCH REPLACED, FUNCTION CHECKS CARRIED OUT, AIRCRAFT RETURNED TO SERVICE. NOTE: ACTIVATION OF ENG FIRE PUSH SWITCH WILL SHUT OFF FUEL/HYD CAUSING ENGINE TO SHUT DOWN. (TC NR 20070823012)                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20080306001392008030600139SO  2008       3          6          CA070823013      120070810G3297                CONNECTOR                               PIPER PA44  PA44180     7104402SO  LYC   O360  O360E1A6D   42305EA  HARTZLHCC2Y HCC2YR2     GL  DOWNLOCK        BROKEN          W      O   OTHER                                                                                           N  FALSE WARNING                                                                 DEDESCENT        1                      CA                                                                      (CAN) WIRE FOUND BROKEN ON DOWNLIMIT SWITCH CONNECTOR. (TC NR 20070823013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A19S0   E286    5  CP920     
20071102000122007110200012EU  2007       11         2          CA070824001      120070803G27521703911         ACTUATOR                                EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF34*            NE                              TE FLAPS        MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH, SLAT FAIL AND COUNTLESS MESSAGES ON EICAS ON INITIAL SELECTION. SLAT 0, FLAP 1. FOUND LT NR 4 ACTUATOR RT NR 4 ACTUATOR AND RT NR 7 ACTUATOR TRIPPED.  ACTUATORS CHANGED IAW AMM 27-81-01. OPERATION CHK C/O, FOUND SYS SERVICEABLE. OTHER P/NS AFFECTED: 1703909, S/N 216 1703911, S/N 229 (TC NR 20070824001)                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA57NM   E15NE                
20070917000542007091700054EA  2007       9          17         CA070824002      120070819G32466A07116002      CYLINDER                                DHAV  DHC3  DHC3        2800202EA  PWA   PT6   PT6A34      52043EA  HARTZLHCB3T HCB3TN3     GL  FLOAT           CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A WHEELS DOWN LANDING OF AN AMPHIBIOUS EQUIPPED AIRCRAFT, THE LANDING GEAR COLLAPSED.   UPON INSPECTION, CORROSION WAS NOTED UNDER THE (ZAP STRAPS), WHICH WERE INSTALLED BY THE MANUFACTURER, ON BOTH LT AND RT NOSE GEAR ACTUATING CYLINDERS.  ON THE LT CYLINDER, THE CORROSION WAS EXTENSIVE ENOUGH THAT HYDRAULIC FLUID WAS LEAKING THROUGH A PIN HOLE THAT HAD FORMED. (TC NR 20070824002)                                                                                                                                                                                                                                                                                                                                   1H71 3R4  T  A815    E4EA    6  CP15EA    
20071102000132007110200013EA  2007       11         2          CA070824003      120070824G2810215640751       FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE                  LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) LEAK FROM BOTTOM SURFACE ON FUEL CELL NR 8 RT.  A/C HOURS 3381     CYCLES 2237.  DROPS 15187 MFG. (TC NR 20070824003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20080306001412008030600141CE  2008       3          6          CA070824004      120070810G5520115610010325    TORQUE TUBE                             BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  ELEVATOR        WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       16                                                             (CAN) ON INSPECTION, THE ELEVATOR WAS FOUND TO HAVE .75 INCH PLAY AT T/E. THE ELEVATOR WAS REMOVED AN THE TORQUE TUBE WAS INSPECTED. ALL 4 TAPER PINS WERE FOUND LOOSE, AND FOUND INSTALLED TO MAXIMUM ALLOWED PENETRATION. UPON DISASSEMBLY THE HOLES WERE FOUND OVERSIZED AND FILLED WITH PAINT FROM MFG. NEW TORQUE TUBE WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070824004)                                                                                                                                                                                                                                                                                                                                                 1L72 3T4  T  A14CE   E4EA    5  CSTC      
20070917000552007091700055EU  2007       9          17         CA070824005      120070730G2910373Q2277        LINE                                    BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  HYDRAULIC SYS   LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) WHILE FLYING BOTH HYDRAULIC PUMP LIGHTS CAME ON.  THE AIRCRAFT LANDED USING ITS BACKUP SYSTEM.  IT WAS FOUND THAT THE HYDRAULIC LINE THAT RUNS BETWEEN THE PUMP AND FILTER ON THE LT NACELLE.  THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.  THE LEAK CAME FROM A SPOT WHERE THE LINE WAS CLAMPED. (TC NR 20070824005)                                                                                                                                                                                                                                                                                                                                                                                                 2L72 3T4  T  A24EU   A196    6  CP899     
20070917000562007091700056NE  2007       9          17         CA070824006      320070813G61108173881         SEAL                        14SF23      DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  PROPELLER       TORN            W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA       85         20060114                            20060114        (CAN) CREW NOTICED A LARGE AMOUNT OF OIL ON THE LT NACELLE WHICH APPEARED TO ORIGINATE FROM THE PROPELLER. THE ENGINE WAS SHUTDOWN DUE TO THE EXCESSIVE LEAKAGE AND THE AIRCRAFT RETURNED TO BASE.  THE PROPELLER NR 1 BLADE SEAL WAS REPLACED AND GROUND LEAK CHECKS CARRIED OUT.  THE SEAL (WHICH WAS FURTHER DAMAGED DURING REMOVAL) APPEARS TO HAVE HAD A TEAR ON THE SURFACE WHICH FACES OB AND IS EXPOSED WHEN INSTALLED. (TC NR 20070824006)                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070917000572007091700057WP  2007       9          17         CA070824007      120070725G7921315341          DOOR                                    CVAC  440   440         2422902WP  ALLSN 501D  501D22      03005GL  HAMSTD54H   54H60       NE  OIL COOLER      INOPERATIVE     W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA            26                                                        (CAN) AIRCRAFT WAS DISPATCHED FOR FIRE ACTION. AFTER DEPARTURE, THE RT OIL TEMPERATURE GAUGE WAS OBSERVED TO BE AT THE BOTTOM OF THE RED ARC, APPROXIMATELY 100 DEGREES C. THE FLIGHT CREW IMMEDIATELY SHUTDOWN THE RT ENGINE AS A PRECAUTION AND RETURNED TO BASE. DURING INSPECTION BY MAINTENANCE, THE RT OIL COOLER DOOR WAS OBSERVED TO BE NOT FUNCTIONING AND POSITIONED FULLY CLOSED. THE RT OIL COOLER DOOR ACTUATOR WAS REMOVED AND INSPECTED. DURING DISASSEMBLY, SEVERAL WIRES AND A TERMINAL BLOCK WERE FOUND TO BE BROKEN IN THE ELECTRICAL BOX. THE OIL COOLER DOOR ACTUATOR WAS REPLACED AND RIGGED IAW MM. AFTER GROUND CHECKED SERVICEABLE, THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070824007)                          2L72 4R4  T  6A6     E282    6  CP906     
20080129000202008012900020CE  2008       1          29         CA070826000      120070825G3245                TUBE            MICHEL                  BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCE4N HCE4N3      NE  TIRE            DETACHED        W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      CA                  6196W00409                                          (CAN) ON TAKEOFF THE CREW NOTICED A STRONG VIBRATION. THEY DECIDED TO CANCEL THE FLIGHT AND LAND BACK AT AIRPORT.  FOUND THE NOSE TIRE BALANCE PATCH (FACTORY INSTALLED) HAD COME DISCONNECTED AND WAS TUMBLING LOOSE INSIDE THE TIRE. (TC NR 20070826000)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 4T4  T  A24CE   E4EA    5  CP10NE    
20070917000602007091700060NE  2007       9          17         CA070827001      220070823G7250311666801       GASKET                                  CESSNA500   S550        2076607CE  PWA   JT15  JT15D4      52112NE                              NR 4 BRG HSG    LEAKING         W      E   ENGINE SHUTDOWN                                                                                 JK WARNING INDICATION        FLUID LOSS                                          APAPPROACH       1                      CA            1840                                                      (CAN) NR 4 BEARING GASKET LEAKED CAUSING COKING AND BLOCKAGE OF THE OIL SCAVENGE TUBE. (TC NR 20070827001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 4F4  FRTA22CE   E1NE                 
20071102000142007110200014NM  2007       11         2          CA070827002      120070725G2761A44700009       HOUSING                                 DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  ACTUATOR        CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                  001677                                              (CAN) WHILE DOING A LAYOVER INSPECTION A HYDRAULIC LEAK WAS FOUND IN THE LT FLAP AREA. THE LEAK WAS FOUND TO BE COMING FROM THE LT OB ROLL SPOILER ACTUATOR.  UPON REMOVAL OF THE ACTUATOR IT WAS FOUND THAT THE HOUSING HAD CRACKED IN THE AREA SUROUNDING ONE OF THE PLUGS CAUSING THE PLUG TO DISLODGE. THE CRACK EXTENDED AROUND THE ENTIRE CIRCUMFERENCE OF THE ACTUATOR BODY WHERE THE PLUG IS THREADED IN. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE (TC NR 20070827002)                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20070917000612007091700061EU  2007       9          17         CA070827003      120070808G5200SP915C16        SEAL                                    BRAERODH125 BAE125800A  1500285EU  GARRTTTFE731TFE7315R    01518WP                              BUTTON          DETERIORATED    W      O   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      CA       6436                                                           (CAN) UPON CLIMB OUT WITH CABIN DIFFERENTIAL PRESSURE APPROACHING APPROXIMATELY 6 PSI, A DISTINCT AUDIABLE DISCERNING NOISE WAS HEARD FROM THE CENTER AREA OF THE CABIN. DURING DESCENT WHERE CABIN DIFFERENTIAL PRESSURIZATION FELL BELOW 6 PSI, NOISE WOULD SUBSIDE AND GO AWAY. NUMEROUS MAINTENANCE ACTIONS WERE CONDUCTED IN ORDER TO ISOLATE CAUSE INCLUDING PRESSURIZATION CHECKS AND CABIN LEAK RATES. NOISE COULD NOT BE REPRODUCED ON THE GROUND WHICH LED TO THE CONCLUSION THAT AIRSPEED WAS ALSO A FACTOR.  FINALLY THE RUBBER RING SEAL WHICH IS HOUSED IN THE EXTERNAL RELEASE BUTTON MECHANISM OF THE EMERGENCY ESCAPE HATCH WAS REPLACED AND THE MECHANISM LUBRICATED. NOISE DISSAPEARED.  CONCLUSION WAS THAT THE BUTTON WAS V2L72 4F4  FRTA3EU    E6WE                 
20071102000152007110200015EA  2007       11         2          CA070827004      120070824G3320BR95005         BALLAST                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              CABIN LIGHT     BURNED          W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA                                                                      (CAN) CREW REPORTED WHEN THEY APPLIED EXT AC POWER TO THE AIRCRAFT AND TURNED ON THE SWITCH IN THE COCKPIT, THEY COULD SMELL SOMETHING BURNING AND SAW A BLUE HAZE IN THE AIR. THEY IMMEDIATELY TURNED POWER OFF AND CALLED MAINTENANCE CONTROL.  MAINTENANCE INSPECTION REVEALED THAT LIGHT BALLAST AT 7DF WAS FOUND TO BE THE SOURCE OF THE SMOKE/SMELL. THE BALLAST WAS REMOVED AND THE LIGHT WAS DIFFERED SO THE A/C COULD RETURN TO DEPARTURE FOR REPAIRS. ONCE IN THE AREA WHERE BALLAST WAS INSTALLED WAS INSPECTED AND BURNED INSULATION WAS FOUND.  AN INSULATED TAPE REPAIR WAS CARRIED OUT AND THE BALLAST AT 7DF WAS REPLACED.  THE APU WAS RUN FOR HALF HOUR WITH PACKS ON TO VERIFY NO OIL SMELL. THE A/C WAS THEN DEODORIZED AND 2L72 4F4  FRTA21EA   E15NE                
20080131000382008013100038CE  2008       1          31         CA070827006      120070727G2497MS33491         CONNECTOR       SAFT                    BEECH 100   B100        1152919CE  GARRTTTPE331TPE3316252B 01514WP  HARTZLHCB4T HCB4TN5     GL  BATTERY         MELTED          W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                  111597                                              (CAN) WHILE IN FORMATION FLIGHT, THE LT (BATTERY CHARGE) LIGHT CAME ON AND STAYED ON FOR 15 MINUTES AND THEN EXTINGUISHED. AFTER LANDING AND ENGINES SHUTDOWN, THERE WAS NO MORE POWER COMING FROM THE BATTERIES.  AN INSPECTION WAS CARRIED OUT AND THE LT BATTERY WAS DISCOVERED (TOASTED) INCLUDING THE BATTERY COMPARTMENT. THE CAUSE WAS DETERMINED TO BE A BAD CONTACT ON THE NEGATIVE POLE. (TC NR 20070827006)                                                                                                                                                                                                                                                                                                                          1L72 4T4  T  A14CE   E2WE    6  CP40EA    
20071102000162007110200016SW  2007       11         2          CA070827008      120070823G7697                WIRE                                    FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  CONNECTOR       DAMAGED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AFTER AIRCRAFT LANDED AND WAS TAXING THE SPEED LEVERS WERE PULLED BACK INTO LOW IDLE THE RT ENGINE OIL LIGHT CAME ON AT WHICH POINT THE CREW REALIZED THE RT ENGINE HAD SHUT ITSELF DOWN. CREW CONTACTED MAINTENANCE. MAINTENANCE INVESTIGATED AND REPAIRED WIRING ON CONNECTOR  PLUG AND RAN AIRCRAFT WHICH THEY WERE NOT ABLE TO DUPLICATE ENGINE SHUT DOWN. TEST FLIGHT WAS COMPLETED AND UPON LANDING ENGINE SHUTDOWN AGAIN WHEN SPEED LEVERS WERE BROUGHT BACK INTO LOW IDLE. FUEL SHUT OFF WAS REPLACED AT THIS TIME AND ENGINE SHUTDOWN COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. (TC NR 20070827008)                                                                                                                 2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20071102000172007110200017EA  2007       11         2          CA070827009      120070808G27112776016105      ACTUATOR                                FRCHLD22    22C7A       3370104EA  GARRTTTPE331TPE331*     01514WP  MCAULY4HFR344HFR34C652  NE  LT AILERONS     STIFF           W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) PILOT COMPLAINED ABOUT AILERON STIFF TO MOVE AND WOULD OCCASIONALLY STICK IN THE FULL RT POSITION.  UPON MAINTENANCE TROUBLESHOOTING IT WAS NOTICED THAT THE LT AILERON TRIM ACTUATOR THAT WAS RECENTLY REPLACED, APPROXIMATLY 80 HOURS PREVIOUS, WAS AGAIN STIFF TO OPERATE. IT WOULD ALSO STICK IN THE FULL EXTENDED POSITION. TRIM ACTUATOR WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. TRIM ACTUATOR WAS PASSED INTO QA WHO SENT TRIM ACTUATOR FOR FURTHER INVESTIGATION.                                                                                                                                                                                                                                                          1H71 3I3  T  ATC438  E2WE    6  C3PNE     
20070917000622007091700062NE  2007       9          17         CA070827011      220070731G730025766304        SERVO                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL SYSTEM     MALFUNCTIONED   W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          TXTAXI/GRND HDL  1                      CA       1765                                                           (CAN) DURING START UP, THE AIRCRAFT COULD DEVELOP AND POWER ABOVE 80 TO 85 PERCENT POWER INPUTS. THE SERVO WAS INSTALLED AND REMOVED WITH A TOTAL OF 3.7 HRS IN OPERATION ON THIS AIRCRAFT. SERVO WAS SENT FOR REPAIR AND CONTAMINATION WAS REPORTED TO BE THE CAUSE OF LACK OF POWER. NO ISSUE WERE NOTED IN AIRCRAFT FUEL SYSTEM AND REPLACEMENT OF SERVO FIXED THE PROBLEM. (TC NR 20070827011)                                                                                                                                                                                                                                                                                                                                              1G71 3O3  O  H11NM   1E4                  
20071102000182007110200018NE  2007       11         2          CA070827012      220070729G7414                MAGNETO                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              BL600646201     FAILED          W      K   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      CA            168                                                       (CAN) DURING START UP THE AIRCRAFT THE RT MAGNETO FAILED.  MAGNETO WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20070827012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3O3  O  H11NM   1E4                  
20071102000192007110200019EA  2007       11         2          CA070827013      220070827G8530AEL11800        VALVE SPRING                            CESSNA172   172M        2072418CE  LYC   O360  O360A4M     41514EA  MCAULY1A200 1A200DFA    GL  INTAKE          BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       313                                                            (CAN) ALUMINUM PARTICLES WERE FOUND IN THE OIL FILTER. UPON TEARDOWN OF THE ENGINE, A BROKEN INTAKE VALVE SPRING (OUTER) HAS DAMAGED THE ALUMINUM CYLINDER HEAD. (TC NR 20070827013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A12    E286    5  NP874     
20071102000202007110200020WP  2007       11         2          CA070827014      120070626G2842A5501           TRANSMITTER                             ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              AUX FUEL CELL   ERRATIC         W      K   NONE                                                                                            N  FALSE WARNING                                                                 ININSP/MAINT     1                      CA       813                                                            (CAN) DURING A 50 HR INSPECTION IT WAS NOTED THAT THE AUX FUEL TANK INDICATION SYSTEM HAD ERRATIC MOVEMENT. THE SENDER WAS REPLACED, FUEL SYSTEM CALIBRATION WAS CARRIED AND NO FURTHER ISSUES WERE NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 3O3  O  H11NM   1E4                  
20071102000212007110200021WP  2007       11         2          CA070827015      120070810G2410ALX8521         ALTERNATOR                              ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              ENGINE          MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA            1760                                                      (CAN) DURING LANDING THE ALTERNATOR LIGHT FAILED TO EXTINGUISH. CHARGING SYSTEM WAS CHECKED AND THE ALTERNATOR WAS THE DEFECTIVE PART. THE ALTERNATOR WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20070827015)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3O3  O  H11NM   E295                 
20071102000222007110200022WP  2007       11         2          CA070827016      120070626G6730D2121           SERVO                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FLT CONTROL     LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1042                                                           (CAN) DURING A 50/300 HR INSPECTION, IT WAS NOTED THAT THE AFT SERVO WAS LEAKING.  SERVO WAS REPLACED AND NO FURTHER DEFECTS WERE NOTED. (TC NR 20070827016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3O3  O  H11NM   1E4                  
20071102000232007110200023WP  2007       11         2          CA070827017      120070626G2822D7431           PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL SYS        DEFECTIVE       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1042                                                           (CAN) DURING A MAINTENANCE INSPECTION A FUNCTION CHECK WAS CARRIED OUT ON THE AUX FUEL PUMP AND SOUNDS BEGAN TO COME FROM THE PUMP WHICH IS NOT PART OF IT`S NORMAL OPERATION. PUMP WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20070827017)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3O3  O  H11NM   1E4                  
20071102000242007110200024EA  2007       11         2          CA070828002      120070824G2910601R75239463    LINE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              HYD SYSTEM      CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       27240                                                          (CAN) DURING C-CHECK INSPECTION, CHAFING DAMAGE WAS NOTED ON THE HYDRAULIC PUMP 3B SUCTION LINE P/N 601R75239-463. THIS HYDRAULIC TUBE LINE WAS RUBBING AGAINST THE UPLOCK NR 3 HYDRAULIC TUBE LINE (P/N 601R75239-273) THAT FEEDS INTO THE EXTEND LINE FOR THE RHS MAIN LANDING GEAR RETRACTION ACTUATOR. THE HYDRAULIC LINE HAS BEEN ORDERED AND WILL BE REPLACED BEFORE THE AIRCRAFT LEAVES THE HEAVY CHECK. (TC NR 20070828002)                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA21EA   E15NE                
20071102000252007110200025EA  2007       11         2          CA070828003      120070824G2910601R75239463    LINE                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              HYD SYSTEM      CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       27240                                                          (CAN) DURING A C-CHECK INSPECTION IN THE RT MAIN LANDING GEAR WHEEL WELL, THE HDRAULIC SUCTION TUBE ASSY(P/N 601R75239-463) OF HYDRAULIC PUMP 3B WAS FOUND WITH CHAFING DAMAGE. THIS TUBE WAS RUBBING AGAINST THE HYDRAULIC LINE(P/N 601R75239-273),WHICH IS THE UPLOCK NR 3 LINE FEEDING INTO THE RT MAIN LANDING GEAR RETRACTION ACTUATOR.THE HYDRAULIC LINE HAS BEEN ORDERED AND WILL BE REPLACED BEFORE THE AIRCRAFT LEAVES THE HEAVY MAINTENANCE CHECK. (TC NR 20070828003)                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20071102000262007110200026SW  2007       11         2          CA070828004      120070821G6420204011761001    BEARING                                 BELL  204   204B        1181404SW  LYC   T53   T5313B      41549NE                              TAIL ROTOR HEAD WORN            W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA                                                                      (CAN) PILOT WAS FLYING HELICOPTER AND FELT TWO SLIGHT YAWS TO THE RT APPROXIMATELY 30 TO 40 SECONDS APART. AT FIRST THE PILOT SUSPECTED IT MIGHT HAVE BEEN A GUST OF WIND, BUT THE SECOND YAW ALERTED THE PILOT TO A PROBLEM WITH THE TAIL ROTOR AS IT WAS ACCOMPANIED BY A NOTICEABLE RELUCTANCE OF THE AIRCRAFT TO RECOVER TO THE NOSE POINTED IN THE DIRECTION OF FLIGHT. THE PILOT MADE A SUCCESSFUL UNSCHEDULED LANDING WITH NO DAMAGE TO THE AIRCRAFT.  UPON A MAINTENANCE INSPECTION OF THE T/R CROSSHEAD, IT WAS DETERMINED THAT THE DUPLEX BEARING INSIDE THE CROSSHEAD, BEARING P/N 204-011-761-001, HAD SEIZED. NEW PARTS WERE SUBSEQUENTLY ORDERED AND INSTALLED.  PARTS HAVE BEEN SHIPPED TO MAIN BASE FOR FURTHER INVESTIGATION. (1G71 4U4  U  H1SW    E17EA                
20080131000392008013100039SW  2008       1          31         CA070828005      120070726G5753240014901       BLOCK                                   MOONEYM20   M20C        5870208SW  LYC   O360  O360A1D     41514EA  HARTZLHCC3Y HCC3YR      GL  FLAP HINGE BLOCKCORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) RT WING CENTER FLAP HINGE BLOCK HAD SERIOUS INTER-GRANULAR CORROSION. CORROSION APPEARS TO HAVE STARTED IN THE PORTION OF THE BLOCK THAT IS USED AS A STOP. THE STOP IS NOT EMPLOYED IN THE LOCATION THIS HINGE BLOCK WAS INSTALLED, (AFFECTED HINGE BLOCK, CENTER HINGE LOCATION). (TC NR 20070828005)                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  O  2A3     E286    5  CP25EA    
20071102000272007110200027NE  2007       11         2          CA070828006      220070827G7250                BLADES                                  CNDAIRCL600 CL6002D24   1390016EA  GE    CF34  CF34*            NE                              NR 1 ENGINE     DAMAGED         W      O   OTHER                                                                                           C  F.O.D.                                                                        TXTAXI/GRND HDL  1                      CA       6692                               194299                      (CAN) ON WALK AROUND ON THE RAMP, IT WAS DISCOVERED THAT NR 1 ENGINE HAD BLADE AND STATOR DAMAGE CAUSED BY UNKNOWN FOD. THE A/C WAS TAXIED TO THE HANGER FOR INSPECTION AND BOROSCOPE. THE INSPECTION REVEALED THAT NR 14 BLADE HAD A SMALL DENT, FURTHER INVESTIGATION REVEALED DAMAGE AT THE 1ST STAGE STATOR AT THE 5 O-CLOCK POSITION AND A PUNCTURE TO THE ENGINE LINER. (APPROX 1.4X1.0 HOLE JUST AFT THE NR1 FAN AND JUST FORWARD OF STATOR AT APPROX 4 OCLOCK POSITION LOOKING AFT.) DUE TO THE SKIN CONTAINMENT DAMAGE 1 INCH X .40 , MM DOES NOT ALLOW FOR ANY DAMAGE IN THIS AREA. ENGINE CHANGE HAS BEEN C/O. PRESENT A/C HOURS:6692:52 AND CYCLES:3126.                                                                           2L72 4F4  FRTA21EA   E15NE                
20071102000282007110200028SO  2007       11         2          CA070828007      220070827G8530637781          EXHAUST VALVE                           CESSNA185   185A        2072804CE  CONT  O520  IO520*      17032SO  MCAULY2A34C D2A34C58    GL  NR 2 CYLINDER   BURNED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A 100 HOUR INSPECTION, FOUND THE NR 2 CYLINDER LOW COMPRESSION, RESULT WAS THE EXHAUST VALVE EDGE WAS BURNED. (TC NR 20070828007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  O  3A24    E5CE    5  CP3EA     
20080131000412008013100041WP  2008       1          31         CA070829001      120070819G2435BC3151004       STARTER GEN                             ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          INTERMITTENT    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1038                                                           (CAN) DURING AN ATTEMPTED START THE STARTER FUNCTION WAS INTERMITTENT. STARTER WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20070829001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3O3  O  H11NM   1E4                  
20080131000442008013100044EA  2008       1          31         CA070829002      220070714G7323D2781           GOVERNOR                                ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              ENGINE          INTERMITTENT    W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       1144                                                           (CAN) DURING CRUISE, THE GOVERNOR CONTROL SETTING BECAME HIGHER. MAINTENANCE INVESTIGATED AND NO ISSUES COULD BE FOUND. GOVERNOR WAS REPLACED AND NO ISSUES WERE NOTED. (TC NR 20070829002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3O3  O  H11NM   E295                 
20071102000292007110200029EA  2007       11         2          CA070829004      120070827G716075420022101     INTAKE DUCT                             DHAV  DHC7  DHC7102     2802708EA  PWA   PT6   PT6A50      52043EA  HAMSTD24PF  24PF305     GL  NACELLE         CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       33785                                                          (CAN) LEVEL 3 CORROSION WAS FOUND BETWEEN THE LOWER INTAKE FORWARD LIP AND THE NACELLE STRUCTURE.  (TC NR 20070829004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H74 4T4  T  A20EA   E4EA    6  CP1NE     
20080221000142008022100014SW  2008       2          21         CA070830001      120070827G5320NAS50134A       BOLT                                    AIRTRCAT802 AT802A      0390308SW  PWA   PT6   PT6A67A     52043NE  HARTZLHCB5M HCB5MA3     GL  DISPERSAL GATE  BROKEN          W      D   RETURN TO BLOCK                                                                                 K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA                                                                      (CAN) RETARDANT WAS DISCOVERED LEAKING FROM AROUND THE TANK DOORS. UPON INVESTIGATION, IT WAS NOTED THAT THE BOLT SECURING THE ANGLE INSIDE THE RT DISPERSAL GATE ASSY WAS BROKEN. THE BOLT WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070830001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20071102000302007110200030GL  2007       11         2          CA070830002      320070719G61142339            HUB                                     CESSNA180   180E        2072612CE  CONT  O470  O470R       17026SO  MCAULY2A36C 2A36C29     GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1251 441                                       61822           (CAN) HUB THREADS FOUND CRACKED DURING OVERHAUL PROCESS (TC NR 20070830002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  5A6     E273    5  CP880     
20071102000312007110200031EA  2007       11         2          CA070830003      120070819G2810215640024       FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  RT WING         LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1407                                                           (CAN) FUEL LEAK, RT WING FUEL CELL, NR 2 REPLACED DUE TO LEAKS IN FUEL CELL (TC NR 20070830003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20071102000322007110200032EA  2007       11         2          CA070830004      120070819G28102156400212      FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  RT WING         LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) FUEL LEAK RT WING, FUEL CELL NR 3 REPLACED DUE TO HOLE IN THE CELL. (TC NR 20070830004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20071102000332007110200033EA  2007       11         2          CA070830005      120070819G28102156400212      FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  RT WING         LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1407                                                           (CAN) FUEL LEAK RT WING FUEL CELL NR 7 REPLACED DUE TO HOLES IN THE FUEL CELL. (TC NR 20070830005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20071102000342007110200034EA  2007       11         2          CA070830006      120070823G276072740251001     ROD                                     DHAV  DHC7  DHC7102     2802708EA  PWA   PT6   PT6A50      52043EA  HAMSTD24PF  24PF305     GL  SPOILER IND     BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING TROUBLESHOOTING, A PFCS INDICATOR PROBLEM, IT WAS NOTICED THAT THE ROD FOR THE RT IB ROLL SPOILER TRANSMITTER HAD SHEARED INSIDE OF THE ROD END AT THE SPOILER END. THERE WAS NO INDICATIONS OF THE ROD CONTACTING ANY OTHER SURFACE TO CAUSE IT TO BREAK, THE BREAK MAY HAVE DEVELOPED FROM A CRACK.  THE ROD WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070830006)                                                                                                                                                                                                                                                                                                                                              2H74 4T4  T  A20EA   E4EA    6  CP1NE     
20080221000152008022100015EU  2008       2          21         CA070831001      120070726G6220                RING                                    SNIAS 350   AS350D      8680803EU  TMECA ARRIELARRIEL1D    60048NE                              M/R HEAD        LOOSE           W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) DURING ENGINE SHUTDOWN THE MAIN ROTOR BLADE DROOP STOP RING FELL DOWN THE MAST ASSY. THE HARDWARE HOLDING THE RING BRACKET ALL CAME OFF ALLOWING THE RING TO FALL DOWN THE MAST TO THE SWASHPLATE DRIVE LINK.   SINCE THIS WAS REPORTED, IT HAS BEEN DETERMINED THAT THIS IS NOT THE FIRST TIME THE HARDWARE FOR THE DROOP RING HAS COME LOOSE AFTER INSTALLATION. THE MAINTENANCE REVIEW BOARD HAS NOTIFIED TO SEE IF ANY ADDTION MAINTENANCE REQUIREMENTS ARE NECESSARY. (TC NR 20070831001)                                                                                                                                                                                                                                            1G71 3U3  U  H9EU    E19EU                
20080306001432008030600143CE  2008       3          6          CA070831002      120070830G2752503801535       DRIVE ASSY      BEECH                   BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCE4N HCE4N3      NE  FLAP ACTUATOR   MISMANUFACTURED W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       240                                                            (CAN) ON LANDING, WHEN FLAPS SELECTED FROM 40 PERCENT TO 100 PERCENT, FLAPS STOPPED AT APPROXIMATELY 60 PERCENT, LT OB FLAP WAS SPLIT APPROXIMATELY 10 PERCENT. FLAP WOULD NOT EXTEND OR RETRACT.  LT OB FLAP ACTUATOR FOUND TO HAVE COME APART AT THE 90 DEGREE DRIVE ASSY ATTACH POINT. CLOSER VISUAL EXAMINATION REVEALED THAT IT HAD NOT BEEN PROPERLY ASSEMBLED DURING AC AND/OR PART MFG.  RETAINING KEYWAY HAD DAMAGED THE SLOTTED COLLAR BY NOT BEING FULLY ENGAGED WHEN RETAINING NUT WAS TIGHTENED. THIS SHOULD HAVE BEEN EVIDENT WHEN PART WAS ASSEMBLED AS THE RETAINING NUT WOULD NOT HAVE BEEN IN SAFETY AFTER BEING TIGHTENED. ALSO THE RETAINING KEYWAY WOULD NOT HAVE BEEN RECESSED (APPROX .1250 INCH ON PROPERLY ASSEMBLED PA1L72 4T4  T  A24CE   E4EA    5  CP10NE    
20071102000352007110200035NE  2007       11         2          CA070831005      220070829G852039785A          PIN             PWA                     BEECH 18    D18S        1151004CE  PWA   R985  R985AN14B   52008NE  HAMSTD22D   22D30       NE  MASTER ROD      LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            575                                                       (CAN) CREW ATTEMPTED TO CHECK FOR HYDRAULIC LOCK PRIOR TO START, AND WAS UNABLE TO TURN THE ENGINE MORE THAN 180 DEGREES. THROUGH DIAGNOSIS AND DISCUSSION WITH ENGINE OVERHAUL FACILITY, IT WAS ELECTED TO REMOVE A CYLINDER AND CONFIRM THE INTEGRITY OF THE MASTER ROD ASSEMBLY. ONE OF THE LINK PINS SECURING THE LINK RODS TO THE MASTER ROD WAS FOUND BACKED OUT OF ITS HOLE AND WAS STRIKING THE INSIDE OF THE CRANKCASE, PREVENTING THE FULL ROTATION OF THE CRANKSHAFT. FAILURE OF THIS LINK PIN WOULD HAVE BEEN CATASTROPHIC FOR THIS ENGINE. (TC NR 20070831005)                                                                                                                                                                     1L72 3R3  R  A765    5E1     5  CP736     
20071102000362007110200036EA  2007       11         2          CA070902001      120070813G2100GG670950093     ACM                                     CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C1          NE                              RIGHT           FAILED          W      D   RETURN TO BLOCK                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA       7563                                                           (CAN) RT PACK GOES FULL HOT AND FAILS WITH BURNING ODOR. (TC NR 20070902001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   EOOO63EN             
20071130000872007113000087EA  2007       11         30         CA070902002      120070812G2730BA6709260213    CONTROL ROD                             CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF34*       30015NE                              VERTICAL STAB   UNKNOWN         W      D   RETURN TO BLOCK                                                                                 F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA                                                                      (CAN)  AFTER ENGINE START FOR DEPARTURE FLIGHT AF 7836 ,THE ELEVATOR WAS FOUND JAMMING DURING CHECK LIST . AIRCRAFT RETURNED TO THE GATE. THE EFFORTS ARE NORMAL ON CONTROL COLUMN UNTIL HALF WAY THE BECOMES HARD. EICAS INDICATION FOR THE ELEVATOR SHOWS FULL DEFLECTION WHEN THE CONTROL COLUMN REACHES HALF WAY .  IN REFERENCE TO  N16/07 THE ACFT WAS IN CHECK AND COMPLETED ALL GROUND AND FLT TESTS SATISFACTORY . THE ACFT WAS REPOSITIONED.  THE SB 670BA-27-022 WAS DONE AND INSPECTED BUT A BUSHING REPLACEMENT WAS PENDING TO FULLY COMPLETE THE SB . DURING THIS BUSHING REPLACEMENT AN INVERSION OF THE ACTUATING RODS WAS DONE BETWEEN UPPER AND LOWER POSITION ON THE LEVER.  THE RODS WERE REPOSITIONED IN NORMAL CONFIGURATI2L72 4F4  FRTA21EA                        
20071102000372007110200037EA  2007       11         2          CA070902003      120070824G5610NP1393219       WINDSHIELD                              CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              LEFT            CRACKED         W      B   EMER. DESCENT                                                                                   O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) FL 330 LT, WINDSHIELD CRACKED. AIRCRAFT CONTINUED TO DESTINATION. NO FURTHER REPORTED DETAILS. (TC NR 20070902003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
20071102000382007110200038NM  2007       11         2          CA070903001      120070902G32338400105         ACTUATOR                                DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  MLG             MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) ON DEPARTURE THE LANDING GEAR RETRACTED NORMALLY. APPROXIMATELY 20 SECONDS LATER, THE NOSE GEAR CYCLED UNSAFE AND THEN RETRACTED. APPROXIMATIVE 10 SEC. LATER IT OCCURRED AGAIN BUT THIS TIME DID NOT RETRACT. FLIGHT CREW CYCLED GEAR DOWN MANUALLY IAW QRH BOOK, RECEIVED 3 GREEN LIGHTS (DOORS CLOSED) AND WHEN SELECTED GEAR UP, THE GEAR RETRACTED NORMALLY AND LOCKED. ON LANDING AT DESTINATION, LANDING GEAR EXTENDED NORMALLY AND AIRCRAFT LANDED NORMALLY. MAINTENANCE REPLACED THE NLG DRAG STRUT ACTUATOR.  (TC NR 20070903001)                                                                                                                                                                                               2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071102000392007110200039EA  2007       11         2          CA070904001      220070902G8530LW19001         EXHAUST VALVE                           ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              NR 1 CYLINDER   WORN            W      C   ABORTED TAKEOFF                                                                                 R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      CA       1836                                                           (CAN) AN INTERMITENT SLIGHT POWER LOSS WAS INITIALY MISDIAGNOSED AS A FAULTY GOVERNOR CONTROL BOX. WHEN THE PROBLEM PERSISTED, IT WAS DETERMINED THAT THE EXHAUST VALVE IN THE NR 1 CYLINDER WAS WORN AND HAD A SMALL PIECE MISSING. THE CYLINDER ASSEMBLY IS CURRENTLY BEING REPLACED. (TC NR 20070904001)                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3O3  O  H11NM   E295                 
20071102000402007110200040NM  2007       11         2          CA070904002      120070902G276085770068003     LEVER                                   DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  GROUND SPOILER  BROKEN          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) THE FLIGHT CREW SNAGGED THAT THE GROUND SPOILER LIGHT ILLUMINATED IN FLIGHT. UPON INVESTIGATION MAINTENANCE FOUND THE LT OB GROUND SPOILER LEVER BROKEN AT THE SPOILER ACTUATOR ATTACH POINT. THE LEVER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070904002)                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071026001142007102600114SO  2007       10         26         CA070904003      120070829G5343                TRUNNION                                LKHEED382   382G        526414USO  ALLSN 501D  501D22A     03006GL  HAMSTD54H   54H60117    NE  NLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       39503                                                          (CAN) DURING THE A-CHECK INSPECTION, MAINTENANCE DETECTED A CRACKED RT NOSE LANDING GEAR TRUNNION FITTING. THE AIRCRAFT WAS RE- POSITIONED FOR PART REPLACEMENT. (TC NR 20070904003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H74 4T4  T  A1SO    E282    6  CP906     
20071026001152007102600115GL  2007       10         26         CA070905001      220070811G7250TBA             BEARING                                 SKRSKYS76   S76A        8143006NE  ALLSN 250C  250C30S     03013GL                              NR 5            DISINTEGRATED   W      BA  EMER. DESCENT           UNSCHED LANDING                                                         XEJENGINE FLAMEOUT           VIBRATION/BUFFET          WARNING INDICATION        CRCRUISE         1                      CA       3576 758                                                       (CAN) FLIGHT CREW ENCOUNTERED A NR 2 ENGINE CHIP WARNING LIGHT FOLLOWED BY COMPLETE ENGINE FAILURE WITHIN 1 MIN EMERGENCY LANDING EXECUTED.  NR 2 ENGINE AND OIL COOLER REPLACED, A/C RETURNED TO SERVICE.  SUBSEQUENT INVESTIGATION CARRIED OUT AT AMO REVEALED FAILURE OF THE NR 5 BEARING. THE BEARING FAILURE CAUSED POWER TURBINE ROTOR VIBRATION AND OSCILLATION RESULTING IN SUBSEQUENT DAMAGE AND DECOUPLING OF TURBINE TO COMPRESSOR (N1) COUPLING. THE GAS GENERATOR TURBINE ENTERED OVER-SPEED OF UNKNOWN VALUE. THE GP TURBINE OVER SPEED CAUSED NR 2 TURBINE BLADES TO PROGRESSIVELY SEPARATE FROM THE DISK. THE NR 5 BEARING HAD BEEN OVERHAUL INSPECTED BY THIS AMO APPROXIMATELY 757.9 HRS PRIOR TO FAILURE AND RE-INSTALLED AS 1G72 3U3  U  H1NE    E1GL                 
20071102000412007110200041EU  2007       11         2          CA070905002      120070828G2421                ALTERNATOR                              BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  NR 2            INOPERATIVE     W      AD  UNSCHED LANDING         RETURN TO BLOCK                                                         J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) AFTER DEPARTING AND ENROUTE, THE CREW OBSERVED NR 2 ALTERNATOR HAD TRIPPED OFFLINE AND DID NOT RESET. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE NR 2 ALTERNATOR. THE AIRCRAFT COMPLETED A SATISFACTORY GROUND RUN AND WAS RETURNED TO SERVICE. (TC NR 20070905002)                                                                                                                                                                                                                                                                                                                                                                                                         2L72 3T4  T  A24EU   A196    6  CP899     
20071026001162007102600116EA  2007       10         26         CA070905003      120070904G2750601R9310511     BPSU                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              TE FLAPS        INOPERATIVE     W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA                                                                      (CAN) WING FLAPS FAILED TO FULLY EXTEND FOR LANDING. AFTER SELECTING FLAPS 8 THE CREW RECEIVED A FLAP FAULT CAUTION MESSAGE AND THE FLAPS WOULD NOT MOVE ANY FURTHER. THE CREW LANDED WITH FLAPS AT 8 DEGREES UNEVENTFULLY. FECU SHOWS LT BPSU AT FAULT. BPSU REPLACED, RIGGED AND FUNCTIONAL TEST COMPLETED SUCCESFULLY.  AIRCRAFT RETURNED TO SERVICE. (TC NR 20070905003)                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20071026001172007102600117EU  2007       10         26         CA070905004      120070828G7930810710000       TRANSMITTER                             AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  OIL PRESSURE    INOPERATIVE     W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 DEDESCENT        1                      CA                                                                      (CAN) WHILE INBOUND, THE CREW OBSERVED LOW OIL PRESSURE ON THE NR 1 ENGINE WITH A LOCAL ALERT LIGHT INDICATION THE CREW SHUT THE ENGINE DOWN AND LANDED WITHOUT FURTHER PROBLEM.  MAINTENANCE VERIFIED THAT THERE WAS NO OIL LOSS AND REPLACED THE NR 1 OIL PRESSURE TRANSMITTER. THE AIRCRAFT WAS GROUND RUN SATISFACTORILY AND RETURNED TO SERVICE. FULL P/N IS 8107-100-00-10 (TC NR 20070905004)                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20071026001182007102600118EU  2007       10         26         CA070905005      120070830G324030Z10322        LEVER                                   BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  PARK BRAKE      FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AFTER ARRIVING AT AIRPORT, THE AIRCRAFT ROLLED FORWARD AFTER THE PARK BRAKE WAS APPLIED WITH ENGINES STILL RUNNING AND THEN CONTACTED GROUND EQUIPMENT.  MAINTENANCE DETERMINED THAT THERE WAS A FAULT WITH THE PARK BRAKE SYSTEM AND THE HANDLE ASSEMBLY WAS REPLACED.  THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070905005)                                                                                                                                                                                                                                                                                                                                                                                                        2L72 3T4  T  A24EU   A196    6  CP899     
20071026001192007102600119CE  2007       10         26         CA070905006      120070810G5312051218712       CHANNEL         CESSNA                  CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160DTM    GL  BULKHEAD        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2923       17263199                                            (CAN)  SEB 97-1 ADDRESSES THE POSSIBILITY OF CRACKING OF THE AFT DOORPOST CHANNELS AT THE LOWER END, IN THE SMALL CUTOUT RADIUS BETWEEN THE VERTICAL AND HORIZONTAL FLANGE BENDS. THE CRACK IS VERY DIFFICULT TO SEE. BOTH DOORPOSTS WILL CRACK, AND IT IS THE SUBMITTERS OPINION THAT THIS CRACKING IS CAUSED CHIEFLY BY TAXIING OVER ROUGHER GROUND SO THAT THE FUSELAGE BULKHEAD THAT INCORPORATES THE AFT DOORPOSTS FLEXES MORE THAN IN MOST OTHER OPERATIONS. THIS IS THE THIRD AC WE HAVE FOUND WITH THIS DEFECT WITHIN THE LAST 7 YEARS. (TC NR 20070905006)                                                                                                                                                                             1H71 3O3  ONT3A12    E274    5  NP910     
20071026001202007102600120    2007       10         26         CA070905007      420070831G31706229820009      DCU                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              NR 3            INOPERATIVE     W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB OUT, CREW REPORTED A (L ENG MISCOMP) MESSAGE FOLLOWED BY A HIGH ITT. THE CREW ELECTED TO SHUTDOWN THE ENGINE. AFTER SHUTDOWN THE ITT REMAINED AT 998 DEGREES CELSIUS. AT TIME OF THE INCIDENT, THE AIRCRAFT WAS OPERATING UNDER MEL31-41-01 DUE TO AN INOPERATIVE DCU NR 3.   DURING TROUBLESHOOTING, IT WAS DISCOVERED THAT SEVERAL SNAGS OCCURRED FOLLOWING THE REPLACEMENT OF ONE DCU WITH A P/N 622-9820-009. ALL OTHERS DCU WERE P/N 622-9820-008. ACCORDING TO SL RJ-SL-31-011 BOTH P/N ARE INTERCHANGEABLE AND INTERMIXABLE.   DCU NR 1 AND NR 3 WERE REPLACED AND THE AIRCRAFT WAS RELEASED INTO SERVICE. NO SIMILAR INCIDENT TO DATE HAS BEEN NOTED. (TC NR 20070905007)                                            2L72 4F4  FRTA21EA   E15NE                
20071102000422007110200042EU  2007       11         2          CA070905009      120070904G2121                FAN                                     AIRBUS330   A330300            EU  RROYCERB211 RB211*      54555NE                                              MELTED          W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                                                      (CAN) AFTER T/O, SMOKE AND UNUSUAL SOUND COMING FROM L2 AREA. HAZE REPORTED IN THE CABIN. FLT RETURNED TO AIRPORT. ELECTRICAL ODOR WAS COMING FROM THE L2/R2 AREA WITH HAZE VISIBLE AT 5 DIFFERENT TIMES. IT WOULD APPEAR AND THEN DISAPPEAR.  AREA INSPECTED AND FOUND MID-GALLEY CHILLER DUCT CLAMP ADRIFT, CAUSING UNUSUAL SOUND (S513) AND THE PROJECTOR 7DG (B-CLASS) OVERTEMP LIGHT ON. FOUND COOLING FAN MELTED. CONNECTOR PLUG REMOVED. NEW CHILLER CLAMP INSTALLED. PROJECTOR REPLACED. (TC NR 20070905009)                                                                                                                                                                                                                            2L72 4F4  FRT        A12EU                
20071026001212007102600121NM  2007       10         26         CA070905010      120070903G291015E0803003      PIPE                                    EMB   ERJ170ERJ170100SU 3260403NM  GE    CF34  CF348E5A1   30015NE                              HYD SYSTEM      CUT             W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) DURING ROUTINE A CHECK INSPECTION A CUT APPROXIMATELY 1 CM LONG WAS NOTICED ON THE ENGINE HYDRAULIC PUMP SUPPLY PIPE. THIS CUT WAS APPROXIMATELY .050 DEEP AND WAS THE RESULT OF CHAFFING WHEN THE COWLS WERE CLOSED. (TC NR 20070905010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA56NM   E00063EN             
20071026001222007102600122EA  2007       10         26         CA070905011      120070903G750016673301        DUCT                                    DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  BLEED AIR SYS   CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CABIN PACK REPORTED AS UNCONTROLLABLE AT LOW POWER SETTINGS. MAINTENANCE GROUND RUNS NOTED NON SUPPLY OF BLEED AIR AT FLIGHT IDLE SETTINGS, ALSO NOTED BLEED AIR LEAK FROM CEILING OF ACM COMPARTMENT. ACCESS GAINED TO INTERNAL OF DORSAL FIN AND FOUND BLEED AIR DUCT P/N 16673-301 CONNECTS TO FUSELAGE DUCT, CRACKED AND SPLIT OPEN APPROX HALF OF ITS DIAMETER. DUCT REPLACED, GROUND RUNS COMPLETED AND AIRCRAFT RETURNED TO SERVICE.  PART IS CONSIDERED AS AN EXPENDABLE AND TIMES NOT TRACKED. AIRFRAME TIMES 36419HR/51123CY (TC NR 20070905011)                                                                                                                                                                                2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071026001232007102600123SO  2007       10         26         CA070905012      220070831G8530TSIN712ACA      CYLINDER HEAD                           CESSNA206   U206E       2073350CE  CONT  O520  IO520F      17032SO  HARTZLHCC3Y PHCC3YF1    GL  ENGINE          CRACKED         W      A   UNSCHED LANDING                                                                                 R  PARTIAL RPM/PWR LOSS                                                          CLCLIMB          1                      CA       1343                               282939R                     (CAN) CRACKED FROM SPARK PLUG HOLE TO EXHAUST VALVE (TC NR 20070905012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  A4CE    E5CE    5  CP25EA    
20071026001242007102600124EU  2007       10         26         CA070906001      120070827G5531                SPAR                                    SNIAS 350   AS350BA     8680817EU  TMECA ARRIELARRIEL1B    6OO30NE                              VERTICAL STAB   CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7617                                                           (CAN) CRACKS DISCOVERED ON BOTH SIDES OF STABILIZER THROUGH LOWER DOUBLER AT SPAR. FOUR RIVETS FOUND MISSING FROM FORWARD SPAR ATTACHMENT OF LOWER STABILIZER FRAME. (VISISBLE UPON REMOVAL ONLY) SUSPECT INCORRECT SHIMMING AT THIS TIME. (TC NR 20070906001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3U3  UNCH9EU    E19EU                
20080306001442008030600144CE  2008       3          6          CA070906002      120070905G5520115610010325    TORQUE TUBE                             BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  MCAULY4HFR344HFR34C762  NE  ELEVATOR        LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       209                                                            (CAN) DURING A ROUTINE INSPECTION THE LT ELEVATOR TORQUE TUBE WAS FOUND TO HAVE AN EXCESSIVE AMOUNT OF PLAY AT THE TAPER PINS ON BOTH COLLARS. THE TORQUE TUBE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THIS TORQUE TUBE ONLY HAD 209.2 HOUR SINCE NEW AND IT IS ONLY REQUIRED TO BE INSPECTED EVERY 1000 HOUR. (TC NR 20070906002)                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3T4  T  A14CE   E4EA    6  C3PNE     
20071102000432007110200043NM  2007       11         2          CA070906003      120070902G534085311176009     ATTACH FITTING                          DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  NLG ACTUATOR    CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING SCHEDULED NOSE LANDING GEAR CHANGE, IT WAS DISCOVERED THAT THE NLG UPLOCK ACTUATOR FITTING ASSEMBLY P/N 85311176-009 WAS CRACKED. FITTING REPLACED AND FITTING FASTENERS INSTALLED IAW RD8-53-3805. AFTT: 42865 HRS. TOTAL CYCLES: 50005. (TC NR 20070906003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071102000442007110200044NM  2007       11         2          CA070906004      120070904G3231483023          SEQUENCE VALVE                          BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  LEFT NACELLE    FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       1411                                                           (CAN) ON DEPARTURE FROM AIRPORT, THE LEFT MAIN LANDING GEAR DOORS REMAINED OPEN. VISUALY CONFIRMED BY THE PURSER THAT THE LT GEAR DOORS WERE LEFT OPEN. CREW SELECTED GEAR DOWN AND LEFT GEAR DOORS CLOSED WHILE THE OTHER GEAR DOORS OPENED. CREW PERFORMED ALTERNATE EXTENSION OF THE MAIN LANDING GEAR AND RETURNED TO CYUL. MAINTENANCE INVESTIGATION REVEALED THAT WHEN THE LEFT GEAR DOOR CLOSED THE MAIN LANDING GEAR CAME DOWN DAMAGING THE LEFT MAIN OUTBOARD GEAR DOOR.                                                                                                                                                                                                                                                               2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20071102000452007110200045GL  2007       11         2          CA070906006      220070903G7210                GEARBOX                                 CVAC  340   340CVAC     242270AWP  ALLSN 501D  501D13D     03004GL  HAMSTD54H   54H60       NE  NR 2            UNKNOWN         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CRCRUISE         1                      CA       192                                                            (CAN) NR 2 ENGINE OIL PRESSURE AND QUANTITY INDICATION BOTH SHOWED A DECREASE UPON REACHING CRUISE ALT.  NR 2 ENGINE SHUTDOWN AND RETURNED TO DEPARTURE.  NR 2 REDUCTION GEARBOX BEING REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070906006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4R4  T  6A6     E282    6  CP906     
20080306001452008030600145CE  2008       3          6          CA070906007      120070904G27501005240741      GEARBOX                                 BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  TE FLAPS        WORN            W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) FLAPS WOULD NOT RETRACT AFTER LANDING. GEARBOX FOUND EXCESSIVELY WORN. (TC NR 20070906007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20071026001252007102600125EA  2007       10         26         CA070906008      120070903G5610NP1393225       WINDOW                                  CNDAIRCL600 CL6002C10   1390015EA                                                               COCKPIT         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA       11434                                                          (CAN) CREW REPORTED THAT ON SHORT FINAL, CAPTAIN LT SIDE WINDOW CRACKED.  REPLACED SIDE WINDOW IAW AMM (TC NR 20070906008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F    RTA21EA                        
20071026001262007102600126NE  2007       10         26         CA070906009      220070813G7250                BLADES                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              NR 2 ENGINE     DAMAGED         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         ERJVIBRATION/BUFFET          PARTIAL RPM/PWR LOSS      WARNING INDICATION        CRCRUISE         1                      CA       25122                                                          (CAN) A/C DIVERTED DUE TO NR 2 ENG. VIBRATION AND LOUD NOISE. NR 2 ENGINE WAS SHUTDOWN IN FLIGHT. PILOT DECLARED AN EMERGENCY. CONTRACT MAINTENANCE FOUND THE EXHAUST TURBINE BLADES DAMAGED.   PRELIMINARY INSPECTION THAT THE LAST STAGE TURBINE WITH TOTAL DAMAGE TO ALL BLADES. APPEARS THAT SOMETHING IN BETWEEN THE FIRST STAGE HPT AND LAST STAGE LPT CAME LOOSE AND DEPARTED THROUGH THE TURBINE.  ENG WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. ENG IS IN ENG SHOP AND IS BEING PREPPED FOR SHIPPING. (TC NR 20070906009)                                                                                                                                                                                                         2L72 4F4  FRTA21EA   E15NE                
20071026001272007102600127NM  2007       10         26         CA070907001      120070906G3297471515          WIRE HARNESS                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NLG             DAMAGED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF, GEAR WOULD NOT RETRACT RESULTING IN AN AIR TURNBACK. DURING GROUND INSPECTION FOUND NOSE GEAR HARNESS TO BE INTERMITTENT DURING TESTING. DETAILED INSPECTION OF HARNESS FOUND IN SHARP BEND OF CONDUIT BOTH WOW SENSOR HARNESS AND NOSE WHEEL CENTERING HARNESS CRACKED AND SHIELDING EXPOSED. NLG WOW 2/CENTERING HARNESS HARNESS REPLACED. (TC NR 20070907001)                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20071102000462007110200046SO  2007       11         2          CA070907002      120070906G3411LPMILH55934     HOSE                                    GULSTMGV    GULFSTREAMGV3980116SO  GARRTTTFE731TFE73140    29001NE                              STATIC SYS      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       985                                                            (CAN) DURING PITOT STATIC CHECKS IT WAS FOUND THE SYSTEM WAS SLIGHTLY LEAKING. FURTHER VISUAL INSPECTION FOUND THE STATIC HOSE GOING TO THE ADC WAS WEATHER CRACKED AND LEAKING NEAR THE FITTING. THE HOSE WAS MFG THE FIRST QUARTER OF 2001.(1Q01).(25W752005-063H) PREVIOUSLY G100 C-FHRL SN NR 150 HAD 3 HOSES REPLACED FOR THE SAME REASON AND BY ERROR AN SDR WAS NOT SUBMITTED. ALSO 1 OF THE SAME BASE NR HOSES WAS REPLACED ON C-FHNS G100 SN NR 156. ASTRA SPX (G100) NR 087 C-FRJZ WERE LOOKED AT AND THE HOSES WERE FINE. THIS SEAMS SOMEWHAT PREMATURE AGING FOR THESE HOSES. THE HOSES ARE LOCATED IN THE NOSE COMPARTMENT AREA AND THERE ARE 2 IAW ADC HAVING THE SAME BASE NR AND DIFFERENT DASH NRS. (TC NR 20070907002)        2L72 4F4  FRTA12EA   E1NM                 
20080306001462008030600146SW  2008       3          6          CA070907003      120070906G574031692           ATTACH FITTING                          BBAVIA7     7ECA        21101NNSW  LYC   O235  O235K2C     41505EA  SNSNCH72C   72CK        EA  WING            FAULTY          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1000                                                           (CAN) AD 96-18-02 AND THE AIRWORTHINESS LIMITATIONS FOR THIS AC REQUIRE THAT THE WING SPAR/STRUT ATTACH FITTINGS BE REMOVED AND NDI WITH FLUORESCENT DYE PENETRANT EVERY 1000 HOURS.  NDI DISCLOSED A FLAW WITHIN THE METAL, APPARENTLY EXISTING WITHIN THE RAW STOCK WHEN MFG, AND THE AMOUNT OF DYE THAT BLED OUT INDICATES THAT THE FLAW EXTENDS DEEPLY INTO THE METAL. IT IS NEAR THE TOP BOLT HOLE WHERE THE STRESSES ARE MINIMAL, AND NO CRACKING WAS NOTED BETWEEN THE FLAW AND THE HOLE. (TC NR 20070907003)                                                                                                                                                                                                                            1H71 3O3  O  A759    E223    5  NP9045    
20080129000262008012900026EA  2008       1          29         CA070907004      220070906G73103040637         FUEL LINE                               BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  ENGINE BAY      CHAFED          W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                                          PCE32232                    (CAN) FUEL LINE ASSY WAS FOUND TO HAVE BEEN CHAFED BY THE STARTER GENERATOR VENT HOSE, CAUSING A VERY SMALL PIN HOLE IN THE RIGID STAINLESS FUEL LINE, RESULTING IN A FUEL LEAK. (TC NR 20070907004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20071102000472007110200047NM  2007       11         2          CA070907005      120070907G575185740337105106  HINGE FITTING                           DHAV  DHC8  DHC8301     1386003NM                                                               AILERON         MIGRATED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       22128                                                          (CAN) THE BEARINGS ON THE AILERON HINGE FITTINGS LOCATED AT YW515.19 WERE FOUND TO BE MIGRATED. IT WAS FOUND THAT THE HINGE FITTING P/N`S 85740337-105/-106 WERE MANUFACTURED INCORRECTLY SINCE THE DISTANCE BETWEEN THE TWO LUG FACES (0.850 INCH NOMINAL) MEASURES 0.970 INCH. (TC NR 20070907005)                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T    RTA13NM                        
20080131000452008013100045SW  2008       1          31         CA070909001      120070908G2421LW10382         BRACKET                                 HUGHES269   269C1       8059504SW  LYC   O360  HIO360*     41514EA                              ALTERNATOR      BROKEN          W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                                                      (CAN) ALTERNATOR BRACKET FOUND WITH BROKEN ATTACHMENT LUG. ALTERNATOR BELT TENSION LOSS AND SUBSEQUENT SYSTEM UNSERVICEABILITY. CAUSE OF FAILURE UNDER INVESTIGATION. (TC NR 20070909001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3O3  OO 4H12    1E10                 
20071026001282007102600128EA  2007       10         26         CA070909002      220070904G7314RG908054AM      PUMP                                    PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          FAULTY          W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          TXTAXI/GRND HDL  1                      CA            7                                                         (CAN) DURING START UP THE ENGINE WOULD NOT MAINTAIN FUEL PRESSURE AT 700 RPM. ENGINE WOULD NOT SUSTAIN POWER AT 2000 RPM AND PRESURE DROPS AND ENGINE QUITS. ENGINE DRIVEN FUEL PUMP WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. ENGINE WAS PREVIOUS OVERHAULED ALONG WITH FUEL PUMP. (TC NR 20070909002)                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20071026001292007102600129GL  2007       10         26         CA070910001      320070907G61101A101           PROPELLER                               CESSNA150   150H        2071818CE  CONT  O200  O200A       17020SO  MCAULY1A100 1A100*      GL                  CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1343                                                      (CAN) WHILE PERFORMING A 5 YEAR CORROSION INSPECTION ON SUBJECT PROPELLER IAW CAR 625 APPENDIX C, PARA.5, CORROSION WAS NOTED IN THE MOUNTING HOLE BORE. IN CONSULTATION WITH THE PROPELLER OVERHAUL AMO, IT WAS DECIDED TO SEND IT TO THEM FOR FURTHER EVALUATION. CURRENTLY AWAITING THEIR REPORT AS TO IT`S STATUS. (TC NR 20070910001)                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  O  3A19    E252    5  NP918     
20080225000802008022500080NE  2008       2          25         CA070910002      220070905G7314D7431           PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              AUX FUEL SYS    UNSERVICEABLE   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AUX FUEL PUMP FOUND UNSERVICEABLE DURING DI REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20070910002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3O3  O  H11NM   1E4                  
20071102000482007110200048EU  2007       11         2          CA070910003      120070906G2910T2C5000605500   LINE                                    BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU                              HYDRAULIC SYS   RUPTURED        W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  DEDESCENT        1                      CA                                                                      (CAN) 10 MINUTES PRIOR TO LANDING, THE PORT AND STARBOARD HYDRAULIC PUMP LIGHTS ILLUMINATED WITH MAIN PRESSURE DEPLETING AND STOPPING AT ACCUMULATOR PRESSURE. THE CREW CARRIED OUT THE APPROPRIATE PROCEDURES AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A HYDRAULIC FLEX LINE, IN THE RT WHEEL BAY, WHICH GOES TO THE HIGH-PRESSURE HYDRAULIC FILTER RUPTURED. THE FLEX LINE, ALONG WITH BOTH HYDRAULIC PUMPS, WAS REPLACED AND THE SYSTEM FUNCTION CHECKED SERVICEABLE. (TC NR 20070910003)                                                                                                                                                                                                                                      2L72 3T4  T  A24EU   A196                 
20071026001302007102600130CE  2007       10         26         CA070910004      120070909G2510110195203       BUCKLE                                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              SEATBELT        DISCONNECTED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE COMPLYING WITH COMPANY CAMPAIGN NOTICE 010-25-10-011 CREW SEAT BELT BUCKLE INSPECTION, (REFER TO FAA SAIB NM-06-29)INTERFERENCE BETWEEN THE COCKPIT SEATBELT BUCKLES AND THE CONTROL COLUMN WOULD UNLATCH THE SEATBELT BUCKLE WHEN THE YOKE WAS MOVED THROUGH FULL TRAVEL LT AND RT.   THERE ARE NO CURRENTLY APPROVED SEAT BELT REPLACEMENTS AVAILABLE TO ELIMINATE THIS HAZARDOUS SITUATION. (TC NR 20070910004)                                                                                                                                                                                                                                                                                                                  1L72 4F4  F  A22CE   E1NE                 
20080225000812008022500081CE  2008       2          25         CA070910005      120070822G57206147514435      WASHER                                  BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  WING            DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE DOING CF-1981-25R6 LOWER FWD WING ATTACH FITTINGS YOU MUST REPLACE THE LOWER FWD. WING BOLT WASHER ASSY UPON RE-INSTALL OF BOLTS. NEW WASHER KITS WERE INSTALLED, BUT WERE UNABLE TO TORQUE IAW THE MFG SIRM., THE TORQUE WAS TOO GREAT TO GET THE REQUIRED READING OF THE SPRING SCALE, THE THREADS ON THE NUTS WERE DAMAGED AND SO WERE THE THREADS ON THE BOLTS. THE BOLTS AND NUTS WERE REPLACED WITH NEW, AND THE WASHER KITS WERE ALSO REPLACED, AND NORMAL TORQUE WAS ATTAINED. (TC NR 20070910005)                                                                                                                                                                                                                          1L72 3T4  T  A14CE   E4EA    5  CSTC      
20071102000492007110200049SO  2007       11         2          CA070910006      220070901G8530641917          CYLINDER                                CESSNA150   150L        2071826CE  CONT  O200  O200A       17020SO  MCAULY1A101 1A101HCM    GL  EXHAUST VALVE   STUCK           W      A   UNSCHED LANDING                                                                                 R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      CA                                          21468372A                   (CAN) ON CLIMB OUT AFTER TAKEOFF, THE PILOT NOTICED MILD TO MODERATE ENGINE VIBRATION WITH A PARTIAL LOSS OF POWER. A RETURN TO THE AIRSTRIP WAS CARRIED OUT WITH A SUCCESSFUL LANDING. ON INVESTIGATION BY AN AME, THE PROBLEM WAS NOTICED AS AN EXHAUST VALVE STUCK OPEN ON THE NR 3 CYLINDER. THE CYLINDER WAS REMOVED AND WAS SENT TO AN ENGINE OVERHAUL SHOP FOR REPAIRS. THE CYLINDER IS STILL BEING REPAIRED AND WILL BE REINSTALLED UPON RETURN FROM THE SHOP. (TC NR 20070910006)                                                                                                                                                                                                                                                      1H71 3O3  O  3A19    E252    5  NP918     
20071026001312007102600131GL  2007       10         26         CA070910007      220070910G732123070606        FUEL CONTROL                            BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              ENGINE          UNSERVICEABLE   W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA            147                                                       (CAN) OVERSPEED OCCURED DURING FLIGHT, FUEL CONTROL REPLACED WITH SERVICEABLE UNIT. WHEN REMOVED, IT WAS NOTED THAT THE FCU INPUT SHAFT BEARING WAS DAMAGED. FCU SENT OUT FOR INSP/REPAIR. (TC NR 20070910007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3U3  U  H2SW    E4CE                 
20071102000502007110200050WP  2007       11         2          CA070910008      220070827G73228978012         FCU                                     FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  RT ENGINE       MALFUNCTIONED   W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA            2302                                                      (CAN) AFTER AIRCRAFT LANDED AND SPEED LEVERS WERE PULLED BACK INTO LOW IDLE THE RT ENGINE LIGHT CAME ON AT WHICH POINT THE CREW REALIZED THAT THE ENGINE HAD SHUTDOWN. THE FCU AND FUEL PUMP WERE REPLACED. AIRCRAFT CHECKED OUT SERVICIBLE AND NO FURTHER REPORTED INCIDENCES. (TC NR 20070910008)                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20071102000512007110200051WP  2007       11         2          CA070910009      120070907G3240147515          BRAKE                                   GRUMANTS2   TS2ACALFORST3951102WP  WRIGHTR1820 982C9HE2    67020EA  HAMSTD43D   43D51       NE  MLG             FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA            177                                                       (CAN) ON LANDING RT BRAKE FAILED. RT BRAKE FOUND TO BE LEAKING A LARGE QUANTITY OF HYDRAULIC FLUID. BRAKE WAS REPLACED. (TC NR 20070910009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4R4  R  A25WE   E259    6  CP8879    
20071102000522007110200052EU  2007       11         2          CA070911001      120070906G24358260123         STARTER GEN                             AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  NR 2            MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) AFTER DEPARTING, THE CREW OBSERVED A NR 2 GENERATOR FAULT AND THE CREW ELECTED TO RETURN TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE NR 2 GENERATOR CONTROL UNIT (GCU) AN THE AIRCRAFT WAS CHECKED SERVICEABLE AN RETURNED TO SERVICE. THE PROBLEM REOCCURRED APPROXIMATELY ONE HOUR AFTER THE AIRCRAFT HAD MADE A SECOND DEPARTURE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE NR 2 STARTER GENERATOR AND THE AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER PROBLEM REPORTED.  (TC NR 20070911001)                                                                                                                                                                                 2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080225000822008022500082EU  2008       2          25         CA070911002      120070906G3240                BRAKE ASSY                              AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  MLG             LOCKED          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) DURING TOUCH DOWN THE RT MLG IB TIRE WENT FLAT. THE FAILURE WAS ATTRIBUTED TO BRAKE LOCKUP. THE AC WAS TOWED FROM THE RUNWAY. MAINT CHECKED THE NR 3 AND NR 4 POSITION BRAKE AND ANTISKID SYSTEMS WITH NO FAULT FOUND. THE NR 3 AND NR 4 WHEEL TIRE ASSEMBLIES WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070911002)                                                                                                                                                                                                                                                                                                                                                                                                2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20071026001322007102600132NM  2007       10         26         CA070911003      120070907G731232015           VALVE                                   BOEING737   737217      1384464NM  PWA   JT8   JT8D17      52049NE                              FUEL HEAT       MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) APPROXIMATELY 25 MINUTES AFTER DEPARTING, THE CREW OBSERVED THE NR 1 ENGINE OIL TEMPERATURE CLIMBING THROUGH THE YELLOW BAND. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE NR 1 FUEL HEAT VALVE AND CONDUCTED THE APPROPRIATE OVERWEIGHT LANDING INSPECTION BEFORE THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070911003)                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  F  A16WE   E2EA                 
20071102000532007110200053NE  2007       11         2          CA070911004      220070827G7250FW35594         TURBINE BLADES                          BOEING717   717200      1383700NM  RROYCEBR700 BR700715A130     NE                              HP1             FAILED          W      C   ABORTED TAKEOFF                                                                                 MJ OVER TEMP                 WARNING INDICATION                                  TOTAKEOFF        1                      CA       2693                               13318                       (CAN) DURING ENGINE THROTTLE FOR TAKEOFF, ISSUED (TGT-OVRTP, MAX=1146 LIMIT=900) AND ENGINE SURGE. THE PILOT THROTTLED DOWN, THE AIRCRAFT WAS RETURNED TO THE GATE AND PASSENGERS WERE UNLOADED.  METAL (TURBINE BLADE PARTICLES) WERE FOUND IN THE TAILPIPE UPON VISUAL INSPECTION. ENGINE JUST BEING INDUCTED AT MFG FOR INVESTIGATION. FURTHER DETAILS WILL BE SUBMITTED AFTER ENGINE DISSASSEMBLY. (TC NR 20070911004)                                                                                                                                                                                                                                                                                                                      2L72 4F4  FTRA6WE    E00061EN             
20071102000542007110200054NM  2007       11         2          CA070911005      120070906G242131708500        ADAPTER         LUCAS                   DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  GENERATOR       PULLED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA       114211454  874                                                 (CAN) WHILE ENROUTE FLIGHT CREW RECEIVED A NR 1 ENGINE OIL PRESSURE LOW INDICATION AND ALSO HAD A VISUAL INDICATION OF DECLINING OIL PRESSURE. CREW SHUTDOWN NR 1 ENGINE AND DIVERTED TO AN ALTERNATE AIRPORT. CREW DID NOT DECLARE AN EMERGENCY AND LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOOTING FOUND THAT THE AC GENERATOR ATTACH STUDS HAD PULLED THROUGH THE ADAPTOR MOUNTING PLATE CAUSING THE AC GENERATOR TO BECOME LOOSE AND LEAK OIL. MOUNTING PLATE AND AC GENERATOR WERE REPLACED. ENGINE WAS SERVICED WITH OIL, FUNCTION AND LEAK CHECKS COMPLETED WITH NO FURTHER FAULTS FOUND. (TC NR 20070911005)                                                                                                        2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071026001332007102600133EU  2007       10         26         CA070911007      120070907G324010903000        PAD             PARKER                  PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  BRAKE ASSY      WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            552   1172                                                (CAN) PILOT REPORTED SPONGY FEELING WHEN RT BRAKE PEDAL ACTUATED. UPON FURTHER INSPECTION FOUND BRAKE WEAR PADS PREMATURELY WORN IN A CUPPING SHAPE BEYOND LIMITS. BRAKE ASSEMBLY REPLACED AND RETURNED TO STORES. (TC NR 20070911007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080306001472008030600147CE  2008       3          6          CA070911008      120070907G323399810057652     ACTUATOR                                BEECH 99    99          1154002CE  PWA   PT6   PT6A20      52043EA  HARTZLHCB3T HCB3TN3     GL  MLG             STRIPPED        W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF GEAR SELECTED UP RT GEAR DID NOT COME UP.   GEAR SELECTED DOWN,  (3) GREEN INDICATIONS OBSERVED AC LANDED.  AC BROUGHT INTO HANGER AND PUT ON JACKS RT MLG ACTUATOR REMOVED.  FOUND THAT NUT, ACTUATOR P/N 115-810029-24 HAD NO TREADS IN IT. PART SENT OUT FOR TEARDOWN REPORT (TC NR 20070911008)                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3T3  T  A14CE   E4EA    6  CP15EA    
20071102000552007110200055CE  2007       11         2          CA070911009      120070830G5730652230553       SKIN                                    CESSNA500   550         2076604CE  PWA   530   PW530A           NE                              WING            CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3401                                                           (CAN) DE-ICE BOOT REPLACEMENT AT MFG. AFTER REMOVAL OF DE-ICE BOOT NOTED AREA OF FUEL STAINING, CORROSION NOTED. DISCONTINUED BOOT REPLACEMENT, OBTAINED FERRY PERMIT AND RELOCATED AIRCRAFT.  FURTHER INVESTIGATION SHOWS: SEVERAL LOCATIONS OF CORROSION DAMAGE WERE NOTED ON THE IB, LT WING, LEADING EDGE SKIN (P/N 6522305-53) BETWEEN WS 86.20 AND WS 91.00. THE DAMAGE WAS SUCH THAT THE SKIN PANEL WAS REQUIRED TO BE REPLACED. CORROSION DAMAGE WAS ALSO NOTED ON THE OB, LT WING, LEADING EDGE SKIN (P/N 5522300-45) BETWEEN WS 91.00 AND WS 91.50. SEE PAGE 2.1 ATTACHED FOR DAMAGE LOCATION. MFG HAS INDICATED OTHER SAME TYPE AIRCRAFT HAVE NEEDED SKIN REPAIRS DUE TO THE SAME TYPE CORROSION PROBLEM. THIS SEVERE CORROSION OCCUR1L72 4F4  F  A22CE   E00053EN             
20071102000562007110200056WP  2007       11         2          CA070911010      220070829G7321307080022       FUEL CONTROL                            BRAERODH125 HS125700A   4230170EU  GARRTTTFE731TFE7313R1H  29001WP                              ENGINE          FAULTY          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       663                                P84414                      (CAN) - MANUAL MODE SELECTION PROVIDES IDLE ONLY FUEL. NO SPOOL UP WITH POWER LEVER INCREASE.   ENGINE FUNCTIONS NORMALLY IN AUTO - COMPUTER (ON) MODE. (TC NR 20070911010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  F  A3EU    E6WE                 
20071102000572007110200057NE  2007       11         2          CA070911011      220070910G7414                UNKNOWN                                 CURTISC46   C46DAIRLIFT        SO  PWA   R2800 R280051M1   52026NE  HAMSTD23E   23E50       NE  ENGINE          UNKNOWN         W      E   ENGINE SHUTDOWN                                                                                 E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA                                                                      (CAN) PRECAUTIONARY SHUTDOWN DUE TO ROUGH RUNNING, ENGINE RUNUP ON GROUND BY MAINTENANCE AND SUSPECT BAD MAGNETO. THE ENGINE WILL BE INSPECTED AND TIMED ACCORDINGLY. (TC NR 20070911011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4R4  R  3A2     5E8     6  CP603     
20071102000582007110200058NE  2007       11         2          CA070911012      220070905G7260547344P3        STUD                                    BOEING727   727260      138408KNM  PWA   JT8   JT8D17      52049NE                              GEARBOX         DISLODGED       W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         K  FLUID LOSS                                                                    CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE, THE NR 2 OIL QUANTITY SLOWLY DECREASED TO ZERO. WHEN THE OIL QUANTITY WENT BELOW THE GREEN ARC THE FLIGHT CREW SHUTDOWN THE ENGINE USING THE APPROPRIATE CHECKLIST AND AN EMERGENCY WAS DECLARED INTO AIRFIELD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE INVESTIGATED AND A STUD WAS FOUND ADRIFT FROM THE ACCESSORY DRIVE GEARBOX, FORWARD LOWER SPLIT LINE. THE THREADS WERE INSPECTED AND FOUND TO BE SERVICEABLE. THE STUD WAS REINSTALLED AND TORQUED. THE ENGINE OIL FILTER WAS REMOVED AND INSPECTED. NO CONTAMINATION WAS FOUND AND THE OIL FILTER WAS REPLACED WITH A NEW UNIT. ENGINE GROUND RUN AND LEAK CHECK WAS CARRIED OUT AND WAS CHECKED SERVICEABLE WITH NO LEAKS.  THE AIRCRAFT DEPART2L73 4F4  FRTA3WE    E2EA                 
20071102000592007110200059EA  2007       11         2          CA070911013      120070908G2750                BPSU                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                                              FAULTED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                                                      (CAN) THE CREW RECEIVED A FLAP FAIL MESSAGE AFTER SELECTING THE FLAP TO 0 DEGREE AFTER LANDING. THE FECU TO LT BPSU WIRING WAS INSPECTED AND NO FAULT WAS FOUND. FECU WAS REPLACED, FUNCTIONAL TEST COMPLETED AND THE AIRCRAFT RELEASED INTO SERVICE,   FOUR FLIGHTS LATER THE CREW EXPERIENCED A FLAP FAIL MESSAGE WHEN FLAP WERE SELECTED FROM 0 TO 8 DEGREES IN PREPARATION FOR TAKE OFF. THE FECU FAULT CODE WAS AGAIN INDICATING PROBLEM WITH WIRING BETWEEN THE LT BPSU AND FECU. WIRING WAS INSPECTED AND NO FAULT WAS NOTICED. FURTHER INVESTIGATION REVEALED THAT THE RT BPSU WAS AT FAULT. R/H BPSU WAS REPLACED, FUNCTIONAL TEST COMPLETED AND THE AIRCRAFT RELEASED INTO SERVICE. (TC NR 20070911013)                               2L72 4F4  FRTA21EA   E15NE                
20080306001492008030600149GL  2008       3          6          CA070911014      120070816G27202027220100      RUDDER PEDAL                            DIAMONDA20  DA20A1      2990000GL  ROTAX 912   ROTAX912F3       EU  HOFMANHOV352HOV352F     NE                  WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4050                                                           (CAN) THE LT PILOT SIDE RUDDER CABLE PASSES THROUGH A TUBE ON THE PILOT RUDDER PEDAL. THIS TUBE WEARS AWAY DUE TO CHAFING AND IS UNDETECTABLE UNTIL THE CABLE HAS TOTALLY WORN THROUGH RESULTING IN BOTH PEDAL ASSY AND CABLE DAMAGE. (TC NR 20070911014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  ONTTA4CH   E00051EN5  CTP5BO    
20071102000602007110200060EA  2007       11         2          CA070911015      220070907G853072877           TAPPET                                  CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA                              ENGINE          BROKEN          W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          ININSP/MAINT     1                      CA                                                                      (CAN) THE ENGINE HAS BEEN DOWN ON POWER FOR QUITE SOMETIME. UPON OVERHAUL TEARDOWN, IT WAS DISCOVERED THAT THE NR 1 AND NR 2 EXHAUST AND INTAKE TAPPET BODIES HAD BROKE. THE PIECES WERE TOO BIG TO BE DISCOVERED IN THE OIL SCREEN. (TC NR 20070911015)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A12    E274                 
20071102000612007110200061SO  2007       11         2          CA070912001      220070827G8520536421          GEAR                                                                       CONT  O520  IO520F      17032SO                              CRANKSHAFT      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE TROUBLESHOOTING A STARTER PROBLEM. THE CRANKSHAFT GEAR WAS FOUND TO BE MISSING 2 TEETH. ENGINE WAS DISASSEMBLED, INSPECTED AND REPAIRED AS NECESSARY. PART OF THE MAGNETO IMPULSE CAM BROKE OFF, FELL DOWN INTO THE CRANK AND CAMSHAFT GEARS. THE GEARS JAMMED AND BROKE THE TEETH OFF. (TC NR 20070912001)                                                                                                                                                                                                                                                                                                                                                                                                                                3  O          E5CE                 
20071102000622007110200062EA  2007       11         2          CA070912002      220070824G8530                EXHAUST VALVE                                                              LYC   O360  AEIO360A1E  41514EA  HARTZLHCC2Y HCC2YK4     GL  ENGINE          BROKEN          W      A   UNSCHED LANDING                                                                                 ER VIBRATION/BUFFET          PARTIAL RPM/PWR LOSS                                CRCRUISE         1                      CA       1170                                                           (CAN) EXHAUST VALVE BROKE AT HEAD. BROKEN PART EJECTED THROUGH EXHAUST PORT.  CYLINDER/VALVES/PISTON REPLACED.  NEW VALVES ON ORDER FOR REMAINING CYLINDER.  ENGINE HAS SPENT MOST OF ITS TOTAL TIME AT HIGH POWER AEROBATIC USE. (NEGLECTABLE WEAR ON PISTON CYLINDER). (TC NR 20070912002)                                                                                                                                                                                                                                                                                                                                                                                                                                                           3  O          1E10    5  CP920     
20071102000632007110200063SO  2007       11         2          CA070912003      220070830G8520536421          GEAR                                    CESSNA206   U206G       2073356CE  CONT  O520  IO520F      17032SO                              CRANKSHAFT      DAMAGED         W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA            940                           826612R                     (CAN) PILOT/OPERATOR CONVEYED A STARTING ABNORMALITY. TROUBLESHOOTING FOUND THAT TWO TEETH WERE MISSING FROM CRANKSHAFT GEAR. ENGINE REMOVED AND SENT FOR FURTHER EVALUATION AT ATC  AMO NR 59-96. SEE SDR NR 20070912001 FROM AMO 59-96 FOR FURTHRER FOLLOW UP. (TC NR 20070912003)                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  O  A4CE    E5CE                 
20071102000642007110200064CE  2007       11         2          CA070912005      120070823G57111217029         SPAR                                    CESSNA210   210J        2073439CE  CONT  O520  IO520J      17032SO  MCAULY3A32C D3A32C*     GL  WING            CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3225                                                           (CAN) DURING A MAINTENANCE FUNCTION SEVERE CORROSION WAS DISCOVERED ON THE BOTTOM OF THE WING SPAR ENTRE SECTION. THIS SECTION OF THE SPAR HAS HIGH DENSITY FOAM GLUED TO THE SPAR WHICH PREVENTS ADEQUATE INSPECTION. THE CORROSION WAS SUCH THAT THE WING SPAR CENTRE SECTION REQUIRED REPLACEMENT. (TC NR 20070912005)                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  O  3A21    E5CE    5  CP21EA    
20080306001502008030600150CE  2008       3          6          CA070912007      120070908G27501013800002      FLEX DRIVE                              BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  TE FLAP         SEIZED          W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                                                      (CAN) ABOUT 2 MINUTES INTO A FLIGHT THE CREW DETECTED AN ELECTRICAL ODOR. THE PILOTS TURNED OFF THE VENT BLOWER SYS WHICH HELPED FOR A BIT BUT NOT LONG. NO SMOKE WAS NOTICED, JUST THE ODOR. ALL OTHER NON-ESSENTIAL ELECTRICS WERE TURNED OFF.  THE SMELL STAYED SO AN EMERGENCY WAS DECLARED AND THE AC PREPARED TO LAND AT ITS INTENDED AIRPORT. WHEN THE AC WAS PREPARING TO LAND 17 DEGREES OF FLAP WAS SELECTED, THE AC INDICATOR SHOWED THAT THEY ONLY MADE IT TO 12 DEGREES. THE FLAPS WERE TRIED AGAIN AND DEEMED FAILED. THE GEAR WAS SELECTED DOWN AND THE LANDING WAS COMPLETED WITHOUT FURTHER INCIDENT. AFTER MAINT ARRIVED AND ASSESSED THE SITUATION IT WAS FOUND THAT THE LT INNER FLAP DRIVE CABLE HAD SLOWLY BOUND UP AND SE2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20071102000652007110200065GL  2007       11         2          CA070912008      220070910G73146899253         PUMP                                    AEROSPAS355 AS355F2     8680812EU  ALLSN 250C  250C20F     03013GL                              FUEL SYSTEM     DEFECTIVE       W      B   EMER. DESCENT                                                                                   RYJPARTIAL RPM/PWR LOSS      ENGINE STOPPAGE           WARNING INDICATION        CRCRUISE         1                      CA            3338                                                      (CAN) ENGINE AUTO-REIGNITION ACTIVATED IN FLIGHT. REPORTS OF SOFT (BANG) PRECEEDING DECEL. INVESTIGATION REVEALED AIR IN FUEL SYSTEM, SUBSEQUENT TROUBLESHOOTING FOUND ENGINE DRIVEN FUEL PUMP DEFECTIVE. (TC NR 20070912008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G72 3U3  U  H11EU   E4CE                 
20071102000662007110200066    2007       11         2          CA070912009      420070910G34607013270936      RMU                                     DORNERDO32  DO328100    2996000NM                                                                               FAILED          W      O   OTHER                                                                                           JB WARNING INDICATION        SMOKE/FUMES/ODORS/SPARKS                            CRCRUISE         1                      CA       7960                                                           (CAN) ENROUTE RMU NR1 FAIL CAS MESSAGE, QRH PROCEDURES COMPLETED, THE ODOR OF ELECTRICAL FIRE/SMOKE WAS DETECTED IN THE COCKPIT.  DECLARED AN EMERGENCY AND INITIATED ODOR OF SMOKE IN COCKPIT DRILL.  PROCEEDED WITHOUT FURTHER INCIDENT.PAX DEPLANED AT GATE ,NORMALLY,FIRE DEPARTMENT INVESTIGATED FOR FURTHER DAMAGE.  MAINTENANCE DETERMINED THAT THE RMU HAD SHORTED INTERNALLY AND CAUSED A SMOKE ODOR IN THE COCKPIT. THE NR 1 RMU WAS DISCONNECTED AND THE CIRCUIT BREAKER PULLED AND COLLERED.THE A/C WAS FERRY FLOWN, THE FOLLOWING DAY, A REPLACEMENT RMU IS IN TRANSIT. (TC NR 20070912009)                                                                                                                                        2H72 4T    RTA45NM                        
20071102000672007110200067CE  2007       11         2          CA070912010      120070910G8011MMU4001         STARTER                                 CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA                                              STICKING        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            179                                                       (CAN) STARTER FOUND STICKING. (TC NR 20070912010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  ONT3A19    E223                 
20071102000682007110200068EA  2007       11         2          CA070913001      120070910G2421820465          ADG                                     CNDAIRCL604 CL604       1900301EA  GE    CF34  CF343B1          NE                              LEFT            UNWANTED DEPLOY W      O   OTHER                                                                                           O  OTHER                                                                         TOTAKEOFF        1                      CA            1                                                         (CAN) DURING TAKEOFF, AS SOON AS A/C LEFT GROUND ADG DEPLOYED. CREW DECIDED TO CONTINUE FLIGHT USING ADG DEPLOY FLIGHT PROCEDURES. A/C LANDED WITHOUT INCIDENT.  ADG AUTODEPLOY UNIT WAS FOUND TO HAVE BEEN REPLACED A FEW HOURS BACK DUE TO FAILURE OF UNIT`S SELF TEST. THE INSTALLED SERVICEABLE REPAIRED UNIT WAS FOUND TO BE AT FAULT. UNIT WILL BE REPLACED AND A/C RETURNED TO SERVICE. (TC NR 20070913001)                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA21EA   E15NE                
20080306001512008030600151CE  2008       3          6          CA070913002      120070913G2421ES4118          BRUSHES                                 CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160DTM    GL  ALTERNATOR      CONTAMINATED    W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA            220   G104183                                             (CAN) EXCESSIVE GREASE WAS APPLIED TO THE REAR ROTOR BEARING DURING OVERHAUL. SOME OF IT ESCAPED AND WAS FLUNG ONTO THE BRUSHES AND SLIP RINGS, FOULING THEM AND CAUSING A BUILDUP OF GREASE AND CARBON ON THE SLIP RINGS AND BRUSH FACES. THE ELECTRICAL RESISTANCE INCREASED AND THE FIELD CURRENT WAS REDUCED TO THE POINT THAT THE ALTERNATOR WAS UNABLE TO KEEP UP WITH THE AIRCRAFT`S REQUIREMENTS. (TC NR 20070913002)                                                                                                                                                                                                                                                                                                                   1H71 3O3  ONT3A12    E274    5  NP910     
20071102000692007110200069WP  2007       11         2          CA070913004      120070820G3246NAS14651        TIE BOLT        LORAL       9540512     CVAC  340   340CVAC     242270AWP  ALLSN 501D  501D13D     03004GL  HAMSTD54H   54H60       NE  MAIN WHEEL      MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            358   285955                                              (CAN) DURING DAILY INSPECTION OF AIRCRAFT, THE NR3 MAIN WHEEL ASSEMBLY WAS FOUND TO HAVE 4 MISSING TIE BOLTS. THE WHEEL ASSEMBLY WAS REPLACED WITH A SERVICEABLE UNIT, AN AXLE INSPECTION WAS CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVICE. AFTER INVESTIGATION, THE OVERHAUL PROCEDURE HAS BEEN REVISED TO DISCARD TIE BOLTS AND NUTS DURING WHEEL OVERHAUL/REPAIR. THE WHEEL OVERHAUL TASK CARD HAS ALSO BEEN REVISED TO INCLUDE THIS INFORMATION. (TC NR 20070913004)                                                                                                                                                                                                                                                                2L72 4R4  T  6A6     E282    6  CP906     
20080306001522008030600152SO  2008       3          6          CA070913005      120070705G57416244802         FITTING                                 PIPER PA28  PA28161     7102803SO  LYC   O320  O320D3G     41508EA  SNSNCH74D   74DM        EA  WING            CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4998                                                           (CAN) ON A SCHEDULED 100 HOUR INSPECTION, BOTH THE LT AND RT LOWER COCKPIT FITTINGS THAT THE REAR WING SPARS ATTACH TO WERE FOUND TO BE HEAVILY CORRODED. THE PARTS WERE REMOVED, THE AREA DECORRODED AS REQUIRED AND NEW FITTINGS INSTALLED. LT P/N 62448-02 AND RT P/N 62448-03. (TC NR 20070913005)                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3O3  O  2A13    E274    5  NP88614   
20071102000702007110200070NM  2007       11         2          CA070913007      120070911G3234574205A         SELECTOR                                DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  LANDING GEAR    MALFUNCTIONED   W      O   OTHER                                                                                           O  OTHER                                                                         DEDESCENT        1                      CA                                                                      (CAN) IN DESCENT, THE PILOT SELECTED GEAR DOWN. THE GEAR FAILED TO EXTEND AND THE PILOT CYCLED THE GEAR 4 TIMES WITH NO RESULT, ON THE 5 CYCLE, THE GEAR EXTENDED. MAINTENANCE PLACED THE AIRCRAFT ON JACKS AND NOTED THAT WHEN GEAR EXTENSION WAS SELECTED, IT TOOK ABOUT 10 SECONDS BEFORE THE GEAR INITIATED THE COMMAND. THE LANDING GEAR SELECTOR WAS FOUND TO BE CAUSING THE DELAY, THE SELECTOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070913007)                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080319001542008031900154EA  2008       3          19         CA070913008      220070911G7200                ENGINE                                  BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCD4N3HCD4N3A     GL                  OVERHEATED      W      E   ENGINE SHUTDOWN                                                                                 MBJOVER TEMP                 SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION        LDLANDING        1                      CA       13899459                           PCE81089                    (CAN) SHORTLY AFTER LANDING, THE PILOT NOTICED AN UNUSUALLY HIGH ITT INDICATION FOLLOWED BY SPARKS EXITING THE RT ENGINE. THE PILOT SHUTDOWN THE ENGINE AND CONTINUED TAXING WITHOUT FURTHER INCIDENT. FURTHER REPORT TO FOLLOW PENDING TEARDOWN REPORT. (TC NR 20070913008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 4T4  T  A24CE   E4EA    5  CSTC      
20071102000712007110200071EU  2007       11         2          CA070913009      120070913G7120                MOUNT                                   EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF34*            NE                              ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT ENGINE MOUNT. THE REVERSER THERMAL BLANKETS CONTACT THE MOUNT AND WITH ENGINE VIBRATION, CAUSE THE DAMAGE. THE MOUNT INSTALLED ON THE SPARE ENGINE SHOWED THE SAME TYPE OF DAMAGE.  THE WEAR DAMAGE WAS APPROXIMATELY .080 IN TO .210 IN IN WIDTH X.600 IN LONG WITH A DEPTH OF .008 IN. THE DAMAGE WAS BEYOND LIMIT IAW THE CF34-10E ENGINE MANUAL. AT THE PRESENT TIME NO DAMAGE LIMIT IS ALLOWED. GE IS PRESENTLY REVISING THE SITUATION.  THE ROOT CAUSE HAS BEEN DETERMINED THAT THE THERMAL BLANKETS HAD NO CLEARANCE WHEN THE ENGINE COWL IS CLOSED.  MFG DIDNT DETERMINE A SOLUTION YET. (TC NR 20070913009)                                                                                                                 2L72 4F4  FRTA57NM   E15NE                
20071102000722007110200072    2007       11         2          CA070914001      420070912G3416066030620010    ALTIMETER                               PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL                  MALFUNCTIONED   W      K   NONE                                                                                            J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) DURING APPROACH THE PILOTS ENCODING ALTIMETER WAS STICKING AND THE FLAG DISPLAYED. THE ALTIMETER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE (TC NR 20070914001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20071105000162007110500016NE  2007       11         5          CA070914002      220070713G7250                TURBINE BLADES                          PIAGIOP180  P180        6960204EU  PWA   PT6   PT6A66      52043NE                              ENGINE          FRACTURED       W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  APAPPROACH       1                      CA                                          104012                      (CAN) THE ENGINE SHUTDOWN IN FLIGHT ON APPROACH. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070914002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H72 3O4  TRTA59EU   E26NE                
20071105000172007110500017NE  2007       11         5          CA070914003      220070718G73203035466         TUBE                                    BAG   ATP   ATP                EU  PWA   PW120 PW126A           NE                              FUEL P3 AIR     FRACTURED       W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE SHUTDOWN UNCOMMANDED IN CRUISE. SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL CONTROL P3 AIR SUPPLY TUBE. (TC NR 20070914003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T4  TRTA27NM   E2ONE                
20071105000182007110500018NE  2007       11         5          CA070914004      220070702G7200                ENGINE                                  AYRES S2    S2RT15RESTD        SO  PWA   PT6   PT6A15AG    52043NE                                              POWER LOSS      W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                                                      (CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION DURING SPRAYING OPERATIONS RESULTING IN A FORCED LANDING AND SUBSTANTIAL AIRFRAME DAMAGE. MFG WILL MONITOR INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070914004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3T4  T  A4SW    E4EA                 
20071105000192007110500019NE  2007       11         5          CA070914005      220070710G73233032490B        SEAL                                    AEROSPATR42 ATR42*      8680900EU  PWA   PW121 PW121       52124NE                              O/SPEED GOVERNORLEAKING         W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) THE LOW ENGINE OIL PRESSURE WARNING ACTIVATED IN CRUISE AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A LEAKING OVERSPEED GOVERNOR HIGH PRESSURE PUMP SEAL. (TC NR 20070914005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA53EU   E20NE                
20071105000202007110500020NE  2007       11         5          CA070914006      220070709G7321324485516       HMU                                     AEROSPATR72 ATR72201    8680943EU  PWA   PW120 PW124B           NE                                              MALFUNCTIONED   W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION IN CLIMB FOLLOWING TAKE-OFF.  SUBSEQUENT INVESTIGATION IDENTIFIED A FAULTY HYDROMECHANICAL FUEL CONTROL UNIT. (TC NR 20070914006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA53EU   E2ONE                
20071105000212007110500021EA  2007       11         5          CA070914007      220070622G7250                TURBINE BLADES                          BELL  412   412         1182202SW  PWA   PT6T  PT6T3       52045EA                              ENGINE          FRACTURED       W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                          TH0729                      (CAN) THE ENGINE COULD NOT BE RELIGHT IN FLIGHT FOLLOWING A SIMULATED ENGINE-OUT TRAINING EXERCISE. SUBSEQUENT INSPECTION REVEALED FRACTURED TURBINE BLADES. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G72 4U4  U  H4SW    E22EA                
20071105000222007110500022NE  2007       11         5          CA070914008      220070708G732132448716        FCU                                     AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              ENGINE          FAULTY          W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  APAPPROACH       1                      CA       104165095                                                      (CAN) THE ENGINE LOST POWER ON APPROACH AND WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A FAULTY MECHANICAL FUEL CONTROL UNIT. (TC NR 20070914008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRT        E20NE                
20071105000232007110500023EA  2007       11         5          CA070914009      220070713G7200                ENGINE                                  BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA                                              MAKING METAL    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA                                          FA0067                      (CAN) ENGINE OIL PRESSURE REDUCED IN FLIGHT FOLLOWED BY A CHIP DETECTOR WARNING INDICATION. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE TURBOMACHINE OIL SYSTEM. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR  20070914009)                                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRTA13NM   E00062EN             
20071105000242007110500024NE  2007       11         5          CA070914010      220070717G732110078001        FCU                                     CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              ENGINE          FAULTY          W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA       60                                                             (CAN) ON TAKEOFF ROLL, THE ENGINE CONTROL FAULT LIGHT ILLUMINATED AND ENGINE POWER WOULD NOT INCREASE TO THROTTLE INPUT. THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED A FAULTY FUEL CONTROL UNIT. (TC NR 20070914010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA22CE   E00053EN             
20071105000252007110500025NE  2007       11         5          CA070914011      220070703G7261                ENGINE                                  BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                                              LEAKING         W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                          118318                      (CAN) ON CLIMB, THE ENGINE LOW OIL PRESSURE WARNING ACTIVATED AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED INTERNAL ENGINE OIL LEAKAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070914011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4F4  FRTA16SW   E25EA                
20071105000262007110500026NE  2007       11         5          CA070914012      220070723G7200                ENGINE                                  FOKKERF27   F27MK50            EU  PWA   PWA120PW125B           NE                                              MAKING METAL    W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                          125236                      (CAN) THE CREW OBSERVED SMOKE IN THE CABIN AND ENGINE OIL PRESSURE FLUCTUATIONS IN FLIGHT. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE TURBOMACHINERY OIL SYSTEM. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070914012)                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA817    E20NE                
20071105000272007110500027NE  2007       11         5          CA070914013      220070723G7320                LINE                                    UROCOPEC135 EC135P1     8680990EU  PWC   PW206CPW206C           NE                              FUEL SYS P3 AIR CONTAMINATED    W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) ON TAKEOFF ENGINE POWER REDUCED UNCOMMANDED. SUBSEQUENT INSPECTION REVEALED CONTAMINATION / BLOCKAGE OF THE FUEL CONTOL P3 AIR PRESSURE FITTING AT THE NR 8 BEARING CARBON SEAL LOCATION. (TC NR 20070914013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G72 3U3  UO H88EU   E42NE                
20071105000282007110500028NE  2007       11         5          CA070914014      220070721G7200                ENGINE                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              UNKNOWN         W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                          19278                       (CAN) FOLLOWING TAKEOFF A LOUD NOISE WAS HEARD ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN ENGINE POWER. A FORCED LANDING WAS CARRIED OUT RESULTING IN AIRFRAME DAMAGE.  MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070914014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3T3  T  A37CE   E4EA                 
20071105000292007110500029NE  2007       11         5          CA070914015      220070714G7314                PUMP                                    AEROSPATR42 ATR42500    8680948EU  PWA   PW120 PW127            NE                              FUEL SYSTEM     FAULTY          W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA                                                                      (CAN) ON TAKEOFF ROLL, THE ENGINE WAS FOUND NOT TO PRODUCE COMMANDED POWER AND THE TAKEOFF WAS ABORTED. THE ENGINE FUEL PUMP AND MFCU WERE SUBSEQUENTLY REPLACED. (TC NR 20070914015)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA53EU   E20NE                
20071105000302007110500030EA  2007       11         5          CA070914016      120070727G7712311555701       TORQUE SENSOR                           CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE                              ENGINE          FAULTY          W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 NRNOT REPORTED   1                      CA       2231                                                           (CAN) IN LEVEL FLIGHT, THE ENGINE LOST POWER ACCOMPANIED BY A LOUD NOISE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A FAULTY TORQUE SENSOR. (TC NR 20070914016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA14EA   E20NE                
20071105000312007110500031NM  2007       11         5          CA070914017      120070730G6120                CONTROL UNIT                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA                              PROPELLER       MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            DEDESCENT        1                      CA                                                                      (CAN) ON LEVELING OFF FROM DESCENT, THE PROPELLER WENT TO AN OVERSPEED CONDITION AND THE ENGINE WAS FOUND NOT TO RESPOND TO THROTTLE INPUT. THE ENGINE WAS SHUTDOWN IN FLIGHT. THE MFG PROPELLER ELECTRIC CONTROL, SPEED SENSOR AND ASSOCIATED ENGINE HARNESS WERE SUBSEQUENTLY REPLACED. MFG WILL MONITOR INVESTIGATION OF THESE COMPONENTS AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070914017)                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA13NM   E00062EN             
20071105000322007110500032EU  2007       11         5          CA070914018      120070907G2997                WIRE HARNESS                            AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  HYD PUMP        SHORTED         W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                                                                      (CAN) DEFECT - BLUE HYDRALULIC PUMP U/S. RECTIFICATION, AC WILD BLUE PUMP WIRING SHORTED AND BURNED IN HYDRAULIC BAY DURING TROUBLESHOOTING OF UNSERVICEABLE BLUE HYDRAULIC PUMP. (TCNR 20070914018)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080129000322008012900032NE  2008       1          29         CA070914019      120070911G62106117020201      BLADE                                   SKRSKYS61   S61N        8142104NE  GE    CT58  CT581401    30011NE                              MAIN ROTOR      LEAKING         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       5456                                                           (CAN) BIM WARNING LIGHT ILLUMINATED IN FLIGHT. SPAR PRESSURE WAS FOUND TO BE .25 LBS BELOW MINIMUM CHECKING PRESSURE. SPAR PRESSURE WAS SERVICED APPROXIMATELY 80 DAYS PREVIOUS. (TC NR 20070914019)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2G72 4U4  U  1H15    1E3                  
20080131000472008013100047SW  2008       1          31         CA070917001      120070914G673030000556001     PIN                                     BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              CYCLIC SERVO    BRINELLED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4523 2276  344                                                 (CAN) DURING ROUTINE MAINTENANCE, FLIGHT CONTROL CHECKS REVEALED A RATCHET SENSATION DURING MOVEMENT OF SHOULDER PIN ON LT LATERAL SERVO. PIN REMOVED AND INSPECTED REVEALING INDICATIONS OF BRINELLING AND THE POSSIBILITY OF PLATING WHICH HAS BEEN ADDRESSED BY AD CF95-11 R2 ( ASB 206-95-84).SERVO AND PIN WILL BE FORWARDED FOR FURTHER INSPECTION. (TC NR 20070917001)                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H2SW    E4CE                 
20071105000332007110500033CE  2007       11         5          CA070917002      120070915G3245302039402       TUBE            GOODYEAR    650C063     CESSNA425   425         2076018CE  PWA   PT6   PT6A112     52043NE  MCAULY4HFR344HFR34C762  NE  TIRE            DESTROYED       W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              LDLANDING        1                      CA       120        62710247                                            (CAN) UPON LANDING EITHER THE TIRE WAS ALREADY FLAT OR IT BLEW OUT. THE PILOT CONTROLLED THE AIRCRAFT TO A STOP WITH OUT ANY HARM TO THE AIRCRAFT. THE LT MAIN TIRE, TUBE WERE DESTROYED DURING THE ROLLOUT. NO DEFINITE CAUSE HAS BEEN DETERMINED TO THIS POINT, BUT THIS IS ONE OF MANY ISSUES WE HAVE HAD SINCE CHANGING AND NOW WILL BE REPLACING ALL PRODUCTS ON OUR FLEET OF AIRCRAFT. (TC NR 20070917002)                                                                                                                                                                                                                                                                                                                                1L72 3T3  TRTA7CE    E4EA    6  C3PNE     
20071105000382007110500038CE  2007       11         5          CA070917003      120070827G3245G156006         TUBE            GOODYEAR                CESSNA425   425         2076018CE  PWA   PT6   PT6A112     52043NE  MCAULY4HFR344HFR34C762  NE  TIRE            SPLIT           W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       123        42520008                                            (CAN) DURING GROUND HANDLING AFTER LANDING THE NOSE TIRE WAS NOTED TO BE LOW IN PRESSURE AND HISSING COULD BE HEARD FROM THE TIRE. T IRE / INNERUBE WAS DISASSEMBLED AND INNER TUBE WAS FOUND TO HAVE SMALL SPILT / CUTS AND PIN PUNCTURES IN SIDE WALLS. TORE WAS INSPECTED FOR ANOMALIES AND NONE WERE FOUND. NEW ASSEMBLIES WERE INSTALLED. (TC NR 20070917003)                                                                                                                                                                                                                                                                                                                                                                              1L72 3T3  TRTA7CE    E4EA    6  C3PNE     
20071105000402007110500040CE  2007       11         5          CA070917004      120070913G3244229K482         TIRE                                    CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              MLG             OUT OF BALANCE  W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              LDLANDING        1                      CA       231                                                            (CAN) PILOTS REPORTED VIBRATION DURING LANDING IN MAIN WHEELS. INSPECTION AND DISASSEMBLY SHOWS LT MAIN WHEEL TIRE BALANCE PATCH IS FALLING OFF CAUSING THE MAIN TIRE TO BE IN AN UNBALANCE CONDITION. ASSEMBLY REPLACED AND NO FURTHER VIBRATIONS NOTED. (TC NR 20070917004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA22CE   E00053EN             
20071105000412007110500041EA  2007       11         5          CA070917005      120070913G2700                UNKNOWN                                 CNDAIRCL601 CL6013A     8070802EA                                                                               MULTIPLE FAIL   W      O   OTHER                                                                                           A  FLAME/FIRE                                                                    TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AIRCRAFT EXPERIENCED FLAP FAILURE ON PREPARATION FOR LANDING, THEN FLEW APPROXIMATELY A FURTHER 10 MINUTES ATTEMPTING,UNSUCCESSFULLY, TO DEPLOY THE FLAPS. ON TOUCHDOWN THE THRUST REVERSERS (TR) DID NOT DEPLOY WHEREUPON THE CREW RECYCLED THE TR ARM SWITCH AFTER WHICH THE TRS DEPLOYED. AFTER LANDING THE AIRCRAFT WAS TAXIED TO THE RAMP AND PARKED. THE BRAKE FIRE WAS OBSERVED POST CREW AND PASSENGER DEPLANE TO ATTEND CUSTOMS.  NR 2 BRAKE CAUGHT FIRE, NRS 3 AND 4 BRAKE FUSES BLEW WHILE NR 1 TIRE HELD PRESSURE. (TC NR 20070917005)                                                                                                                                                                                        2L72 4F    RTA21EA                        
20071105000422007110500042SO  2007       11         5          CA070917006      120070912G760312694002        THROTTLE CABLE                          PIPER PA12  PA12        7101202SO  LYC   O320  O320A2B     41508EA  SNSNCH74DM  M74DM       EA  ENGINE          FAILED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AIRCRAFT ON FLOATS. PILOT DEPARTED RIVER AND WHEN THE PILOT PULLED THE ENGINE BACK THE RPM WOULD NOT RETARD. PILOT TURNED ONE MAG OFF AND HELD THE AIRCRAFT NOSE UP TO PREVENT ENGINE OVER-SPEED AND RETURNED TO STARTING POINT. PILOT PULLED MIXTURE WHEN HE KNEW HE COULD MAKE THE LANDING SUCCESSFULLY. THROTTLE CABLE REPLACED WITH NEW PART. (TC NR 20070917006)                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  A780    E274    5  NP88614   
20071105000432007110500043EA  2007       11         5          CA070917007      120070913G27501104SD100201    FLEX DRIVE                              CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              TE FLAPS        WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CREW REPORTED THAT THE FLAPS OPERATED NORMALLY ON APPROACH, WHEN SELECTED TO FLAPS 45. AFTER LANDING AND DURING TAXI, WHEN THE CREW SELECTED FLAPS 0, THEY RECEIVED A FLAP FAIL AND THE FLAPS REMAINED AT 45. CONTRACT MAINTENANCE RETRIEVED THE CODES FROM THE FECU AND THE IDENTIFIED A POSSIBLE MISRIG OF THE BPSU. THE FLAPS WERE THEN CYCLED THREE TIMES WITH NO FAULTS FOUND, A/C WAS RETURNED TO SERVICE. BPSU RIGGING WAS CHECKED SERVICEABLE. THE A/C WAS FLOWN FOR A BEAM REPAIR AND IT WAS DECIDED THAT TASK RJ2-275002 (FLAP LUBE AND INSPECTION WOULD BE COMPLETED.) IT WAS DISCOVERED THAT LT AND RT NR 2 FLAP FLEX DRIVES WERE UNSERVICEABLE, ONE WAS WORN, THE OTHER HAD A SLIGHT KINK AND REQUIRED REPLACEMENT. BOTH WERE2L72 4F4  FRTA21EA   E15NE                
20071105000442007110500044NE  2007       11         5          CA070917008      220070829G7414BL60064620      MAGNETO                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              RIGHT           FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            171                                                       (CAN) DURING START UP THE AIRCRAFT THE RT MAGNETO FAILED. MAGNETO WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20070917008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3O3  O  H11NM   1E4                  
20080131000482008013100048EU  2008       1          31         CA070917009      120070901G6730SC5083          SERVO CONTROL                           SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                              MAIN ROTOR      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA            2003                                                      (CAN) M/R SERVO REMOVED FROM RT POSITION DUE TO LEAKAGE. (TC NR 20070917009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3U3  U  H9EU    E00054EN             
20071105000452007110500045EU  2007       11         5          CA070917011      120070417G2820ST3367009       PACKING                                 AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              FUEL MANIFOLD   LEAKING         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) ST3367-009 PACKINGS SUPPLIED, FOUND LEAKING AT FUEL MANIFOLD.  SUSPECTED UNAPPROVED PARTS - PACKINGS MANUFACTUED / SUPPLIED WITHOUT PMA AUTHORIZATION FROM MFG. ST3367 IS A MFG PROPRIETARY SPECIFICATION. (TC NR 20070917011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRT        E20NE                
20080225001312008022500131EA  2008       2          25         CA070917013      220070914G7322                SEAL                                    AVIAT A1    A1B         2210406GL  LYC   O360  O360A1P     42259EA  HARTZLHCC2Y HCC2YK1     GL  INDUCTION SYS   DISLODGED       W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          LDLANDING        1                      CA       310                                                            (CAN) ON FINAL APPROACH THE ENGINE SUDDENLY EXPERIENCED A SEVERE LOSS OF POWER WHEN CARB HEAT WAS SELECTED. DURING INSPECTION, AFTER LANDING, A (3) INCH PIECE OF FOAM SEAL WAS FOUND LODGED IN THE CARB VENTURI. ON FURTHER INSPECTION, A CORRESPONDING GAP WAS FOUND IN THE SEAL BETWEEN THE COWL INTAKE SCOOP AND THE INDUCTION AIR FILTER.  THE REMAINING PIECES OF FOAM SEAL WERE REMOVED AND A SATISFACTORY GROUND RUN WAS CARRIED OUT. THE AC WAS RETURNED TO SERVICE. INSP OF A SECOND AC OF THE SAME MODEL DISCOVERED SIMILAR PIECES MISSING FROM THE SEAL BETWEEN THE COWL AND THE INDUCTION AIR FILTER. (TC NR 20070917013)                                                                                                          1H71 3O3  ONCA22NM   E286    5  CP920     
20080225001332008022500133EA  2008       2          25         CA070918001      220070914G7397476284          CIRCUIT BOARD                           BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  FUEL COLLECTOR  SHORTED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) A SHORT ON THE NR 2 ENGINE FUEL COLLECTOR DRAIN PUMP CIRCUIT (TC NR 20070918001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20071105000462007110500046WP  2007       11         5          CA070918002      120070916G57308398011         PANEL                                   LKHEED188   188A        5262602WP  ALLSN 501D  501D13      03004GL  ALLSN A6441 A6441FN606  GL  LT WING         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFTER A (WATER - FIRE SUPPRESSION) BOMBING MISSION, FUEL WAS FOUND LEAKING FROM A CRACK THAT WAS COMING FROM AN OLD REPAIR. THE A/C WAS DOWN LOADED WITH WEIGHT AND THE A/C WAS FERRIED TO THE COMPANY MAINTENANCE STATION. (TC NR 20070918002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L74 4T4  TRT4A22    E282    6  CP898     
20071105000472007110500047NE  2007       11         5          CA070918003      320070917G61118173881         SEAL                                    DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  PROP BLADE      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       104        20060115                                            (CAN) AFTER FLIGHT, OIL LEAK NOTED FROM NR 2 PROP LEAK TRACED TO NR 2 BLADE SEAL. NR 2 SEAL REPLACED. ABRASION MARKS NOTED ON SEALING SURFACE. (TC NR 20070918003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080306001532008030600153CE  2008       3          6          CA070918004      120070914G53401018200363      BRACKET                                 BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  NLG WW          BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA       11317                                                          (CAN) THE AC WAS ON A RETURN LEG . UPON SELECTING THE LANDING GEAR TO THE DOWN POSITION, THERE WAS NO INDICATION OF A DOWN AND LOCKED NOSE AS WELL AS THE (IN TRANSIT LIGHT) REMAINED ON IN THE GEAR HANDLE. THE CREW CARRIED OUT AN EMERGENCY LOWERING AND STILL NO DOWN AND LOCKED INDICATION FOR THE NOSE. AT THIS TIME A (FLY BY) THE TOWER CONFIRMED THE NOSE GEAR HAD EXTENDED. AN EMERGENCY LANDING WAS CARRIED OUT WITHOUT INCIDENT. MAINTENANCE DISCOVERED THAT THE BRACKET P/N 101-820036-3, WHICH HOLDS THE NOSE LANDING GEAR DOWN, MICROSWITCH HAD BROKEN AND CAUSED THE PROBLEM. THE BRACKET WAS REPLACED WITH A SERVICEABLE UNIT AND THE MICROSWITCH ADJUSTED. SEVERAL GEAR SWINGS WERE CARRIED OUT THE SYSTEM CHECKED SERVICEABLE2L72 4T4  T  A24CE   E4EA    6  CP56GL    
20080319001582008031900158EA  2008       3          19         CA070918005      220070907G8530ST203           PISTON RING                             PIPER PA23  PA23250     7102308SO  LYC   O540  TIO540C1A   41532EA  HARTZLHCE2Y HCE2YR2     GL  CYLINDER ASSY   DAMAGED         W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA       296        104573                                              (CAN) THE PROBLEM STARTED WITH HIGH OIL TEMP ON LT ENG, NEAR THE RED LINE IN TURBOBOOST AND WITH SMALL SPLIT OF MANIFOLD PRESS BETWEEN BOTH ENGINES. WE TROUBLESHOOT ALL SYS REGARDING HIGH OIL TEMP AND MANIFOLD PRESS UNTIL REPLACEMENT OF TURBO BY ITSELF BUT WITH NO CHANGE. ONLY WHAT WE FOUND WAS (2) CYLINDER WITH 65,67 OVER 80 PSID. MAKE THE DECISION TO REMOVED THOSE (2) CYLINDER ASSY. FOUND THE COMPRESSOR RING UNPLATING AT DIFFERENT LOCATIONS. THE ENG TSO IS 864.5 AND ALL THE CYLINDERS WAS OVERHAUL AT 568.5 FOR THE SAME SITUATION, RING UNPLATING. SO WE TOOK THE DECISION TO REMOVED THE OTHER 4 CYLINDER LT ON THE ENGINE AND WE FOUND RING UNPLATING ALSO. WE REINSTALLED 6 O/H CYL ASSY ON LT ENGINE AND EVERY THING R1L72 3O3  O  1A10    E14EA   5  CP9EA     
20080306001542008030600154SO  2008       3          6          CA070918006      120070822G273141234028        CONTROL CABLE                           PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ELEVATOR TRIM   CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2440                   317952033                               (CAN) DURING AN INSPECTION OF THE ELEVATOR TRIM SYSTEM, A CRACK WAS FOUND IN THE SWAGED END OF THE TRIM CABLE. THE SWAGED BARREL WAS CRACKED ALL THE WAY THROUGH TO THE CABLE ON ONE SIDE AND SHOWED INDICATIONS OF A CRACK ON THE OPPOSITE SIDE. THE CRACK IS APPROXIMATELY 3 INCHES LONG AND PRETTY WELL RUNS THE LENGTH OF THE SWAGE. (TC NR 20070918006)                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080306001552008030600155SW  2008       3          6          CA070918007      120070917G541226009121        BULKHEAD        AEROCD                  GULSTM690TP 695A        7630519SW  GARRTTTPE331TPE33110    01514WP  ROTOL R306  R306382F7   GL  NACELLE         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6654 6654                                                      (CAN) DURING WINTER MAINTENANCE, REAR NACELLE BULKHEAD FOUND CRACKED IN THE RADIUS.  BULKHEAD TO BE REPLACED. (TC NR 20070918007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H72 4T4  T  2A4     E4WE    6  CP8EU     
20071105000482007110500048SO  2007       11         5          CA070919001      120070917G2820641098          TUBE                                    PIPER PA28  PA28R201T   7102813SO  CONT  O360  TSIO360F    17025SO  HARTZLHCC2Y BHCC2YF1    GL  FUEL DISCHARGE  BROKEN          W      A   UNSCHED LANDING                                                                                 KRJFLUID LOSS                PARTIAL RPM/PWR LOSS      WARNING INDICATION        CRCRUISE         1                      CA            650                           305114                      (CAN) FUEL DISCHARGE TUBE BROKE, ENGINE LOST POWER. SUSPECT MID-TUBE CLIP P/N: 626477-2 MAY HAVE FAILED FIRST. (TC NR 20070919001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  O  2A13    E9CE    5  CP920     
20071105000492007110500049EA  2007       11         5          CA070919003      120070916G7714311090801       PROBE                                   DHAV  DHC8  DHC8311     1386006EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  NR 2 TORQUE     FAULTED         W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 TXTAXI/GRND HDL  1                      CA                                                                      (CAN) ON FIRST START OF THE DAY, THE NR 1 ENGINE OVERTORQUED TO AN UNDETERMINED VALUE. TORQUE WAS SEEN TO BE DECREASING THROUGH 70 PERCENT. IT WENT BACK TO 30 PERCENT AND THEN STARTED TO ACCELERATE AGAIN. ENGINE WAS SHUTDOWN AT 50 PERCENT TORQUE. FDR DOWNLOADED AND READ MAX TQ EXPERIENCED ON FDR READING IS 69 PERCENTS. TROUBLESHOOTING FOUND THE NR 2 TORQUE PROBE TO BE AT FAULT. TORQUE PROBE REPLACED ON NR1 ENGINE. GROUND RUNS COMPLETED, CHECKED SERVICEABLE.                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071105000502007110500050GL  2007       11         5          CA070919004      220070919G725023062462        RING                                    CESSNA750   750         2076810CE  ALLSN AE3007AE3007C          GL                              VANES           MISINSTALLED    W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       6979                               CAE330181                   (CAN) DURING ENGINE DISASSEMBLY IT WAS FOUND THAT 1 OFF LOCATING PLUG WAS INTERCHANGE WITH THE BOROSCOPE PLUG. THE LPT2 VANE RING IS HELD IN PLACE BY 3 LOCATING PLUGS, 2 PLUGS ONLY WERE FOUND CORRECTLY INSTALLED. LPT2 VANE RING WAS FOUND HEAVILY RUBBED ON THE TRAILING EDGE AT THE OUTER SHROUD LOCATION OVER AN ARC OF 75 DEG. APPROX.. THE INNER SHROUD LOCATION WAS ALSO FOUND HEAVILY RUBBED AT THE INNER PLATFORM LOCATION OVER THE SAME ARC DISTANCE. THE LPT2 BLADES (L/E SIDE), WAS FOUND HEAVILY RUBBED AT THE INNER AND OUTER SHROUD LOCATIONS, MATCHING THE LPT2 VANE RING RUB. THE LOCATING PLUG THAT WAS FOUND INSTALLED AT THE WRONG LOCATION WAS WORN. PREVIOUS SIMILAR EVENT HAD CAUSED A MAJOR ENGINE FAILURE AND ABORTED2L72 4J4  FRTT00007WITE6CH                
20080306001562008030600156    2008       3          6          CA070919006      420070917G2562200610          ANTENNA         POINTER                 ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              ELT             MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  409016                                              (CAN) DURING A POST FLIGHT CHECK THE ELT ANTENNA CONNECTOR WAS FOUND BROKEN OFF THE ELT CASE. UPON FURTHER INVESTIGATION IT WAS ALSO NOTED THAT THE PORTABLE ANTENNA WAS MISSING. A THOROUGH SEARCH WAS CARRIED OUT FOR THE MISSING PARTS WITHIN THE AREA. NO PARTS WERE FOUND, THE ELT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070919006)                                                                                                                                                                                                                                                                                                                                                                                  1G71 3O3  O  H11NM   E295                 
20071105000512007110500051EU  2007       11         5          CA070919007      120070917G32131847L           ROD                                     BAG   JETSTMJETSTM3101  1500215EU                                                               LT MLG          LEAKING         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA            1951                                                      (CAN) ON A WALKAROUND OF THE AIRCRAFT, THE LT MLG RADIUS ROD WAS FOUND TO BE LEAKING A SIGNIFICANT AMOUNT OF MIL-5606 HYDRAULIC FLUID FROM THE PISTON SEAL AREA. THE OVERHAUL INTERVAL FOR THIS PART IS 10000 CYCLES OR 6 YEARS, AND THIS ROD WAS INSTALLED FOR ONLY 1421 CYCLES AND APPROXIMATELY 21 MONTHS. THIS RADIUS ROD WAS PURCHASED ON PO NR 1609. THIS ROD WAS REMOVED FROM SERVICE 09/18/2007 AND REPLACED WITH AN OVERHAULED UNIT. (TC  20070919007)                                                                                                                                                                                                                                                                                 2L72 4T    RTA21EU                        
20071105000522007110500052GL  2007       11         5          CA070919008      220070914G7323                SHAFT           HONEYWELL               BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              GOVERNOR        SEIZED          W      EC  ENGINE SHUTDOWN         ABORTED TAKEOFF                                                         J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA            183   19671                                               (CAN) WHILE THE PILOT WAS DOING HIS PREFLIGHT SYSTEM CHECKS, HE NOTICED THAT HIS GOVERNOR RANGE HAD SHIFTED DOWN FROM THE NORMAL RANGE OF 100 PERCENT DOWN TO 97 NR ROTOR RPM. THE GOVERNOR WAS INSPECTED BY THE ENGINEER AND HE FOUND THAT THE GOVERNOR LEVER SHAFT WAS SEIZED. HE CONTINUED INSPECTING THE GOVERNOR CONTROL LINKAGE AND NOTICED THAT THE DROOP COMPENSATION TORQUE SHAFT WAS TWISTED DO TO THE GOVERNOR SHAFT BEING SEIZED. THE GOVERNOR AND THE DROP COMPENSATION LEVER ASSEMBLY WERE REPLACED, GOVERNOR RIGGED AND BEEP RANGE SET. THE HELICOPTER WAS TEST FLOWN AND FOUND SATISFACTORY. (TC NR 20070919008)                                                                                                                1G71 3U3  U  H2SW    E4CE                 
20071105000532007110500053EU  2007       11         5          CA070919009      120070918G3211B00A703066A     LANDING GEAR                            BAG   JETSTMJETSTM3212  1500217EU                                                               RIGHT           MISOVERHAULED   W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       18944138                                                       (CAN)  (AD)2006-0087 WAS REVIEWED AS PART OF THE NEW AIRCRAFTS BRIDGING INSPECTION. DURING REVIEW OF THIS AD IT WAS FOUND THAT THE RT MAIN LANDING GEAR HAD BEEN REASSEMBLED AT OVERHAUL WITH THE WRONG PART NUMBER UPPER AND LOWER TOGGLES INSTALLED. THE INSTALLED UPPER TOGGLE P/N 184514 IS OF THE WRONG EFFECTIVITY FOR THIS GEAR LEG AND SHOULD BE P/N 100A703090. THE INSTALLED LOWER TOGGLE P/N 184513 IS ALSO OF THE WRONG EFFECTIVITY FOR THIS GEAR AND SHOULD BE P/N 100A703093 OR 101A703093. THE AIRCRAFT WILL NOT ENTER SERVICE UNTIL THIS ISSUE HAS BEEN RECTIFIED. MLG LEG S/N BADL 479 WAS OVERHAULED ON THE SECOND OF AUGUST 2006.  IT WAS THEN INSTALLED ON SEPTEMBER 1 2006. THE AIRCRAFT WAS OPERATED WITH THIS GEAR FROM D2L72 4T    RTBA15CAA                      
20071105000542007110500054NM  2007       11         5          CA070921001      120070917G3230483023          SEQUENCE VALVE                          BOMBDRDHC8  DHC8400            NM                                                               NLG             FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       2763                                                           (CAN) DURING LANDING GEAR `UP` SELECTION FOLLOWING TAKEOFF, THE NLG `RED` GEAR UNSAFE LIGHT REMAINED `ON`. CREW LOWERED THE LANDING GEAR BY ALTERNATE EXTENSION, WITH ALL LANDING GEARS INDICATING THREE GREENS GEAR SAFE, THE AIRCRAFT WAS RETURNED TO BASE WHERE A NORMAL APPROACH AND LANDING WAS CARRIED OUT WITHOUT INCIDENT.  LINE MAINTENANCE INVESTIGATION IDENTIFIED FAILURE OF THE NLG SOLENOID SEQUENCE VALVE. AFFECTED VALVE WAS REPLACED AND FOLLOWING APPROPRIATE CHECKS IAW THE AIRCRAFT`S MM THE AIRCRAFT WAS RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. (TC NR 20070921001)                                                                                                                                                 2H72 4T    RTA13NM                        
20080306001572008030600157CE  2008       3          6          CA070921002      120070919G553110164000033     RIB                                     BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA                              VERTICAL STAB   CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CRACK FOUND IN VERTICAL STABILIZER AT RIB CSS 11.500. CRACK REPAIRED IAW SRM 51-70-17-001.  CRACKED RIB REPAIR (NON-PRESSURIZED AREA). (TC NR 20070921002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4T4  TRTA24CE   E4EA                 
20071105000552007110500055NE  2007       11         5          CA070921003      220070921G8530                CYLINDER        PWC                     DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            413   4217366                                             (CAN) AIRCRAFT CAME IN FOR 100 HOUR INSPECTION WITH ENGINE OIL LEAK UPPER LT SIDE.  ON GROUND RUN ENGINE VIBRATION WAS EVIDENT, MAG CHECKS WERE NORMAL, ONCE COWLINGS WERE REMOVED IT WAS DISCOVERED THAT THE CYLINDER HEAD OF NR 1 CYLINDER WAS LOOSE ON THE BARREL. FURTHER INVESTIGATION REVEALED THAT THE CYLINDER HEAD HAD COMPLETELY SEPARATED FROM THE CYLINDER BARREL.  ASSY WAS REMOVED AND REPLACED WITH SERVICEABLE CYLINDER ASSY. (TC NR 20070921003)                                                                                                                                                                                                                                                                               1H71 3R3  RRCA806    5E1                  
20080129000332008012900033GL  2008       1          29         CA070921004      120070921G7160                SEAL                                    AVIAT A1    A1B         2210406GL  LYC   O360  O360A1P     42259EA  HARTZLHCC2Y HCC2YK1     GL  INDUCTION SYS   LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) REFERENCED TO SDR NR 20070917013 AFTER FINDING COWLING SEAL LODGED IN THE CARB VENTURI. THE PILOT/OWNER OF THIS AIRCRAFT WAS REQUESTED TO CHECK THE CONDITION OF THE COWLING SEAL, IT WAS FOUND TO BE LOOSE AND DETERIORATED AS WELL. ALL OF THE SEAL WAS REMOVED FROM THE COWLING.  (TC NR 20070921004)                                                                                                                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONCA22NM   E286    5  CP920     
20071105000562007110500056NM  2007       11         5          CA070921005      120070919G3251SJ5049172       SWIVEL          MENASCO                 BOMBDRDHC8  DHC8402     1390042NM                                                               MANIFOLD        LOOSE           W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       2007       MAL0178                                             (CAN) FLIGHT CREW NOTICED A PUDDLE OF FLUID AROUND THE NLG WHILE DOING A WALK AROUND. MAINTENANCE REPORTED THAT THE JAMB NUT FOUND ON THE STEERING MANIFOLD PRESSURE AND RETURN LINE WERE LOOSE. TIGHTEN JAMB NUTS. (TC NR 20070921005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T    RTA13NM                        
20071105000572007110500057EA  2007       11         5          CA070924001      220070924G7314RG9080JAM       PUMP                                    PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  FUEL SYSTEM     WEAK            W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                                                      (CAN) RT ENGINE DRIVEN PUMP WEAK. (TC NR 20070924001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080131000492008013100049WP  2008       1          31         CA070924002      120070911G6320369D2512311     DRIVE GEAR                              HUGHES369   369D        4470706WP  ALLSN 250C  250C20      03013GL                              M/R TRANSMISSIONBROKEN          W      K   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      CA       594                                                            (CAN) MAIN ROTOR TRANSMISSION REMOVED DUE TO CHIP LIGHT ILLUMINATION. TRANSMISSION RETURNED TO HELICOPTERS COMPONENT OVERHAUL SHOP FOR REPAIR. UPON DISMANTLE IT WAS DISCOVERED THAT THE I/P GEAR HAD FAILED AND EXHIBITED ONE COMPLETE TOOTH BROKEN OFF FROM THE GEAR. (TC NR 20070924002)                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  H3WE    E4CE                 
20071105000582007110500058NM  2007       11         5          CA070924004      120070915G56108SC0043013      WINDSHIELD                              DHAV  DHC8  DHC8*              NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  COCKPIT         BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA       25492                                                          (CAN) AN AIRCRAFT WAS CRUISING AT 23,000 FT WHEN THE LHS WINDSCREEN SHATTERED. THE OPERATOR BELIEVES THE HEATING ELEMENT FUSED, CREATING A HOT SPOT AND SHATTERING THE OUTER GLASS PAIN OF THE WINDSCREEN. LHS WINDSHIELD REPLACED AND THE AIRCRAFT RETURNED WAS TO SERVICE. (TC NR 20070924004)                                                                                                                                                                                                                                                                                                                                                                                                                                                2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071105000592007110500059EA  2007       11         5          CA070924005      120070924G2710                FITTING         BOMBDR                  DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  CONTROL CABLE   MISMANUFACTURED W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) NEW AILERON CABLE P/N JNL-C6CF1125-3 FROM JNL (W.O. 091) THE CSP FITTING ON IT MEASURES .4405. THE CSP FITTING WILL NOT ENGAUGE INTO THE RECEPTICAL ON THE QUADRANT. THE CABLE REMOVED MEASURES .4310. (TC NR 20070924005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20071105000652007110500065EU  2007       11         5          CA070924006      120070923G2910                O-RING                                  AIRBUS320   A320211     3930320EU  CFMINTCFM56 CFM565A1         NE                              PTU MANIFOLD    FAILED          W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) FOLLOWING A YELLOW HYDRAULIC SYSTEM FAILURE, THE AIRCRAFT SUBSEQUENTLY EXPERIENCED A GREEN HYDRAULIC SYSTEM FAILURE, AND DIVERTED BACK TO DEPARTURE POINT. THE FLIGHT DECLARED AN EMERGENCY, AND LANDED 4000 KG OVERWEIGHT. AFTER LANDING, A NR 1 AND 3 BRAKE FIRE WAS ENCOUNTERED, WHICH WAS EXTINGUISHED BY CFR. THE AIRCRAFT WAS TOWED TO THE HANGAR. THE YELLOW SYSTEM WAS WORKED ON THE 18TH, AND A CHECK VALVE PACKING WAS REPLACED FOLLOWING AN INFLIGHT PRESSURE LOSS. (TC NR  20070924006)                                                                                                                                                                                                                                       2L72 4F4  FRTA28NM   E29NE                
20071105000662007110500066EA  2007       11         5          CA070924007      120070924G2710                FITTING                                 DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  CONTROL CABLE   DAMAGED         W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) NEW AILERON CABLE P/N JNL-C6CF1153-3 FROM JNL (W/O 022. THE CSP FITTING MEASURES .4405. THE CSP FITTING WILL NOT ENGAUGE INTO THE AILERON QUARDRANT. ORIGINAL CABLE CSP FITTING MEASURES .4320 (TC NR 20070924007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20080306001582008030600158GL  2008       3          6          CA070925001      120070922G3246138892629       CONE                                    BOMBDRBD100 BD1001A10   1390044GL  HNYWL AS907 AS90711A    33908WP                              NLG BEARING     CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       315  315                                                       (CAN) TO COMPLY WITH SB 100-32-10 (NLG REPLACEMENT OF THE LOCKING SEGMENT WITH A LOCKING COLLAR) BOTH NOSE WHEEL ASSY. WERE REMOVED TO GAIN ACCESS, CORROSION WAS FOUND ON ALL BRG CONES AND ON ALL BEARING CUPS. THE AXLE WAS ALSO FOUND TO HAVE CORROSION AND WAS REMOVED AND REPLACED. (2) SERVICEABLE NOSE WHEEL WERE ALSO INSTALLED. SINCE NO CAUSE WAS FOUND TO BE THE ROOT OF THE PROBLEM, THE OTHER CHALLENGER 300 SN 20107 303.3 TTSN FROM OUR FLEET WAS ALSO INSPECTED FOR CORROSION. THE LT NOSE WHEEL ASSY. WAS FOUND TO HAVE HEAVY BRG CONE AND CUP CORROSION. THE BRG CONE HAD TO BE DESTROYED TO REMOVE IT FROM THE AXLE. THE AXLE WAS INSPECTED AND FOUND SERVICEABLE. NO NOSE WHEEL ASSY HAD BEEN REPLACED SINCE BOTH AC HAD BE2L72 4F4  FRTT00005NYE00010LA             
20071105000672007110500067NE  2007       11         5          CA070925002      220070925G8550                ENGINE                                  DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE                  LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) ENGINE LEAKING EXCESSIVE OIL OUT OF GENERATOR DRIVE. ENGINE CASE FILLING WITH OIL. (TC NR 20070925002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3R3  RRCA806    5E1     5  CP206     
20071105000682007110500068EA  2007       11         5          CA070925003      120070923G323046193           PRIORITY VALVE                          CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              MLG             FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF THE FOLLOWING MESSAGES WERE DISPLAYED IN THE COCKPIT: STEERING INOP, GEAR DISAGREE, W.O.W. SENSOR FAILURE AND W.O.W. STATUS. NOSE GEAR REMAINED IN DOWN POSITION WITH MAIN GEAR RETRACTED. AIRCRAFT TURNED-BACK AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE MLG PRIORITY VALVE AND THE ELECTRIC MOTOR DRIVEN PUMP HYDRAULIC SYSTEM 3B (P/N 848847), FOLLOWED BY SUCCESSFUL GEAR SWINGS.                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20071105000692007110500069CE  2007       11         5          CA070926001      120070924G77123012347         VALVE                                   BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  TORQUE METER    WORN            W      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                TXTAXI/GRND HDL  1                      CA                                          PCE32270                    (CAN) FOUND WORN TORQUE METER VALVE IN POWER SECTION OF ENGINE GIVING ERRATIC ENGINE TORQUE INDICATION AT COCKPIT INDICATOR. VALVE REPLACED. NO OTHER PROBLEMS NOTED. (TC NR 20070926001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20080306001592008030600159SW  2008       3          6          CA070926002      120070726G7930206075187003    INDICATOR                               BELL  206   206L1       1182107SW  ALLSN 250C  250C28B     03013GL                              ENG OIL PRESS   FLUCTUATES      W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) THE AC WAS DEPARTING FROM BASE WHEN IT WAS NOTICED THAT THE ENGINE OIL PRESSURE INDICATOR WAS FLUCTUATING. THE PILOT RADIO A PAN TO ATC AND DID A PRECAUTIONARY LANDING. NO INCIDENT ON LANDING. THE ENGINEER WAS DISPATCHED TO THE LANDING SITE AND IT WAS DETERMINED THAT THE INDICATOR WAS AT FAULT. REPLACED INDICATOR (TC NR 20070926002)                                                                                                                                                                                                                                                                                                                                                                                            1G71 3U3  U  H2SW    E1GL                 
             20080520     CE  2008       5          20         CA070927001      120070831G32464040A           WHEEL                                   CESSNA310   310R        2074245CE  CONT  O520  IO520M      17032SO  HARTZLHCC3Y PHCC3YF2    GL  RT MLG          BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING MAINT THE RT MAIN WAS FOUND WITH PART OF THE BEAD MISSING, PILOT SAID THE WHEEL WAS OK PRIOR TO DEPARTURE AND LANDING NORMAL. TOWER ADVISED AND CREW SENT OUT FOR INSP, NO PIECES FOUND. (TC NR 20070927001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3O3  O  3A10    E5CE    5  CP25EA    
20071105000762007110500076EU  2007       11         5          CA070927002      120070924G2434                GCU                                     AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  NR 2 GENERATOR  FAILED          W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA                  813133                                              (CAN) AFTER DEPARTURE, THE CREW OBSERVED A NR 2 DC GENERATOR TRIP. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE REPLACED THE NR 2 GENERATOR CONTROL UNIT AND THE AIRCRAFT WAS RETURNED TO SERVICE AFTER SATISFACTORY GROUND RUN. (TC NR 20070927002)                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20071105000772007110500077EU  2007       11         5          CA070927003      120070925G3220A1029E          BOLT                                    BAG   JETSTMJETSTM3101  1500215EU  GARRTTTPE331TPE33110UG  01514WP  MCAULY4HFR344HFR34C652  NE  NLG             SHEARED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING INSPECTION IAW AD 024-05-87 BAE SB 53-A-JA870510R1 PART B, IT WAS NOTED THAT THE TWO UPPER BOLTS WERE SHEARED. THE AIRCRAFT WAS REMOVED FROM SERVICE AT THIS TIME. THE LOWER 2 BOLTS HAVE NOT YET BEEN REMOVED FOR INSPECTION.   DUE TO THIS FINDING AND THE POSSIBLE SAFETY RISK, HAVE ELECTED TO CARRY OUT A DVI OF THE NLG RETRACT JACK ATTACH FITTINGS FOR THE REMAINING J-3112`S IN OUR FLEET. NO OTHER DEFECTS WERE FOUND. EVALUATING WHAT CHANGES TO THE INSPECTION FREQUENCY AND POSSIBLE BOLT LIFE LIMITS MAY BE REQUIRED.  REMAINING BOLTS AND SURROUNDING STRUCTURE WILL BE INSPECTED TODAY, A REPORT WILL FOLLOW. (TC NR 20070927003)                                                                                  2L72 4T4  TRTA21EU   E4WE    6  C3PNE     
20080114002022008011400202WP  2008       1          14         CA070927004      220070926G7261307481812       LINE                                    RAYTHN850   HAWKER850XP 7150016CE  GARRTTTFE731TFE7315BR        WP                              ENGINE          CHAFED          W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       307  307                                                       (CAN) DURING SCHEDULE INSPECTION FOUND 2 OIL LINES CHAFING. THE SAME PROBLEM WAS ON BOTH ENGINES.THE PROBLEM COMES FROM THE FACTORY SINCE THE AIRCRAFT IS NEW AND LOW TIME. THE AIRCRAFT HISTORY DOES NOT SHOW ANY MAINTENANCE ACTION BEING PERFORMED IN THAT AREA SINCE THE AIRCRAFT WAS DELIVERED NEW AND IS STILL UNDER WARRANTY.  LINE PN 3074818-1 AND PN 3072083-2  (BOTH ENGINES ARE TFE731-5BR SERIES) (TC NR 20070927004)                                                                                                                                                                                                                                                                                                              1L72 4F4  FRTA3EU    E6WE                 
20071105000782007110500078SO  2007       11         5          CA070927005      220070926G741436066           GEAR                                    DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  MAGNETO         LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       155        07032007                                            (CAN) FOLLOWING A 50HR OIL CHANGE, IT WAS NOTED THE AC WAS VERY DIFFICULT TO START TO CARRY OUT THE REQUIRED LEAK CHECK. TROUBLESHOOTING REVEALED A DEFECTIVE MAGNETO. WHEN THE MAG WAS REMOVED IT WAS NOTED THAT THE DRIVE GEAR P/N 36066 WAS LOOSE ON THE DRIVE GEAR SUPPORT CASTING (P/N N/A). UPON REMOVAL OF THE NUT P/N M3019 IT WAS NOTED THAT A AN960-616L WASHER WAS NEXT TO THE GEAR, AND BEHIND THE LARGE P/N M3172 WASHER. THIS INSTALLATION SEQUENCE WOULD NOT ALLOW FOR SUFFICIENT CLAMP UP OF THE P/N M3172 WASHER NEXT TO THE P/N 36066 DRIVE GEAR, AND OVER TIME WOULD LEAD TO THE LOOSENESS ENCOUNTERED. THE MAGNETO WAS REPLACED AND THE WASHER INSTALLATION REVERSED, WITH THE AN 960-616L WASHER PLACED NEXT TO THE NUT. TH1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20071105000792007110500079SO  2007       11         5          CA070927006      220070926G741436066           GEAR                                    DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  MAGNETO         LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       132        07032004                                            (CAN) THE AIRCRAFT WAS HARD TO START WITH NO APPARENT REASON. AFTER TROUBLESHOOTING, A HARD STARTING PROBLEM ON ONE OTHER A/C IN THE FLEET AND FINDING A LOOSE DRIVE GEAR ON THE LT MAG IT WAS DECIDED TO CHECK THIS A/C FOR A SIMILAR PROBLEM. THE LT MAG WAS REMOVED AND IT WAS NOTED THAT THE MAG DRIVE GEAR WAS LOOSE AS WAS THE CASE WITH THE OTHER A/C. (REFER: SDR 9/27/07 C-FNTJ) THE GEAR P/N 36066 AND WASHER P/N M3172 WERE REMOVED AND INSPECTED. AS WITH THE OTHER A/C IT WAS NOTED THAT A AN960-616L WASHER HAD BEEN PLACED ON THE BACKSIDE OF THE M3172 WASHER AND NEXT TO THE 36066 GEAR, RESULTING IN INSUFFICIENT CLAMP UP OF THE GEAR. THE GEAR WAS REASSEMBLED TO THE MAG WITH THE WASHER POSITIONS REVERSED AND THE NUT RET1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20071105000802007110500080GL  2007       11         5          CA070927007      220070905G7230                STATOR VANE     ALLSN                   HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              COMPRESSOR      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            389   CAC30263F                                           (CAN) NR 6 STATOR VANE FAILURE (1 VANE ONLY). NO EROSION TO NEIGHBORING VANES OR PLASTIC COATING. FOUND BY HELICOPTER OPERATOR. (TC NR 20070927007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U3  U  H3WE    E4CE                 
20071105000812007110500081GL  2007       11         5          CA070928001      220070831G723023057142        STATOR VANE     ALLSN                   HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              COMPRESSOR      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            389   CAC30263F                                           (CAN) PILOT REPORTS UNUSUAL NOISE COMING FROM AIRCRAFT DURING GROUND RUN.  AIRCRAFT IS GROUNDED UNTIL ENGINEER INVESTIGATES THE UNUSUAL NOISE. NOISE IS DESCRIBED AS A (KNOCKING NOISE COMING FROM THE ENGINE) AND TOT HOTTER THAN USUAL. DURING THE GROUND RUN THE EXACT SYMPTOMS WERE DUPLICATED. THE ENGINEER DISASSEMBLED THE ENGINE TO FIND THE 6TH AXIAL ROW OF STATORS IN THE COMPRESSOR HAD A MISSING BLADE. BOTH COMPRESSOR AND TURBINE WERE SENT INTO THE ENGINE SHOP FOR REPAIR. ENGINE REPAIR SHOP ALSO FILED SDR REPORT. (TC NR 20070928001)                                                                                                                                                                                       1G71 3U3  U  H3WE    E4CE                 
20071105000822007110500082NE  2007       11         5          CA070928002      220070927G72616087T04P05      SCAVENGE PUMP                           CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              NR 1 ENGINE OIL FLUCTUATES      W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       2514825148                                                     (CAN) SHORTLY AFTER TAKEOFF THE NR ONE ENGINE OIL HIGH TEMPERATURE/LOW PRESSURE CAUTION LIGHT CAME ON. FLIGHT RETURNED TO DEPARTURE AIRPORT. FLIGHT LANDED APPROX 1000 POUNDS OVERWEIGHT. NO EMERGENCY DECLARED BUT EMERGENCY VEHICLES ON STANDBY. MAINTENANCE TROUBLESHOOTING DRAINED 1 LITER OF OIL FROM OIL TANK, INSPECTED OIL PRESSURE AND TEMPERATURE WIRE HARNESSES AND COMPLETED GROUND ENGINE RUNS. OIL PRESSURE SLOW TO RISE ON START. OIL TEMP ROSE 1 EVERY 2 SECONDS. TEMPERATURE ROSE TO 156 WITH YELLOW CAUTION. FUEL FLOW ALSO FLUCTUATING. AFTER GROUND RUN FOUND OIL OVER SERVICED AGAIN. AGB FOUND WITH 5 LITERS OF OIL, SHOULD HAVE ONLY .75 LITERS. NR 1 LUBE/SCAVENGE OIL PUMP REPLACED AND OIL SYSTEM ADJUSTED TO CORRECT 2L72 4F4  FRTA21EA   E15NE                
20071105000832007110500083SO  2007       11         5          CA070928003      120070921G8120LW16840         CONTROLLER                              PIPER PA31  PA31350     7103110SO  LYC   O540  LTIO540J2BD 41533EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          LEAKING         W      A   UNSCHED LANDING                                                                                 KR FLUID LOSS                PARTIAL RPM/PWR LOSS                                CLCLIMB          1                      CA                                          6890550                     (CAN) DURING TAKEOFF A VIBRATION AND LOW EGT WAS FELT ON THE LT ENGINE. TAKEOFF POWER WAS STILL ACHIEVED FOR THE FLIGHT. THE AIRCRAFT RETURNED TO LAND. BOTH THE DENSITY AND DIFFERENTIAL CONTROLLERS WERE FOUND TO HAVE OIL LEAKS. THE OIL WOULD CONTAMINATE THE AIR PASSAGES IN THE FCU AND CAUSE THE LOSS OF POWER AND VIBRATION. THE CONTROLLERS WERE REPLACED AND RUNUPS COMPLETED WITH NO FURTHER PROBLEMS. (TC NR 20070928003)                                                                                                                                                                                                                                                                                                           1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080306001602008030600160GL  2008       3          6          CA070928004      220070925G7311369D25623       BELT                                    HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              OIL COOLER      WORN            W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         E  VIBRATION/BUFFET                                                              APAPPROACH       1                      CA       800        HL8615                                              (CAN) ON LANDING, THE PILOT FELT A STRANGE VIBRATION. AFTER LANDING, THE AC WAS GROUNDED PENDING MAINTENANCE TROUBLESHOOTING. A CLOSE INSP WAS COMPLETED AND DETERMINED TO BE A LOOSE COOLER BELT CAUSING EXCESSIVE VIBRATION AT 100  PERCENT.  THE BELT WAS REPLACED SHIMED PROPERLY AND GROUND RUN AND FLIGHT TEST COMPLETED. (TC NR 20070928004)                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U3  U  H3WE    E4CE                 
20071105000912007110500091NE  2007       11         5          CA071001001      220070909G7250FW35594         TURBINE BLADES                          BOEING717   717200      1383700NM  RROYCEBR700 BR700715A130     NE                              ENGINE          FAILED          W      C   ABORTED TAKEOFF                                                                                 MJ OVER TEMP                 WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       3091                               13218                       (CAN) DURING ENGINE THROTTLE FOR TAXI OVERTEMP SIGNAL, AIRCRAFT ABORTED TAKEOFF. VISUAL INSPECTION REPORTED METAL IN TAIL PIPE, SUSPECT HP 1 TURBINE BLADE FAILURE. FURTHER INFORMATION WILL BE SUBMITTED AFTER ENGINE TEAR DOWN. ENGINE BEING INDUCTED AT RRC. (TC NR 20071001001)                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FTRA6WE    E00061EN             
20080306001612008030600161SW  2008       3          6          CA071001002      120070712G2820206063607101    TUBE                                    BELL  206   206L4       1182110SW                                                               FUEL SYSTEM     LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) HELICOPTER DEVELOPED FUEL LEAK SITTING IN HANGER. BONDING MATERIAL BETWEEN ALUMINUM FLANGE AND RUBBER TUBE IS ALMOST NON-EXISTENT. THE RUBBER ALSO SEEMS TO HAVE SWELLED. (TC NR 20071001002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U    NCH2SW                         
20071105000922007110500092EA  2007       11         5          CA071001003      120070929G331018271           POWER SUPPLY                            DHAV  DHC6  DHC6300     2802606EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  COCKPIT LIGHTS  DAMAGED         W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA       7521                                                           (CAN) DURING CRUISE, THE INTERNAL COCKPIT LIGHTING WAS SWITCHED ON, OVERHEAD PANEL LIGHTS DID NOT ILLUMINATE. OVERHEAD PANEL LIGHT CIRCUIT BREAKER WAS OBSERVED AS TRIPPED. CIRCUIT BREAKER WAS RESET. A FEW MINUTES LATER A SUSPECTED ELECTRICAL BURNING SMELL WAS OBSERVED.  F/A 1 WAS CONTACTED AND ASKED TO COME TO THE FLIGHTDECK. F/A 1 CONFIRMED THE SMELL AND STATED IT WAS STRONGER NEAR THE WARDROBE. QRH ACTIONS FOR FIRE/SMOKE UNKNOWN SOURCE WERE CARRIED OUT. A UNSCHEDULED LANDING COMPLETED. ENGINEERING INVESTIGATION REVEALED THAT THE NR 2 DC POWER SUPPLY EXHIBITED SIGNS OF OVERHEATING, AND DAMAGE DUE TO POSSIBLE EXCESSIVE CURRENT DRAW. UNIT ALSO HAD STRONG BURNED SMELL. THE NR 2 DC POWER SUPPLY WAS REPLACED IAW TH1H72 3T4  TRTA9EA    E20NE   6  CP7NE     
20071105000932007110500093NM  2007       11         5          CA071001004      120070930G2612285T03855       WARNING SYSTEM                          BOEING767   767328      1385290NM  GE    CF6   CF680C2B6F  30025NE                              FIRE/OVERHEAT   NO TEST         W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) DURING DAILY CHECK AN OPERATIONAL CHECK OF AUTOMATIC FIRE/OVERHEAT LOGIC TEST SYSTEM WAS CARRIED OUT AND WAS DISCOVERED THAT AURAL WARNING IS INOPERATIVE. SYSTEM BELL AND CHIME MODULE REPLACED AND SYSTEM FUNCTION CHECKED SERVICEABLE. (TC NR 20071001004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA1NM    E13NE                
20071130000912007113000091EU  2007       11         30         CA071001005      220070928G7230RK49612         IMPELLER                                BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  ENGINE          DAMAGED         W      EFA ENGINE SHUTDOWN         ACTIVATE FIRE EXT.      UNSCHED LANDING                                 AXTFLAME/FIRE                ENGINE FLAMEOUT           ENGINE CASE PENETRATION   CLCLIMB          1                      CA       4842 4842                          14796                       (CAN) WHILE ON CLIMB AFTER DEPARTING, THE WAS A BANG FROM THE RT ENGINE, TOTAL LOSS OF POWER AND FIRE WARNING. THE FWD PART OF THE ENGINE WAS SEEN TO BE ON FIRE, WHICH WAS EXTINGUISHED BY (2) SHOTS OF THE EXTINGUISHER SYSTEM. THE AIRCRAFT RETURNED TO DEPARTURE AND MADE AN EMERGENCY LANDING WITH NO FURTHER INCIDENT. INSPECTION REVEALED THAT THE LP IMPELLER CASING WAS PUNCTURED IN SEVERAL PLACES AROUND ITS EDGE. THE COWLINGS WERE ALSO SEVERELY DAMAGED BY THE FIRE. THIS ENGINE WILL BE RETURNED TO MFG FOR INVESTIGATION.                                                                                                                                                                                                       2L72 3T4  T  A24EU   A196    6  CP899     
20071105000942007110500094GL  2007       11         5          CA071001006      220070621G725023037413        SHAFT                                   BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              ENGINE          CRACKED         W      O   OTHER                                                                                           KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            TXTAXI/GRND HDL  1                      CA       232                                CAT40248                    (CAN) POWER TURBINE ACTION DISMANTLED TO DETERMINE CAUSE OF OIL CONSUMPTION AND SMOKING. UPON TEARDOWN AND DETAIL INSPECTION IT WAS NOTED THAT THE PT OUTER SHAFT HAD A LARGE CRACK ORIGINATING AT ROOT OF 1 CURVIC COUPLINGS AND SPLITTING INTO 2 FURTHER DOWN SHAFT. CRACKING AND MATERIAL DAMAGE TO CURVIC RESULTED IN LOSS OF 1 OF CURVICS WHICH WAS NOT RECOVERED. FRETTING DAMAGE IS ALSO OBSERVED ON MATING CURVICS OF 3RD AND 4TH STAGE WHEELS. REPORTED OIL CONSUMPTION AND SMOKING ASSOCIATED WITH THIS TURBINE LIKELY RESULT OF OIL AND OIL MIST MOVING THROUGH TIGHT FIT OF PT INNER AND OUTER SHAFT. NORMAL TIGHT FIT BETWEEN THESE COMPONENTS WOULD HAVE BEEN AFFECTED BY CRACKING OF OUTER SHAFT RESULTING IN OIL FLOW ACROSS THI1G71 3U3  U  H2SW    E4CE                 
20071105000952007110500095EA  2007       11         5          CA071001007      120070928G520033130131        PISTON                                  CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 AWASP       52016NE  HAMSTD43E   43E60       NE  WATER DOOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE DOING A C CHECK OUR NDT CONTRACTOR ADVISED US THAT HE HAS BEEN FINDING CRACKS IN THIS AREA WHILE WORKING FOR OTHER CUSTOMERS. WE ARE CHECKING THE REST OF OUR FLEET AS THIS FAILURE WOULD RESULT IN A UNCOMMANDED BOMB DOOR OPENING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2H72 4R3  RRTA14EA   ATC14   6  CP871     
20080319001602008031900160    2008       3          19         CA071001008      420070919G3457GPS430WX2       GPS                                     FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  COCKPIT         FAILED          W      L   ABORTED APPROACH                                                                                J  WARNING INDICATION                                                            APAPPROACH       1                      CA       2                                                              (CAN) ON APPROACH, THE GPS430W UNITS INDICATED A DISTANCE OF 30 MILES WHICH THEN, SUDDENLY CHANGED TO AN INDICATED DISTANCE OF (2) TO (3) MILES CAUSING A LOSS OF CREW SITUATION AWARENESS. THE APPROACH WAS ABORTED. MFG WAS CONTACTED AND INFORMED OF THE PROBLEM. MFG REPLIED, STATING THE ERROR WAS CAUSED BY THE SOFTWARE VERSION IN USE WHICH WOULD BE CORRECTED ASAP. A COPY OF THE PILOT`S REPORT IS ENCLOSED. (TC NR 20071001008)                                                                                                                                                                                                                                                                                                      2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20080306001622008030600162SO  2008       3          6          CA071001009      120070907G32104028400         BRACE                                   PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  MLG             BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA       12435                                                          (CAN) ON LANDING THE LT MLG COLLAPSED.  UPON INSPECTION IT WAS DETERMINED THAT THE MLG LOWER SIDE BRACE LINK ASSY HAD FAILED AT THE AFT HOLE CONTAINING MLG LOCK PIN. THE LOCK PIN WAS GONE AND UNABLE TO LOCATE.  MLG SIDE BRACE PN 40284-00 MLG P/N 40376-00 (TC NR 20071001009)                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080306001632008030600163SW  2008       3          6          CA071001010      120070922G6410206310105101    BEARING RACE    BELL                    BELL  206   206L1       1182107SW  ALLSN 250C  250C28B     03013GL                              T/R BLADE       CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         HOHOVERING       1                      CA       1737 764   CS12475                                             (CAN) PILOT REPORTED AN INCREASE OF FORCE REQUIRED TO PUSH THE T/R PEDALS AT 100 PERCENT RPM WHICH EXCEEDED THE OPERATIONAL LIMITS. HOWEVER, AT ZERO RPM THE FORCE WAS NORMAL.  IT WAS DETERMINED THAT THE CAUSE WAS ASSOCIATED WITH THE T/R FEATHERING BEARINGS.  INSPECTION SHOWED THAT THE BEARINGS ALTHOUGH SOMEWHAT WORN DID NOT HAVE EXCESSIVE WEAR.  FURTHER INSPECTION FOUND THAT ONE OF THE IB BEARINGS HAD A CRACKED INNER RACE RUNNING FULL LENGTH PARALLEL TO IT`S AXIS.  THE BEARING IS THE ORIGINAL BEARING INSTALLED BY THE MFG.  INSTALLATION OF NEW T/R BLADES RECTIFIED THE EXCESSIVE T/R FORCE AT 100 PERCENT RPM DEFECT. (TC NR 20071001010)                                                                                1G71 3U3  U  H2SW    E1GL                 
20071105001052007110500105EA  2007       11         5          CA071001011      220070715G7240310926302       DUCT            PWC         PT6A34      DHAV  DHC3  DHC3        2800202EA  PWA   PT6   PT6A34      52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4180       RB0196                                              (CAN) WHILE PERFORMING A BOROSCOPE INSPECTION DURING A REGULARLY SCHEDULED FUEL NOZZLE CHANGE, DAMAGE WAS FOUND ON THE LARGE EXIT DUCT (LED). THE LED WAS CHANGED AND UPON CLOSER INSPECTION IT WAS FOUND THAT A LARGE HOLE HAD BEEN BURNED THROUGH ONE LAYER OF THE DUCT. A CRACK THAT TRAVELED APPROXIMATELY .2500 OF THE CIRCUMFERENCE OF THE OUTER PORTION OF THE LED WAS ALSO NOTICED. (TC NR 20071001011)                                                                                                                                                                                                                                                                                                                                 1H71 3R4  T  A815    E4EA    6  CP15EA    
20071105001072007110500107GL  2007       11         5          CA071001012      220070928G7200                ENGINE                                  EMB   135   EMB135ER    3260203SO  ALLSN AE300 AE3007A          GL                              NR 1            MAKING METAL    W      B   EMER. DESCENT                                                                                   YJ ENGINE STOPPAGE           WARNING INDICATION                                  APAPPROACH       1                      CA       16065                              CAE311496                   (CAN) N13992/145284 ENGINE NR 1 (A1P, CAE311496) EXPERIENCED AN UNCOMMANDED INFLIGHT SHUTDOWN ON APPROACH TO EWR FROM MEM, FLIGHT 2144, ON 27 SEP. THE CREW OBSERVED AN ENG 1 OUT MESSAGE ON THE EICAS DURING FINAL APPROACHED AND ATTEMPTED AN UNSUCCESSFUL RESTART. UPON SAFE LANDING, MAJOR AMOUNTS OF METAL CHIPS AND FLAKES WERE FOUND ON BOTH OIL TANK MCDS WITH LIGHT AMOUNTS OF DEBRIS ON REMAINING MCDS. ENGINE ALLOCATED TO ROLLS-ROYCE CANADA FOR INVESTIGATION, FURTHER DETAIL WILL BE SUBMITTED FOLLOWING ENGINE TEARDOWN (TC NR 20071001012)                                                                                                                                                                                      2L72 4F4  FRTT00011ATTE6CH                
20071105001082007110500108NM  2007       11         5          CA071002002      120071002G2910DSC1896         CHECK VALVE                             DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  NR 2 HYD SYS    CRACKED         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) AN AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC SYSTEM NR 2 DURING TAKEOFF. FLIGHT ABORTED. ALTERNATE LDG EXTENSION USED. MAINTENANCE FOUND SPU NR 2 CHECK VALVE WITH A CIRCUMFERENTIAL CRACK ON ITS BODY. (TC NR 20071002002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080306001642008030600164CE  2008       3          6          CA071002003      120070925G3397                WIRE                                    CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  LANDING LIGHT   FAILED          W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                                                      (CAN) DURING TAKEOFF, ODOR NOTICED IN COCKPIT. FLIGHT CONTINUED. SMOKE AND SPARKS NOTICED FROM BEHIND AREA WHERE LANDING LIGHT SWITCH IS LOCATED. MASTER TUNRED OFF AND AC RETURNED TO FIELD. DURING THIS TIME, A FIRE HAD STARTED RIGHT BEHIND THE LANDING LIGHT SWITCH AND WAS EXTINGUISHED USING THE ONBOARD FIRE EXTINGUISHER. AC LANDED WITHOUT FURTHER INCIDENT.  UPON INVESTIGATION, FOUND WIRES FROM BEHIND LANDING LIGHT HAD FALLEN OFF DUE TO LANDING LIGHT SWITCH OVER HEATING AND TERMINALS FROM THE SWITCH FALLING OFF. THIS ALLOWED THE SUPPLY WIRE FOR THE LANDING LIGHT SWITCH TO CONTACT GROUND AND START ARCING WHICH STARTED THE FIRE. THE CIRCUIT BREAKER WAS FOUND IN THE CLOSED POSITION INDICATING IT DID NOT OPEN DURING1H71 3O3  ONT3A19    E223    5  NP50GL    
20080319001612008031900161EA  2008       3          19         CA071002004      220070930G853016A23033        CYLINDER                                CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  NR 3            CONTAMINATED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ENG COMPRESSION CHECK WAS COMPLETED DUE TO REPORTED ROUGH RUNNING ENG. CYL NR 3 FOUND TO HAVE NO COMPRESSION AND WAS BOROSCOPED. DURING BOROSCOPE, A PIECE OF WIRE WAS FOUND TO BE HUNG UP BETWEEN THE INTAKE VALVE AND THE EXHAUST VALVE. CYLINDER WAS REMOVED. BOTH VALVES WERE REMOVED FROM THE CYL AND THE WIRE THAT WAS NOTICED DURING BOROSCOPING FELL OUT. UPON INVESTIGATION OF THE WIRE, IT WAS DETERMINED THAT THIS WIRE WAS FROM A SCAT HOSE WHICH WAS ATTACHED TO THE CARBURATOR AIR BOX. THE WIRE WAS APPROX 3 INCHES LONG AND WAS SUCKED UP THROUGH THE AIR BOX, CARBURATOR, INDUCTION SYS AND RT INTO THE CYL. DURING CLOSE INSP OF THE WIRE, CHAF MARKS WERE NOTICED ON THE WIRE WHERE IT HAD BEEN RUBBING ON THE EDGE OF 1H71 3O3  ONT3A19    E223    5  NP50GL    
20071105001092007110500109SO  2007       11         5          CA071002005      220070928G8530                PISTON                                  BEECH 95    95B55       1152729CE  CONT  O470  IO470L      17026SO  HARTZLHCA3V PHCA3VF2    GL  ENGINE          DAMAGED         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         ERJVIBRATION/BUFFET          PARTIAL RPM/PWR LOSS      WARNING INDICATION        CRCRUISE         1                      CA       1414 98                            297694R                     (CAN) DURING CRUISE FLT, RT ENGINE BEGAN TO LOOSE OIL PRESSURE. OIL TEMP & CHT INCREASED. PILOT ELECTED TO SHUTDOWN ENGINE AS A VIBRATION BECAME APPARENT & OIL PRESSURE DECREASED TO NEAR ZERO. AN EMERGENCY DECLARED & AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTION, NR 5 CYLINDER & PISTON FOUND DAMAGED. PISTON FOUND WITH A HOLE IN SIDE JUST BELOW COMPRESSION RINGS. HOLE DOES NOT APPEAR TO BE CAUSED BY OPERATIONAL DAMAGE & ONLY 98 HRS TSO IS UNLIKELY. LOOKS LIKE A MANUFACTURING DEFECT OR SOME TYPE OF MECHANICAL DAMAGE. HOLE CAUSED CRANKCASE TO PRESSURIZE & THERFORE CAUSE ENGINE TO VENT IT`S OIL OVERBOARD THROUGH BREATHER TUBE.  SAME AIRCRAFT & ENGINE EXPERIENCED SAME PROBLEM A WEEK PRIOR TO THIS EVENT B1L72 3O3  ORT3A16    3E1     5  CP6EA     
20071105001102007110500110NM  2007       11         5          CA071002006      120070930G291220011610        FILTER ADAPTER                          BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  HYD SYSTEM      CLOGGED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF, CREW HAD TROUBLES WITH LANDING GEAR, MAIN GEARS WOULD NOT RETRACT. NOSE RETRACTED NORMALLY. ALTERNATE LANDING GEAR EXTENSION ACC. CHECKLIST DONE. UNEVENTFUL LANDING. AIRCRAFT HANDED OVER TO MAINTENANCE.  NO FAULTS CODES.  FOUND BYPASS VALVE FILTER COLLAPSED, FILTER REPLACED, A/C RTS. (TC NR 20071002006)                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20071105001112007110500111EA  2007       11         5          CA071003001      120071002G3230750005000       SELECTOR VALVE                          CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              MLG             INOPERATIVE     W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH (GEAR DISAGREE) WARNING MESSAGE AT LDG SELECTION. MLG`S WOULD NOT COME DOWN, NLG OK. CYCLED LDG SAME. ALTERNATE EXTENSION USED, OK. AIRCRAFT LANDED. SNAG CAN BE REPRODUCED ON JACKS. MLG SELECTOR VALVE FOUND INOPERATIVE. REPLACED VALVE. A/C RTS. (TC NR 20071003001)                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA21EA   E15NE                
20071105001122007110500112EA  2007       11         5          CA071003002      120071002G2497                BUSS BAR                                CNDAIRCL600 CL6002D24   1390016EA  GE    CF34  CF34*            NE                              COCKPIT         OVERHEATED      W      LA  ABORTED APPROACH        UNSCHED LANDING                                                         H  ELECT. POWER LOSS-50 PC                                                       APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH CREW RECEIVED WING ANTI ICE FAULT STS MSG FOLLOWED BY DC BUS 1 CAUTION MESSAGE. AIR TURN BACK MAINTENANCE FOUND CB`S D6, D7 AND THEIR BUS BAR OVERHEATED. REPLACED C/B`S AND BUS BAR.   PARTS REPLACED: BUS BAR CIRCUIT BREAKER D6 (80A) CIRCUIT BREAKER: D7 (3A)  BUS BAR: S6938-1 CIRCUIT BREAKER D6 (80A): MS25361-80 CIRCUIT BREAKER D7 (3A): MS22073-3 (TC NR 20071003002)                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20071105001132007110500113EA  2007       11         5          CA071003003      120071001G2752852D10019       ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              TE FLAP         MALFUNCTIONED   W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       11009                                                          (CAN) FLAPS FAIL CAUTION MSG AND 40 DEG. RAN QRH PROCEDURES AS REQUIRED AND COMPLIED WITH INSTRUCTIONS. A/C DISPATCHED UNDER PROVISIONS OF FAA AD 2006-12-21 (DEFERRAL FOR 72 HRS).  AT OVERNIGHT MAINTENANCE, FOUND RT WING FLAP DRIVE SYSTEM TORQUE VALUE AT 25 IN/LBS. FOUND RT IB ( NR 1 ACTUATOR) WITH HIGH TORQUE. REPLACED RT NR 1 FLAP ACTUATOR IAW CRJ AMM 27-53-01. (TC NR 20071003003)                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20071105001142007110500114EA  2007       11         5          CA071003004      120071003G321321587525        PLATE                                   CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 AWASP       52016NE  HAMSTD43E   43E60       NE  MLG             MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ADJUSTING PLATE P/N 215-87525 MISSING ON A NEWLY OVERHAULED LOWER MEMBER P/N 160-600-35 S/N H126.  A/C HOURS 4658.7 CYCLES 2973 DROPS16691 (TC NR 20071003004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4R3  RRTA14EA   ATC14   6  CP871     
20080306001652008030600165SO  2008       3          6          CA071003005      120070920G323074087002        ROD END         PIPER                   PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  MAIN GEAR DOOR  STIFF           W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA                                                                      (CAN) ON SEPT 12, THE DOWNLOCK HOOK ON THE RT GEAR DID NOT COMPLETELY LOCK TO ACTIVATE THE DOWNLOCK SWITCH. THE RETRACTION SYS WAS TROUBLESHOT AND FOUND THE ROD END ON THE DOWNLOCK CABLE ASSY WAS STIFF AND THE SWITCH WAS STICKING. THE GEAR WAS CLEANED AND LUBRICATED.  RETRACTION TESTS CARRIED OUT AND AC RETURNED TO SERVICE. ON THE SEPT 20, THE SAME SNAG HAPPENED. THE ROD END HAD STIFFENED UP AGAIN. THE ROD END WAS CHANGED AND NO MORE PROBLEM. THE ROD END AT FAULT WAS LUBRICATED AND FOUND TO MOVE FREELY BUT AFTER BEING LEFT ON THE BENCH FOR A FEW DAYS SEIZED UP AGAIN. (TC NR 20071003005)                                                                                                                               1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20071105001152007110500115NM  2007       11         5          CA071003006      120071002G554472760059101     MOUNT                                   DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  ACTUATOR        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4487744877                                                     (CAN) DURING RIGGING OF LOWER RUDDER ACTUATOR SPRING STRUT, NOTICED ACTUATOR ADAPTOR FLEXING. ADAPTOR FOUND TO BE CRACKED FROM OUTER FLANGE HORIZONTALLY ACROSS RADIUS TO INNER FLANGE. ADAPTOR REPLACED. (TC NR 20071003006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071105001212007110500121EA  2007       11         5          CA071003007      220070810G8550LW13383         BAFFLE                                  FOUND FBA   FBA2C2      3640104EA  LYC   O540  IO540L1A5   41532EA  HARTZLHCC3Y HCC3YR      GL  OIL SUMP        FAILED          W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       10                                                             (CAN) ENGINE OIL SUMP BAFFLE CONTACTING BOTTOM OF OIL SUMP. REPLACED OIL SUMP WITH A NEW ONE FROM MFG. INSPECTION ACCOMPLISHED BECAUSE OF REQUEST FROM CUSTOMER WHO SUBMITTED FAA SDR NR 2007FA0000760 AND 1. (TC NR 20071003007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  ONCA7EA    1E4     5  CP25EA    
20080306001662008030600166CE  2008       3          6          CA071003008      120070914G55400510128         BRACKET                                 CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA  MCAULY1C160 1C160DTM    GL  RUDDER          WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       16797                                                          (CAN) ON A 100 HOUR INSPECTION, MAINT DISCOVERED THE RUDDER PEDAL TORQUE TUBE SPRING ATTACHMENT BRACKET HOLE WAS WORN MORE THAN HALF THRU. THIS IS A HARD TO INSPECT AREA AT THE FWD TUNNEL CENTER SECTION UNDER THE DASH. THE BRACKET WAS REPLACED AND RUDDER RE-RIGGED AS REQUIRED. (TC NR 20071003008)                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  ONT3A12    E274    5  NP910     
20071105001222007110500122NE  2007       11         5          CA071003009      220070802G72613034677         TUBE                                    AEROSPATR72 ATR72202    8680940EU  PWA   PW120 PW124B           NE                              ENGINE OIL      LEAKING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB, ENGINE OIL PRESSURE WAS SEEN TO DECREASE AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A LEAKING OIL PRESSURE TUBE AT THE REAR INLET CASE. (TC NR 20071003009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA53EU   E2ONE                
20071105001232007110500123NE  2007       11         5          CA071003010      220070803G7200                ENGINE                                  FOKKERF27   F27MK50            EU  PWA   PWA120PW125B           NE                                              MAKING METAL    W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      DEDESCENT        1                      CA                                                                      (CAN) DURING DESCENT OIL ODOR AND SMOKE WERE EVIDENT IN THE CABIN. ENGINE BLEED WAS SELECTED OFF. SUBSEQUENT INSPECTION REVEALED METAL PARTICLES IN THE ENGINE OIL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA817    E20NE                
20071105001242007110500124EU  2007       11         5          CA071003011      120070805G7712                SENSOR                                  AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              AUTOFEATHER SYS MISINSTALLED    W      O   OTHER                                                                                           RWJPARTIAL RPM/PWR LOSS      INADEQUATE Q C            WARNING INDICATION        DEDESCENT        1                      CA                                                                      (CAN) ON DESCENT THE ENGINE EXPERIENCED AN UNCOMMANDED REDUCTION IN POWER ACCOMPANIED BY FEATHERING OF THE PROPELLER. PRELIMINARY INSPECTION REVEALED IMPROPERLY TORQUED TORQUE SENSOR AND POOR CONTINUITY BETWEEN THE AFU AND FUEL CONTROL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRT        E20NE                
20071105001252007110500125NE  2007       11         5          CA071003012      220070808G7200                ENGINE                                  DHAV  DHC8  DHC8106     2809020NM  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF7       NE                  SMOKE           W      E   ENGINE SHUTDOWN                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                          120696                      (CAN) FOLLOWING TAKEOFF OIL ODOR AND SMOKE WERE EVIDENT IN THE CABIN. THE ENGINE WAS SHUTDOWN IN FLIGHT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071105001262007110500126NE  2007       11         5          CA071003013      220070805G7200                ENGINE                                  AGUSTAA109  A109E       0260119EU  PWC   PW206CPW206C           NE                                              POWER LOSS      W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA                                          BC0541BC0542                (CAN) DURING TAKEOFF, THE PILOT REPORTED A POWER LOSS ACCOMPANIED BY AN LOW TORQUE WARNING INDICATION. THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G72 3U3  URTH7EU    E42NE                
20071105001272007110500127NE  2007       11         5          CA071003014      220070808G73218273002         FCU                                     CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              ENGINE          UNRESPONSIVE    W      O   OTHER                                                                                           RF PARTIAL RPM/PWR LOSS      FLT CONT AFFECTED                                   DEDESCENT        1                      CA                                                                      (CAN) ON DESCENT, THE ENGINE WAS FOUND NOT TO RESPOND TO THROTTLE INPUT. THE FUEL CONTROL UNIT WAS REPLACED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA22CE   E00059EN             
20071105001022007110500102NE  2007       11         5          CA071003015      220070807G7200                ENGINE                                  AEROSPATR72 ATR72              EU  PWA   PW120 PW124B           NE                                              MAKING METAL    W      A   UNSCHED LANDING                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                          124623                      (CAN) THE ENGINE FLAMED OUT IN CRUISE. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE OIL SYSTEM.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRT        E2ONE                
20071026001342007102600134EA  2007       10         26         CA071003016      220070630G7230FRACTURE        BLADES                                  AIRTRCAT500 AT502A      0390306SW  PWA   PT6   PT6A65B     52043EA                              COMPRESSOR      FRACTURED       W      C   ABORTED TAKEOFF                                                                                 RA PARTIAL RPM/PWR LOSS      FLAME/FIRE                                          TOTAKEOFF        1                      CA                                                                      (CAN) ON TAKEOFF, THE ENGINE EXPERIENCED A POWER LOSS ACCOMPANIED BY FLAMES EXITING THE EXHAUST. THE AIRCRAFT WAS DAMAGED, RESULTING IN A FORCED LANDING. SUBSEQUENT INSPECTION REVEALED FRACTURED COMPRESSOR BLADES. MFG WILL MONITOR THE INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003016)                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3T4  TNCA17SW   E4EA                 
20071026001352007102600135NE  2007       10         26         CA071003017      220070810G7200                ENGINE                                  UROCOPEC135 EC135P1     8680990EU  PWA   PW206 PW206B      0    NE                                              POWER LOSS      W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      CA                                                                      (CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION IN FLIGHT. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003017)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G72 3U3  UO H88EU   E42NE                
20071026001362007102600136NE  2007       10         26         CA071003018      220070813G7200                ENGINE                                  CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                                              SMOKE           W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                          70176                       (CAN) IN CRUISE SMOKE BECAME EVIDENT IN THE AIRCRAFT CABIN REQUIRING THE ENGINE AIR BLEED TO BE SELECTED OFF.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003018)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 4F4  F  A22CE   E1NE                 
20071026001372007102600137NE  2007       10         26         CA071003019      220070813G732132448716        FUEL CONTROL                            AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              ENGINE          FAULTY          W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          NRNOT REPORTED   1                      CA                                                                      (CAN) IN FLIGHT, ENGINE POWER REDUCED UNCOMMANDED AND THE ENGINE WAS SHUTDOWN. AN IN-FLIGHT RELIGHT ATTEMPT WAS UNSUCCESSFUL. SUBEQUENT INSPECTION REVEALED A FAULTY FUEL CONTROL UNIT. (TC NR 20071003019)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRT        E20NE                
20071105000012007110500001NM  2007       11         5          CA071003020      120070930G2622                SEAL                                    BOEING737   737800*            NM  CFMINTCFM56 CFM567B26US      NE                              EXTINGUISHER    FAILED          W      O   OTHER                                                                                           K  FLUID LOSS                                                                    CRCRUISE         1                      CA       9918       W856080                                             (CAN) ON SEPTEMBER 30, 2007 THE FLIGHT CREW REPORTED THAT THE PORTABLE FLIGHT DECK FIRE EXTINGUISHER PARTIALLY DISCHARGED DURING CRUISE ON A/C 803. THE FIRE EXTINGUISHER WAS REPLACED WITH NO FURTHER ACTION REQUIRED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA16WE   E00055EN             
20071130000932007113000093NE  2007       11         30         CA071003021      220070807G7230                ENGINE                                  CESSNA510   510         2076617CE  PWC   PW615 PW615FA     52282NE                                              MALFUNCTIONED   W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                          LB0013                      (CAN) IN CRUISE IN LIGHT ICING CONDITIONS, ENGINE N1 SPEED REDUCED UNCOMMANDED. THE N1 RETURNED TO NORMAL SETTINGS IN DESCENT.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 4F4  FRTA00014WIE00073EN             
20071026001382007102600138NE  2007       10         26         CA071003022      220070819G7250                TURBINE BLADES                          BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              ENGINE          DAMAGED         W      A   UNSCHED LANDING                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CLCLIMB          1                      CA                                          JA0236                      (CAN) THE ENGINE FLAMED OUT IN FLIGHT AND AN ATTEMPTED RELIGHT WAS UNSUCCESSFUL.  SUBSEQUENT INSPECTION REVEALED DAMAGED POWER TURBINE BLADES.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003022)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4F4  FRTA16SW   E25EA                
20071026001392007102600139NE  2007       10         26         CA071003023      220070812G723030B285501       FAN BLADE                               LEAR  60    60LEAR      5170707CE  PWA   305   PW305A      52128NE                              COMPRESSOR      FRACTURED       W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         E  VIBRATION/BUFFET                                                              CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE, THE ENGINE EMITTED A LOUD NOISE AND WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED TWO FRACTURED FAN BLADES.  MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003023)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA10CE   E35NE                
20071026001402007102600140CE  2007       10         26         CA071003024      120070824G7931                OIL SYSTEM                              BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                              ENGINE          FLUCTUATES      W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                          114070                      (CAN) ON APPROACH, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  MFG WILL MONITOR INVESTIGATION OF THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003024)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4T4  TRTA24CE   E26NE                
20071026001412007102600141EU  2007       10         26         CA071003025      320070825G6197                WIRE HARNESS                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  ENGINE          UNKNOWN         W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          FA0249                      (CAN) IN CRUISE, THE PROPELLER ELECTRONIC CONTROL (PEC) AND POWER PLANT WARNINGS ACTIVATED. THE ENGINE WAS SHUTDOWN IN FLIGHT. THE PEC, SENSOR AND RELATED HARNESS WERE SUBSEQUENTLY REPLACED.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003025)                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20071026001422007102600142CE  2007       10         26         CA071003026      120070826G7603                COUPLING                                BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE                              THROTTLE        FRACTURED       W      E   ENGINE SHUTDOWN                                                                                 FJ FLT CONT AFFECTED         WARNING INDICATION                                  DEDESCENT        1                      CA                                                                      (CAN) ON INITIATING DESCENT, THE ENGINE WAS FOUND NOT TO RESPOND TO THROTTLE INPUT. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL CONTROL (PLASTIC) DRIVE COUPLING. (TC NR 20071003026)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 4T4  T  A24CE   E4EA                 
20071026001432007102600143EA  2007       10         26         CA071003027      220070829G7200                ENGINE                                  BELL  412   412EP       1182205SW  PWA   PT6T  PT6T3       52045EA                                              MAKING METAL    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                          TH0736                      (CAN) AN ENGINE CHIP DETECTOR WARNING ACTIVED AND THE POWER SECTION WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL SYSTEM.  MFG WILL INVESTIGATE AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003027)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G72 4U4  U  H4SW    E22EA                
20071026001442007102600144NE  2007       10         26         CA071003028      220070823G7261                STRAINER                                CESSNA500   S550        2076607CE  PWA   JT15  JT15D4      52112NE                              NR 4 BEARING    BLOCKED         W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            DEDESCENT        1                      CA                                                                      (CAN) IN DESCENT, ENGINE OIL PRESSURE REDUCED AND THE ENGINE WAS SHUTDOWN IN FLIGHT.  SUBSEQUENT INSPECTION REVEALED OIL COKING AND BLOCKAGE OF THE NR 4 BEARING SCAVENGE OIL STRAINER. (TC NR 20071003028)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 4F4  FRTA22CE   E1NE                 
20071026001452007102600145EU  2007       10         26         CA071003029      120070829G7720                THERMOCOUPLE                            FOKKERF27   F27MK50            EU  PWA   PWA120PW125B           NE                              ENGINE          UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 NRNOT REPORTED   1                      CA                                                                      (CAN) THE ENGINE OVER-TEMPERATURE WARNING ACTIVATED IN FLIGHT AND THE ENGINE WAS SHUTDOWN. SUBSEQUENT INSPECTION REVEALED TWO UNSERVICEABLE T6 THERMOCOUPLES. (TC NR 20071003029)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2H72 4T4  TRTA817    E20NE                
20071026001462007102600146WP  2007       10         26         CA071004001      120071003G801114924HTH        STARTER                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                                              INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) ZERO TIMED STARTER INSTALLED ON AIRCRAFT.  WOULD NOT TURN OVER DURING FUNCTIONAL CHECK. (TC NR 20071004001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3O3  O  H11NM   1E4                  
20071105000102007110500010NM  2007       11         5          CA071004002      120070928G2497                WIRE HARNESS                            DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE                                              CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       17156                                                          (CAN) WIRE BUNDLE AT STATION FS 510 (BELOW FLOOR BOARD) CROSSING OVER FROM STARBOARD TO PORT SIDE. WIRE BUNDLE CURVES UPWARD RUNNING BENEATH SEAT RAIL STRUCTURE THEN GOES FORWARD ONTRAY.  WIRE BUNDLE FOUND NOT PROTECTED AS IT CURVES UP BENEATH SEAT RAIL STRUCTURE (PORT SIDE). FOUR WIRES WERE CHAFING AGAINST THIS STRUCTURE OF WHICH 3 OF THEM HAD WORN THROUGH THE INSULATOR. WIRES WERE REPAIRED AND WIRE BUNDLE PROTECTED. (TC NR 20071004002)                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA13NM   E20NE                
20080306001672008030600167CE  2008       3          6          CA071004003      120071001G5210231127416       ARM                                     LEAR  35    35LEAR      5170600CE  GARRTTTFE731TFE73122B   01518WP                              PAX DOOR        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       19829      1010                                                (CAN) DURING ROUTINE DAILY INSP, FOUND LOWER DOOR AFT LATCH ARM CRACKED ALL THE WAY THROUGH DUE TO CORROSION FATIGUE. (TC NR 20071004003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  F  A10CE   E6WE                 
20080129000362008012900036WP  2008       1          29         CA071004005      120070918G6730D2121           SERVO                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              HYDRAULIC SYS   LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1123 1123                                                      (CAN) DURING 50/100 HOUR INSPECTION HYDRAULIC SERVO FOUND LEAKING FROM PILOT VALVE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3O3  O  H11NM   1E4                  
20080129000382008012900038CE  2008       1          29         CA071004006      120071001G7602991027114       CABLE                                   CESSNA414   414         2075908CE  CONT  O520  TSIO520N    17040SO  MCAULY3AF32C3AF32C505   GL  MIXTURE CONTROL BROKEN          W      D   RETURN TO BLOCK                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       10177                                                          (CAN) DURING THE ENGINE RUN-UP, THE RT ENGINE DID NOT RESPOND TO MIXTURE CONTROL. THE MIXTURE CONTROL CABLE WAS FOUND BROKEN UNDER THE ENGINE CONTROL PEDISTAL. THE BRAKE WAS INSIDE THE CONTROL CABLE HOUSING AND COULD NOT BE SEEN WITH ANY INSPECTION. (TC NR 20071004006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3O3  ORTA7CE    E8CE    5  CP22EA    
20071105000342007110500034WP  2007       11         5          CA071004007      120070918G801114924HTH        STARTER                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       227  227                                                       (CAN) STARTER WOULD NOT DISENGAGE AFTER START. AFTER SHUTDOWN GEAR HAD TO BE PRYED BACK TO DISENGAGE. (TC NR 20071004007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3O3  O  H11NM   1E4                  
20080306001682008030600168EA  2008       3          6          CA071004008      220071001G8550LW15628         SEAL            LYC                     PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  CRANKCASE       UNSECURE        W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) OIL FOUND IN COWLING ON LT ENGINE NEAR FRONT, FWD CRANKCASE OIL SEAL FOUND TO HAVE POPPED OUT OVERHAUL INFORMED THIS COMPANY THAT THEY WERE HAVING PROBLEMS WITH THE ADHESIVE THAT THEY USE TO SECURE THIS SEAL (TC NR 20071004008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20071105000352007110500035EA  2007       11         5          CA071005001      120071004G5320CA447           SHROUD                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30015NE                              BS 559          CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A HEAVY CHECK THE FUEL SHROUD ASSY AND FUEL LINES AT FRAME 559 WERE REMOVED TO FACILITATE A SHEET METAL REPAIR. IT WAS DISCOVERED THAT BOTH SHROUD AND FUEL LINES HAVE CHAFING BEYOND LIMITS. THIS SAME REPAIR IS BEING C/O ON A/C C-FZSI(126) AND SIMILAR DAMAGE WAS FOUND IN THE SAME LOCATION. THE FUEL LINES AND SHROUD ASSY. HAVE BEEN ORDERED FOR BOTH A/C AND WILL BE REPLACED BEFORE THE A/C LEAVES THE HEAVY CHECK. (TC NR 20071005001)                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA21EA   E15NE                
20080306001692008030600169EU  2008       3          6          CA071005002      120071003G67307050A4673006    SERVO CONTROL                           UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              ROTOR           UNLOCKED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1533                                                           (CAN) PILOT REPORTED, WHEN PREFLIGHT HYDRAULIC TEST ACTIVATED, CYCLIC MOTORED RT. CYCLIC SHOULD STAY CENTERED DURING HYD TEST. SERVO REPLACED WITH O/H UNIT. GROUND TESTED, SERVICEABLE.  AFTER REMOVAL OF SERVO, NOTICED THAT INPUT LEVER WAS SLIGHTLY LOOSE. AFTER MOVING THE INPUT LEVER A FEW TIMES, LEVER APPEARED TO LOCK, AS REQUIRED. SUSPECT STICKY INTERNAL LOCK PIN. (TC NR 20071005002)                                                                                                                                                                                                                                                                                                                                             1G72 3U3  UNCR0001RD E34NE                
20080306001702008030600170EU  2008       3          6          CA071005003      120070928G32225321012193      RING            PILATS                  PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  SHOCK ABSORBER  SWOLLEN         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  IL512                                               (CAN) DURING ANNUAL INSPECTION IT WAS FOUND THAT STRUTS WERE STIFF, NOT EXTENDING ALL THE WAY. FOUND MICARTA GUIDE RINGS TOO TIGHT. SANDED MICARTA GUIDE RINGS SAME WAY AS MOD TO NOSE OLEO. SERVICED STRUTS WITH FLUID AND NITROGEN. RETURNED TO SERVICE. (TC NR 20071005003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20071105000362007110500036SW  2007       11         5          CA071005004      120071002G3210AN17722         BOLT                                    FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  RT MLG          MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) PILOT CALLED AND REPORTED THAT THE BOLT WAS MISSING FROM THE RT MLG TORQUE KNEE.  MAINTENANCE INSPECTED TORQUE KNEE ASSEMBLY AND NO SECONDARY DAMAGE WAS NOTED.  NEW BOLT WAS INSTALLED AND SECURED AND AIRCRAFT RETURNED OUT OF SERVICE. (TC NR 20071005004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20071105000372007110500037EA  2007       11         5          CA071009001      120071005G2752852D10021       ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              TE FLAPS        FROZEN          W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  DEDESCENT        1                      CA                                                                      (CAN) ON DESCENT CREW RECEIVED FLAP FAIL MESSAGE UPON SELECTION OF FLAPS DOWN. FLAPS FAILED AT ZERO DEGREES. FLIGHT LANDED WITHOUT INCIDENT. UPON INVESTIGATION IT WAS FOUND THAT THE ACTUATORS WERE FROZEN. ALL IB AND OB ACTUATORS REPLACED (8), FLAP RIGGING CARRIED OUT AND SYSTEM OPERATIONAL CHECK CARRIED OUT WITH NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE. (TC NR 20071009001)                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
20071105000392007110500039EA  2007       11         5          CA071009002      120071007G5712601R120474      RIB                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              RT WING         DENTED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) REMNANTS OF A BIRD WAS FOUND ON ARRIVAL. INSP REVEALED A DENT IN THE RT WING LEADING EDGE AT WING. THE DENT WAS APPROXIMATELY 4 INCHES BY 2 INCHES AND .25 INCHES DEEP. MAINTENANCE REMOVED THE DENT AND REPLACED RIB AT WING STATION 167.00 AND THE L/E WAS RE-INSTALLED AND WING ANTI ICE WAS FUNCTION CHECKED SERVICEABLE. (TC NR 20071009002)                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA21EA   E15NE                
20071105000602007110500060NM  2007       11         5          CA071010001      120071005G28241321536250      CONTROL VALVE                           DHAV  DHC8  DHC8315     2809010NM  PWA   PW120 PW123            NE                              FUEL SYSTEM     OBSTRUCTED      W      K   NONE                                                                                            C  F.O.D.                                                                        ININSP/MAINT     1                      CA       21                                                             (CAN) DURING TEST FLIGHT, RT AUX TO MAIN FUEL TRANSFER SYSTEM STOPPED TRANSFERRING. BOLT FOUND IN LEVEL CONTROL VALVE CAUSING VALVE TO STOP TRANSFER SYSTEM. BOLT REMOVED, SYSTEM FUNCTIONED NORMALLY. SAME SNAG REPORTED DURING CUSTOMER ACCEPTANCE FLIGHTS AT MFG. THIS F.O.D. HELD THE VALVE CLOSED INTERMITTENTLY. (TC NR 20071010001)                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA13NM   E20NE                
20080306001712008030600171CE  2008       3          6          CA071010002      120071008G750012991003315     HOSE                                    BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  BLEED AIR       CRACKED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) BLEED AIR FAIL LIGHT CAME ON DURING THE TAKEOFF PROCESS. THE AC CAME AROUND AND LANDED. MAINTENANCE WAS CALLED. IT WAS DISCOVERED THAT A BLEED AIR LINE WAS CRACKED AT THE FLANGE. LINE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20071010002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20080319001622008031900162GL  2008       3          19         CA071010003      220071009G72406870992         COMBUSTION CASE                         BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              ENGINE          CRACKED         W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          CAE821328                   (CAN) PILOT RETURNING TO BASE REPORTED HIGHER THAN NORMAL ENGINE TEMP. INSP OF THE ENG INDICATION SYS FOUND SERVICEABLE.  INSP OF THE ENGINE FOUND A CRACK IN THE COMBUSTION CASE. COMBUSTION CASE REPLACED. AC GROUND RUN AND FOUND SERVICEABLE AND RETURNED TO SERVICE. (TC NR 20071010003)                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H2SW    E4CE                 
20080306001722008030600172CE  2008       3          6          CA071010004      120070926G2421                BRUSHES                                 LEAR  35    31          5170530CE                                                               MOTOR           BURNED          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                  1080S                                               (CAN) BRUSH ASSEMBLIES BURNED. (TC NR 20071010004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F    RTA10CE                        
20080306001732008030600173SW  2008       3          6          CA071010005      120070828G6210204011250001    BLADE                                   BELL  204   204B        1181404SW  LYC   T53   T5311B      41549NE                              MAIN ROTOR      CRACKED         W      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              APAPPROACH       1                      CA       1851                                                           (CAN) ON TUESDAY THE 28TH OF AUGUST 2007, AT APPROX 19:00, LANDED AT THE STAGING AREA. THE PILOT COMMENTED THAT THERE WAS A VIOLENT LATERAL VIBRATION. AT THIS TIME THE TRANSMISSION WAS OBSERVED SHAKING EXCESSIVELY AND IT WAS DECIDED TO SHUT THE AIRCRAFT DOWN WHERE IT SAT. AS THE MAIN ROTOR BLADES SPOOLED DOWN THE PILOT OBSERVED A LARGE CRACK IN ONE OF THE BLADES. FURTHER INSPECTION REVEALED A CRACK THROUGH THE ENTIRE THICKNESS OF THE BLADE. BOTH THE TOP AND BOTTOM SKIN ARE BROKEN. THE CRACK/BREAK IS LOCATED 98 INCHES FROM THE ROOT OF THE BLADE AND RUNS FROM THE T/E TO 6 INCHES FROM THE L/E (ASCENDING, THE LEADING EDGE SPAR). AT THE START OF THE CRACK (THE TRAILING EDGE) THE SKIN HAS SPREAD APPROXIMATELY .1250 I1G71 4U4  U  H1SW    E1EA                 
20071105000612007110500061NE  2007       11         5          CA071010006      220070927G7250500310401       TURBINE WHEEL                           BOEING727   727225      1384077NM  PWA   JT8   JT8D15      52051NE                              ENGINE          FAILED          W      C   ABORTED TAKEOFF                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  TOTAKEOFF        1                      CA       20974                              700585                      (CAN) AT THE RUNWAY THRESHOLD THE FLIGHT CREW ADVANCED THE THROTTLES TO 1.2 EPR, STABLE ENGINES WERE CALLED. ADVANCED THRUST LEVERS AND APPROACHING TAKEOFF THRUST, BEFORE REACHING APPROXIMATELY 20 KTS, A LOUD BANG AND VIBRATION OCCURRED. THE FLIGHT CREW REJECTED THE TAKEOFF AND CLEARED THE RUNWAY. THE NR1 ENGINE WAS SHUT DOWN AFTER OBSERVING N2 SPOOL DOWN AND INCREASING EGT INDICATION. THE AIRCRAFT RETURNED TO THE GATE.  MAINTENANCE FOUND THAT THE ENGINE TURBINE HAD FAILED. THE ENGINE WAS REMOVED AND REPLACED WITH A SERVICEABLE ASSEMBLY. (TC NR 20071010006)                                                                                                                                                             2L73 4F4  F  A3WE    E2EA                 
20080306001742008030600174SO  2008       3          6          CA071010007      120070906G32602124800         RHEOSTAT                                PIPER PA24  PA24250     7102404SO  LYC   O540  O540A1C5    41532EA  MCAULY3D32C B3D32C417   GL  MLG INDICATOR   MALFUNCTIONED   W      B   EMER. DESCENT                                                                                   HP ELECT. POWER LOSS-50 PC   NO WARNING INDICATION                               LDLANDING        1                      CA                                                                      (CAN) PILOT SELECTED GEAR DOWN AND DID NOT SEE THE GREEN LIGHT, FOR THE GEAR DOWN POSITION. PILOT THEN STARTED EMERGENCY GEAR DOWN PROCEDURES. IT JAMMED WITH THE GREAR IN NEUTRAL POSITION, BECAUSE THE ELECTRIC SWITCH WAS NOT IN NEUTRAL. THE PILOT LANDED WITH THE GEAR UP. AFTER THE AIRPLANE WAS PUT ON THE JACKS AND THE GEAR WAS LOCKED. THE RHEOSTAT WAS TURNED TO THE DAYLIGHT RUNNING POSITION AND THE GREEN LIGHT, FOR THE GEAR DOWN LOCK POSITION CAME ON. (TC NR 20071010007)                                                                                                                                                                                                                                                     1L71 3O3  O  1A15    E295    5  CP58GL    
20080129000412008012900041CE  2008       1          29         CA071010008      120071003G27111295210325      ACTUATOR                                BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  LT AILERON TRIM SEIZED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       99948                                                          (CAN) DURING A 50 HOUR ROUTINE INSPECTION MAINTENANCE PERSONEL DISCOVERED THAT THE AILERON TRIM WAS NOT MOVING. UPON INSPECTION OF THE SYSTEM IT WAS DISCOVERED THAT THE AILERON TRIM ACTUATOR WAS SEIZED. THE ACTUATOR WAS REMOVED AND DISSASSEMBLED. THERE WAS INTERNAL RUST IN THE TRIM ACTUATOR HOUSING AND ONE BEARING WAS SEIZED. (TC NR 20071010008)                                                                                                                                                                                                                                                                                                                                                                                     2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20080129000432008012900043SW  2008       1          29         CA071010009      120071005G2911223002          ACCUMULATOR                             FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  HYD SYSTEM      CRACKED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            DEDESCENT        1                      CA       18203                                                          (CAN) AIRCRAFT WAS INBOUND WHEN CREW REPORTED THE AIRCRAFT HAD LOST ALL HYDRAULIC PRESSURE. EMERGENCY GEAR EXTENSION WAS USED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A 6 CENTIMETER CRACK LOCATED ON THE TOP SHOULDER AREA OF THE HYDRAULIC ACCUMULATOR CAP. (TC NR 20071010009)                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20080129000442008012900044SW  2008       1          29         CA071010011      120071005G3230750069501       SHAFT                                   GULSTM690TP 690         0141720SW  GARRTTTPE331TPE3315251K      NM  HARTZLHCB3T HCB3TN5     GL  NLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  3600                                                (CAN) DURING ANNUAL INSPECTION, THE SHAFT THAT PIVOTS THE NOSE GEAR UPPER LINK ASSY P/N ES10107 WAS FOUND CRACKED. THE CRACK IS LOCATED ON THE IB END OF THE SHAFT IN THE NOSE WHEEL WELL, WHERE IT IS FLUSH WITH THE EDGE OF THE HOLE IN THE UPPER LINK ASSEMBLY. THE CRACK IS APPROXIMATELY .5 INCH IN LENGTH AND PROGRESSES TO THE THRU BOLT HOLE. THE PIECE WILL BE REPLACED WITH A SERVICEABLE PART. (TC NR 20071010011)                                                                                                                                                                                                                                                                                                                   1H72 3T4  T  2A4     E2WE    6  CP15EA    
20080129000462008012900046CE  2008       1          29         CA071011001      120070914G32301153800025      MOTOR                                   BEECH 100   B100        1152919CE  GARRTTTPE331TPE3316252B 01514WP  HARTZLHCB4T HCB4TN5     GL  LANDING GEAR    UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                                                      (CAN) IN DESCENT FOR LANDING, THERE WERE ONLY 2 GREEN GEAR DOWN INDICATION LIGHTS INSTEAD OF THREE. AFTER RECYCLING THE GEAR, THE PROBLEM PERSISTED.  THE EMERGENCY LANDING GEAR SYSTEM WAS DEPLOYED AND THE 3 GREEN LIGHTS WERE ON AS REQUIRED. AIRCRAFT LANDED WITHOUT INCIDENT.  FURTHER INSPECTION REVEALED THE LANDING GEAR MOTOR WAS UNSERVICEABLE. (TC NR 20071011001)                                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A14CE   E2WE    6  CP40EA    
20080129000482008012900048CE  2008       1          29         CA071011002      120071003G7820                MUFFLER                                 CESSNA185   A185E       2072818CE  CONT  O520  IO520D      17032SO  MCAULY2A34C D2A34C58    GL  ENGINE          CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) MUFFLER CRACKED AROUND PIPE AFTER BACKFIRE. (TC NR 20071011002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3O3  O  3A24    E5CE    5  CP3EA     
20080306001752008030600175    2008       3          6          CA071011006      220071009G73206047T74P13      FCU                                     CNDAIRCL600 CL600*      1900302EA                                                               ENGINE          MALFUNCTIONED   W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) WHILE ENROUTE AND AT FL 400, THE NR 1 ENGINE FLAMED OUT.  AC DESCENDED TO FL200 AND RESTARTED IAW AFM.  AC ARRIVED SAFELY.  MFG REP IS ON SITE AND RECOMMENDED THAT THE FUEL CONTROL UNIT BE REPLACED. (TC NR 20071011006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RTA21EA                        
20071105000622007110500062EU  2007       11         5          CA071011007      120070914G534325FN1609        ATTACH FITTING                          HWKSLYDH125 HS125600A   4230158EU  GARRTTTFE731TFE7313R    01518WP                              NLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFTER REPAINT OF A/C INSPECTION REVEALED A CRACK ON SIDE OF ATTACH POINT. LDG WAS PULLED TO REPLACE ATTACH POINT BRACKET AND ATTACH POINT BRACKET BOLTS. THESE BOLTS WERE SHOWING WEAR MARKS ON THE SHANK, SUGGESTING THE NUTS WERE THREAD BOUND, INDICATING NOT ENOUGH WASHERS WERE USED. THE LDG SIDEWALL WAS ALSO SHOWING WEAR DUE TO THE BRACKET VIBRATING. WITH ALL THESE FINDING IT WAS DECIDED TO CHECK BOLT HOLE CLEARANCE ON THE LDG SIDEWALL, ALL BOLT HOLES WERE ELONGATED. DUE TO INSUFFICIENT WASHER BUILD UP THE TORQUES WERE INACCURATE CAUSING THE BRACKET TO SHIFT WITH EACH LDG CYCLE. THE CRACKS FOUND ON BRACKET COULD BE AN INDICATION OF EXCESSIVE SIDE LOAD POSSIBLY DURING CROSSWIND LANDING, INCORRECT TAXI PROCE2L72 4J4  F  A3EU    E6WE                 
20080306001762008030600176SO  2008       3          6          CA071011008      120071005G300050363007        INLET SCREEN                            PIPER PA31T PA31T       7103124SO  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL                  CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A ROUTINE EVENT INSPECTION, A SMALL 1.5 INCH CRACK WAS NOTED IN THE INLET ICE SCREEN. DURING THE NEXT EVENT INSPECTION IT WAS NOTED THAT THE CRACK HAD SPREAD SIGNIFICANTLY AND CAUSED SEPARATION FROM THE ASSEMBLY. THE STAINLESS STEEL AIR INLET WAS ALSO CRACKED AND NEEDED REPAIRS. THE SCREEN WAS REPLACED WITH A NEW UNIT. (TC NR 20071011008)                                                                                                                                                                                                                                                                                                                                                                               1L72 3T4  T  A8EA    E4EA    6  CP15EA    
20071105000632007110500063SO  2007       11         5          CA071011009      220071011G8530652984          ROCKER SHAFT                            CESSNA180   180A        2072604CE  CONT  O470  O470K       17026SO  MCAULY2A34C 2A34C203    GL  NR 4 CYLINDER   DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       400                                                            (CAN) POOR DIFF ON INSPECTION, EXH VALVE ROCKER SHAFT FOUND DAMAGED DUE TO LACK OF OIL, CAUSING OVERHEATING AND FAILURE OF ROCKER BUSHING. VALVE DAMAGED DUE TO LACK OF COOLING OIL ALSO.  CAUSE OF OIL LOSS TO ROCKER UNKNOWN, MAY POSSIBLY HAVE BEEN A BLOCKED GALLERY AT SOME POINT. (TC NR 20071011009)                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  5A6     E273    5  CP3EA     
20080129000492008012900049CE  2008       1          29         CA071011010      120070514G323311013880141     ACTUATOR                                BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  MLG             BYPASSING       W      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      CA       473                                                            (CAN) WHILE CONDUCTING A LANDING, THE PILOTS NOTED THAT WHILE SELECTING THE GEAR DOWN THE GEAR MOTOR RAN LONGER THAN NORMAL. THEY THEN NOTED THAT THE RT GEAR INDICATION LIGHT HAD FAILED TO SHOW A DOWN AND LOCKED POSITION. THEY TRIED AN EMERGENCY GEAR EXTENSION WITH NO LUCK. THEY FLEW THE AC TO A BIGGER CENTER WHERE EMERGENCY SERVICES WHERE AVAILABLE. CONDUCTED A FLYBY AND THE GEAR WAS VERIFIED TO BE IN THE DOWN AND LOCKED POSITION. THE AIRCRAFT LANDED WITH NO INCIDENT. MAINTENANCE CREW FLEW NORTH TO INVESTIGATE. DURING THIS TIME IT WAS NOTED BY THE ENGINEERS THAT THE GEAR ACTUATOR WAS BY-PASSING INTERNALLY, FAILING TO BUILD SUFFICIENT PRESSURE TO COMPLETELY LOCK THE GEAR SYSTEM. THE AIRCRAFT WAS FLOWN BACK SOUT2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20071105000702007110500070EU  2007       11         5          CA071012001      120071010G5280137414B100      BRACKET                                 BAG   JETSTMJETSTM3212  1500217EU                                                               RT MLG DOOR     BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) RT MAIN LANDING GEAR DOOR AFT HINGE BRACKET FOUND BROKEN (ONE LUG OF TWO) DURING INSPECTION. NEW BRACKET INSTALLED, GEAR SWINGS CARRIED OUT. (TC NR 20071012001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4T    RTBA15CAA                      
20071105000712007110500071NE  2007       11         5          CA071012002      320071012G61116903A10         BLADE           HAMSTD      43E60583    CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 CWASP       52016NE  HAMSTD43E   43E60       NE  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            405   N196694                                             (CAN) DURING COMPLIENCE WITH AD 81-13-06R2 AND S/B 664 A CRACK WAS FOUND EMINATING FROM ONE OF THE BUSHING RETENTION SCREW HOLES. CRACK HAS BECOME LARGER DURING REWORK PROCEDURES RENDERING THE BLADE U/S. (TC NR 20071012002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4R3  RRTA14EA   ATC14   6  CP871     
20080319001642008031900164    2008       3          19         CA071012003      220071009G7320442324          HMU             HONEYWELL               BOMBDRBD100 BD1001A10   1390044GL                                                               ENGINE          MALFUNCTIONED   W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA                  118130                                              (CAN) PILOT REPORTED, THEY LINED UP FOR TAKEOFF WITH PASSENGERS ON BOARD. WHEN HE ADVANCED THE THROTTLES FOR TAKEOFF, THE RT ENGINE DID NOT COME OUT OF IDLE.  NO CAS MESSAGES. NO CURRENT FAULTS. NO CURRENT SERVICE MESSAGES.  ONCE BACK AT THE FBO PASSENGERS DEPLANED. THE PILOT STILL HAD THE RT ENG RUNNING. HE ADVANCED THE RT THROTTLE. AGAIN, NOTHING HAPPENED. SYS PARAMETERS SHOWED THE CORRECT TQA TLA. HE HIT THE EVENT BUTTON.  REMOVED RT ENGINE HMU AND INSTALLED A REPLACEMENT. OPS CHECK GOOD (TC NR 20071012003)                                                                                                                                                                                                             2L72 4F    RTT00005NY                     
20080129000502008012900050SO  2008       1          29         CA071015001      120070928G2560010816811       SEAT BELT                               PIPER PA31  PA31350     7103110SO  LYC   O540  LTIO540J2BD 41533EA  HARTZLHCE3Y HCE3YR2A    GL  COCKPIT         BROKEN          W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                              317552130                               (CAN) AFTER STARTUP THE CAPTAIN WENT TO ATTACH AND TENSION HIS LAPBELT. AT THAT POINT THE LAP BELT DISCONNECTED FROM THE SEAT. CLOSER INSPECTION SHOWED CORROSION IN THE AREA OF THE BOLT HOLE OF THE FEMALE SIDE. THE SEATS ARE PROVIDED WITH A COVER OVER THIS AREA FOR COSMETIC REASONS. IT MAKES THE AREA DIFFICULT TO INSPECT UNLESS THE BOLT IS REMOVED AND THE COVER ALSO REMOVED.  DURING FOLLOWUP INSPECTIONS WITH OTHER SEATS IN THIS AC, MORE CORROSION WAS FOUND ON THE ATTACHMENT BRACKETS OF THE SEAT BELTS. IN ALL 3 SETS OF SEAT BELTS WERE REPLACED ON THE AIRCRAFT.  A FLEETWIDE INSPECTION OF SEAT BELTS IN THIS AREA IS BEING CARRIED OUT. AS WELL ALL COSMETIC COVERS THAT MAY INTERFERE WITH A PROPER INSPECTION HAVE BEEN1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20071105000722007110500072EA  2007       11         5          CA071015002      120071011G2750855D10011       BPSU                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1          NE                              FLAP SYSTEM     FAULTED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                                                      (CAN) EVENT OCCURRED AT GATE PUSHBACK, PREFLIGHT FLAP SELECTION. FLAP FAIL CAUTION ILLUMINATED WHEN SELECTED TO 20 DEGREES. LT FLAPS SHOWING 2 DEGREES/RT SIDE SHOWING ZERO. BOTH FLAPS WERE PHYSICALLY AT 2 DEGREES. FAULT CODES SHOWED BPSU AT FAULT. DURING REPLACEMENT WAS ALSO FOUND THE FLAP DRIVE SHEARED. BOTH PARTS REPLACED AND RIGGED. FLAP SYSTEM TEST COMPLETED WITH NO FURTHER FAULT NOTED. SYSTEMS CHECKS SERVICEABLE. (TC NR 20071015002)                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA21EA   E15NE                
20071105000732007110500073NM  2007       11         5          CA071015003      120071015G5720                BRACKET                                 DHAV  DHC8  DHC8102     2809003NM                                                               SPOILER         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING THE ACCOMPLISHEMENT OF A PRE CHECK, A SPACE WAS OBSERVED BETWEEN THE SPOILER ACTUATOR AND THE SPOILER ACTUATOR BRACKET.   FURTHER INVESTIGATION FOUND THAT THE BRACKET WAS CRACKED. (TC NR 20071015003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T    RTA13NM                        
20071105000742007110500074GL  2007       11         5          CA071015004      220071012G7323                SPLINE          RROYCE                  HUGHES369   369D        4470706WP  ALLSN 250C  250C20      03013GL                              GOVERNOR        FAILED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA            1844  22451                                               (CAN) PILOT COMPLAINED OF EXCESSIVE (ROTOR) DROOPING. CHECKED AIRCRAFT RIGGING AND LOOSE ENGINE AIR LINES. REMOVED GOVERNOR FOR BLEED CLEANING AND THE DRIVE ASSY ON THE GOVERNOR WAS COMPLETELY DISCONNECTED FROM THE PT GOVERNOR. COMPONENT WAS SHIPPED FOR FURTHER ANALYSIS. (TC NR 20071015004)                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U3  U  H3WE    E4CE                 
20080129000512008012900051NE  2008       1          29         CA071015005      220071012G7420CH5339906       IGNITION LEAD                           BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE CARRYING OUT A FUEL NOZZLE REPLACEMENT, FOUND A DAMAGED INSULATOR ON THE IGNITER END OF THE IGNITION LEAD. REPLACED IGNITION LEAD AND TESTED SERVICEABLE. (TC NR 20071015005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20080129000522008012900052GL  2008       1          29         CA071015006      220070920G732123065104        FCU                                     BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              ENGINE          OUT OF ADJUST   W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                          CAE832736                   (CAN) FCU SN 304536 REMOVED FOR OVERHAUL(RUNNING NORMAL)FCU SN 308210 TSO 0 INSTALLED (FROM SAE)AND REQUIRED MAXIMUM ADJUSTMENTS,START DERICH AND START ACCEL.TO GET ENGINE TO START.  AFTER 7.3HRS, OUR AME DEEMED IT NECESSARY TO CHANGE IT FOR A BETTER ONE. A LOANER FCU WAS RECEIVED AND SN 308210 WAS REMOVED AND SN 87041003 WAS INSTALLED AGAIN FROM SAE. THIS UNIT WOULD NOT EVEN START THE AC EVEN AFTER ALL ADJUSTMENTS. ANOTHER FCU WAS RECEIVED FROM ESSENTIAL TURBINES SN BR54951 AND IT WAS INSTALLED WHICH STARTED NORMALLY WITH LITTLE ADJUSTMENT.  NEEDS TO CHECK ITS FLOW BENCH FOR CALIBRATION. (TC NR 20071015006)                                                                                                         1G71 3U3  U  H2SW    E4CE                 
20071105000752007110500075NE  2007       11         5          CA071016001      220070831G7250                TURBINE BLADES                          DHAV  DHC8  DHC8103     1386005NM  PWA   PW121 PW121       52124NE                              ENGINE          FAILED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) FOLLOWING TAKEOFF, THE ENGINE EMITTED A LOUD NOISE AND WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. ASSOCIATED FRACTURE OF THE EXHAUST DUCT CLAMP RESULTED IN EXHAUST IMPINGING ON THE LANDING GEAR STRUT IN THE AIRCRAFT WHEELWELL, TRIGGERING A FIRE WARNING INDICATION.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071016001)                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA13NM   E20NE                
20071105000842007110500084NE  2007       11         5          CA071016002      220070902G7200                ENGINE                                  AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE                                              DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          120891                      (CAN) ENGINE TORQUE AND OIL PRESSURE WERE SEEN TO FLUCTUATE AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED INTERNAL ENGINE DAMAGE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071016002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA53EU   E20NE                
20071105000852007110500085NE  2007       11         5          CA071016003      220070905G7200                ENGINE                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              POWER LOSS      W      A   UNSCHED LANDING                                                                                 REJPARTIAL RPM/PWR LOSS      VIBRATION/BUFFET          WARNING INDICATION        CRCRUISE         1                      CA                                                                      (CAN) IN CRUISE, THE ENGINE EMITTED A NOISE ACCOMPANIED BY VIBRATION AND A COMPLETE LOSS OF POWER. THE AIRCRAFT CRASHED DURING FORCED LANDING.  WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071016003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3T3  T  A37CE   E4EA                 
20071105000862007110500086NE  2007       11         5          CA071016004      220070620G7200                ENGINE                                  AYRES S2    S2RT15RESTD        SO  PWA   PT6   PT6A34AG    52053NE                                              POWER LOSS      W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          AGAGRICULTURE    1                      CA                                          56068                       (CAN) DURING SPRAYING OPERATIONS, THE ENGINE LOST POWER AND THE AIRCRAFT SUBSEQUENTLY CRASHED. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071016004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3T4  T  A4SW    E4EA                 
20071105000872007110500087    2007       11         5          CA071016005      420070906G8300                GEARBOX                                 BELL  412   412EP       1182205SW  PWA   PT6T  PT6T3       52045EA                                              MAKING METAL    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) THE POWER SECTION CHIP DETECTOR ACTIVATED AND THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ACCESSORY GEARBOX.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071016005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G72 4U4  U  H4SW    E22EA                
20071105000882007110500088NE  2007       11         5          CA071016006      220070802G7250                TURBINE BLADES                          BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                              ENGINE          DAMAGED         W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                                                      (CAN) ON TAKEOFF ROLL THE ENGINE EMITTED A LOUD NOISE AND THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED DAMAGED POWER TURBINE BLADES. (TC NR 20071016006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4T4  TRTA24CE   E26NE                
20080129000532008012900053NE  2008       1          29         CA071016007      220070908G7250311608001       BEARING                                 DOUG  MD900 MD900       3027375NM  PWA   PW206 PW206A           NE                              ENGINE          FAILED          W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE CHIP DETECTOR ACTIVATED, ACCOMPANIED BY VIBRATION AND A TEMPERATURE INCREASE, AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED A DAMAGED NR3 BEARING AND RESULTANT TURBOMACHINERY DAMAGE. (TC NR 20071016007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G72 3U3  UNCH19NM   E42NE                
20071105000892007110500089NM  2007       11         5          CA071016008      120070906G2421                ADAPTER                                 DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  GEARBOX         LEAKING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF ENGINE OIL PRESSURE WAS LOST AND THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A LEAKING GENERATOR MOUNTING PAD ADAPTER. (TC NR 20071016008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20071105000902007110500090EU  2007       11         5          CA071016009      120070828G6123                AUTOFEATHER SYS                         AEROSPATR42 ATR42500    8680948EU  PWA   PW120 PW127            NE                                              FAULTY          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB THE PROPELLER FEATHERED UNCOMMANDED AND RECOVERED. SUBSEQUENT INSPECTION REVEALED A FAULTY AUTOFEATHER UNIT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA53EU   E20NE                
20071105000962007110500096NE  2007       11         5          CA071016010      220070911G7200                ENGINE                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              POWER LOSS      W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                          PC0605                      (CAN) FOLLOWING TAKEOFF THE ENGINE LOST POWER. THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3T3  T  A37CE   E4EA                 
20071105000972007110500097NE  2007       11         5          CA071016011      220070831G7200                ENGINE                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              POWER LOSS      W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                          PC0643                      (CAN) THE ENGINE LOST POWER FOLLOWING TAKEOFF AND THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3T3  T  A37CE   E4EA                 
20071105000982007110500098NE  2007       11         5          CA071016012      220070915G7200                ENGINE                                  AEROSPATR72 ATR72202    8680940EU  PWA   PW120 PW124B           NE                                              MAKING METAL    W      A   UNSCHED LANDING                                                                                 XBJENGINE FLAMEOUT           SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION        CLCLIMB          1                      CA                                          124371                      (CAN) DURING CLIMB THE ENGINE FLAMED OUT AND OIL SMELL WAS EVIDENT IN THE CABIN. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071016012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA53EU   E2ONE                
20071105000992007110500099NE  2007       11         5          CA071016013      220070914G7200                ENGINE                                  AIRTRCAT602 AT602       0390309SW  PWA   PT6   PT6A65AG    52043NE                                              POWER LOSS      W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                          PN0060                      (CAN) THE ENGINE LOST POWER IN FLIGHT AND THE AIRCRAFT WAS DAMAGED IN THE RESULTING FORCED LANDING. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071016013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3T4  TNCA19SW   E4EA                 
20071105001002007110500100EU  2007       11         5          CA071016014      120070831G7931310573401       REGULATOR VALVE                         AEROSPATR42 ATR42300    8680920EU  PWA   PW121 PW121       52124NE                              ENGINE OIL PRESSFAULTY          W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) THE ENGINE LOW OIL PRESSURE WARNING ACTIVATED AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A FAULTY OIL PRESSURE REGULATING VALVE. (TC NR 20071016014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA53EU   E20NE                
20071105001012007110500101NE  2007       11         5          CA071016015      220070917G7200                ENGINE                                  AIRTRCAT802 AT802A      0390308SW  PWA   PT6   PT6A65AG    52043NE                                              POWER LOSS      W      A   UNSCHED LANDING                                                                                 R  PARTIAL RPM/PWR LOSS                                                          FFFIRE FIGHTING  1                      CA                                                                      (CAN) THE ENGINE LOST POWER DURING FIREFIGHTING OPERATIONS RESULTING IN A FORCED LANDING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3T4  TNCA19SW   E4EA                 
20071105001062007110500106EA  2007       11         5          CA071016016      220070820G7200                ENGINE                                  AIRTRCAT400 AT401       0390204SW  PWA   PT6   PT6A34      52043EA                                              POWER LOSS      W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  AGAGRICULTURE    1                      CA                                                                      (CAN) DURING SPRAYING OPERATIONS THE ENGINE EMITTED A LOUD NOISE AND LOST POWER, RESULTING IN A FORCED LANDING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3R4  T  A17SW   E4EA                 
20071105001162007110500116NE  2007       11         5          CA071016017      220070925G7240                LINER                                   CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              COMBUST CHAMBER DAMAGED         W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                                                                      (CAN) THE ENGINE WAS REPORTED TO HAVE REPEATEDLY FLAMED OUT DURING TAXI OPERATIONS. INSPECTION REVEALED A DAMAGED/WORN COMBUSTION CHAMBER LINER. (TC NR 20071016017)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA22CE   E25EA                
20071105001172007110500117EA  2007       11         5          CA071016018      220070927G7250                TURBINE BLADES                          PILATSPC6   PC6         7090102EU  PWA   PT6   PT6A27      52043EA                              ENGINE          FRACTURED       W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) DURING AIRCRAFT STALL RECOVERY TRAINING, THE ENGINE FLAMED OUT. SUBSEQUENT RE-LIGHT ATTEMPTS WERE UNSUCCESSFUL. INSPECTION REVEALED FRACTURED COMPRESSOR TURBINE BLADES. (TC NR 20071016018)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1H71 3O4  T  7A15    E4EA                 
20080129000552008012900055NE  2008       1          29         CA071016020      120071014G28207630700701041   HOSE                                    SKRSKYS76   S76A        8143006NE  ALLSN 250C  250C30S     03013GL                              FUEL DIST       COLLAPSED       W      C   ABORTED TAKEOFF                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  TOTAKEOFF        1                      CA                                                                      (CAN) FUEL HOSE INTERNAL COLLAPSE (TC NR 20071016020)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G72 3U3  U  H1NE    E1GL                 
20080129000672008012900067EU  2008       1          29         CA071016021      120071016G2810257PV6589A      FLOAT VALVE                             BRAERODH125 BAE125800A  1500285EU  GARRTTTFE731TFE7315R    01518WP                              VENTRAL TANK    STUCK           W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA       6452       DHB97                                               (CAN) DURING REFUELLING USING SINGLE-POINT SYS & FILLING BOTH MAIN (WINGS) & VENTRAL TANK. AS VENTRAL TANK REACHED 1.5 TO 3 QUARTERS CAPACITY FUEL WOULD FLOW THROUGH VENT SYS INTO LT SURGE TANK & SHUTDOWN BY CLOSING MAIN VALVE. COMPLETION OF REFUELLING COULD ONLY RESUME ONCE SURGE TANK EMPTIED & VENTRAL TANK FUELED VIA FUELING CAP. ON REMOVAL OF VENTRAL TANK, DISCOVERED RT VENT FLOAT INADVERTENTLY GLUED TO VALVE BODY & NEEDLE HARD TO OPERATE. BOTH CONDITIONS LEFT RT VENT VALVE OPEN DURING ALL CONDITIONS CAUSING FUEL TO ENTER VENT PIPING THOUGH NONE EXISTED.  FLOAT REMOVED & NEW NEEDLE INSTALLED, OPS OF VALVE CHECKED FOR SMOOTHNESS & PROPER SEALING OF NEEDLE TO SEAT. MODIFICATION (25G137A) EMBODIED TO INCORPORAT2L72 4F4  FRTA3EU    E6WE                 
20071105001182007110500118GL  2007       11         5          CA071017001      120071016G2434A3579101        GENERATOR                               BOMBDRBD100 BD1001A10   1390044GL  HNYWL AS907 AS90711A    33908WP                              RIGHT           FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       330                                                            (CAN) IN CRUISE FLIGHT RT GENERATOR FAILED. AFTER FOLLOWING PROCEDURES A/C LANDED WITHOUT ANY MORE INCIDENT. TROUBLESHOOTING WITH MDC REPORTED PCB6 AT FAULT FROM GCU P/N R608-003. FURTHER TROUBLESHOOTING REVEALED RT GENERATOR WAS AT FAULT NOT THE GCU. GENERATOR WAS REMOVED AND REPLACED AND A/C RETURNED TO SERVICE. NORMAL TBO FOR GENERATOR IS 3000 HRS GENERATOR HAD ONLY 329.7 HRS. MANUFACTURER OF GENERATOR IS AUXILEC (F0296) TAKEN ON DATA PLATE. (TC NR20071017001)                                                                                                                                                                                                                                                             2L72 4F4  FRTT00005NYE00010LA             
20080306001772008030600177EA  2008       3          6          CA071017002      120071017G281021564002        FUEL CELL                               CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE                  LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1893                                                           (CAN) FUEL LEAK ON BOTTOM OF FUEL CELL NR 5 LT.    (TC NR 20071017002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20080306001782008030600178EA  2008       3          6          CA071017003      220071012G7414104001667       IMPULSE COUPLINGCONT                                                       LYC   O320  O320H2AD    41508EA                              MAGNETO         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       671        G05KA029R                                           (CAN) IMPULSE CAM ASSEMBLY FOUND CRACKED AT KEY WAY AREA. REPLACED WITH NEW ASSY. (TC NR 20071017003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  3  O          E274                 
20071105001192007110500119SO  2007       11         5          CA071018001      220071016G8500IO240B          ENGINE                                  DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA                  STALLED         W      O   OTHER                                                                                           RY PARTIAL RPM/PWR LOSS      ENGINE STOPPAGE                                     NRNOT REPORTED   1                      CA       979                    C0416                                   (CAN) DURING POWER ON STALL THE PROPELLER CAME TO A FULL STOP, THROTTLE WAS AT 1700 RPM AND THE NOSE POINTED UP FOR A STALL CONFIGURATION AND ON POWER APPLICATION THE ENGINE CAME TO A FULL STOP. THE AIRCRAFT WAS THEN POINTED NOSE DOWN, THE PROPELLER STARTED WIND MILLING AND ON THROTTLE APPLICATION THE ENGINE RE-STARTED.  A/C RETURNED TO BASE WITH NO PROBLEM. THIS WAS A NEW RETROFIT EQUIPPED A/C WITH A COMPLETE -54 ENGINE CONFIGURATION. MFG WERE INFORMED AND THE COMPONENTS ARE SCHEDULED TO BE TESTED AND REMOVED BY MFG AT THE END OF THIS WEEK. (TC NR 20071018001)                                                                                                                                                         1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20080131000512008013100051SW  2008       1          31         CA071018003      120071017G2911223003          ACCUMULATOR                             SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE331*     01514WP  MCAULY4HFR344HFR34C652  NE  HYD SYSTEM      INOPERATIVE     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ACCUMULATOR WAS REMOVED FOR TROUBLESHOOTING HYDRAULIC LEAKS IN SYSTEM. IT WAS SUSPECTED THAT THE ACCUMULATOR WAS NOT DOING ITS JOB OF ABSORBING THE HYDRAULIC SHOCKS. UPON REMOVAL IT WAS NOTED THAT THE INTERNAL PISTON WAS INSTALLED BACKWARDS. THE -3 ACCUMULATOR DOES NOT SHOW UP IN THE PRESENT IPC. THE ACCUMULATOR WAS INSTALLED IN 2002 AND CAME INTO INVENTORY IN 1999 AND WAS CERTIFIED IN 1997. (TC NR 20071018003)                                                                                                                                                                                                                                                                                                            2L72 4T3  TRTA8SW    E2WE    6  C3PNE     
20080129000682008012900068EA  2008       1          29         CA071018004      120071015G5510C6FSM181421     ADAPTER                                 DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA                                              MISINSTALLED    W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA  57RF 18455                  688                                     (CAN)   WHILE REMOVING ATTACHMENT ADAPTER P/N C6FSM1814-21, IT WAS NOTED THAT THE RIVETS INSTALLED IN THE VERTICAL WEBS TO ADAPTER WERE THE INCORRECT TYPE. THE RIVETS REMOVED FROM THIS ADAPTER PLATE WERE A.D. RIVETS. THE CORRECT RIVET WOULD HAVE BEEN D.D.  ADAPTER SHOWS SIGNS OF FRETTING CORROSION CAUSED BY SLIGHT MOVEMENT.                                                                                                                                                                                                                                                                                                                                                                                                           1H72 3T4  TRTA9EA    E4EA                 
20080129000692008012900069WP  2008       1          29         CA071019001      120071017G6520B5631           SIGHT GLASS                             ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              TAIL ROTOR      LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       818                                                            (CAN) DURING INSPECTION, IT WAS NOTED THAT THERE WAS FLUID LEAKING AROUND THE TAIL ROTOR GEARBOX SIGHT GLASS. THE PART WAS REMOVED AND REPLACED WITH A NEW PART. IT WAS FURTHER EXAMINED AND NOTED THE GLASS COULD ROTATE IN THE HOUSING, NO LONGER SECURE ALLOWING FLUID TO BYPASS AND LEAKING. THERE IS NO ISSUE OF THE GLASS DEPARTING THE AIRCRAFT AND POSSIBLY STRIKING THE T/R BLADES. (TC NR 20071019001)                                                                                                                                                                                                                                                                                                                                1G71 3O3  O  H11NM   1E4                  
20080129000702008012900070CE  2008       1          29         CA071019002      120071019G5740NAS680A08       NUT PLATE                               CESSNA172   172K        2072430CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160CTM    GL  FUEL TANK BAYS  MISREPAIRED     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) UPON INSPECTING THE FUEL TANKS, FOUND SEVERAL NUTPLATES PREVIOUSLY DAMAGED. UPON FURTHER INSPECTION FOUND THAT AT A PREVIOUS TIME, SOME SCREWS BROKE OFF IN THE NUTPLATES AND RATHER REPAIR/REPLACE THE NUTPLATES, IT APPEARS THE DAMAGED NUTPLATES WERE DRILLED AND SHEET METAL SCREWS WERE INSTALLED WHERE STRUCTURAL SCREWS SHOULD HAVE BEEN. THE REPAIR WAS SIMPLE, DRILL OUT THE OLD NUTPLATES AND NEW NUTPLATES INSTALLED. AS THE FUEL TANK COVERS ARE A STRUCTURAL PART OF THE WING I RECOMEND KEEPING THIS AREA IN GOOD REPAIR. (TC# 20071019002)                                                                                                                                                                                 1H71 3O3  ONT3A12    E274    5  NP910     
20080306001792008030600179NE  2008       3          6          CA071019003      220071013G7314C8187B          PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              AUX FUEL        FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1122                                                           (CAN) DURING AN ATTEMPTED START UP THE AIRCRAFT FAILED TO START. IT WAS FOUND THAT THE AUXILIARY FUEL PUMP HAD FAILED. PUMP WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20071019003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3O3  O  H11NM   1E4                  
20080306001802008030600180NE  2008       3          6          CA071019004      220070712G7250                TURBINE BLADES                          EMB   120   EMB120      3260201SO  PWA   118   PW118            NE                              ENGINE          FRACTURED       W      A   UNSCHED LANDING                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) ENGINE FLAMEOUT OUT IN CLIMB. RELIGHT ATTEMPT WAS UNSUCCESSFUL. SUBSEQUENT INSPECTION REVEALED FRACTURED TOWERSHAFT AND DAMAGED POWER TURBINE BLADES. (TC NR 20071019004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4T4  TRTA31SO   E20NE                
20080306001812008030600181NE  2008       3          6          CA071022001      220071019G732022852402115     TUBE                                    CNDAIRCL601 CL6013A     8070802EA  GE    CF34  CF343A2     30067NE                              FUEL            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5991                                                           (CAN) DURING POWER PLANT BUILD UP, FOUND LINE P/N 228-52402-115 FOR PYLON STATIC PRESSURE TO FCU CRACKED AT MIDDLE. THE CRACK WAS HIDDEN BY A LINE IDENTIFICATION DECAL. LINE WAS REMOVED AND REPLACED AIRCRAFT WILL BE RETURNED TO SERVICE. (TC NR 20071022001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20080306001822008030600182EA  2008       3          6          CA071022002      220071009G8520LW10292         IDLER GEAR                              PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  GEAR SHAFT      WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6311 1154                          L41868A                     (CAN) DURING A SCHEDULED INSP OF THE ENGINE, THE OIL FILTER WAS REMOVED AND DISASSEMBLED. IT WAS NOTED THAT THE FILTER MEDIA CONTAINED AN ABNORMAL AMOUNT OF METAL. THE AIRCRAFT WAS FLOWN AN ADDITIONAL 10 HRS AND THE FILTER WAS AGAIN INSPECTED. UPON INSPECTION THE FILTER CONTAINED AN ABNORMAL AMOUNT OF METAL AND AS A RESULT THE ENGINE WAS REMOVED AND SENT TO AN OVERHAUL FACILITY. THE OVERHAUL FACILITY FOUND THE CRANKSHAFT IDLER GEAR HAD EXCESSIVE PLAY AND WAS CAUSING WEAR ON THE IDLER GEAR BUSHING. THE BUSHING GEAR WAS REPLACED AND ENGINE REASSEMBLED. (TC NR 20071022002)                                                                                                                                                1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080306001832008030600183WP  2008       3          6          CA071022003      120070930G801114924HTH        STARTER                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       202  202                                                       (CAN) REMOVED DUE TO CRACKED BASE. (TC NR 20071022003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3O3  O  H11NM   1E4                  
20080129000712008012900071NE  2008       1          29         CA071022004      220071018G7320                SWITCH                                  SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                              HMU             MALFUNCTIONED   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA  CGSGH1275 1275                                                      (CAN) DURING GROUND RUN THE FORCED IDLE FUNCTION OF THE TWIST GRIP WAS BEING TESTED WHEN IT WAS OBSERVED TO NOT ACCELERATE BACK TO FLIGHT IDLE WHEN RETURNED TO THE (VOL) POSITION. THIS FUNCTION IS USED TO SIMULATE ENGINE FAILURE DURING PRACTICE AUTOROTATION. SUCCESSIVE ATTEMPTS OF ROLLING THE THROTTLE FROM (VOL) TO (MIN) TO (VOL) PRODUCED ERRATIC RESULTS, THE ENGINE EITHER STAGNATED AT IDLE NG OR WAS SLOW TO RESPOND BACK TO FLIGHT IDLE, (NO ERROR CODES WERE RECORDED ON THE VEMD). THE FORCED IDLE MICRO SWITCH WAS TESTED IAW MFG ALERT SB NR 05.00.49, NO ANOMALIES WERE FOUND. THE SWITCH IN QUESTION PN DHS772-400.30 WAS REPLACED AS A TROUBLESHOOTING MEASURE. MFG MANDATORY SB A292 73 2814, INSPECTION AND LUBRICATION1G71 3U3  U  H9EU    E00054EN             
20080129000722008012900072SW  2008       1          29         CA071022005      120071018G32207500761         BOLT                                    GULSTM690TP 695A        7630519SW  GARRTTTPE331TPE33110    01514WP  ROTOL R306  R306382F7   GL  DRAG BRACE      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6654 6654                                                      (CAN) DURING DISASSEMBLY OF NOSE LANDING GEAR FOR ITS 5 YEAR INSPECTION/OVERHAUL, BOLT P/N 750076-1 OF THE NOSE LANDING GEAR DRAG BRACE-NOSE LANDING GEAR STRUT WAS FOUND BENT WITH VISIBLE CRACK. CRACK WAS CONFIRMED BY NDT(LPI AND MPI). THIS WAS THE AIRCRAFTS FIRST OVERHAUL OF ITS LANDING GEAR SINCE COMPANY PURCHASED AIRCRAFT 2 YEARS AGO. RECORDS CHECK INDICATED MINIMAL PARTS REPLACEMENT DURING PREVIOUS 5 YEAR OVERHAULS (TC NR 20071022005)                                                                                                                                                                                                                                                                                     1H72 4T4  T  2A4     E4WE    6  CP8EU     
20080129000732008012900073EU  2008       1          29         CA071022006      120071003G63206894171         GEARBOX                                 BOLKMS105   BO105S      5626006EU  ALLSN 250C  250C20B     03013GL                              NR1 ENGINE      MAKING METAL    W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       6479 3017                                                      (CAN) APPROXIMATELY 5 MILES FROM AIRPORT, MAGI NR1 LIGHT ILLUMINATED. PULSED OFF AND 2 MINUTES LATER LIGHT ILLUMINATED AGAIN. AN EMERGENCY LANDING WAS CARRIED OUT. BOTH NR1 AND NR2 MAGNETIC PLUGS CHECKED AND FOUND CONTAMINATED WITH METAL. THE GEARBOX WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TIC NR 20071022006)                                                                                                                                                                                                                                                                                                                                                                                                              1G72 3U3  U  H3EU    E4CE                 
20080131000522008013100052WP  2008       1          31         CA071022007      120070909G6310C0183           CLUTCH                                  ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              MAIN ROTOR      SLIPPED         W      A   UNSCHED LANDING                                                                                 L  NO TEST                                                                       CLCLIMB          1                      CA       1864 1864                                                      (CAN) CLUTCH REMOVED DUE TO PROBLEMS AT HIGH POWER SETTINGS. POSSIBLE CLUTCH SLIPPAGE. (TC NR 20071022007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 3O3  O  H11NM   1E4                  
20080131000532008013100053NE  2008       1          31         CA071022008      220071009G732225766304        ARM                                     ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL CONTROL    BINDING         W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA       1470 1470                                                      (CAN) INTERMITTENT ROTOR DROOP. FOUND BINDING ARM ON FUEL CONTROL CAUSING ERRATIC GOVERNOR OPERATION. (TC NR 20071022008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3O3  O  H11NM   1E4                  
20080131000552008013100055WP  2008       1          31         CA071022009      120070912G2913                LINE                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              HYD PUMP        LEAKING         W      E   ENGINE SHUTDOWN                                                                                 K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA       301  301   0814                                                (CAN) PUMP REPLACED DURING TROUBLESHOOTING SMALL LEAK AT SPLIT LINE ON PUMP. (TC NR 20071022009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3O3  O  H11NM   1E4                  
20080131000572008013100057WP  2008       1          31         CA071022010      120070912G2916D2112           RESERVOIR                               ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              HYD SYSTEM      VENTING         W      E   ENGINE SHUTDOWN                                                                                 K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA       362  362                                                       (CAN) HYDRAULIC RESERVOIR VENTING. (TC NR 20071022010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3O3  O  H11NM   1E4                  
20080131000592008013100059EA  2008       1          31         CA071022011      220071019G7200                ENGINE                                  BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  RIGHT           MAKING METAL    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            DEDESCENT        1                      CA            1765                          PCE51107                    (CAN) RT ENGINE CHIP DETECTOR LIGHT CAME ON IN FLIGHT SO WE SHUTDOWN THE RT ENGINE.  ENGINE BEING REMOVED AND SENT TO ENGINE O/H FACILITY FOR REPAIR. LOANER ENGINE TO BE INSTALLED. (TC NR 20071022011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T4  T  A14CE   E4EA    5  CSTC      
20071105001202007110500120GL  2007       11         5          CA071022012      120071022G5511C2TP57          SPAR                                    DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD22D   22D30       NE  STAB            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4200                                                           (CAN) STAB SPAR FOUND CRACKED IAW AWD CF-1991-42R1 S.B 2/47. INSPECTED IAW PEN REQUIREMENTS, SPAR CRACKED ABOVE BOTH FWD ATTACH BRACKETS. ALL SPAR MODS C/W 4200HRS AGO ALONG WITH A NEW VIKING SPAR. (1992). CRACKS ABOUT .7500 INCH LENGTH RUNNING HORIZONTALLY .2500 ABOVE TOP ATTACH BOLTS, NOT IN RADIUS OF SPAR. VIKING NOTIFIED OF CRACKS IAW SB. (TC NR 20071022012)                                                                                                                                                                                                                                                                                                                                                                    1H71 3R3  RRCA806    5E1     5  CP736     
20080306001992008030600199SW  2008       3          6          CA071023001      120071022G7931                OIL SYSTEM                              BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              ENGINE          LOW PRESSURE    W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          CAE821945F                  (CAN) LOSS OF ENGINE OIL PRESSURE IN FLIGHT. ENGINE WILL BE REMOVED AND SENT FOR INVESTIGATION. (TC NR 20071023001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U3  U  H2SW    E4CE                 
20080129000742008012900074SW  2008       1          29         CA071023002      120071022G6230206040078103    NUT             BELL                    BELL  206   206L4       1182110SW  ALLSN 250C  250C30P     03013GL                              MAST ASSY       LOOSE           W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       620                                                            (CAN) WHILE INVESTIGATING MAST BEARING PLAY. UNABLE TO REMOVE NUT (BEARING TORQUED). MAST ASSY SENT TO MFG FOR INVESTIGATION. NEW MAST ASSY PROVIDED BY MFG (TC NR 20071023002).                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3U3  UNCH2SW    E1GL                 
20080129000752008012900075CE  2008       1          29         CA071023003      120071015G27501013800005      CABLE                                   BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  LT FLAP DRIVE   SHEARED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       6577                                                           (CAN) ON APPROACH , PILOTS SELECTED APPROACH FLAP. FLAPS STOPPED MOVING JUST PRIOR TO 17 DEGREES APPROACH FLAP POSITION. THE FLAP ASYMMETRY SWITCH WAS ACTIVATED. UPON INSPECTION THE LT OB FLAP DRIVE CABLE WAS CEASED. THE FLAP DRIVE CABLE WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT. FURTHER INSPECTION OF THE CABLE REVEALED IT WAS SHEARED AT APPROXIMATELY 85 INCHES OB OF FLAP MOTOR AND TRANSMISSION ASSEMBLY. EVIDENCE OF CORROSION AND MOISTURE WERE FOUND IN THE FLAP DRIVE SHEATHING AND CABLE WHICH LIKELY CONTRIBUTED TO THE CABLE FAILURE. (TC NR 20071023003)                                                                                                                                                           2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20080129000762008012900076SW  2008       1          29         CA071023004      120071022G6230206040078103    NUT             BELL                    BELL  206   206L4       1182110SW  ALLSN 250C  250C30P     03013GL                              MAST BEARING    FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       620        52351                                               (CAN) WHILE INVESTIGATION MAST BEARING PLAY, UNABLE TO REMOVE NUT (BEARING TORQUE). MAST ASSEMBLY SENT TO MFG FOR INVESTIGATION. NEW MAST ASSEMBLY PROVIDED BY MFG. (TC NR 20071023004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  UNCH2SW    E1GL                 
20080129000772008012900077SW  2008       1          29         CA071023005      120071022G7931                OIL SYSTEM                              BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              ENGINE          LOW PRESSURE    W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          CAE821945F                  (CAN) LOSS OF ENGINE OIL PRESSURE IN FLIGHT. ENGINE WILL BE REMOVED AND SENT FOR INVESTIGATION. (TC NR 20071023005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U3  U  H2SW    E4CE                 
20080129000782008012900078EU  2008       1          29         CA071023006      120071003G63206894171         GEARBOX                                 BOLKMS105   BO105S      5626006EU  ALLSN 250C  250C20B     03013GL                              NR 1 ENGINE     MAKING METAL    W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       6473 3017                                                      (CAN) APPROXIMATELY 5 MILES FROM DESTINATION, MAG NR1 LIGHT ILLUMINATED. PULSED OFF AND 2 MINUTES LATER LIGHT BACK ON. NR1 THROTTLE ROTATED TO IDLE, CONTINUED APPROACH TO DESTINATION, CRASH TRUCK ADVISED. ON FINAL,  NR1 THROTTLE ADVANCED AND NORMAL LANDING CARRIED OUT. ENGINE SHUTDOWN AND MAINTENANCE ADVISED. UPON INSPECTION OF UPPER MAG PLUG, 7 SLIVERS OF METAL WERE FOUND AND THE LOWER PLUG WAS COVERED WITH MANY PARTICLES AND FUZZ. THE ESCAPED OIL WAS CAPTURED AND METAL PARTICLES WERE VISIBLE IN THE OIL. OIL TANK DRAINED, N1 CAP FILTER REPLACED, GEARBOX OIL FILTER INSPECTED AND SCAVEMGE LINE FLUSHED. GEARBOX REPLACE WITH OVERHAULED UNIT (TC NR 20071023006)                                                       1G72 3U3  U  H3EU    E4CE                 
20080306002002008030600200SO  2008       3          6          CA071023007      120071022G3710441CC7          PUMP                                    PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  VACUUM SYS      INOPERATIVE     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            473                                                       (CAN) WHILE PERFORMING AN COMPRESSION TEST, THE ENGINEER HEARD A SQUEAKING AS THE PROP WAS BEING ROTATED. THE SOURCE WAS INDENTIFED COMING FROM THE VACUUM PUMP. PUMP WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20071023007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080306002012008030600201SW  2008       3          6          CA071023008      120071022G6420206010743013    MECHANISM                               BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              PITCH CHANGE    WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING THE TAIL ROTOR PITCH CHANGE MECHANISM PORTION OF THE 100 HOUR INSP, THE PITCH CONTROL TUBE BUSHING AND/OR BEARING WERE FOUND WORN BEYOND LIMITS ON THE CONTROL TUBE ASSY.  AN EXHAUSTIVE CHECK OF PAPER WORK WAS CARRIED OUT FOR THE TSN AND TSO, THESE COULD NOT BE CONFIRMED. THE PITCH CHANGE MECHANISM HAS PASSED INSPECTION ON THE LAST (2) 600 HOUR INSPECTIONS. (TC NR 20071023008)                                                                                                                                                                                                                                                                                                                                         1G71 3U3  U  H2SW    E4CE                 
20080306002022008030600202EA  2008       3          6          CA071024001      120071021G2750855D10011       BPSU                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAPS        INOPERATIVE     W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) THE AC SUFFERED FROM (2) SIMILAR FLAP PROBLEMS IN A SHORT PERIOD OF TIME.  THE 1ST OCCURRENCE HAPPENED ON OCTOBER 20TH 2007. THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE AFTER TAKEOFF WHEN FLAPS WERE SELECTED UP. THE AC TURNED BACK AND LANDED SAFELY. THE CREW COMPLETED A VISUAL INSP OF THE FLAPS, THE SYS WAS RESET AND SEVERAL CYCLES COMPLETED. UPON DESTINATION, THE FAULT CODES WERE DOWNLOADED AND THE SYS CHECKED SERVICEABLE BY MAINT.  ON OCTOBER 21ST, CREW REPORTED A FLAP FAIL CAUTION MESSAGE AFTER TAKEOFF. THE EICAS SECONDARY DISPLAY FLIGHT CONTROLS PAGE WAS INDICATING LT FLAP POSITION AT 6 DEGREES AND RT AT 8 DEGREES. THE FLIGHT CREW ELECTED TO CONTINUE THE FLIGHT AND LANDED WITHOUT INCIDENT AT DESTINA2L72 4F4  FRTA21EA   E15NE                
20080306002032008030600203SW  2008       3          6          CA071024002      120071019G6310CL422501        CLUTCH          BELL                    BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              FREEWHEEL UNIT  CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA       1045       BLA20067                                            (CAN) THE A/C HAD A FREEWHEEL CHIP LIGHT AND LANDED AT MAIN BASE, AFTER DOING THE 2 MINUTE COOLDOWN THE ENGINE WAS SHUTDOWN. WHILE SPOOLING DOWN A NOISE WAS NOTICED THAT WAS NOT NORMAL. THE FREEWHEEL WAS REMOVED AND DISASSEMBLED. THE CLUTCH CAGE WAS FOUND CRACKED ON ONE SIDE AND THE INNER SHAFT HAD BRINNELLING MARKS. THESE ITEMS HAVE BEEN SCRAPPED. (TC NR 20071024002)                                                                                                                                                                                                                                                                                                                                                              1G71 3U3  U  H2SW    E4CE                 
20080129000792008012900079NE  2008       1          29         CA071024003      220071023G7314                DIAPHRAGM       LYC                     ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL PUMP       TORN            W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1215 1215  3803                                                (CAN) FUEL PUMP CHANGED DUE TO EXTERNAL OIL LEAKAGE. THIS USER HAS HAD 14 OF THESE FUEL PUMPS FAIL OVER THE LAST 8 MONTHS. THIS WAS THE FIRST PUMP DIASSEMBLED. IT WAS QUITE EVIDENT THAT THE UPPER DIAPHRAM HAD RUPTURED. THE SIDE OF UPPER DIAPHRAM MATERIAL EXPOSED TO THE ENGINE OIL SHOWED A DEFINITE INDICATION OF DETERIORATION AND THE RUBBER MATERIAL BREAKING DOWN. WHEREAS THE MATERIAL ON THE FUEL SIDE SHOWS NO DETERIORATION, EXCEPT WHERE THE DIAPHRAM HAD TORN. THIS LEADS US TO WONDER IF THE FUEL COMPATIBLE DIAPHRAM MATERIAL IS NOT COMPATIBLE WITH THE W80 ENGINE OIL USED. (TC NR 20071024003)                                                                                                                            1G71 3O3  O  H11NM   1E4                  
20080129000802008012900080NM  2008       1          29         CA071024004      120071023G291082920010265     LINE                                    DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  SELECTOR VALVE  SEVERED         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) THE NR 2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED APPROXIMATELY 27 NAUTICAL MILES AFTER TAKEOFF. SHORLTY FOLLOWING THIS, THE NR2 SYSTEM HYDRAULIC FLUID DEPLETED. THE CREW CARRIED OUT THE APPLICABLE QRH PROCEDURES AND RETURNED TO BASE. MAINTENANCE FOUND A SEVERED HYDRAULIC TUBE AT THE LANDING GEAR SELECTOR VALVE. THE HYDRAULIC TUBE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20071024004)                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080129000812008012900081SW  2008       1          29         CA071024005      120071023G673041103750017     SERVO                                   BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              HYDRAULIC SYS   WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1695                                                           (CAN) PLAY NOTED IN CYCLIC CONTROL. ONCE INVESTIGATED THE PILOT VALVE LINKAGE ON RT CYCLIC SERVO FOUND WORN BEYOND LIMITS. (TC NR 20071024005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3U3  U  H2SW    E4CE                 
20080129000822008012900082GL  2008       1          29         CA071024006      120071004G2823PV332010        SHUTOFF VALVE                           DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  FUEL SYSTEM     LEAKING         W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA       10229                                                          (CAN) STRONG FUEL ODOR IN COCKPIT. INVESTIGATED AND FOUND FUEL SHUTOFF VALVE WAS LEAKING. OVERHAULED PN PV3320-10 INSTALLED AND SYSTEM CHECKED FOR LEAKS. AIRCRAFT SERVICEABLE. (TC NR 20071024006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3R3  RRCA806    5E1     5  CP206     
20080129000832008012900083NE  2008       1          29         CA071024007      120071022G334050316           BEACON                                  SKRSKYS92   S92A               NE  GE    CT7TS CT78A       30136NE                                              FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) DURING FERRY FLIGHT (CRASH POSITION INDICATOR) DEPARTED AIRCRAFT FOR NO APPARENT REASON. UNIT DID NOT TRANSMIT.  THE DEPLOYABLE BEACON WAS INSTALLED IAW MFG DWG NR 92604-40331. (TC NR 20071024007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2G72 4U4  U  R00024BOE8NE                 
20080129000842008012900084NE  2008       1          29         CA071024008      220071004G7200                ENGINE                                  BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE                                              FAILED          W      E   ENGINE SHUTDOWN                                                                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CRCRUISE         1                      CA                                          93447                       (CAN) AT FL260, ITT INCREASED TO NEAR MAXIMUM. POWER WAS REDUCED TO FLIGHT IDLE HOWEVER ITT REMAINED HIGH. HEAVY SMOKE WAS OBSERVED COMING FROM EXHAUST. CREW ELECTED TO SHUTDOWN ENGINE AND PERFORM SINGLE ENGINE LANDING. POST FLIGHT INSPECTION REVEALED OIL DRIPPING FROM EXHAUST AND SEIZED PROPELLER SHAFT.   MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.                                                                                                                                                                                                                                                                                                                                                   1L72 4T4  T  A24CE   E4EA                 
20080129000852008012900085EU  2008       1          29         CA071024009      120071013G3246MS2125006038    TIE BOLT                                AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  MLG WHEEL       BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            398   CAA10                                               (CAN) MAINTENANCE CREWS NOTED A BROKEN MAIN WHEEL TIE BOLT. THE MAIN WHEEL ASSEMBLY AND BRAKE ASSEMBLY WERE REPLACED. (TC NR 20071024009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080129000862008012900086CE  2008       1          29         CA071024010      120071021G321050810323        TORQUE KNEE                             BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  MCAULY4HFR344HFR34C762  NE  LANDING GEAR    CRACKED         W      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              LDLANDING        1                      CA                                                                      (CAN) AFTER LANDING, UPON DECELERATING THROUGH 60 KIAS THE AIRCRAFT BEGAN TO VIOLENTLY SHAKE, SHUDDER AND APPEAR TO SKIP WHILE VEERING TOWARD THE LT SIDE OF THE RUNWAY. CONTROL WAS MAINTAINED AND THE AIRCRAFT WAS BROUGHT TO A SLOW TAXI AT WHICH TIME THE CONDITIONS CEASED. UPON EXAMINATION OF THE AIRCRAFT, IT WAS DISCOVERED THAT THE LT MAIN GEAR LOWER TORQUE KNEE HAD FAILED. THE TORQUE KNEE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THIS PART,4 YEARS SINCE INSPECTION, DUE EVERY 8000 LANDING OR 6 YEARS.  (TC NR 20071024010)                                                                                                                                                                                         1L72 3T4  T  A14CE   E4EA    6  C3PNE     
20080129000872008012900087NM  2008       1          29         CA071024011      120070921G7931                OIL SYSTEM                              DHAV  DHC8  DHC8202     2809007NM  PWA   120   PW123D      52152NE                              ENGINE          LOW PRESSURE    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                          AG0054                      (CAN) DURING CLIMB, LOW OIL PRESSURE WARNING ANNUNCIATED. PILOT INITIATED SHUTDOWN PROCEDURES AND SINGLE ENGINE LANDING. ENGINE WAS REMOVED FOR INVESTIGATION.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071024011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRTA13NM   E20NE                
20080129000902008012900090EU  2008       1          29         CA071025001      120071023G6200V40G3911AA      SPRING                                  BOLKMS105   BO105S      5626006EU  ALLSN 250C  250C20B     03013GL                              EJECTOR         MISMANUFACTURED W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       20                                                             (CAN) POOR METAL COMPOSITION IN PART CAUSES CRACKING. THESE PARTS WILL CRACK WITHOUT BEING SUBJECT TO FLIGHT. ONE BATCH HAS BEEN DISPOSED OF AND THE NEXT BATCH HAS THE SAME ISSUE. THE MFG HAS BEEN NOTIFIED. REF MBB-BO-105 IPC 60-00-00 FIG 8 ITEM NR 440. (TC NR 20071025001)                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G72 3U3  U  H3EU    E4CE                 
20080129000912008012900091EA  2008       1          29         CA071025002      120071020G2750855D1009        BPSU                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAPS        FAILED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       1298612986                                                     (CAN) DURING APPROACH, AIRCRAFT RECEIVED A FLAPS FAIL MESSAGE WITH FLAPS AT 30 DEGREES. FLAPS WERE NOT RESELECTED.  RECTIFICATION: RT BRAKE POSITION SENSOR UNIT (BPSU) FOUND TO BE AT FAULT. BPSU REPLACED AND RIGGED IAW AMM. (TC NR 20071025002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA21EA   E15NE                
20080129000942008012900094NE  2008       1          29         CA071025003      220071004G7261PT08001A01      OIL CAP                                 DHAV  DHC8  DHC8*              NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  OIL FILLER      MISINSTALLED    W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         WKJINADEQUATE Q C            FLUID LOSS                WARNING INDICATION        CLCLIMB          1                      CA                                          120848                      (CAN) DURING CLIMB, THE LOW OIL PRESSURE WARNING ILLUMINATED. THE CREW ELECTED TO PERFORM AN INFLIGHT SHUTDOWN OF THE ENGINE AND RETURN TO POINT OF DEPARTURE.  GROUND INSPECTION REVEALED THAT THE OIL FILLER CAP HAD BEEN IMPROPERLY INSTALLED, AND THAT THE SEALING FUNCTION OF THE POST-SB 21150 FILLER NECK CHECK VALVE HAD BEEN RENDERED INEFFECTIVE THROUGH FLATTENING OF THE O-RING AND MECHANICAL DAMAGE. (TC NR 20071025003)                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080129000972008012900097EU  2008       1          29         CA071025004      120071015G2820                HOSE                                    EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF3410E5A1  30022NE                              FUEL SYSTEM     LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       4425                                                           (CAN) APU FUEL FEED LINE LEAK WITHIN THE HYDRAULIC SERVICE COMPARTMENT. FUEL LEAKS FROM HOSE CORE AND SOAKS FABRIC BRAID. LEAK IS IN THE AREA OF SECOND AND THIRD SUPPORTING CLAMPS. SUGGEST THAT THIS MAY BE A MATERIAL SPECIFICATION PROBLEM. SUPPORT CLAMPS ARE INTACT AND DO NOT APPEAR TO BE CHAFFING LINE. (TC NR 20071025004)                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA57NM   E00070EN             
20080129001002008012900100EA  2008       1          29         CA071025005      120071006G7931                O-RING                                  DHAV  DHC6  DHC6300     2802606EA  PWA   PW120 PW123            NE                              OIL PRESSURE    FAILED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          123357                      (CAN) PILOT OBSERVED A SUDDEN DROP IN OIL PRESSURE AND ELECTED TO PERFORM AN IN FLIGHT SHUTDOWN. FLIGHT WAS DIVERTED.  GROUND INSPECTION REVEALED A DEFECTIVE O-RING ASSOCIATED WITH THE PCU (PROPELLOR CONTROL UNIT) ASSEMBLY. (TC NR 20071025005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H72 3T4  TRTA9EA    E20NE                
20080129001072008012900107NE  2008       1          29         CA071025006      220071011G7200                ENGINE                                  BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE                                              MAKING METAL    W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                          93724                       (CAN) 15 MINUTES INTO FLIGHT, THE ENGINE CEASED OPERATION AND SIMUTANEOUSLY ILLUMINATED THE CHIP DETECTOR INDICATOR. THE CHIP DETECTOR CIRCUIT BREAKER WAS THEN REPORTED TO HAVE `POPPED`. AIRCRAFT RETURNED TO POINT OF DEPARTURE.  POST FLIGHT INSPECTION REVEALED SUBSTANTIAL INTERNAL ENGINE DISTRESS. THE CHIP DETECTOR HAD `POPPED` ON THE PREVIOUS FLIGHT AND HAD BEEN RESET.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.                                                                                                                                                                                                                                                                                 1L72 4T4  T  A24CE   E4EA                 
20080129001082008012900108CE  2008       1          29         CA071025007      120071024G5753                ROLLER          BEECH                   BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCE4N HCE4N3      NE  RT TE FLAP      SEIZED          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) ON APPROACH WHEN FLAPS WERE SELECTED DOWN, THE RT WING BECAME HEAVY. AILERON CONTROL WAS REDUCED AND FELT DIFFERENT THAN NORMAL. THE PILOT LANDED WITHOUT FURTHER INCIDENT AND SELECTED FLAPS UP. THE FLAPS DID NOT MOVE WHEN SELECTED UP, SPLIT-FLAP SAFETY MECHANISM WAS ACTUATED.  THE RT OB FLAP, IB AFT ROLLER APPEARS TO HAVE SEIZED AND TORE OUT OF THE FLAP BRACKET. WHEN THE AMO DRILLED APART THE FLAP FOR REPAIR, THEY NOTED THAT THE BRACKET WAS WORN THIN FROM THE ROLLER. THIS, WOULD ONLY BE VISIBLE ONCE THE ROLLER WAS REMOVED.  THE MM DOES NOT SPECIFICALLY REQUIRE REMOVAL OF FLAPS OR ROLLERS FOR INSPECTION OR LUBRICATION. A REGULAR REMOVAL OF ALL FLAPS TO INSPECT CONDITION OF ROLLERS AND FLAP BRACKETS WOULD L1L72 4T4  T  A24CE   E4EA    5  CP10NE    
20080129001092008012900109NM  2008       1          29         CA071025008      120071022G7931                OIL SYSTEM                              DHAV  DHC8  DHC8*              NM  PWC   150   PW150A           EA                              ENGINE          LOW PRESSURE    W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                          FA0060                      (CAN) DURING CRUISE, THE LOW OIL PRESSURE WARNING WAS ACTIVATED FOLLOWED BY SURGING AND UNCOMMANDED SHUTDOWN. THE FLIGHT WAS DIVERTED.   MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071025008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA13NM   E00062EN             
20080129001102008012900110NE  2008       1          29         CA071025009      220071020G7250                ACCESSORY UNIT                          DHAV  DHC8  DHC8201     2809001NM  PWA   PW120 PW123            NE                              ENGINE          DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA                                          123012                      (CAN) THE ENGINE WAS REPORTED TO HAVE HAD AN IFSD. GROUND INSPECTION REVEALED THE POWER TURBINES DID NOT TURN FREELY AND THE ACCESSORY DRIVE WAS DAMAGED.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071025009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA13NM   E20NE                
20080129001112008012900111NM  2008       1          29         CA071025010      120071015G3242                CABLE                                   EMB   ERJ170ERJ170200SU NIR    NM  GE    CF34  CF348E5A1   30062NE                              PARKING BRAKE   BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4928                                                           (CAN) AFTER PUSHBACK, PARKING BRAKE CABLE BROKE. EMERGENCY PARKING BRAKE CABLE ASSY REPLACED IAW AMM 32-44-03 (TC NR 20071025010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA56NM   E00063EN             
20080129001122008012900112EA  2008       1          29         CA071025011      120071017G541022850080        COWLING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              THRUST REVERSER LOOSE           W      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           LDLANDING        1                      CA       12626                                                          (CAN) ACTUALLY WE HAVE A AOG A/C AT PRG. DURING THRUST REVERSER OPERATING AFTER TOUCHDOWN AT PRG WERE LOSING THE UPPER AND LOWER RT ENGINE COWLINGS. ONE OF THE COWLINGS HIT THE A/C AT FS 700 IN BETWEEN STR 5 TO 7 AND DAMAGED THE FUSELAGE AND ALSO THE FRAME FS STN 700.  (TC NR 20071025011)                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA21EA   E15NE                
20080129001132008012900113SW  2008       1          29         CA071026001      120071012G2435150SG117Q       STARTER GEN                             BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                                              DEFECTIVE       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4132 251                                                       (CAN) DURING SHUTDOWN, IT WAS NOTED THAT A NOISE WAS COMING FROM THE ENGINE BAY AREA. FURTHER INVESTIGATION NOTED THE STARTER GEN REQUIRED TO BE REPLACED. STARTER GEN WAS REPLACED FOR NO FURTHER DEFECTS. (TC NR 20071026001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3U3  U  H2SW    E4CE                 
20080129001142008012900114EA  2008       1          29         CA071026002      120071024G5711215003268       SPAR CAP                                CNDAIRCL215 CL2151A10   1900320EA  PWA   R1340 CWASP       52016NE  HAMSTD43E   43E60       NE  WS 50.0         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4279                                                           (CAN) WHILE PERFORMING AD 92-26R1 IAW SB 215-A454 REV 3, NO DEFECTS WERE FOUND IAW OUTLINED ULTRASONIC INSPECTION PROCEDURES. THE NDI TECH NOTED THAT HE WAS PICKING UP WHAT HE THOUGHT WAS A SUSPECTED CRACK OUTSIDE THE AREA OUTLINED IN THE SB AND PROCEEDED TO ENQUIRE ABOUT THE SURROUNDING STRUCTURE WITH A COMPANY AME. FS 434.8 REAR SPAR WS 50.0 THE SUSPECTED CRACK ON THE ULTRASOUND WAS SHOWN TO THE AME AND A LINEAR MEASUREMENT WAS MADE AS TO THE SCALE ON THE INSTRUMENT. IT WAS BELIEVED THAT THE CRACK WOULD BE AT APPROXIMATELY LT WING WS 50.0 IN LINE WITH THE REAR OUTER VERTICAL PICK-UP ANGLE TO REAR SPAR CAP ATTACHMENT VIA LOCK FASTENER. NR 2 FUEL CELL AND FUEL BAY LINERS WERE REMOVED AND A CRACK IN THE PAINT PR2H72 4R3  RRTA14EA   ATC14   6  CP871     
20080129001162008012900116SW  2008       1          29         CA071026003      120071025G6710204001363015    CYCLIC STICK                            BELL  212   212         1181420SW  PWA   PT6T  PT6T3       52045EA                                              CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       24962                                                          (CAN) PILOTS CYCLIC STICK DISASSEMBLED FOR PAINT AND REFURBISH. STEEL RING PN 204-001-369-001 IS RIVETED ON THE CYCLIC STICK. THE STEEL RING IS USED FOR APPLICATION OF FRICTION. THE STEEL RING WAS REMOVED AND EXTREME CORROSION PITTING WAS FOUND IN THE CYCLIC STICK. IF THE CORROSION DEPTH COULD BE MEASURED ACCURATELY IT WOULD BE 40-50 PERCENT OF THE TUBE THICKNESS. PULLED A USED CYCLIC STICK ASSY OUT OF OUR STOCK INVENTORY DISASSEMBLED IT ONLY TO FIND IT CORRODED AS WELL NOT QUITE AS BAD BUT BEYOND SERVICEABLE. FINDING 2 HAS PROMPTED US TO CONSIDER THIS TO BE MORE THAN A ONE OF ISSUE CORROSION ISSUE. (TC NR 20071026003)                                                                                              1G71 4U4  U  H4SW    E22EA                
20080129001182008012900118WP  2008       1          29         CA071026004      120071023G3251                ACTUATOR                                CVAC  440   440         2422902WP  ALLSN 501D  501D13D     03004GL  ALLSN A6441 A6441FN606  GL  NLG STEERING    MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA            2882                                                      (CAN) DURING APPROACH WHEN LANDING GEARS SELECTED DOWN, THE LANDING GEARS UNLOCK LIGHT CAME ON, HOWEVER, NO NOSE WHEEL DOWN LIGHT CAME ON. THE CREW CONFIRMED VISUALLY GEAR NOT DOWN. AFTER A FEW CYCLES GEAR UP AND GEAR DOWN AND EMERGENCY UPLATCH RELEASE TO NO AVAIL. AFTER TURNING NOSE GEAR STEERING THE NOSE GEAR CAME DOWN AND LOCKED NORMALLY. THE NOSE GEAR STEERING ACTUATOR FOUND TO BE CREEPING TO THE RT ON ITS OWN INTERMITTENTLY. SUBSEQUENT INSPECTION FOUND THAT THE UPPER PIVOT POINT WAS WORN. STEERING ASSY REMOVED AND SENT TO OVERHAUL SHOP FOR INVESTIGATION AND OVERHAUL.                                                                                                                                              2L72 4R4  T  6A6     E282    6  CP898     
20080129001192008012900119EU  2008       1          29         CA071026005      120071016G2722793500501       ACTUATOR                                ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE73131G   29003NE                              RUDDER TRIM     FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE PERFORMING AN A-CHECK, THE RUDDER TRIM ACTUATOR (PN: 793500-501) FAILED THE FREE PLAY CHECK IAW MM 5-20-06 PARA: 1.F.(4) AND MM 27-20-00 PAGE 503 PARA: 4.A. A NEW RUDDER TRIM LOWER ACTUATOR (PN: 793500-501) (ALTERNATE PN:1092AS100-3) WAS ORDERED. WHEN RECEIVED, THE NEW ACTUATOR 8130-3 RELEASE FORM STATED THAT THE UNIT WAS OVERHAULED. THE PART HAD 3 DISCREPANCIES, BOTH ROD ENDS WERE WORN, CORRODED, SCORED, ALSO THE ELECTRICAL LEAD, CONNECTOR PLUG WAS CORRODED. THE UNIT WAS RETURNED TO VENDOR. (TC NR 20071026005)                                                                                                                                                                                                2M72 4F4  F  A2SW    E6WE                 
20080131000602008013100060SW  2008       1          31         CA071026006      120071024G62104711012050      BLADE                                   BELL  47    47G2        1181008SW  LYC   O435  VO435A1D    41516EA                              MAIN ROTOR      BROKEN          W      RA  AUTOROTATION            UNSCHED LANDING                                                         DE INFLIGHT SEPARATION       VIBRATION/BUFFET                                    APAPPROACH       1                      CA            1664                                                      (CAN) DURING NORMAL TRAINING FLIGHT, VIBRATION WAS FELT AND AUTOROTATION LANDING CARRIED OUT. UPON SHUTDOWN AND INSPECTION OF BLADES, A FIVE (5) FOOT SECTION OF BLADE COVERING WAS DISCOVERED MISSING FROM THE UNDERSIDE OF THE BLADE FROM THE TIP EXPOSING THE WOOD BLADE CORE CAUSING THE ABNORMAL VIBRATION. BLADES WERE REMOVED AND AIRCRAFT TRANSPORTED BACK TO THE MAINTENANCE FACILITY. NTSB WERE ON SITE SHORTLY AFTER AND REQUESTED THAT THE BLADES BE SHIPPED OFF FOR A DETAILED EXAMINATION. (TC NR 20071026006)                                                                                                                                                                                                                    1G71 3O3  O  H1      E279                 
20080131000612008013100061EU  2008       1          31         CA071026007      120071018G324050028053        BRAKE ASSY                              ISRAEL1124  1124        4500102EU  GARRTTTFE731TFE73131G   29003NE                              RT MLG          FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA            3                                                         (CAN) A-CHECK INSPECTION COMPLETED AT AIRCRAFT. FOLLOWING INSPECTION A TEST FLIGHT WAS COMPLETED, ON RETURN TO BASE, IT WAS NOTED THAT THE RT BRAKE WAS DRAGGING. MAINTENANCE FOUND TOP AFT GRIP AND TUBE OUT OF ADJUSTMENT. REMOVED AND RESET ASSEMBLY TO NEUTRAL POSITION, OPS CHECK BRAKE SERVICEABLE. AC DEPARTED, UPON LANDING THE PILOT NOTED THAT THE BRAKE WAS DRAGGING, AND FOUND THE RT BRAKE WAS NOT FULLY RELEASING. MAINTENANCE WAS CALLED IN, REMOVED RT BRAKE ASSEMBLY (PN: 5002805-3 S/N: S-MAR88-2), AND INSTALLED OVERHAULED BRAKE ASSEMBLY (PN: 5002805-3 S/N: OCT 85-522) PER MM 32-43-01. AIRCRAFT RETURNED TO SERVICE. UNSERVICEABLE BRAKE ASSEMBLY RETURNED TO VENDOR (TSO: 2.7 HRS, 2 LANDINGS).REQUESTING VENDER TO SUP2M72 4F4  F  A2SW    E6WE                 
20080204001562008020400156EU  2008       2          4          CA071026008      120071023G2910137311D1233     LINE                                    BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33110UG  01514WP  MCAULY4HFR344HFR34C652  NE  HYD SYSTEM      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) DURING A ROUTINE 200 HOUR AIRFRAME INSP, HYD FLUID WAS FOUND TO BE LEAKING FROM ABOVE THE BAGGAGE POD ON THE BELLY OF THE AC. THE AIRCRAFT`S IMPENDING DEPARTURE WAS CANCELLED, AND THE POD REMOVED TO INVESTIGATE.   IT WAS FOUND THAT THERE WAS A CLAMP MISSING ON THE MAIN HYD RETURN LINE, WHICH ALLOWED THE BACKSIDE OF AN ADELL CLAMP ON A HYD PRESS LINE TO CHAFF ON THE MAIN RETURN LINE. THIS CHAFFING ACTION WAS FOUND TO HAVE BREACHED THE RETURN LINE, P/N 137311D1233. THE RETURN LINE WAS REMOVED AND REPLACED WITH A SERVICEABLE LINE, ALL CLAMPS AND LINES IN THE AREA WERE INSPECTED FOR PROPER ASSEMBLY AND CHAFFING AND NO OTHER DEFECTS WERE NOTED. THE AIRCRAFT HYDRAULIC SYSTEM WAS SERVICED AND BLED AND THE AIRCRA2L72 4T4  TRTBA15CAA E4WE    6  C3PNE     
20080131000632008013100063NM  2008       1          31         CA071026009      120071026G5315147A55067       FLOORBEAM                               BOEING737   737790      13844CNNM                                                               BS 986.5        CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT CABIN BS 986.5 BEAM UPPER CAP CORRODED AT LBL24, LBL18, RBL10, RBL, RBL32, RBL28, RBL22, RBL17 REPAIRED IAW CUSTOMER EA. (TC NR 20071026009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F    RTA16WE                        
20080131000642008013100064GL  2008       1          31         CA071026010      120071026G3246C2US1285A       LINK ASSY                               DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD22D   22D30       NE  AT SKI ATTACH   CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       10                                                             (CAN) SKIS OLD SURPLUS PARTS, 0 HRS, PUT INTO SERVICE 1 YR AGO. SKIS INSPECTED TO REATTACH TO AIRCRAFT, DISASSEMBLED FOR MAINTENANCE. UPON REMOVAL OF LINK ASSY FROM SKI PIVOT ATTACHMENT, BASE OF LINK FOUND CORRODED OUT AND U/S. CORROSION WOULD HAVE ONLY BEEN APPARENT DURING FULL DISASSEMBLE OF SKI, NOT A NORMAL PRACTICE. SKIS APPEAR TO HAVE BEEN OILED IAW ENGINEERING DWG, BUT 1 PLUG SCREW IS MISSING AND ANOTHER LOSE, LIKELY CAUSE OF WATER TO ENTER LINK ASSY. (TC NR 20071026010)                                                                                                                                                                                                                                              1H71 3R3  RRCA806    5E1     5  CP736     
20080131000662008013100066NM  2008       1          31         CA071026011      120071026G5320453A26113       STRIP                                   BOEING737   737790      13844CNNM                                                               BS 847-947      CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) CORROSION ON CAP STRIP BETWEEN BS 847 AND BS 947 RT SIDE AFT CARGO REPAIRED IAW CUSTOMER EA. (TC NR 20071026011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F    RTA16WE                        
20080131000672008013100067NM  2008       1          31         CA071029002      120070815G2701MS21919WDG9     CLAMP                                   EMB   ERJ170ERJ170200SU NIR    NM  GE    CF34  CF348E5A1   30062NE                              COLUMN ROD      LOOSE           W      D   RETURN TO BLOCK                                                                                 F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA                                                                      (CAN) PRIOR TO PUSHBACK, WHEN TOE BRAKES WERE PRESSED TO RELEASE PARK BRAKE, THE CONTROL COLUMN YOKE MOVED AFT APPROX 1 INCH. REF: LOAD CELL INSTALLATION. THE CLAMP IS INSTALLED ON THE CONTROL COLUMN ROD ASSY ON THE TAPERED SECTION OF THE ROD. THE CLAMP CANNOT BE PROPERLY TIGHTENED DUE TO THE ANGLE IN THE ROD AND EVENTUALLY BECOMES LOOSE. WHEN THE CLAMP IS FREE TO MOVE ALONG THE ROD, IN CERTAIN CONDITIONS,  THE CLAMP CAN INTERFERE WITH CONTROL COLUMN MOVEMENT. MFG HAS CORRECTED THE PROBLEM ON OTHER AC, NOT ON THIS AC, THUS A MODIFICATION IS REQUIRED. (TC NR 20071029002)                                                                                                                                                2L72 4F4  FRTA56NM   E00063EN             
20080131000682008013100068NE  2008       1          31         CA071029003      220071019G8530399357          CYLINDER                                AYRES S2    S2RHGT65    0970110SO  PWA   R1340 R1340AN1    52016NE  HAMSTD23D   23D40       NE  NR 7            CRACKED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA       910  910                                                       (CAN) PILOT REPORTED FAILURE OF ENGINE TO MAINTAIN FULL POWER AT THE TAKEOFF SETTING. AIRCRAFT RETURNED TO THE RAMP. COMPRESSION TEST REVEALED CYLINDER NR 7, WAS LOW ON COMPRESSION AND LEAKING VIA A CRACK IN THE EXHAUST PORT AREA OF THE CYLINDER. THE OFFENDING CYLINDER WAS REMOVED AND AN OVERHAULED CYLINDER WAS INSTALLED. AIRCRAFT RETURNED TO FLIGHT STATUS. (TC NR 20071029003)                                                                                                                                                                                                                                                                                                                                                     1L71 3T3  RNC        5E2     6  CP719     
20080131000692008013100069SW  2008       1          31         CA071029004      120070809G6320                HOUSING                                 BELL  206   206L        1181522SW  ALLSN 250C  250C20R2         GL                              M/R TRANSMISSIONCRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                  BMC00040                                            (CAN) OIL FOUND ON TRANSMISSION DECK AFTER BRIEF DAILY INSPECTION, OIL LEAK FOUND FROM THE BOTTOM OF THE TRANSMISSION.  UPON FURTHER INVESTIGATION TRANSMISSION REMOVED AND BOTTOM CASING FOUND TO BE CRACKED AT LOWER MAST SUPPORT BRG. (TC NR 20071029004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G71 3U3  U  H2SW    E4CE                 
20080131000702008013100070CE  2008       1          31         CA071029005      120071027G324010310300        BOLT            CLEVELAND               BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCE4N HCE4N3      NE  TORQUE PLATE    MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       337                                                            (CAN) DURING MAINTENANCE ON AIRCRAFT, NR 4 MAIN TIRE WORN TO LIMITS.  DURING NR 4 MAIN WHEEL AND TIRE CHANGE, FOUND 3 OUT OF 6 BRAKE TORQUE PLATE ATTACH BOLTS MISSING AND REMAINING ATTACH BOLTS LOOSE. A LOOSE BOLT WAS FOUND LODGED IN WHEEL BETWEEN A WHEEL HALF TIE BOLT HEAD AND THE BRAKE DISC.  3 NEW BOLTS WERE INSTALLED AND ALL 6 BOLTS WERE INSTALLED AND TORQUED TO MFG SPECS. OTHER 3 BRAKE INSTALLATIONS AND 4 BRAKE INSTALLATIONS VISUALLY VERIFIED NO BOLTS MISSING.  HAVE CONTACTED MFG TO PURSUE THE USE OF DRILLED AND LOCKWIRED BOLTS. (TC NR 20071029005)                                                                                                                                                                 1L72 4T4  T  A24CE   E4EA    5  CP10NE    
20080129001202008012900120    2008       1          29         CA071029006      420071025G3197MS2524475       CIRCUIT BREAKER                         BELL  205   205B               SW  LYC   T53   T5317BLYC   41616NE                                              ODOR            W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA                                                                      (CAN) SMOKE AND ODOR IN CABIN. LANDED BACK AT PAD. (TC NR 20071029006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 4U4  U  H1SW    E17EA                
20080129001212008012900121EA  2008       1          29         CA071029007      120071029G5544DAT4864A        BEARING                                 CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  RUDDER          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       421                                                            (CAN) RUDDER BEARING FOUND DAMAGED ON  C-CHECK. THE BEARING WAS INCORPORATED BY SB ON WINTER WORK 2005-2006 AND CUMULATE 421 HOURS SINCE INSTALLATION.  A/C HOURS 2141 CYCLES 1316 DROPS 11678 (TC NR 20071029007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20080129001222008012900122EU  2008       1          29         CA071029008      120071026G5320120A6050        FRAME                                   GROB  120   G120A       1660208EU  LYC   O540  AEIO540D4D5      EA  HARTZLHCC3Y HCC3YR      GL  OIL COOLER      DAMAGED         W      H   DEACTIVATE SYST/CIRCUITS                                                                        J  WARNING INDICATION                                                            CRCRUISE         1                      CA       659                                                            (CAN) FLIGHT DEPARTED AT 1344 FOR AT TRAINING FLIGHT TO THE WEST PRACTICE AREA. APPROXIMATELY 5 MINUTES OUT WHILE CRUISING AT 4000 FT AND 120 KTS THE INSTRUCTOR OBSERVED (ALT OFF) ANNUNCIATION. A SCAN OF INTEGRATED ENGINE DISPLAY REVEALED (AMPS) TO BE READING -24A AND VOLTAGE READING 24.7V. THE INSTRUCTOR THEN OBSERVED (VOLT) ANNUNCIATION. THE INSTRUCTOR FOLLOWED EMERGENCY CHECKLIST AND SELECTED (ALTERNATOR) SWITCH OFF AND REMOVED NON-ESSENTIAL ELECTRICAL LOADS. THIS RESULTED IN A REDUCED NEGATIVE LOAD OF -9A. INSTRUCTOR THEN BRIEFLY CONFIRMED FAULT BY RETRYING (ALTERNATOR) SWITCH ON - LOAD WENT BACK TO -24A , (ALTERNATOR) SWITCH WAS IMMEDIATELY SELECTED OFF AGAIN. THE INSTRUCTOR MADE (PAN) CALL AND RETURNED . 1L71 3O3  ORTA49CE   1E4     5  CP25EA    
20080129001232008012900123NM  2008       1          29         CA071029009      120071027G3220273A45141       SHAFT                                   BOEING737   737*               NM  CFMINTCFM567CFM567B22   13802NE                              NLG             CONTAMINATED    W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       6885                                                           (CAN) THE FLIGHT CREW REPORTED THAT AFTER TAKEOFF, (THE NOSE GEAR INDICATES DOWN IN THE UP POSITION. WHEN GEAR HANDLE PUT IN THE OFF POSITION, THE NOSE GEAR CAME DOWN.) THE FLIGHT RETURNED TO BASE AND MADE AN UNEVENTFUL LANDING.  MANUAL EXTENSION ARM FOUND IN THE EXTEND POSITION AND WOULD NOT RELEASE. PAINT FOUND ON THE P/N 273A4514-1 SHAFT. PAINT REMOVED, MICARTA BUSHINGS CLEANED AND SHAFT REINSTALLED IAW OHM 32-35-05 AND SOPM 20-50-01. NOSE GEAR RETRACT TEST C/W IAW AMM 32-33-00 WITH NO FAULT FOUND.  HAVE ADVISED MFG OF THE EVENT AND THE REPORT OF PAINT FOUND ON THE SHAFT ASSEMBLY. (TC NR 20071029009)                                                                                                              2L72 4F4  FRTA16WE   E00055EN             
20080129001242008012900124EA  2008       1          29         CA071029010      120071028G282163E951          HOUSING         GRIMES                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              FUEL FILTER     DAMAGED         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA                  GWD16759                                            (CAN) JUST BEFORE PUSHBACK, THE RAMP CREW OBSERVED A FUEL LEAK COMING FROM THE APU AREA. CAPTAIN PERFORMED RAPID PASSENGER DEPLANEMENT WITH EMERGENCY CREWS ON STAND-BY.  MAINTENANCE FOUND THE FUEL LEAK COMING FROM THE NR 2 ENGINE- FUEL FILTER HOUSING, BY THE FUEL FILTER IMPENDING BYPASS PLUG. IN THIS AREA, THE FUEL FILTER HOUSING AND THE SQUARE PLUG WERE FOUND GROOVED AND THE SQUARE PLUG SEAL WAS FOUND DAMAGED AS WELL. MAINTENANCE REPLACED THE ALL FUEL FILTER ASSY. (TC NR 20071029010)                                                                                                                                                                                                                                       2L72 4F4  FRTA21EA   E15NE                
20080129001252008012900125CE  2008       1          29         CA071029011      120071027G2710                CONTROL CABLE                           BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  AILERONS        CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) GRINDING NOISE UNDER PILOT FLOOR WHEN AILERONS ARE MOVED. CONTROL CABLE FOUND CHAFING ON STEEL BRAIDED NITROGEN LINE. APPROX 3 INCH DEFLECTION OF CONTROL CABLE CAUSED, DUE TO INCORRECT ROUTING OF NITROGEN LINE. NITROGEN PRESSURE LINE REROUTED.  AILERON CABLE HAS 1 BROKEN STRAND WITHIN ACCEPTABLE LIMITS IAW AMM CH20-04-00-201 (TC NR 20071029011).                                                                                                                                                                                                                                                                                                                                                                               1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20080129001272008012900127SW  2008       1          29         CA071030001      120071024G2915204076437003    CHECK VALVE                             BELL  412   412EP       1182205SW                                                               HYD SYSTEM      OBSTRUCTED      W      C   ABORTED TAKEOFF                                                                                 F  FLT CONT AFFECTED                                                             TOTAKEOFF        1                      CA       4                                                              (CAN) DURING GROUND RUN, FIRST START OF THE DAY, BOTH HYDRAULIC SYSTEMS NR 1 AND NR 2 INDICATED GOOD PRESSURE AND BOTH HYDRAULIC CAUTIONS WERE EXTINGUISHED. THE FORCE TO DISPLACE PEDALS WAS NOTED TO BE ABNORMALLY HIGH. TO CONFIRM SYSTEM NR 1 WAS FUNCTIONING CORRECTLY, SYSTEM NR 2 WAS SELECTED OFF. A TOTAL LOSS OF HYDRAULICS WAS ENCOUNTERED TO BOTH CYCLIC AND COLLECTIVE. THE AIRCRAFT WAS IMMEDIATELY SHUTDOWN.   DURING INVESTIGATION, FOD WAS FOUND OBSTRUCTING THE CHECK VALVE, ORIGIN OF FOD IS UNKNOWN AND UNDER INVESTIGATION. (TC NR 20071030001)                                                                                                                                                                            1G72 4U      H4SW                         
20080129001282008012900128CE  2008       1          29         CA071030002      120071025G5753501600183       FLAP TRACK                              BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  TE FLAPS        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       26566                                                          (CAN) ON MAINTENANCE WALKAROUND THE RT OB FLAP HAD MORE PLAY THAN USUAL. FLAP WAS REMOVE AND THE OB FLAP TRACK WAS FOUND TO BE CRACKED ON THE REAR TIP. TRACK REPLACED AND AIRCRAFT RETURNED TO SERVICE.  (TC NR 20071030002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3T4  T  A14CE   E4EA    5  CSTC      
20080129001302008012900130GL  2008       1          29         CA071030004      220071029G72616898607         CARBON SEAL     ALLSN                   BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              NR 1            DAMAGED         W      K   NONE                                                                                            KJ FLUID LOSS                WARNING INDICATION                                  ININSP/MAINT     1                      CA       36         CAC39586                                            (CAN) DURING AN OIL LEAK WAS DISCOVERED BY THE BLEED VALVE.  NR 1 BEARING CARBON SEAL FOUND DAMAGED, THE BEARING WAS REMOVED AND UPON INSPECTION FOUND UNSERVICEABLE. THE BEARING WHEN TURNED HAD A ROUGH, COURSE FEELING TO IT. (TC NR 20071030004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3U3  U  H2SW    E4CE                 
20080129001312008012900131    2008       1          29         CA071030005      420071016G3418                CONNECTOR                               LEAR  35    35A         5170602CE  GARRTTTFE731TFE73122B   01518WP                              STALL WARNING   TRANSPOSED      W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) DURING A 300HR INSPECTION THE STALL WARNING ACCELEROMETER CHECK WAS DUE ( IAW AD 82-01-05). WHEN CHECK WAS CARRIED OUT, THE STALL WARNING SYSTEM FAILED. WHEN SYSTEM WAS TROUBLESHOT, IT WAS DISCOVERED THAT CONNECTORS BNC 3 AND BNC 4 (FORM PIN D AND PIN F RESPECTIVELY) WERE FOUND REVERSED. CONNECTORS SWITCHED BACK AND STALL WARNING SYSTEM FUNCTIONED CHECKED SERVICEABLE. SYSTEM LAST CHECKED AT A MFG SERVICE CENTER. (TC NR 20071030005)                                                                                                                                                                                                                                                                                       2L72 4F4  F  A10CE   E6WE                 
20080129001322008012900132NM  2008       1          29         CA071030006      120071030G5730112A41029       SKIN PANEL                              BOEING737   737790      13844CNNM                                                               LWS 260 & 240   CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) LT WING LWR SKIN PANEL CHAFFING DAMAGE FROM CONTACT WITH NACELLE STRUT AFT FAIRING BLADE SEAL APPROX WSTA 260, 240 REPAIRED IAW EA 5720-01337. (TC NR 20071030006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F    RTA16WE                        
20080129001342008012900134NM  2008       1          29         CA071030007      120071030G5730112A410210      SKIN PANEL                              BOEING737   737790      13844CNNM                                                               RWS 240,260     CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) RT WING LWR WING SKIN PANEL CHAFFING DAMAGE FROM CONTACT WITH NACELLE STRUT AFT FAIRING BLADE SEAL APPROX WSTA 240,262 REPAIRED IAW EA 5720-01338. (TC 20071030007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F    RTA16WE                        
20080129001352008012900135SO  2008       1          29         CA071030008      120071025G772041506           INDICATOR                               PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  OIL TEMP        ERRATIC         W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       TXTAXI/GRND HDL  1                      CA                                                                      (CAN) DURING RUN-UP, OIL TEMP INDICATOR DROPPED OFF SCALE. THEN WENT BACK TO NORMAL INDICATION. THE ERATIC OPERATION COULD BE INDUCED BY ENERGIZING DIFFERENT ELECTRICAL EQUIPMENT.  HOURS IN USE, NONE AT THIS TIME.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080129001362008012900136NE  2008       1          29         CA071030009      220071029G7314LW15473         PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL SYS        LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1460                                                           (CAN) DURING AN INSPECTION, THE ENGINEER NOTED THAT THE ENGINE DRIVEN FUEL PUMP HAD EVIDENCE OF OIL LEAKAGE AROUND THE SEAL AREA (BODY). PUMP WAS REMOVED, REPLACED AND NO FURTHER ISSUES WERE NOTED. THERE HAS BEEN MANY OF THE THESE PUMPS LATELY WITH VARIOUS HRS OF FAILURE. (TC NR 20071030009)                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3O3  O  H11NM   1E4                  
20080129001382008012900138SW  2008       1          29         CA071030010      120071030G79206899246         HOUSING                                 BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              OIL FILTER      MISMANUFACTURED W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                          CAG34008                    (CAN) DUE TO A INTERNAL CASTING DEFECT INSIDE THE OIL FILTER HOUSING, THE PRESSURE REGULATING POPPET CANNOT FULLY BOTTOM OUT WHEN INSTALLED. THIS THEN GIVES A FALSE INDICATION OF PROPER POSITION OF THE POPPET WHEN (BACKED OUT) 5.5 TURNS FOR INITIAL ADJUSTMENT FOLLOWING OVERHAUL. THE MFG WAS ADVISED AND RECOMMENDS THAT AN APPROVED FACILITY MACHINE THE INTERNAL SURFACE OF THE HOUSING TO REMOVE THE DEFECT. (TC NR 20071030010)                                                                                                                                                                                                                                                                                                      1G71 3U3  U  H2SW    E4CE                 
20080129001392008012900139NE  2008       1          29         CA071030011      220071008G7314                DIAPHRAGM       LYC                     ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL PUMP       LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       797        4105                                                (CAN) DURING INSPECTION, ENGINEER DISCOVERED OIL LEAKAGE FROM VENT. SUSPECT DAMAGED DIAPHRAGM. (TC NR 20071030011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1G71 3O3  O  H11NM   1E4                  
20080124003332008012400333GL  2008       1          24         CA071031002      120070417G71606552241         INTAKE PIPE                             CIRRUSSR    SR20        05628AJGL  CONT  O360  IO360ES          SO  HARTZLHCJ2Y BHCJ2YF1    GL  ENGINE          DETERIORATED    W      K   NONE                                                                                            E  VIBRATION/BUFFET                                                              TXTAXI/GRND HDL  1                      CA       394                                                            (CAN) INTAKE PIPE FLANGE DETERIORATED AND AIR LEAK OCCURRED. ENGINE IDLE INCREASED AND ENGINE RUNS SLIGHTLY ROUGH. INSTALLED NEW INTAKE PIPE P/N 655224-1 AND GASKET 554227 (NR 3 CYLINDER) (TC NR 20071031002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  ONTA00009CHE1CE    5  CP37EA    
20080131000922008013100092SO  2008       1          31         CA071031004      220070621G85306552241         TUBE                                    CIRRUSSR    SR20        05628AJGL  CONT  O360  IO360ES          SO  HARTZLHCJ2Y BHCJ2YF1    GL  CYLINDER INTAKE DETERIORATED    W      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              TXTAXI/GRND HDL  1                      CA       470                                                            (CAN) INTAKE TUBE AT FLANGE TO CYLINDER DETERIORATED. NEW INTAKE PIPE 655224-1 AND GASKET 554227 INSTALLED (NR 3 CYLINDER). (TC NR 20071031004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  ONTA00009CHE1CE    5  CP37EA    
20080131000952008013100095SO  2008       1          31         CA071031005      220071023G853050339001        TUBE                                    CIRRUSSR    SR20        05628AJGL  CONT  O360  IO360E      17025SO  HARTZLHCJ2Y BHCJ2YF1    GL  CYLINDER INTAKE DAMAGED         W      K   NONE                                                                                            E  VIBRATION/BUFFET                                                              TXTAXI/GRND HDL  1                      CA       623                                360074                      (CAN) INTAKE PIPE ON NR 1 CYLINDER FLANGE DAMAGED. (TC NR 20071031005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3O3  ONTA00009CHE1CE    5  CP37EA    
20080131000982008013100098EA  2008       1          31         CA071031006      120071030G5350600330061       RADOME                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              FUSELAGE        DAMAGED         W      O   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) FLIGHT ON CLIMB OUT THE CREW HEARD A LOUD BANG IN THE NOSE AND SAW A BIRD TRAVEL PAST THE COCKPIT WINDOW. ALL FLIGHT SYSTEMS WERE NORMAL AND FLIGHT CONTINUED. UPON ARRIVAL MAINTENANCE MET THE AIRCRAFT AND FOUND A HOLE IN THE RADOME AS WELL AS A DAMAGE TO THE LT FUSELAGE AFT OF PITOT HEAD. DAMAGE ASSESSMENT IS UNDER WAY AND IT WILL BE UPDATED AS SOON AS MORE INFOMATION IS AVAILABLE. (TC NR 20071031006)                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA21EA   E15NE                
20080131001012008013100101NE  2008       1          31         CA071031007      220071029G8530                CYLINDER HEAD                           DOUG  DC4   C54EDC      3021528WP  PWA   R2000 R20007M2    52023NE  HAMSTD23E   23E50       NE  FUSELAGE        CRACKED         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         EJ VIBRATION/BUFFET          WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) CRACK DISCOVERED AT SPARK PLUG HOLE, RETURNED TO BASE AND REPLACED CYLINDER AND A/C RETURNED TO SERVICE. (TC NR 20071031007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L74 4R4  R  A762    5E5     6  CP603     
20080131001122008013100112CE  2008       1          31         CA071031008      120071030G3246950476          BEARING         BEECH                   BEECH 99    B99         1154004CE  PWA   PT6   PT6A28           EA  HARTZLHCB3T HCB3TN3     GL  MAIN WHEEL      FAILED          W      A   UNSCHED LANDING                                                                                 D  INFLIGHT SEPARATION                                                           TOTAKEOFF        1                      CA                                                                      (CAN) ON TAKEOFF THE CREW NOTED THAT THEY FELT A SLIGHT VIBRATION, BUT FELT THAT IT WAS LIKELY THE RAISED RUNWAY LIGHTS. AFTER TAKEOFF THEY WERE ADVISED THAT THEY HAD LOST A TIRE. THE AIRCRAFT WAS LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT ONE OR BOTH WHEEL BEARINGS HAD FAILED. THIS ALLOWED THE WHEEL TO DEPART FROM THE AXLE. INSPECTION SHOWED NO DAMAGE TO ANY OTHER PART OF THE AIRCRAFT, INCLUDING AXLE AND BRAKE. THE WHEEL ASSY. INCLUDING BEARINGS WERE REPLACED AND THE AIRCRAFT WAS RELEASED TO SERVICE. (TC NR 20071031008)                                                                                                                                                                                             1L72 3T4  T  A14CE   E4EA    6  CP15EA    
20080131001152008013100115    2008       1          31         CA071031009      420071021G2397EH19565         WIRE HARNESS                            AIRBUSA319  A319114     3930350NM  CFMINTCFM56 CFM565A1         NE                              CABIN           BROKEN          W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      NRNOT REPORTED   1                      CA                                                                      (CAN) AN APPARENT NOTICEABLE ELECTRICAL ODOR WAS DETECTED IN VICINITY OF SEATS 19 DEF BY IN FLIGHT CREW AND PASSENGER. ODOR PERSISTED FOR APPROX 5 MIN AND STOPPED AT THE TIME WHEN INFLT VIDEO SYSTEM WAS SHUTDOWN.  FOUND BROKEN WIRE IN THE HARNESS THAT RUNS FROM UNDER SEATS 18 DEF TO UNDER THE FLOOR.  BROKEN WIRE CAPPED AND STOWED INSIDE HARNESS CONNECTOR. THIS APPEARS TO BE AN INSTALLATION ERROR.  THE WHITE WIRE APPEARS TO HAVE BEEN INSTALLED UNDER TOO MUCH TENSION, AND WAS PULLED FROM THE BACK OF THE CONNECTOR. (TC NR 20071031009)                                                                                                                                                                                       2L72 4F4  FRTA28NM   E29NE                
20080204001552008020400155CE  2008       2          4          CA071101001      120071019G3260MS21090348      SQUAT SWITCH                            CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              MLG             LOOSE           W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) ON FINAL APPROACH APPROXIMATELY 3 MILES FROM TOUCH DOWN, THE LT THRUST REVERSER (T/R) ARM AND UNLOCK LIGHTS ILLUMINATED BRIEFLY. AT APPROXIMATELY 1.5 FROM TOUCH DOWN THE LT T/R ARM, UNLOCK AND DEPLOY LIGHTS ILLUMINATED AND THE LT POWER LEVER AUTOMATICALLY MOVED TO IDLE. ALL (3) LIGHTS EXTINGUISHED BEFORE EITHER OF THE PILOTS COULD TAKE ACTION TO EMERGENCY STOW THE T/R. THE FACT THAT THE MECHANICAL T/R POWER LEVER INTERCONNECT CAUSED THE POWER LEVER TO RETARD TO IDLE INDICATES THAT THE T/R DID ACTUALLY DEPLOY AND THAT THIS WAS NOT AN ERRONEOUS ANUNNCIATOR. THE LANDING GEAR SQUAT SWITCHES SHOULD HAVE PREVENTED INADVERTENT T/R DEPLOYMENT, WITH ONLY THE T/R ARM LIGHT ILLUMINATING EVEN IN THE EVENT OF A COMMAN1L72 4F4  F  A22CE   E1NE                 
20080131001182008013100118EA  2008       1          31         CA071101002      220071031G7200                ENGINE                                  BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU                  POWER LOSS      W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                          FA0268                      (CAN) DURING FLIGHT, A LOUD NOISE WAS HEARD FOLLOWED BY A LOSS OF POWER RESULTING IN AN INFLIGHT SHUTDOWN OF THE ENGINE. POST FLIGHT EXAMINATION REVEALED SEVERE INTERNAL DAMAGE.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071101002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080319001652008031900165EU  2008       3          19         CA071101003      120071029G3246                BEARING                                 EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF3410E5A1  30022NE                              NR 4 WHEEL      SEIZED          W      D   RETURN TO BLOCK                                                                                 MJ OVER TEMP                 WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA       786                                                            (CAN) THE A/C LANDED NORMALLY, TAXIED TO THE GATE AND STOPPED SHORT OF ITS FINAL POSITION.  THE CREW REPORTED 60 PERCENT N1 REQUIRED (SINGLE ENG TAXI) TO MOVE THE AC FROM A HOLD SHORT OF THE GATE. THE GROUND CREW ARRIVING THE AC HEARD A LOT OF NOISE FROM THE RT GEAR AS IT MOVED TO THE GATE. NO OTHER FAULT INDICATIONS IN THE COCKPIT.   UPON INSP OF THE RT LANDING GEAR IT WAS IDENTIFIED THAT THE (NR 4 WHEEL WAS DRAGGING AND INTERFERING WITH BRAKE CARRIER).  FURTHER INSP FOUND THE WHEEL BRG SEIZED ON THE GEAR AXLE, WITH  NR 4 TIRE AND THE BRAKE DAMAGED.  DECOLONIZATION OF THE AXLE WAS NOTED DUE TO EXCESSIVE HEAT BUILD UP.  THE RT LANDING GEAR ASSY, BRAKE AND TIRE WAS REPLACED IAW AMM.  INVESTIGATION CONTINUES TO I2L72 4F4  FRTA57NM   E00070EN             
20080131001202008013100120GL  2008       1          31         CA071101005      220071029G721078023061        MAGNETIC SEAL                           CESSNA206   U206G       2073356CE  ALLSN 250C  250C20      03013GL  HARTZLHCC3Y HCC3YN      GL  PROP RGB        LEAKING         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  NRNOT REPORTED   1                      CA       22   22    074                                                 (CAN) ONE OF THE PILOTS NOTICED A SMALL ENGINE OIL LEAK ON BOTTOM OF ENGINE COWLING. REMOVED THE ENGINE COWLING AND FOUND LEAK ON PROP REDUCTION GEARBOX INPUT SEAL AREA. REMOVED PROP REDUCTION GEARBOX, INPUT QUILL ASSY AND REPLACED MAGNETIC SEAL. UNDER 10X MAGNIFYING GLASS, A SCRATCH AT 90 DEGREE ACROSS THE CARBON SEALING SURFACE WAS FOUND. AIRCRAFT GROUND RUN, NO LEAKS, RETURN TO SERVICE. DEFECTIVE MAGNETIC SEAL RETURN TO MFG. (TC NR 20071101005)                                                                                                                                                                                                                                                                             1H71 3O3  U  A4CE    E4CE    5  CP25EA    
20080131001222008013100122EA  2008       1          31         CA071102001      120071029G2752852D10019       ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              TE FLAPS        FAILED          W      O   OTHER                                                                                           JF WARNING INDICATION        FLT CONT AFFECTED                                   APAPPROACH       1                      CA       7986 7986                                                      (CAN) DURING APPROACH, THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WHEN THE FLAPS WERE SELECTED FROM 0 TO 8 DEGREES. THE EICAS FLIGHT CONTROL PAGE WAS INDICATING 0 DEGREE ON BOTH SIDES. THE CREW CONTINUED THE APPROACH AND COMPLETED A FLAPLESS LANDING WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED.  THE SYSTEM WAS RESET, THE FLAPS SET TO 8 DEGREES AND THE AC WAS FERRIED FOR MAINTENANCE.  ALL FLAP ACTUATORS WERE REMOVED AND SENT TO THE SHOP. THE LT NR1 FLAP ACTUATOR FAILED THE -60 DEGREES TORQUE CHECK. DECISION WAS MADE TO REPLACE ALL FLAP ACTUATORS. FLAP ACTUATORS WERE REPLACED, ADJUSTED, TESTED AND THE AIRCRAFT WAS RELEASED. A SUCCESSFUL TEST FLIGHT WAS CONDUCTED AND THE AIRCRAFT RETURNED INTO SERVICE. (TC NR 202L72 4F4  FRTA21EA   E15NE                
20080131001232008013100123CE  2008       1          31         CA071102002      120071031G2497CM358930        SWITCH                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  AVIONICS 2      OVERHEATED      W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA       4804                                                           (CAN) SHORTLY AFTER DEPARTURE THE PILOT BECAME AWARE OF A BURNING ODOR. HE NOTICED THAT THE AVIONICS 2 SWITCH WAS HOT TO TOUCH. THE PILOT RETURNED TO BASE. INVESTIGATION FOUND THAT THE AVIONICS 2 SWITCH HAD OVERHEATED TO THE POINT OF FAILURE. A NEW SWITCH P/N 7270-5-30 WAS INSTALLED. ( REF CAB97-8 ) (TC NR 20071102002)                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20080131001242008013100124SW  2008       1          31         CA071102003      120071029G6510206040272101    BOOT            BELL                    BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              DRIVE SHAFT     DETERIORATED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       21         A2000807                                            (CAN) DRIVE SHAFT WAS RECENTLY INSPECTED, GREASED AS REQUIRED AT MFG.   OLD BOOTS WERE SERVICEABLE, BUT AGE WAS NOT KNOWN SO REPLACEMENT WAS ELECTED AS A SAFETY PRECAUTION.  NEW BOOTS INSTALLED AND DRIVE SHAFT SERVICED.   21.1 HOURS AFTER REPACK GREASE LEAK WAS DETECTED BY PILOT AND DRIVE SHAFT REMOVED.   AS A SERVICEABLE DRIVE SHAFT WAS AVAILABLE THE LEAKING ONE IN QUESTION WAS (RED TAGGED).  UNSERVICEABLE DRIVE SHAFT DISASSEMBLED AND BOOT FOUND DETERIORATED, ALMOST TO A DISSOLVED STATE, RUBBER SEEMS MORE LIKE A PLASMA THEN RUBBER STATE.  BOOT INFO SKF BO201 SKF BCO-BO-7206 MFG 1/19/07. (TC NR 20071102003)                                                                                                          1G71 3U3  U  H2SW    E4CE                 
20080131001252008013100125GL  2008       1          31         CA071102004      120071031G324530200530001110  TUBE                                    DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO                              MLG TIRE        DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3                                                              (CAN) DURING A SPECIAL INSPECT TO THE MAIN AND NOSE WHEEL ASSEMBLIES, DEFECTS WERE NOTED IN THE TIRE-TUBES INSTALLED INTO BOTH MAIN AND THE NOSE WHEELS. REPORTS HAVE BEEN MADE OF TIRE-TUBES FAILING WITH VERY LOW TIME. AFTER RECEIVING THESE REPORTS AN INSPECTION WAS PERFORMED ON ALL 3 WHEEL ASSEMBLIES ON 2 AIRCRAFT ALL TIRE-TUBES INSPECTED WERE DEFECTIVE, SHOWING THE SAME DEFECTS AS REPORTED. PHOTOGRAPHS OF THE REPORTED TIRE-TUBES FAILURES ARE ATTACHED TO THIS SDR. THE TUBES INSPECTED ARE IDENTICAL IN APPEARANCE. SEVERAL TUBES P/N 5.00-5 TR 67 AND 30200530001110 HAVE BEEN FOUND WITH SIMILAR DISCREPANCIES (TC NR 20071102004)                                                                                          1L71 3O3  ONTTA4CH   E7SO                 
20080131001262008013100126EA  2008       1          31         CA071102005      220071026G8530LW167035C       ROCKER BOSS                             CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  CYLINDER HEAD   CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            145                           L2371415                    (CAN) ON CYLINDER NR 3 THE ROCKER SHAFT RT BOSS HAS BEEN FOUND BROKEN (SPLIT) IN THE MIDDLE SECTION. THE BROKEN PART/ALL AND REST JUST BESIDE THE EXHAUST VALVE. (TC NR 20071102005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1H71 3O3  ONT3A19    E223    5  NP50GL    
20080131001272008013100127CE  2008       1          31         CA071102006      120071031G32601CH25           DOWNLOCK SWITCH                         BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  MLG             INOPERATIVE     W      O   OTHER                                                                                           N  FALSE WARNING                                                                 APAPPROACH       1                      CA                                                                      (CAN) UNABLE TO GET NLG (GREEN LIGHT) ON APPROACH. RECYCLED 3 TIMES AND GREEN LIGHT OBTAINED.  NLG DRAG LINK DOWN AND LOCK SWITCH REPLACED. GEAR SWINGS COMPLETED. NO FURTHER FAULTS AT THIS TIME. (TC NR 20071102006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20080131001292008013100129SO  2008       1          31         CA071102008      120071031G5210                DOOR                                    PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL                  DEPARTED        W      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           NRNOT REPORTED   1                      CA                                                                      (CAN) UPPER DOOR ASSEMBLY DEPARTED THE AIRCRAFT WHILE IN FLIGHT, UPPER DOOR REPLACED AND DAMAGED STRUCTURE REPAIRED. THINK THE PROBLEM AROSE WITH THE FACTORY PIPER SLIDING LOCK. WE SUSPECT THAT IT WAS WORN THOUGH THERE WAS NO PRIOR INDICATION. (TC NR 20071102008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080131001302008013100130EA  2008       1          31         CA071102009      120071030G2761601R107022      ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              SPOILERON       FRACTURED       W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                  SBRJ75                                              (CAN) DURING SHORT FINAL, THE FLAPS WERE SELECTED TO 45 DEGREES AND THE AIRCRAFT ROLLED TO THE RT.  FULL AILERON TRIM AND A LITTLE BIT OF AILERON WAS REQUIRED TO KEEP THE AIRCRAFT LEVEL. THE EICAS FLIGHT CONTROL PAGE WAS REVIEWED AND THE RT SPOILERON WAS SHOWING UP. THE AIRCRAFT LANDED WITHOUT INCIDENT.  MAINTENANCE DISCOVERED THAT THE RT SPOILERON OB ACTUATOR ATTACHMENT HAS FRACTURED. THE RT SPOILERON ASSY AND BOTH ACTUATORS WERE REPLACED, ADJUSTED AND THE SYSTEM TESTED SERVICEABLE. THE AIRCRAFT WAS RELEASED AND RETURNED INTO SERVICE. (TC NR 20071102009)                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20080131001312008013100131NM  2008       1          31         CA071102010      120071017G5230                SENSOR                                  BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  CARGO DOOR      FALSE INDICATIONW      B   EMER. DESCENT                                                                                   N  FALSE WARNING                                                                 CRCRUISE         1                      CA                                                                      (CAN) AIRCRAFT WAS ALREADY UNDER MEL 52-10-05 DUE FORWARD BAGGAGE DOOR GIVES A FALSE (OPEN) INDICATION IN THE COCKPIT.  AIRCRAFT COULD FLY PRESSURIZED BUT PRESSURIZATION SYSTEM MUST BE CONTROL IN MANUAL MODE.  AIRCRAFT SUFFERED A DEPRESSURIZATION AT 20,000 FT.  ALL SYSTEM CHECK AND NO FAULT WAS FOUND IN MANUAL AND AFTER DOOR SENSOR WAS REPAIR SYSTEM WORK ALSO IN AUTO MODE.  STILL UNDER INVESTIGATION. (TC NR 20071102010)                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080131001322008013100132EA  2008       1          31         CA071102011      220071031G7200                ENGINE                                  BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  LEFT            NOISY           W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         EJ VIBRATION/BUFFET          WARNING INDICATION                                  CRCRUISE         1                      CA       2047                               PCEFA0268                   (CAN) AROUND 20000 FT, AFTER HEARING A STRANGE SOUND THAT SEEM TO COME FROM THE LT ENGINE, PILOT NOTICED THAT THE LT ENGINE SUDDENLY STOPPED BY ITSELF. PILOT WAS ABLE TO FEATHER THE PROP. EMERGENCY WAS DECLARED. A/C LANDED WITHOUT OTHER PROBLEM. NO ONE INJURED.  UNDER INVESTIGATION (TC 20071102011)                                                                                                                                                                                                                                                                                                                                                                                                                                     2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080131001332008013100133CE  2008       1          31         CA071102012      120071102G321105412024        BUSHING                                 CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  MLG             SEPARATED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4792 4792                                                      (CAN) THE MAIN GEAR LEG BUSHINGS ARE A STEEL OUTER TUBE, WITH A THICK INNER URETHANE CENTER. DURING PROGRESSIVE CARE OPERATION  NR 4, INSPECTION OF THE LT MAIN GEAR LEG REVEALED THAT THAT THE URETHANE INNER BUSHING MATERIAL HAD DEPARTED FROM THE OUTER STEEL BUSHING (P/N 0541202-4). IT HAD MOVED LOOSELY ALONG THE TUBULAR GEAR LEG TOWARDS THE CENTER OF THE AIRCRAFT. THIS ALLOWED THE TUBULAR GEAR LEG TO RATTLE ON THE INSIDE OF THE STEEL OUTER BUSHING. THE STEEL OUTER BUSHING IS HELD IN PLACE WITH 2 (C) CLIPS, HOWEVER THE URETHANE INNER PART OF THE BUSHING LOOKS TO BE ONLY A PRESS FIT. (TC NR 20071102012)                                                                                                                1H71 3O3  ONT3A12    1E10    5  NP857     
20080131001372008013100137SW  2008       1          31         CA071102013      120071101G6320476206283       BEARING CAGE    BELL                    BELL  47    47G2        1181008SW  LYC   O435  VO435A1E    41516EA                              M/R TRANSMISSIONMAKING METAL    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            100   B125159                                             (CAN) DURING ROUTINE INSPECTION, SMALL AMOUNT OF BRASS WAS FOUND IN OIL SCREEN, THE TRANSMISSION WAS DISASSEMBLED TO LOCATE THE FAILED ITEM AND IT WAS FOUND TO BE ONE OF THE BEARING CAGES IN THE DUPLEX BEARING THAT THE UPPER SUN GEAR GOES THROUGH, THIS IS THE NEW AND IMPROVED BEARING INSTALLED IAW TB 47-75-4 (TC NR 20071102013)                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3O3  O  H1      E279                 
20080131001432008013100143EA  2008       1          31         CA071103001      120071101G497021188002        ECU             HONEYWELL               CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              APU             FAULTY          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       189836143                                                      (CAN) FLIGHT RETURNED DUE TO APU OIL PRESSURE MESSAGE CAUSING THE APU TO FAIL. AIRCRAFT WAS ALREADY OPERATING WITH 1 IDG GENERATOR UNSERVICEABLE. MAINTENANCE CHECKED THE SYSTEM AND FOUND AN ECU FAULT MESSAGE. THE APU ECU WAS REPLACED AND THE A/C WAS CHECKED SERVICEABLE.  NR 1 IDG WAS ALSO REPLACED AT THIS TIME AND CHECKED SERVICEABLE CLEARING THE MEL. CYCLES SINCE OVERHAUL:4860 (TC NR 20071103001)                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20080131001442008013100144NE  2008       1          31         CA071105001      220071101G7200                ENGINE                                  BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                                              MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CRCRUISE         1                      CA                                          114284                      (CAN) CREW OBSERVED LOW OIL PRESSURE WARNING, FOLLOWED BY SMOKE IN THE CABIN. ELECTION WAS MADE TO PERFORM AN INFLIGHT ENGINE SHUTDOWN.  MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.   FULL ENGINE SN GAS GENERATOR MODULE: 114283 POWER SECTION MODULE: 114135 (TC NR 20071105001)                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4T4  TRTA24CE   E26NE                
20080131001462008013100146EU  2008       1          31         CA071105002      120071102G29109433772104      HOSE                                    PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  LT MAIN GEAR    FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHEN TRYING TO INSTALL THE NEW LINE IT WOULD BIND UP HALF WAY ON,   HAD 2 NEW HOSES AND WHEN WE TRIED THE OTHER HOSE IT WENT ON WITH NO PROBLEMS, SUSPECT THREADS ON  B-NUT FITTING ON NEW HOSE. (TC NR 20071105002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080131001492008013100149NE  2008       1          31         CA071105003      220071024G7200                TRANSDUCER                              FOKKERF27   F27MK50            EU  PWA   PWA120PW125B           NE                              ECU             DEFECTIVE       W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA                                          125146                      (CAN) TAKEOFF WAS ABORTED DUE TO UNCOMMANDED POWER CHANGES OBSERVED ON GAUGES IN CONCERT WITH AIRCRAFT YAWING MOTION.  TROUBLESHOOTING DETERMINED THAT THE PT TRANSDUCER IN THE ELECTRONIC CONTROL WAS DEFECTIVE. PN AND SN TO BE SUPPLIED IN DUE COURSE. (TC NR 20071105003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA817    E20NE                
20080131001522008013100152EA  2008       1          31         CA071105004      120071030G5610601R3303312     WINDOW                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              COCKPIT         BROKEN          W      BA  EMER. DESCENT           UNSCHED LANDING                                                         O  OTHER                                                                         CRCRUISE         1                      CA       12170                                                          (CAN) OUTBOUND THE FOS SIDE WINDOW BROKE GOING THROUGH 20,000 FT.  MX REPLACED SIDE WINDOW (TC NR 20071105004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
20080131001572008013100157NE  2008       1          31         CA071105005      220071026G7200601R6000267     ENGINE                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              NR 1            FAILED          W      O   OTHER                                                                                           CE F.O.D.                    VIBRATION/BUFFET                                    CLCLIMB          1                      CA       4404                               872911                      (CAN) AFTER TAKEOFF, THE CREW SENT ACARS INDICATING THAT THE LT ENGINE HAD A HIGH VIB.  AFTER FOLLOWING THE QRH. THEY REDUCED POWER TO ACCOMMODATE THE VIB IN THE GREEN. IN SEPARATE ACARS, THEY HAD ANTI SKID MESSAGE. THEY CONTINUED AND ONCE ON THE GROUND DISCOVERED THAT THE NR 2 MAIN TIRE HAD SHREDDED AND PART OF THE DEBRI WENT INTO THE NR 1 ENGINE. 2 FAN BLADES WERE BENT AND 2 STATORS WERE CRACKED. THE NOSE COWL HAS A DENT THAT IS OUT OF LIMITS. THE REMAINING MAIN WHEEL TIRE PRESSURES WERE ALL ABOVE 200 PSI.  PARTS REPLACED:  STATOR SPACER PN 5128T05G01 NSN,  FAN BLADE C-25 PN 6018T30P06 SN KLAJ6586  FAN BLADE L-11 PN 6018T30P06 SN KGAR3406 FAN BLADE C-22 PN 6018T30P14 SN KGACR870 FAN BLADE L-8 PN 6018T30P14 SN2L72 4F4  FRTA21EA   E15NE                
20080131001602008013100160NM  2008       1          31         CA071106001      120071017G5610NP17820110      WINDSHIELD                              GULSTM200   200         4500308NM                                                               COCKPIT         BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA       830                                                            (CAN) PILOT REPORTED RT WINDSHIELD CRACKED ON RETURN. C/O INSPECTION ON RT WINDSHIELD AND COULD NOT FAULT THE WINDSHIELD. THE AIRCRAFT WAS RELEASE FOR RETURN TO SERVICE. THE AIRCRAFT MADE (3) OTHER TRIPS. THE PILOTS REPORTED THE SAME CRACK ON THE RT WINDSHIELD. AGAIN C/O THE INSPECTION ON THE RT WINDSHIELD AND COULD NOT FAULT. PILOTS REPORTED THEY COULD ONLY SEE THE CRACK WHEN THE AIRCRAFT IS AT ALTITUDE. SPOKE TO MFG AND DECIDED TO REPLACE THE WINDSHIELD. THE UNIT REMOVED WILL BE SENT BACK TO MFG AND THEY WILL REPORT ON THE FAILURE OF THE WINDSHIELD. THE NEW RT WINDSHIELD WAS INSTALLED AND THE AIRCRAFT HAD SEVERAL FLIGHTS WITH NO FURTHER REPORTS. (TC NR 20071106001)                                             2L72 4F    RTA53NM                        
20080131001612008013100161CE  2008       1          31         CA071106002      120071105G3244226K084         TIRE                                    LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312     01518WP                              MLG             DELAMINATED     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       412                                                            (CAN) DURING AN INSPECTION, A BULGE WAS NOTICED ON THE NR 2 TIRE. THIS BULGE WAS NOTICED IN 3 SPOTS ON THE TIRE, EACH EXTENDING FOR ABOUT 3 INCHES. THE BULGE STARTED AT THE CORNER OF THE TREAD AND EXTENDED TO THE SIDEWALL AND. THE TIRE WAS REPLACED. (TC NR 20071106002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTT00008WIE6WE                 
20080131001642008013100164NM  2008       1          31         CA071106003      120071106G5330146A323110      SKIN                                    BOEING737   737990             NM                                                               BS 777-830 RBL26SCRATCHED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) SCRATCHES ON FUSELAGE SKIN BELOW AFT CARGO PIT LOWER SILL BS 777 TO BS 830, RBL 26 REPAIRED IAW CUSTOMER EA. (TC NR 20071106003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L74 4F    RTA16WE                        
20080131001672008013100167NM  2008       1          31         CA071106004      120071106G5730112A4102209     SKIN                                    BOEING737   737990             NM                                                               LWS 240         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) LT WING LOWER SKIN PANEL CHAFFING AT WSTA 240, IB OF BLADE SEAL. REPAIRED IAW CUSTOMER EA (TC NR 20071106004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L74 4F    RTA16WE                        
20080131001702008013100170NM  2008       1          31         CA071106005      120071106G5730112A4102209     SKIN                                    BOEING737   737990             NM                                                               LWS 260         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) LT WING LOWER SKIN PANEL CHAFFING DAMAGE AT WSTA 260, OB OF BLADE SEAL FAIRING. REPAIRED IAW CUSTOMER EA (TC NR 20071106005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L74 4F    RTA16WE                        
20080131001722008013100172NM  2008       1          31         CA071106006      120071106G5730112A4102210     SKIN                                    BOEING737   737990             NM                                                               RWS 240         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) RT WING LOWER SKIN CHAFING DAMAGE AT WSTA 240, IB OF FAIRING SEAL REPAIRED IAW CUSTOMER EA (TC NR 20071106006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L74 4F    RTA16WE                        
20080131001762008013100176CE  2008       1          31         CA071106007      120071106G29319536830         INDICATOR                               BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  HYD SYSTEM      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) WE HAD A PRESSURE GAUGE THAT HAD A SMALL LEAK SO WE PURCHASED A NEW GAUGE FROM MFG AND INSTALLED IT ON THE AIRCRAFT. WHEN SYSTEM WAS BROUGHT UP TO THE PROPER PRESSURE THE NEW GAUGE LEAKED WORSE THAN THE ORIGINAL GAUGE. THE GAUGE WAS SENT BACK TO BEECH AND WE ARE WAITING FOR A REPLACEMENT. THIS IS A QUALITY CONTROL ISSUE. (TC NR 20071106007)                                                                                                                                                                                                                                                                                                                                                                                    1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20080131001792008013100179NE  2008       1          31         CA071106008      320071025G611031025731        RETAINER                                FRCHLDSA227 SA227CC     3377522SW  GARRTTTPE331TPE33111U   01514WP  MCAULY4HFR344HFR34C652  NE  PROP SHAFT      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                          P44738                      (CAN) WHILE ENGINE WAS BEING REPLACED MAINTENANCE NOTICED FATIQUE CRACKS EMINATING FROM THE (PROP SHAFT) RETAINING BOLT AREA. (TC NR 20071106008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20080131001822008013100182SW  2008       1          31         CA071106009      120071026G32202752530001      ARM                                     SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE33111U   01514WP  MCAULY4HFR344HFR34C652  NE  NLG CENTER      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ROLLER BEARING OUTER CASE FOUND CRACKED COMPLETLY THROUGH. REPLACED AND RETURNED TO SERVICE (TC NR 20071106009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4T4  TRTA8SW    E4WE    6  C3PNE     
20080131001862008013100186WP  2008       1          31         CA071106010      220071030G731331032359        FUEL NOZZLE                             SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE3311     01514WP  MCAULY4HFR344HFR34C652  NE  ENGINE          CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) FUEL NOTICED IN ENGINE COWL DURING INSPECTION. NOZZLE IN NR 3 POSITION FOUND CRACKED WHERE PRIMARY/SECONDARY LINES HOOK UP TO NOZZLE. CRACK WAS 95 PERCENT THROUGH CIRCUMFERENCE. (TC NR 20071106010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4T3  TRTA8SW    E3WE    6  C3PNE     
20080131001872008013100187EU  2008       1          31         CA071106011      120071025G282030733341        TUBE                                    BRAERODH125 HS125700A   4230170EU  GARRTTTFE731TFE7313R1H  29001WP                              FUEL SYSTEM     CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ON A PREFLIGHT INSPECTION, MAINTENANCE DISCOVERED THE FIRE DETECTOR (P/N 3001-31-900-400-17) AGAINST THE FUEL TUBE ASSEMBLY (P/N P-84417). UPON REPOSITIONING THE FIRE DETECTOR INTO POSITION, A CHAFED MARK ON THE NR 1 ENGINE FUEL TUBE ASSEMBLY WAS DISCOVERED. THE FUEL TUBE ASSEMBLY WAS ORDERED AND REPLACED. AN ENGINE RUN WAS CARRIED OUT FOR A LEAK CHECK INSPECTION. (TC NR 20071106011)                                                                                                                                                                                                                                                                                                                                        2L72 4F4  F  A3EU    E6WE                 
20080131001882008013100188    2008       1          31         CA071106012      420071104G2210BACC18AE35      CIRCUIT BREAKER                         BOEING737   737*               NM  PWA   JT8   JT8D17A     52049NE                                              FAILED          W      A   UNSCHED LANDING                                                                                 S  AFFECT SYSTEMS                                                                CRCRUISE         1                      CA                                                                      (CAN) ENROUTE AT FL300, THE CREW EXPERIENCED AN AUTO PILOT DISENGAGEMENT AS WELL AS THE LOSS OF THE FOLLOWING, YAW DAMPER, MACH TRIM, CAPTS. PITOT STATIC, NR 1 ENG ANTI ICE, RADAR ALTIMETER, NO 2 EGT AND SEVERAL OTHERS.   THE CREW ATTEMPTED A RESET OF THE NR 1 NORMAL TRANSFER BUS CIRCUIT BREAKER, WHICH FAILED. THE AIRCRAFT WAS DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CIRCUIT BREAKER AND THE AIRCRAFT HAS RETURNED TO SERVICE WITHOUT FURTHER PROBLEM. (TC NR 20071106012)                                                                                                                                                                                                                           2L72 4F4  FRTA16WE   E2EA                 
20080131001902008013100190EA  2008       1          31         CA071107001      220071103G7200                ENGINE                                  DHAV  DHC6  DHC6100     2802610EA  PWA   PT6   PT6A20      52043EA  HARTZLHCB3T HCB3TN3     GL  RIGHT           FAILED          W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          PCE50661                    (CAN) PILOTS HAD TO SHUTDOWN RT ENGINE. MAINTENANCE INSPECTION FOUND PROP WOULDN`T TURN, EXPECT POWER SECTION FAILURE. (TC NR 20071107001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H72 3T3  TRTA9EA    E4EA    6  CP15EA    
20080131001932008013100193EA  2008       1          31         CA071107002      220071105G7230                BLADES                                  BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A41      52043EA  HARTZLHCB3T HCB3TN3     GL  COMPRESSOR      FAILED          W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      LDLANDING        1                      CA                                          PCE85202                    (CAN) PILOTS OBSERVED SPARKS COMING OUT RT ENGINE EXHAUST ON LANDING. MAINTENANCE INSPECTION FOUND COMPRESSOR BLADES LAYING IN THE ENGINE BAY. (TC NR 20071107002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20080131001972008013100197CE  2008       1          31         CA071107003      120071107G273155657544        LEVER                                   CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              TRIM INDICATOR  WORN            W      C   ABORTED TAKEOFF                                                                                 F  FLT CONT AFFECTED                                                             TOTAKEOFF        1                      CA       6834                                                           (CAN) PILOT ABORTED TAKEOFF DUE TO NO RESPONSE TO CONTROL COLUMN INPUT. UPON INSPECTION FOUND ELEVATOR TRIM TAB WAS ALMOST ON FULL NOSE DOWN POSITION AND TRIM INDICATION IN COCKPIT WAS AT TAKEOFF. FOUND INDICATOR LEVER AND CONTROL WHEEL WORN, INDICATOR LEVER HAD JUMPED ON CONTROL WHEEL TO GIVE WRONG INDICATION. TRIM CONTROL WHEEL AND INDICATOR LEVER REPLACED AND INDICATION SYSTEM RIGGED IAW AMM AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20071107003)                                                                                                                                                                                                                                                                             1L72 4F4  F  A22CE   E1NE                 
20080131002002008013100200EU  2008       1          31         CA071107004      120071107G5320MS24693C273     SCREW                                   EMB   ERJ190ERJ190100IGW3260408EU  GE    CF34  CF3410E5A1  30022NE                              P-ACE RACK      WRONG PART      W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4104                                                           (CAN) RETAINING SCREW FOR THE P-ACE (PRIMARY- ACTUATOR CONTROL ELECTRONICS) LT AND RT RACKS WERE THE WRONG SIZE (DIAMETER AND LENGTH TOO SMALL). THE RT P-ACE AND RACK WERE FREE FLOATING IN THE SLOT. THE LT P-ACE AND RACK WERE SECURED WITH THE WRONG HARDWARE. THE CORRECT P/N OF THE RETAINING SCREW IS MS24693C273.  (TC NR  20071107004)                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA57NM   E00070EN             
20080131002022008013100202EA  2008       1          31         CA071107005      120071012G2730TBC6CF11461     CABLE                                   DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  ELEVATORS       CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1532                                                           (CAN) WHILE INSPECTING THE CONTROL CABLES IAW TRANSPORT,  ALERT (SDA) AL-2007-03, THE ELEVATOR CABLE WAS FOUND CHAFED AT THE PULLEYS AT STA 262.0.  THE LOCATION OF THE WEAR ON THE CABLE, IS DIRECTLY OVER THE PULLEYS WHEN THE CONTROL LOCKS ARE IN. (TC NR 20071107005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20080131002092008013100209SW  2008       1          31         CA071108001      120071105G2400                ELECTRICAL SYS                          SWRNGNSA227 SA227AC     8780603SW                                                                               FAILED          W      O   OTHER                                                                                           H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA                              AC739B                                  (CAN) A/C ENROUTE AT 6000 FT, EXPERIENCED TURBULENCE AND ST.ELMO`S FIRE. AFTER SOME TIME, LIGHTNING APPEARED AS A BLUE LIGHT (AS REPORTED BY PASSENGER. IMMEDIATELY AFTER, ALL ELECTRICAL POWER (BOTH BATTERIES AND GENERATORS) WAS LOST. AIRCREW RESET THE BATTERIES AFTER ESTABLISHING A SAFE FLIGHT ATTITUDE WITH THEIR PERSONAL FLASH LIGHTS. POWER WAS RESTORED AS SOON AS BATTERY RESET WAS ATTEMPTED. FLIGHT CONTINUED. MAINTENANCE WAS CONTACTED. AS THERE WAS NO OBVIOUS DAMAGE, ENTRIES WERE MADE IN THE JOURNEY LOG AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20071108001)                                                                                                                                                    2L72 4T    RTA8SW                         
20080131002122008013100212GL  2008       1          31         CA071108003      120071102G5740                ATTACH FITTING  DHAV                    DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HARTZLHCB3R HCB3R304    GL  LIFT STRUTS     CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9690       0140                                                (CAN) WHILE ACCOMPLISHING THE REQUIREMENTS OF SB 2/55, CRACKS WERE DETECTED ON THE LOWER LUGS OF BOTH WING LIFT STRUTS. IN BOTH CASES THE CRACKS WERE LOCATED ON THE IB FACE OF THE LUG AND WERE .7500 INCH LONG LT STRUT P/N C2W1103A, S/N 0140 WAS CRACKED ON THE AFT FACE OF THE FWD LUG RT STRUT P/N C2W1104A S/N 0113 WAS CRACKED ON THE FWD FACE OF THE AFT LUG. S. B. 2/41 WAS COMPLETED 1 YEAR AGO WITH NO FAULTS FOUND AT THAT TIME. THE AC OPERATES EXCLUSIVELY ON FLOATS IN A CORROSIVE ENVIRONMENT. BOTH STRUTS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. TAT 18060.1 (TC NR 20071108003)                                                                                                                             1H71 3R3  RRCA806    5E1     5  CP28EA    
20080131002162008013100216NE  2008       1          31         CA071108004      220071025G73208228224004      EEC                                     CESSNA680   680CE       2076811CE  PWC   PW306 PW306C      52169NE                              ENGINE          DEFECTIVE       W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          CG0214                      (CAN) DURING FLIGHT, THE CREW RECIEVED A YELLOW, HIGH TEMPERATURE, (WARNING LIGHT). THE POWER WAS REDUCED AND THE FLIGHT WAS DIVERTED. TROUBLESHOOTING REVEALED A DEFECTIVE ELECTRONIC ENGINE CONTROL. (TC NR 20071108004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRCT00012WIE35NE                
20080131002182008013100218NM  2008       1          31         CA071108005      120071105G2820LJ35801         LINE                                    BOEING757   75728A      1384976NM  RROYCERB211 RB211535E43754555NE                              NR 1 ENGINE     CHAFED          W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB, THE CREW NOTICED THAT NR1 ENGINE PARAMETERS WERE NOT AS SCHEDULED. AIRCRAFT RETURNED TO THE AIRPORT. WITH DECREASING ALTITUDE THE NR1 ENGINE PARAMETERS IMPROVED AND A NORMAL LANDING WAS PERFORMED. FOUND P1 LINE CHAFED THROUGH. LINE REPLACED. TEST FLIGHT CONDUCTED. ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. (TC NR 20071108005)                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA2NM    E12EU                
20080204001542008020400154NM  2008       2          4          CA071108006      120071107G32332630000004      ACTUATOR                                GULSTM200   200         4500308NM                                                               MLG             FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       855                                                            (CAN) AFTER TAKEOFF THE CREW REPORTED THAT THE GEAR WAS SELECTED UP AND THE NOSE AND RT MAIN GEAR RETRACTED WITH NO FAULT, THE LT GEAR DID NOT RETRACT.  THE CREW REPORTED THEY CYCLED THE GEAR DOWN AND THE (3) GREEN LIGHTS WAS ON EICAS INDICATING DOWN AND LOCK.  ANOTHER ATTEMPT WAS MADE TO CYCLE THE GEAR UP, AGAIN ONLY THE NOSE AND THE RT MAIN RETRACTED. THE LT UNSAFE INDICATION WAS INDICATED ON EICAS.  THE CREW ELECTED TO CYCLE THE GEAR DOWN AGAIN AND WAS COMPLETED SUCCESSFULLY, (3) GREENS ON EICAS.THE AIRCRAFT WAS RETURNED TO POINT OF DEPARTURE AND LANDED NO PROBLEMS. MAINTENANCE WAS CALLED AND THE AIRCRAFT WAS PLACED ON JACKS C/O GEAR SWINGS. TROUBLESHOOTING REVEALED THAT THE LT GEAR ACTUATOR INTERNAL LOCKING2L72 4F    RTA53NM                        
20080131002222008013100222EU  2008       1          31         CA071108007      120071107G3210200915254       LINK                                    BAG   BAE146BAE146200A  1500266EU  LYC   ALF502ALF502R5    41580NE                              MLG             UNSERVICEABLE   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       323568282                                                      (CAN) IT HAS BEEN DISCOVERED DURING INSPECTION OF THE ABOVE MENTIONED PART THAT IT IS IN AN UNSERVICEABLE CONDITION. WHILE ON JACKS THE COMPONENT WAS INSPECTED AND MOVEMENT COULD BE FELT BETWEEN THE ROD ASSY AND EYE END. THE EYE END IS THREADED INTO THE ROD FOLLOWED BY A JAMB NUT AND SAFETY ASSY. NO MOVEMENT IS PERMITTED. THERE IS EVIDENCE OF CORROSION DEPOSITS LEACHING THROUGH THE SEALANT. THIS IS THE SUSPECTED CAUSE. (TC NR 20071108007)                                                                                                                                                                                                                                                                                      2H74 4F4  FRTA49EU   E6NE                 
20080131002232008013100223NM  2008       1          31         CA071109001      120071105G24324011769         BATTERY                                 BOMBDRDHC8  DHC8402     1390042NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  MASTER          FAILED          W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA       16205176                                                       (CAN) DURING ENGINE NR 2 START UP, THE NR STALLED AT 20 NR AND THE ITT INDICATOR REACHED 800 DEGREES CELSIUS. THE ENGINE START WAS ABORTED FOLLOWING BY A LOUD BANG FROM THE NOSE COMPARTMENT.  MAINTENANCE WAS CALLED IN AND THEY FOUND THE MAIN BATTERY TOP COVER POPPED OUT. NO STRUCTURAL DAMAGE WAS OBSERVED. THE MAIN AND AUXILIARY BATTERIES WERE REPLACED. THE AIRCRAFT WAS RELEASE AND RETURNED INTO SERVICE. (TC NR 20071109001)                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080131002242008013100224CE  2008       1          31         CA071109002      120071107G273155657544        LEVER                                   CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              TRIM WHEEL      INOPERATIVE     W      C   ABORTED TAKEOFF                                                                                 F  FLT CONT AFFECTED                                                             TOTAKEOFF        1                      CA       6834                                                           (CAN) PILOT ABORTED TAKEOFF. UPON INSPECTION FOUND ELEVATOR TRIM TAB WAS ALMOST ON FULL NOSE DOWN TRIM POSITION. TRIM INDICATION IN THE COCKPIT WAS AT TAKEOFF. FOUND THAT THE INDICATOR LEVER HAD JUMPED ON THE CONTROL WHEEL TO GIVE THE WRONG INDICATION. TRIM CONTROL WHEEL AND INDICATOR LEVER REPLACED AND INDICATION SYSTEM RIGGED IAW AMM. (TC NR 20071109002)                                                                                                                                                                                                                                                                                                                                                                          1L72 4F4  F  A22CE   E1NE                 
20080131002252008013100225EU  2008       1          31         CA071109003      120071109G7820L24266710000    BAFFLE                                  ZLIN  242   Z242L       9970204EU  LYC   O360  AEIO360A1B6 41514EA  MUHBR MTV   MTV9*       EU  EXHAUST SILENCERCRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A 100 HOUR INSPECTION, ONE INTERNAL BAFFLE OF THE PRIMARY EXHAUST SILENCER WAS FOUND TO BE CRACKED 25 PERCENT OF THE ATTACHING WELD. SILENCER WAS SUBSEQUENTLY REPLACED. (TC NR 20071109003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1L71 3O3  O0 A76EU   1E10    5  CP24NE    
20080131002262008013100226NE  2008       1          31         CA071109004      220071005G852016475           CRANKCASE                               DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HARTZLHCB3R HCB3R304    GL  ENGINE          CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA            1141                          21739                       (CAN) DURING RUNUP AFTER INSPECTION, INVESTIGATION OF A MINOR OIL LEAK REVEALED THAT THE ENGINE CRANKCASE WAS CRACKED NEAR AN ENGINE THROUGHBOLT AT THE BASE OF NR 2 CYLINDER, BETWEEN CYLS NR 2 AND NR 3. THE ENGINE WAS REPLACED. (TC NR 20071109004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3R3  RRCA806    5E1     5  CP28EA    
20080204001532008020400153NE  2008       2          4          CA071109005      220071108G73217898435010      ECU                                     AEROSPATR42 ATR42300    8680920EU  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF5       NE  NR 2  ENGINE    FAILED          W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  DEDESCENT        1                      CA                                          PCE120178                   (CAN) AC EXPERIENCED AN IN FLIGHT ENGINE SHUTDOWN OF THE NR 2 ENG ON DESCENT ABOUT 20 MILES FROM DESTINATION. CREW REPORTED NO DISCREPANCIES PRIOR TO THE INCIDENT. THE CREW DID NOT ATTEMPT A RESTART BUT DECIDED TO LAND AS CONFIGURED. THE ECU FAULT LIGHT DID NOT ILLUMINATE AFTER ENGINE SHUTDOWN. THE RT UP-TRIM LIGHT ILLUMINATED AFTER THE ENGINE QUIT IN FLIGHT AS REPORTED BY THE PILOTS. MAINT VISUALLY INSPECTED THE ENGINE FOR OBVIOUS DEFECTS, NONE NOTED. THE ENGINE DRIVEN FUEL PUMP AND HMU WERE REMOVED TO CHECK FOR FUEL PUMP CONDITION. NO FAULTS NOTED. FUEL FILTERS AND ENGINE OIL FILTERS WERE INSPECTED OK. NO BYPASS OR FUEL CLOG ANNUNCIATIONS NOTED. THE ENGINE WAS DRY MOTORED TO LISTEN FOR UNUSUAL NOISES (TOWER S2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080131002442008013100244SW  2008       1          31         CA071109006      120071108G7720850568503       INDICATOR                               GULSTM690TP 690A        0141722SW  GARRTTTPE331TPE3315     01514WP  HARTZLHCB3T HCB3TN5     GL  ITT             UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 CRCRUISE         1                      CA                              11192                                   (CAN) DURING CRUISE THE NR2 ENGINE ITT INDICATION BECAME ERRATIC, THEN CLIMBED THROUGH THE RED LINE. THE FLIGHT CREW SHUTDOWN THE ENGINE AND FEATHERED THE PROP. THE AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE TESTED THE ITT SYSTEM AND FOUND THE INDICATOR TO BE AT FAULT. THE ITT INDICATOR WILL BE REPLACED WITH A SERVICEABLE UNIT AND THE AIRCRAFT WILL BE RETURNED TO SERVICE. (TC NR 20071109006)                                                                                                                                                                                                                                                                                                                                       1H72 3T4  T  2A4     E4WE    6  CP15EA    
20080131002462008013100246CE  2008       1          31         CA071109007      120071013G2750C1450046        GEAR            CESSNA                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  HARTZLHCB3T HCB3TN3     GL  TRANSMISSION    BROKEN          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             DEDESCENT        1                      CA       2880                                                           (CAN) THE PILOT WAS ON DECENT AND WENT TO SELECT FLAPS AND THE CIRCUIT BREAKER POPPED AFTER THE FLAPS WERE AT ABOUT 10 DEGREES. HE THEN LANDED THE AIRCRAFT NORMALLY. MAINTENANCE FOUND THE FLAP TRANSMISSION TO BE MAKING NOISE OUT OF THE NORM. THE INTERNAL GEAR THAT DRIVES THE TRANSMISSION JACK SCREW WAS FOUND TO HAVE CHIPS OUT OF A FEW TEETH. THE TRANSMISSION WAS REPLACED AND SYSTEM FUNCTIONED NORMAL. (TC NR 20071109007)                                                                                                                                                                                                                                                                                                         1H71 3T3  T  A37CE   E4EA    6  CP15EA    
20080131002482008013100248NE  2008       1          31         CA071109008      220071103G7314LW15473         PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL SYSTEM     WEAK            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1859 407                                                       (CAN) ENGINE DRIVEN PUMP FOUND TO BE WEAK WILL NOT SUSTAIN ENGINE IDLE ON IT`S OWN. (TC NR 20071109008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3O3  O  H11NM   1E4                  
20080131002502008013100250WP  2008       1          31         CA071109009      120071103G2822D7431           PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL SYSTEM     WEAK            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       902  902                                                       (CAN) ELECTRIC AUX FUEL PUMP WEAK, MOTOR SOUNDED LIKE IT WAS OVERWORKING. (TC NR 20071109009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3O3  O  H11NM   1E4                  
20080131002522008013100252NE  2008       1          31         CA071109010      220071103G732225766304        FUEL CONTROL                            ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          INOPERATIVE     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1859 1859                                                      (CAN) DURING MAINTENANCE GROUND RUN, THE ENGINE WAS HESITATING AT 70 PERCENT AND THEN DROOPS TO 65 PERCENT OR LESS. FUEL CONTROL NOT RESPONDING TO THROTTLE INPUT CORRECTLY. (TC NR 20071109010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3O3  O  H11NM   1E4                  
20080131002542008013100254EA  2008       1          31         CA071109011      220071108G8530LW13870         CYLINDER                                ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              ENGINE          INOPERATIVE     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            438                                                       (CAN) DURING A 50 HOUR INSPECTION, BOTTOM SPARK PLUG ON CYLINDER NR 5 REVEALED UNUSUAL AMOUNT OF OIL. A COMPRESSION TEST WAS CARRIED OUT AND CYLINDER NR 5 WAS NOTED TO HAVE 18 OVER 80 PSI COMPRESSION.  TSO WILL HAVE TO BE VERIFIED. (TC NR 20071109011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3O3  O  H11NM   E295                 
20080131002552008013100255NM  2008       1          31         CA071112001      120071111G3297473901          WIRE HARNESS                            BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  NLG             FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF, NOSE GEAR UNSAFE ILLUMINATED. CREW PERFORMED NORMAL EXTENSION AND THE NLG DOORS DID NOT OPEN. ALSO, NLG NOT SHOWING DOWN AND LOCKED. SECOND ATTEMPT FOR EXTENSION, NOSE DOOR AMBER LIGHT ILLUMINATED. CREW PERFORMED ALTERNATE EXTENSION AND LANDED WITHOUT FURTHER INCIDENTS.   MAINTENENCE DISCOVERED PSEU REPORTED FAULT, NLG LOCK PROX 1. NOSE LOCK SENSOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20071112001)                                                                                                                                                                                                                                                                                              2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080131002562008013100256WP  2008       1          31         CA071112002      120071026G2720369A75058       BRACKET                                 HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              RUDDER PEDELS   BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       15663                                                          (CAN) RUDDER PEDALS WERE FOUND TO BE LOOSE IN MOUNTS ON FURTHER INVESTIGATION IT WAS FOUND THE BRACKET THAT THE RUDDER PEDALS MOUNT IN WAS BROKEN ON (3) OF THE (4) MOUNTING BOLT EARS. (TC NR 20071112002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  H3WE    E4CE                 
20080131002582008013100258EU  2008       1          31         CA071112003      120071109G2612                FIRE LOOP                               BRAERO748   HS7482A     4231001EU  RROYCEDART  DART5342         EU  ROTOL R4304 R2124304    EU  NR 1 NACELLE    FAULTY          W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF, ENGINE NR 1 FIRE-WARNING ALARM WENT OFF. THE FLIGHT CREW INFORMED TOWER AND RETURNED TO AIRPORT.  A HOLE WAS FOUND IN THE FLEXIBLE DUCT AT THE SUPERCHARGER OUTLET.  ALSO, (2) FIRE DETECTION LOOPS WERE REPLACED BECAUSE THEY FAILED THE RESISTANCE CHECK LIMITS FOUND IN THE HS 748 MM. (TC NR 20071112003)                                                                                                                                                                                                                                                                                                                                                                                                              2L72 3T4  T  A24EU   A196    6  CP899     
20080131002592008013100259NM  2008       1          31         CA071113001      120071110G6120699018002       CONTROLLER                              BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  PROPELLER       MALFUNCTIONED   W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         FJ FLT CONT AFFECTED         WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) DURING FLIGHT, CREW REPORTED A NR 2 PEC CAUTION LIGHT ILLUMINATED FOLLOWED BY THE NR 2 ENGINE NP SURGE. THE QRH CONSULTED AND THE NR 2 ENGINE WAS SHUTDOWN.  EMU DOWNLOAD C/O, FAULT ISOLATION C/O FOR CODES 236 AND 260 IAW TASK 61-20-05-810-822, 61-20-06-810-818. SERVO VALVE CONNECTORS RT J26 AND J27 CLEANED AND TREATED WITH STABILANT. PEC CONNECTORS 20 AND 21 CLEANED AND TREATED WITH STABILANT. AUTO FEATHER AND UP TRIM CHECKED SERVICEABLE FOR RETURN TO SERVICE IAW TASK 61-20-00-710-801. FURTHER FAULT CODE 131 DISPLAYED IN CDS.  RT PEC REPLACED IAW AMM 61-20-36 AND C/O IAW AMM 71-00-00, NIL FAULTS EVIDENT. (TC NR 20071113001)                                                                                   2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080131002602008013100260NE  2008       1          31         CA071113003      220071106G7200                ENGINE                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              POWER LOSS      W      A   UNSCHED LANDING                                                                                 R  PARTIAL RPM/PWR LOSS                                                          CLCLIMB          1                      CA                                          PC1078                      (CAN) SHORTLY AFTER TAKEOFF WHILE PERFORMING A LOW LEVEL TURN, THE ENGINE REPORTEDLY LOST POWER. EMERGENCY POWER LEVER WAS ACTIVATED WITH NO RESPONSE. AIRCRAFT LANDED ON A STREET, NO FATALITIES. INITIAL INVESTIGATION REVEALED NO EVIDENCE OF PRE-IMPACT ANOMALIES. FUEL SYSTEM COMPONENTS WILL BE INVESTIGATED.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071113003)                                                                                                                                                                                                                                                                                                                    1H71 3T3  T  A37CE   E4EA                 
20080131002612008013100261NE  2008       1          31         CA071113005      220071106G732132448809        FUEL CONTROL                            CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              ENGINE          FAILED          W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  APAPPROACH       1                      CA                                          JC0359                      (CAN) DURING APPROACH, ENGINE SPEED DESCENDED TO SUBNORMAL VALUE. NO/SLOW RESPONSE FROM THRUST LEVER. CONDITION WAS REPEATABLE ON GROUND FOLLOWING THE INCIDENT. FUEL CONTROL CHANGED AS PART OF TROUBLESHOOTING. (TC NR 20071113005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA22CE   E25EA                
20080204001522008020400152EA  2008       2          4          CA071113006      120071112G3340BJ10021003      CAMLOCK         BRUCE       BJ10021003  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              LIGHT           WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  0075                                                (CAN) DURING AN OVERNIGHT MAINTENANCE INSPECTION IT WAS DISCOVERED THAT THE LT WING INSPECTION LIGHT LENS WAS MISSING TOGETHER WITH THE BULB HOLDER LEAVING THE WIRES EXPOSED. WHEN THE FAIRING WAS REMOVED TO REPLACE THE ASSEMBLY IT WAS NOTICED THAT A CAMLOC NUT HAD BEEN STRETCHED CAUSING THE FASTENER TO BE LOOSE. FORTUNATELY THE MISSING PARTS DID NOT DAMAGE THE AIRCRAFT OR THE ENGINE. (TC NR20071113006)                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA21EA   E15NE                
20080204001512008020400151EU  2008       2          4          CA071113007      120071108G25105PC41301001     DOUBLER         ISRAEL                  PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  SEAT PAN        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2763       386                                                 (CAN) DOUBLER INSTALLED ON CRACKED SEAT PAN WEB IAW SB 5PC41000-MOD1, FOUND CRACKED. NEW DOUBLER PN 5PC41301-001 INSTALLED. (TC NR 20071113007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080204001502008020400150EA  2008       2          4          CA071113008      120071106G5610NP13932111      WINDOW                                  CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C1     30049NE                              COCKPIT         BROKEN          W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       11455                                                          (CAN) CREW REPORT THAT AT 360 THE CAPTS FWD WINDOW SHATTERED AND THEY DIVERTED WINDOW REPLACED (TC NR 20071113008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA21EA   E00063EN             
20080204001492008020400149NE  2008       2          4          CA071113009      220071108G7261                CARBON SEAL                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              ACTUATOR        DEFECTIVE       W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      CA       17457                                                          (CAN) AFTER TAKEOFF, CREW GOT A (SMOKE TOILET CAUTION MESSAGE). CABIN WAS FILLED WITH SMOKE. AFTER QRH WAS COMPLETED RETURNED TO FIELD AND MESSAGE WAS GONE A SHORT WHILE AFTER.   MX FOUND OIL LEAKING FROM ENGINE VARIABLE GUIDE VANE (VG) ACTUATOR STRUTS AND LEAKING INTO THE BLEEDS. SUSPECT NR 3 CARBON SEAL. SLC REPLACED THE RT ENGINE. (TC NR 20071113009)                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA21EA   E15NE                
20080204001482008020400148NE  2008       2          4          CA071113010      220071105G7261                CARBON SEAL                             CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              NR 3            LEAKING         W      A   UNSCHED LANDING                                                                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) JUST AFTER TAKEOFF, THE CABIN STARTED TO FILL WITH SMOKE AND THE LAV SMOKE DETECTOR WENT OFF. THEY DECLARED EMERGENCY AND RETURNED TO THE FIELD. NO EVACUATION, SMOKE CLEARED ON LANDING. MX FOUND THE RT ENGINE NR3 CARBON SEAL TO BE FAULTY.  MX REPLACED RT ENGINE (TC NR 20071113010)                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
20080204001472008020400147SO  2008       2          4          CA071114001      120071022G2435                HOUSING                                 PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2B   41532EA  HARTZLHCE3Y HCE3YR2A    GL  STARTER GEN     FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       112        FN2407123                                           (CAN) MOTOR ATTACH BOLT PULLING OUT OF HOUSING. NOT AN INFLIGHT SAFETY CONCERN. (TC NR 20071114001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080204001462008020400146SO  2008       2          4          CA071114002      120071109G2435                CASE                                    PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  STARTER GEN     FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       50         FNR510603                                           (CAN) MOTOR ATTACH BOLT PULLING OUT OF HOUSING. (TC NR 20071114002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080204001452008020400145CE  2008       2          4          CA071114003      120070924G324631607           WHEEL                                   CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              MLG             CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2114                                                           (CAN) RIM WAS EDDY CURRENT INSPECTED FOR CRACKS IAW MM AND CORROSION PITS WERE FOUND ON RIMS (IB AND OB) WHERE TIRE MAKES AIR SEAL.  THE CORROSION PITS WERE MORE THAN 0.010 INCH ALLOWED AND WHEEL WAS SCRAPPED. (TC NR 20071114003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA22CE   E00053EN             
20080204001442008020400144WP  2008       2          4          CA071114004      120071005G2140C16932          SHROUD                                  ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              HEATER          CRACKED         W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA       1288                                                           (CAN) THE PILOT SMELLED EXHAUST FUMES IN THE CABIN WHILE IN CRUISE FLIGHT. THE PILOT THEN CLOSED THE HEATER CONTROL AND OPENED THE VENTS FOR FRESH AIR. THE PILOT THEN FLEW  BACK TO THE BASE FOR THE ENGINEER TO INSPECT.  THE ENGINEER FOUND A CRACK IN THE EXHAUST SYSTEM INSIDE THE HEAT SHROUD AT THE ELBOW WHERE THE EXHAUST EXITS THE MUFFLER. THE EXHAUST SYSTEM WAS THEN REPLACED WITH A NEW PART. (TC NR 20071114004)                                                                                                                                                                                                                                                                                                                 1G71 3O3  O  H11NM   1E4                  
20080204001432008020400143    2008       2          4          CA071114005      420071109G3418                TRANSMITTER                             PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  AOA             INOPERATIVE     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1873       0321                                                (CAN) DURING ROUTINE 150 HR INSP , LT AOA VANE HEAT WAS FOUND INOPERATIVE. PROBE AND PLATE HEAT WERE FUNCTIONING NORMAL. COMPLETE ASSY REPLACED. (TC NR 20071114005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080204001422008020400142CE  2008       2          4          CA071114006      120070928G2435300SGL129Q2     STARTER GEN                             CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                                              FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA            671                                                       (CAN) AC INFLIGHT HAD RT GENERATOR OUTPUT FLUCTUATING. CHECKED ON GENERATOR IAW MM WAS FOUND OK. BUT INFLIGHT FLUCTUATING, REPLACED GENERATOR AND PROBLEM WENT AWAY. (TC NR 20071114006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA22CE   E00053EN             
20080204001412008020400141EU  2008       2          4          CA071114007      120071012G6320BM1021          CHIP DETECTOR   UROCOP                  UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              M/R GEARBOX     SHORTED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       33         M672                                                (CAN) MAIN GEARBOX MAGNETIC CHIP PLUG SHORTED INTERNALLY. (TC NR 20071114007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G72 3U3  UNCR0001RD E34NE                
20080204001402008020400140CE  2008       2          4          CA071114008      120071102G3297                WIRE HARNESS                            CESSNA525   525         2076601CE                                                               BRAKES          SHORTED         W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) THE EMERGENCY BRAKE HAD TO BE USED UPON LANDING AS IT WAS DISCOVERED THAT THE ANTI-SKID WIRING HARNESS HAD A SMALL AMOUNT OF SLACK BETWEEN THE TRAILING LINK AND THE TRUNNION. THIS ALLOWED IT TO RUB AGAINST THE TIRE, WEARING OFF THE COATING AND UPON LANDING ON A WET SURFACE CAUSED SHORTING. (TC NR 20071114008)                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 4F    RTA1WI                         
20080204001392008020400139CE  2008       2          4          CA071114009      120070913G3211998100287       BRACE                                   BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCB4T HCB4TN3     GL  MLG TORQUE LINK CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA            6269                                                      (CAN) FLIGHT CREW CONDUCTED A CROSSWIND LANDING, SHUTDOWN, AND PASSENGERS DEPLANED ON REMOTE RAMP LOCATION. UPON TAXIING TO THE TERMINAL FOR THE NEXT FLIGHT, CREW NOTICED THE AIRCRAFT FELT DIFFERENT. MAINTENANCE WAS CALLED, AND A VISUAL INSPECTION FOUND THAT THE LT MLG TRUNNION BOSS ASSY HAD BROKEN AWAY. FURTHER INVESTIGATION REVEALED THE RT MLG WAS CRACKED IN THE SAME AREA. A HARD-LANDING INSPECTION WAS COMPLETED IAW CARS 625 APP G, AND  AMM 5-50-00 AS A PRECAUTIONARY MEASURE. MAIN LANDING GEAR ASSEMBLIES WERE REPLACED, SERVICED, AND GEAR SWINGS CONDUCTED IAW AMM. (TC NR 20071114009)                                                                                                                                 1L72 3T4  T  A14CE   E4EA    6  CP40EA    
20080204001382008020400138CE  2008       2          4          CA071114010      120071114G57510523809         RIB                                     CESSNA150   A150M       2071831CE  CONT  O200  O200A       17020SO  MCAULY1A102 1A102OCM    GL  LT AILERON      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9500 9500                                                      (CAN) AILERON CENTER RIB P/N 0523809 FOUND CRACKED MULTIPLE LOCATIONS ON FWD VERTICAL ANGLE COMMON TO CONTROL ROD ATTACH BRACKET.  IN ADDITION THE CONTROL ROD ATTACH BRACKET P/N 0760011-2 WAS ALSO CRACKED IN 2 LOCATIONS COMMON TO AILERON SPAR. (TC NR 20071114010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  3A19    E252    5  NP918     
20080204001372008020400137EU  2008       2          4          CA071115001      120071110G5343S53578400000    FITTING                                 AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF5       NE  MLG ACTUATOR    FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA       29987                                                          (CAN) DURING THE APPROACH, THE CREW HEARD A LOUD BANG WHEN THE LANDING GEAR WAS SELECTED DOWN. THE CREW DID NOT OBSERVE ANY OTHER WARNING INDICATIONS AND A NORMAL LANDING WAS COMPLETED. THE CREW CONDUCTED A POST LANDING CHECK AND FOUND THE LT MLG EXTENTION/RETRACTION ACTUATOR SEPARATED FROM THE AIRCRAFT. THE FUSELAGE MOUNTING FITTING HAD FAILED. THE AIRCRAFT MOVED FOR MAINTENANCE ACTION. THE COMPANY HAS INITIATED A FLEET CAMPAIGN TO INSPECT ALL ACTUATOR FITTINGS. (TC NR 20071115001)                                                                                                                                                                                                                                         2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080204001362008020400136EA  2008       2          4          CA071115002      120071024G3246L814749         BEARING                                 DHAV  DHC7  DHC7102     2802708EA  PWA   PT6   PT6A50      52043EA  HAMSTD24PF  24PF305     GL  WHEEL ASSY      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFTER LANDING THE LT OB MAIN WHEEL HUBCAP WAS DISCOVERED MISSING. FURTHER INVESTIGATION FOUND THE INNER BEARING WAS BLOWN APART, THE WHEEL AND BRAKE ASSY HAD EXTENSIVE DAMAGE FROM THE WHEEL RUBBING ON THE BRAKE ASSY. THE AXLE WAS INSPECTED, NO DAMAGE WAS FOUND. DUE TO ALL THE RAIN IN THE AREA, THIS AIRCRAFT IS OPERATING IN A EXTREMELY MUDDY ENVIRONMENT, WE SUSPECT THAT MUD AND WATER MAY HAVE ENTERED THE BEARING AREA CAUSING PREMATURE FAILURE OF BEARING. THIS BEARING HAD 144 LANDINGS SINCE NEW.  CURRENTLY, THE BEARINGS ARE INSPECTED AND RE-LUBRICATED AT THE (A) CHECK (150 HOURS). THIS INSPECTION ALONG WITH THE LUBRICATION OF THE LANDING GEAR WILL BE REDUCED TO 50 HOURS FOR THE DURATION OF THE OPERATION IN 2H74 4T4  T  A20EA   E4EA    6  CP1NE     
20080204001352008020400135GL  2008       2          4          CA071115003      220071115G72306871259         BOLT            ALLSN                                                      ALLSN 250C  250C20J     03013GL                              COMPRESSOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3486                               CAC43118                    (CAN) COMPRESSOR TIEBOLT S/N KU506716 FOUND CRACKED AXIALLY UPON REWORK AT MPI AFTER REMOVAL OF SILVER PLATING ON EXTERIOR OF PART. PART SCRAPPED.  CRACK WAS NOT DISCOVERED UPON INITIAL MPI, MOST LIKELY BECAUSE OF THE SILVER PLATE BRIDGING THE CRACK SURFACE.   SEM EVALUATION OF CRACK INDICATED A DEPTH OF APPROXIMATELY 600 MICRO METERS RADIALLY . EDS EVALUATION OF THE CRACK INDICATED THAT THE CRACK WAS FULL TO EXTREMITIES WITH IRON OXIDE. THIS APPEARS TO BE A MANUFACTURING DEFECT. NO ASSOCIATED DAMAGE OR SERVICE ISSUES NOTED ON REMAINDER OF COMPRESSOR ASSEMBLY. HARDNESS OF MATERIAL WAS WITHIN SPECIFICATIONS. FAILURE OF BOLT WOULD BE CATASTROPHIC. (TC NR 20071115003)                                                      3  U          E4CE                 
20080204001342008020400134EA  2008       2          4          CA071115004      120071115G7120CSP28229        BOLT                                    DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE MOUNT    DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1739                                                           (CAN) ENGINE MOUNT BOLTS THAT DAMAGED THE THREADS UPON REMOVAL. BOLTS WHERE INSTALLED ON 12/22/2005. (2) OF THE (4) TOP MOUNT BOLTS HAVE DAMAGED THREADS AND ARE NOT RE-USABLE. THREADS IN ENGINE CASE REQUIRE CLEAN-UP. (TC 20071115004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20080204001332008020400133EU  2008       2          4          CA071115005      120071115G6400355A12004008    TAIL ROTOR                              SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                                              OUT OF BALANCE  W      K   NONE                                                                                            EF VIBRATION/BUFFET          FLT CONT AFFECTED                                   ININSP/MAINT     1                      CA                                                                      (CAN) UNABLE TO BALANCE T/R WITH OUT LARGE AMOUNTS OF BALANCE WEIGHT. T/R WOULD GO OUT OF BALANCE EVERY 3 TO 4 DAYS. SENDING T/R TO MFG FOR EVALUATION. (TC NR 20071115005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  H9EU    E19EU                
20080204001322008020400132EA  2008       2          4          CA071115006      120071115G2497                BUSS BAR                                CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  DAMAGED         SPARKS          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                              1968                                    (CAN) CPB1 CENTER BUS BAR LINK W57PD SPARKING UNDER LOOSED SCREW.  BUS BAR W57PD AND W440PD REPLACED.  10029 DROPS (TC NR 20071115006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20080204001312008020400131NE  2008       2          4          CA071115007      120071114G6320SB2151107       BEARING                                 SKRSKYS76   S76C        8143008NE                                                               M/R GEARBOX     SPALLED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2969       A23100240                                           (CAN) MGB REMOVED DUE TO MAKING METAL, THE ABOVE BEARING WAS FOUND TO BE SPALLED (TC NR 20071115007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G72 3U    NCH1NE                         
20080131002622008013100262GL  2008       1          31         CA071115008      120071031G7602HF3M            BEARING         DIAMON                  DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  ROD END         SEIZED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       244                                                            (CAN) PILOT REPORTED MIXTURE STICKING DIFFICULT TO MOVE. INSPECTION REVEALED MIXTURE CONTROL ROD END AT MECHANICAL FUEL PUMP SEIZED. ROD END WAS REPLACED WITH NEW UNIT. THIS ROD END IS OF THE SAME PN WHICH SEIZED ON ANOTHER AIRCRAFT`S THROTTLE CONTROL WHICH RESULTED IN AN OFF AIRPORT LANDING AND DAMAGE TO THE AIRCRAFT BACK IN FEB. 2005. HOPING TO HAVE THE BEARING ANALYZED BY A LAB. (TC NR 20071115008)                                                                                                                                                                                                                                                                                                                            1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20080131002632008013100263EU  2008       1          31         CA071115009      120071115G6410355A12004008    TAIL ROTOR                              SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                                              UNBALANCED      W      K   NONE                                                                                            E  VIBRATION/BUFFET                                                              ININSP/MAINT     1                      CA       1067                                                           (CAN) EXCESSIVE AMOUNT OF TIP BALANCE WEIGHT TO BALANCE TAIL ROTOR. (TC NR 20071115009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  U  H9EU    E19EU                
20080131002642008013100264EA  2008       1          31         CA071115010      120071112G5312C6W11509        RIB                                     DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A34      52043EA  HARTZLHCB3T HCB3TN3     GL  WING            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       29229                                                          (CAN) RIB FLANGE FOUND CRACKED ON IB SIDE WHERE IT IS RIVETED TO THE TOP SKIN CORRUGATIONS. CRACKING FOUND WHEN INSPECTING RIBS 8-22 IAW MFG STRUCTURAL LIFE LIMITS. (TC NR 20071115010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20080131002652008013100265EA  2008       1          31         CA071115011      120071114G5532C6TFM102527     PLATE                                   DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  VERTICAL STAB   CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       31743                                                          (CAN) CRACK INDICATION FOUND IN A CORROSION PIT IN THE AFT ATTACH PLATE WHEN INSPECTING IT IAW SB 454. (TC NR 20071115011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20080131002662008013100266SW  2008       1          31         CA071116001      120071114G3040                SENSOR                                  SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  WINDSHIELD TEMP OVERHEATED      W      O   OTHER                                                                                           MB OVER TEMP                 SMOKE/FUMES/ODORS/SPARKS                            APAPPROACH       1                      CA       4805       87H0829830                                          (CAN) THE FOLLOWING WAS REPORTED BY THE FLIGHT CREW FOLLOWING THE CO-PILOTS HEATED WINDSHIELD FAILURE: (WHILE ON THE ILS FO MENTIONED A BURNING SMELL, AND NOTICED IT AS WELL.) TOOK MY FLASHLIGHT OUT BUT COULD NOT NOTICE ANY DETECTABLE SMOKE IN THE CABIN OR COCKPIT. CONTINUED THE APPROACH WITH BLEED HEAT OFF AND FRESH AIR FAN RUNNING. BY THE TIME WE LANDED, THE SMELL WAS STRONGER BUT COULD NOT SEE ANY SMOKE. ON THE GROUND WE SHUTDOWN THE ELECTRONICS AS SOON AS POSSIBLE AND THEN SHUT DOWN THE AIRCRAFT. PASSENGERS NOTICED THE SMELL IN THE BACK AS WELL. IT WAS OBVIOUS THAT IT WAS AN ELECTRICAL SMELL, AND THERE WAS SMOKE EVIDENT WHEN WE TOOK OUT OUR FLASHLIGHTS AGAIN ON THE GROUND.  UPON INSPECTION BY MAINTENANCE IT2L72 4T4  TRTA8SW    E4WE    5  CP10NE    
20080131002672008013100267CE  2008       1          31         CA071116002      120071115G36101013800273      REGULATOR VALVE                         BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  PNEUMATIC PRESS INOPERATIVE     W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA            210                                                       (CAN) WHILE IN CRUISE FLIGHT AT FL230 THE FLIGHT CREW OBSERVED THE PNEUMATIC PRESSURE GUAGE RAPIDLY FLUCTUATING BETWEEN 18 AND 23 PSI. THERE WAS AN ASSOCIATED CHATTERING HEARD IN THE AIRFRAME, IN CONJUNCTION WITH THE FLUCTUATING INDICATOR. FLIGHT CREW DECIDED TO RETURN TO BASE AND PNEUMATIC INDICATIONS RETURNED TO NORMAL DESCENDING THROUGH 15,000 FEET AND REMAINED THAT WAY TO LANDING. MAINTENANCE REPLACED PNEUMATIC PRESSURE VALVE/REGULATOR PN 101-380027-3 (PN 1H75-12). (TC NR 20071116002)                                                                                                                                                                                                                                   2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20080131002692008013100269EA  2008       1          31         CA071118001      120071115G2730510009          ROD END         MENASCO     510009      CNDAIRCL600 CL6002D24   1390016EA  GE    CF34  CF348C5     30050NE                              PCU             BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  MAL2449                                             (CAN) REPORT FROM AIR ONE:  REF /A/ - AIPC 27-33-01, FIG 1  WHILE PERFORMING TASK CARD 000-27-220-010 - OPERATIONAL TEST OF THE ELEVATOR PCUS, AIR ONE FOUND THAT WITH HYD 1 ONLY, THE ELEVATOR WOULD NOT MOVE.  AFTER INSPECTION, THEY FOUND THAT PCU 1 ROD END (ON THE ELEVATOR ATTACHING LUG) WAS BROKEN IN (2) PIECES AT THE PCU PISTON THREADS.  PRIOR REMOVING ANYTHING, IT WAS NOTICED THAT THE ROD END SEEMED JAMMED (UNABLE TO TURN THE ROD END AROUND THE BOLT) ON ITS ATTACHING BOLT (REF /A/ ITEM 275)  WHILE ATTEMPTING TO REMOVE THE BROKEN ROD END, THE ATTACHING NUT (REF /A/, ITEM 295) WAS EASILY REMOVABLE. HOWEVER, IT WAS NOT POSSIBLE TO TURN OR REMOVE THE BOLT (REF /A/, ITEM 275) FROM THE ELEVATOR PCU FITTING (REF SR2L72 4F4  FRTA21EA   E00063EN             
20080131002702008013100270EA  2008       1          31         CA071118002      120071108G5610NP13932113      WINDSHIELD                              CNDAIRCL600 CL6002C10   1390015EA  GE    CF34  CF348C5B1   30052NE                              COCKPIT         CRACKED         W      B   EMER. DESCENT                                                                                   O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) IN FLIGHT LT WINDSHIELD CRACKED, AIRCRAFT CONTINUED TO DESTINATION. NO FURTHER REPORTED DETAILS. (TC NR 20071118002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA21EA   E00063EN             
20080131002712008013100271    2008       1          31         CA071119001      420071106G2210065008617       CONTROL MODULE                          PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  EADI            INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) (ALT) LAMP DID NOT ILLUMINATE ON MODE CONTROL. ALTITUDE CAPTURE WAS NORMAL WITH ALT CAPTIONS (ON) AS DISPLAYED ON BOTH EADI SCREENS. (TC NR20071119001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080131002722008013100272    2008       1          31         CA071119002      420071115G3497                CONNECTOR                               PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  OAT INDICATOR   DAMAGED         W      O   OTHER                                                                                           N  FALSE WARNING                                                                 CRCRUISE         1                      CA       7326                                                           (CAN) OAT INDICATION ON EIS ERRACTIC. ONE OF THE PINS IN OAT CONNECTOR FOUND LOOSE. NEW CONNECTOR INSTALLED WITH 2 NEW PINS. SYSTEM NORMAL.  (TC NR 20071119002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080131002732008013100273EU  2008       1          31         CA071119003      120071115G31100660312525      DISPLAY                                 PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  EADI            INTERMITTENT    W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) PILOT`S EADI DISPLAY REPORTED TO GO (FUZZY) AND INTERMITTENTLY GOING BLANK. ED462 REPLACED WITH SERVICEABLE UNIT. (TC NR 20071119003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080221000042008022100004NM  2008       2          21         CA071120001      120071115G291082970010149     LINE                                    DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  HYD SYSTEM      CHAFED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            DEDESCENT        1                      CA       20516                                                          (CAN) AIRCRAFT WAS RETURNING TO BASE WHEN THE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. UPON SELECTION OF GEAR DOWN A LOUD (BANGING) NOISE WAS HEARD. GEAR EXTENDED NORMALLY, ALTHOUGH THE LOW PRESSURE LIGHTS WERE FLICKERING IN CONJUNCTION WITH THE (BANGING) NOISE. AC WAS PLACED IN HANGER AND HYDRAULIC SYSTEM INSPECTED. THE RESERVOIR WAS FOUND TO BE LOW. RESERVOIR WAS REFILLED AND HYDRAULIC SYSTEM BLED, IT WAS AT THIS TIME THAT FLUID WAS OBSERVED TO BE LEAKING FROM ABOVE THE NR 2 ENGINE EXHAUST PIPE.  UPON FURTHER INSPECTION THE PRESSURE LINE (82970010-149, PRE-MOD 8/670) WAS FOUND TO BE SEVERELY CHAFED. IT APPEARS TO HAVE BEEN CHAFED BY SPIRAL WRAP APPLIED TO THE SUCTION LINE, THE LINE WAS ALSO CLAMPED, BUT IMPR2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080221000052008022100005NE  2008       2          21         CA071120002      220071115G7230                COMPRESSOR                              SAAB  SF340 340B        7860101EU  GE    CT7TP CT79B       30030NE  ROTOL R390  R3904123F27 NE  ENGINE          STALLED         W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA       259724926                          GEE785555                   (CAN) TAKEOFF ROLL HAD NO PROBLEMS, BUT WHEN CHANGING THROTTLE SETTING FROM CLIMB POWER TO CRUISE POWER THE LT ENGINE EXPERIENCED A COMPRESSOR STALL. THEN THE A/C YAWED, THEN ANOTHER COMPRESSOR STALL OCCURRED AND THE (ENGINE) OVER TEMP`D.   LITE FOR THE ITT CAME ON, THE PILOTS THEN SHUT THE LT ENGINE DOWN AND RETURNED TO AIRPORT ON THE RT ENGINE. (TC NR 20071120002)                                                                                                                                                                                                                                                                                                                                                                2L72 4T4  TRTA52EU   E8NE    6  CP31NE    
20080221000062008022100006SW  2008       2          21         CA071120004      120071116G6420476411731       SHIM            BELL                    BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              T/R HUB         INOPERATIVE     W      O   OTHER                                                                                           E  VIBRATION/BUFFET                                                              NRNOT REPORTED   1                      CA                  A3402                                               (CAN) T/R VIBRATION DISCOVERED AND SUBSEQUENT STROBING WAS NOT EFFECTIVE AT REMOVING THE VIBRATION. DURING INSPECTION OF THE T/R HUB ASSEMBLY WAS FOUND TO HAVE BOTH PRE AND POST (TB: 206-91-139) METHODS OF TRUNNION CENTERING PERFORMED. SHIM 120-006C15-0 AND THRUST PLUG 47-641-173-1 USED ON ONE SIDE AND SHIM 206-011-861-101 AND THRUST PLUG 206-011-862-101 USED ON THE OTHER. TAIL ROTOR HUB ASSEMBLY WAS REPAIRED. (TC NR 20071120004)                                                                                                                                                                                                                                                                                               1G71 3U3  U  H2SW    E4CE                 
20080204001302008020400130    2008       2          4          CA071120005      420071119G3160066031252500    DISPLAY                                 PILATSPC12  PC1245      7090551EU  PWA   PT6   PT6A67B     52043NE  HARTZLHCE4A HCE4A3D     GL  COCKPIT         INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) PILOT REPORTED LT EHSI WENT BLANK AND BACK ON TWICE DURING FLIGHT. DEFECT WAS CONFIRMED IN THE HANGAR AS THE DISPLAY WENT BLANK APPROX. 3 MINUTES AFTER POWER UP. (TC NR 20071120005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L71 3T4  TRTA78EU   E26NE   5  CP210NE   
20080204001292008020400129EU  2008       2          4          CA071120006      120071106G2140704A34402034    HOSE                                    SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              HEATER          BURST           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) HEATER LINE FROM ENGINE FOUND BURST AND NOT SUPPLYING ALL THE HEAT TO THE CABIN. (TC NR 20071120006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1G71 3U3  U  H9EU    E19EU                
20080221000072008022100007EU  2008       2          21         CA071120007      120071110G7921350A5310520351  BLOWER MOTOR                            SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              OIL COOLER      UNSERVICEABLE   W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) HEARD NOISE AFTER LANDING AND SHUT THE AIRCRAFT DOWN. UPON INSPECTION FOUND THE BLOWER ROTOR COMPLETELY GONE. REPLACED THE ROTOR, DUCT AND MOTOR TO GET THE AIRCRAFT SERVICEABLE. (TC NR 20071120007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  H9EU    E19EU                
20080221000082008022100008GL  2008       2          21         CA071121001      320071118G6111                BUSHING                                 CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  PROP HUB        WORN            W      A   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      CA       3729                                           962459          (CAN) THE PILOTS FELT A VIBRATION ON CLIMB. THEY REDUCED THE POWER BUT THE VIBRATION REMAINED. THEY RETURNED TO THE AIRPORT WHERE THE AME INSPECTED THE ENGINE AND PROPELLER. NO DISCREPANCIES WERE NOTED ON THE ENGINE. ONE BLADE OF THE PROP WAS ABLE TO BE TWISTED BY HAND APPOX 3-5 DEGS. WE SUSPECT A FAILURE OF A BUSHING IN THE HUB AND HAVE SENT A REPLACEMENT PROP BEFORE FURTHER FLIGHT. (TC NR20071121001)                                                                                                                                                                                                                                                                                                                           1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20080221000092008022100009SW  2008       2          21         CA071121003      120071115G2497AN3230          SWITCH                                  SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE331*     01514WP  MCAULY4HFR344HFR34C652  NE  BUSS TIE        BURNED          W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) PILOT REPORTED STRANGE SMELL COMING FROM LT BLEED IN COCKPIT. AFTER TROUBLESHOOTING BY MAINTENANCE IT WAS FOUND THAT LT ESSENTIAL BUS TIE SWITCH WAS CRACKED AND THE WIRE CONNECTORS GOING TO THE LT CB PANEL HAD BECOME OVERHEATED AND MELTED THE HEAT SHRINK AND THE RUBBER PROTECTIVE BOOT AT THE TERMINALS. BUS TIE SWITCH REPLACED AND BOTH CONNECTORS REPAIRED. (TC NR 20071121003)                                                                                                                                                                                                                                                                                                                                                 2L72 4T3  TRTA8SW    E2WE    6  C3PNE     
20080221000102008022100010NM  2008       2          21         CA071121004      120071120G2150                TURBINE                                 DORNERDO32  DO328100    2996000NM  PWA   119   PW119C           NE  HARTZLHDE6C HDE6C3B     NE  A/C PACK        SEIZED          W      D   RETURN TO BLOCK                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA       350                                                            (CAN) AIRCRAFT DEVELOPED WHITE SMOKE IN CABIN WHILE TAXING FOR TAKEOFF. PILOTS NOTICED A CAS LT PACK FAIL LIGHT AND AN AFT LAV SMOKE DETECT CAS MESSAGE. AIRCRAFT RETURNED TO BLOCKS AND PASSENGERS DEBOARDED. CAUSE OF SMOKE WAS TURBINE SEIZED CAUSING A LT PACK OVERHEAT. ENVIROMENTAL CONTROL UNIT (ECU) REPLACED. (TC NR 20071121004)                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA45NM   E20NE   6  CP34NE    
20080221000112008022100011EU  2008       2          21         CA071122001      120071116G3234F10A793         CONTROL HANDLE                          AMD   FALC10FALCON10    2730101EU  GARRTTTFE731TFE7312     01518WP                              MLG EMER EXTEND INOPERATIVE     W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA       5874                                                           (CAN) DURING THE CLIMB, THE LT MAIN LANDING GEAR INTRANSIT STAYED ON DURING GEAR RETRACTION. THE CREW FLEW BACK TO DEPARTURE WITH THE GEAR DOWN. AFTER THEY LANDED AT DEPARTURE AIRPORT. WE INSPECTED THE GEAR IAW THE MM AND CAR 605.88. IT WAS FOUND THAT THE MANUAL EMERGENCY HANDLE WAS OFF SET SLIGHTLY CAUSING THE GEAR NOT TO FULLY LOCK IN THE UP POSITION. THE EMERGENCY CONTROL SYS WAS RESET IAW THE MM. SATISFACTORY GEAR SWINGS WERE CARRIED OUT.  CALLED FOR A TEST FLIGHT, THE TEST FLIGHT WAS CARRIED OUT WITH NO FAULTS. (TC NR 20071122001)                                                                                                                                                                                   2L72 4F4  F  A33EU   E6WE                 
20080221000122008022100012CE  2008       2          21         CA071122002      120071121G3210508103237       TORQUE LINK                             BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  MCAULY4HFR344HFR34C762  NE  MLG             CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A SPECIAL LPI INSP (SELF IMPOSED INSPECTION DUE TO BROKEN LINK SEE SDR NR 2007024010) OF THE UPPER AND LOWER TORQUE LINKS ON (2) OF OUR AC, (3) TORQUE LINKS WERE FOUND CRACKED IN THE RADIUS AREA.  ONE LINK HAS 2 CRACKS SIDE BY SIDE THE OTHER HAD ONE SMALLER CRACK. THE CRACK IN THE THIRD LINK WAS VERY SMALL AND DID NOT SHOW IN THE PHOTOS. (TC NR 20071122002)                                                                                                                                                                                                                                                                                                                                                            1L72 3T4  T  A14CE   E4EA    6  C3PNE     
20080221000162008022100016NM  2008       2          21         CA071122003      120071122G3246296852629       BEARING                                 BOMBDRDHC8  DHC8400            NM                                                               NR 4 WHEEL      FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1584 70                                                        (CAN) WHILE SERVICING THE MAINT OBSERVED SWARF AND GREASE AROUND THE HUBCAP OF NR 4 MAIN WHEEL ASSY. IB BEARING HAD FAILED. (TC NR 20071122003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T    RTA13NM                        
20080221000172008022100017SW  2008       2          21         CA071122004      120071123G281071494R          TANK                                    BBAVIA8     8GCBC       1220803SW  LYC   O360  O360C2E     41514EA  MCAULY1A200 1A200*      GL  FUEL SYS        CRACKED         W      K   NONE                                                                                            KB FLUID LOSS                SMOKE/FUMES/ODORS/SPARKS                            ININSP/MAINT     1                      CA       3206                                                           (CAN) AIRCRAFT WAS IN FOR A 50 HR INSPECTION. AFTER ENGINE RUN UP, MECHANIC DETECTED GAS FUMES AND LOOKED ON THE RT SIDE ON THE AC WINGS NEAR TRAILING EDGE NOTICE FUEL STAINING. RT OB TANK WAS REMOVED AND 1 INCH CRACK WAS FOUND ON THE RADIUS OF THE LATERAL RE-ENFORCEMENT INDENT OF TANK. (TC NR 20071122004)                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  O  A21CE   E286    5  NP874     
20080221000182008022100018NM  2008       2          21         CA071122006      120071109G3230656021132       ACCESSORY UNIT                          BOEING727   727223      1384074NM  PWA   JT8   JT8D15      52051NE                              MLG             INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) THE CREW DISCOVERED THAT THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE (OFF) POSITION WITHOUT THE USE OF THE OVERRIDE TRIGGER. AT THE TERMINATING STATION, MAINTENANCE REPLACED THE LANDING GEAR ACCY UNIT AND RETURNED THE AIRCRAFT TO SERVICE. (TC NR 20071122006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L73 4F4  F  A3WE    E2EA                 
20080221000192008022100019NE  2008       2          21         CA071122007      220071121G7414BL600646201     MAGNETO                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       1242 1242                                                      (CAN) ENGINE START ATTEMPTED, RT MAGNETO FAILED TO OPERATE. (TC NR 20071122007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3O3  O  H11NM   1E4                  
20080221000202008022100020SO  2008       2          21         CA071123001      120071120G8120                BEARING         GARRTT                  PIPER PA31  PA31        7103102SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  TURBOCHARGER    FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       357  357   JJR00638                                            (CAN) DURING A RT ENGINE INSPECTION AN EXHAUST STAIN WAS WAS NOTICED IN THE AREA OF THE TURBOCHARGER.  UPON CLOSER INVESTIGATION, IT WAS DISCOVERED THAT THE TURBOCHAGERS EXHAUST BEARING SEAL BETWEEN THE COMPRESSOR AND TURBINE HAD FAILED. THE TURBO WAS REPLACED AND AC RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. (TC NR 20071123001)                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080221000212008022100021EU  2008       2          21         CA071123002      120071123G7700                ENGINE                      ARRIEL2B    SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                                              MALFUNCTIONED   W      R   AUTOROTATION                                                                                    J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          22360                       (CAN) PILOT IN CRUISE FLIGHT, APPROX 2000 FEET, EXPERIENCED ENGINE PROBLEMS WITH ANNUNCIATOR INDICATIONS . PROCEEDED WITH SUCCESSFUL AUTOROTATION LANDING IN FIELD.  REST IS UNDER INVESTIGATION (TC NR 20071123002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3U3  U  H9EU    E00054EN             
20080221000222008022100022CE  2008       2          21         CA071123003      120071122G7120595104814       MOUNT                                   CESSNA425   425         2076018CE  PWA   PT6   PT6A112     52043NE  MCAULY4HFR344HFR34C762  NE  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6126                                                           (CAN) WHILE PERFORMING MFG 100 HR ENGINE INSPECTION ON THE RT ENGINE, THE OB ENGINE MOUNT WAS FOUND CRACKED. THE MOUNT WAS REPLACED WITH A NEW UNIT. (TC NR 20071123003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T3  TRTA7CE    E4EA    6  C3PNE     
20080221000232008022100023EA  2008       2          21         CA071123004      120071116G5610NP1393226       WINDOW                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) RT SIDE WINDOW CRACKED ON FLIGHT. AC RETURNED.  NO FURTHER INFORMATION REPORTED BY CREW.  RT SIDE WINDOW CHANGED AND AC RETURNED TO SERVICE. (TC NR 20071123004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20080221000242008022100024WP  2008       2          21         CA071123005      220071122G7210                REDUCTION GB                            BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33110    01514WP  ROTOL R333  R333482F12  GL  LT ENGINE       FAILED          W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA       189254525                          P63283                      (CAN) WHILE IN CRUISE AT 16000 FT,  A THUMP WAS FELT AND HEARD FROM THE LT ENGINE.  A LARGE POWER DROP WAS NOTICED THEN A SECOND THUMP FROM THE LT ENGINE WHICH WAS FOLLOWED BY THE OIL CAP ANNUNCIATION ILLUMINATION.  IMMEDIATELY TURNED BACK AND SHUT THE ENG DOWN. ATC, COMPANY, AND PASSENGERS WERE ADVISED AND REQUESTED THE EMERGENCY VEHICLES BE ON STANDBY, THE REMAINDER OF THE FLIGHT AND LANDING WERE UNEVENTFUL.  MAINT INSP OF LT ENGINE REVEALED LIMITED ENGINE ROTATION WHEN TURNING THE PROP, INDICATING RGB INTERNAL COMPONENT/S FAILURE. LT ENGINE CHIP DETECTOR AND OIL FILTER WERE REMOVED AND METAL CONTAMINATION WAS OBSERVED IN BOTH AREAS. THE ENGINE WAS REMOVED FOR SHIPMENT TO A REPAIR FACILITY FOR TEAR DOWN DAMAG2L72 4T4  TRTBA15CAA E4WE    6  CP61GL    
20080221000252008022100025NE  2008       2          21         CA071126001      220071123G731087620102007015  CONTROL ROD                             DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  FUEL SYS        SEPARATED       W      C   ABORTED TAKEOFF                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  TOTAKEOFF        1                      CA                                                                      (CAN) ON TAKEOFF ROLL, THE NR 1 ENG PROPELLER RPM ONLY REACHED 900 RPM (NORMAL 1200RPM) AND THE TORQUE INDICATION REACHED 115 PERCENT FOR APPROX  2 SECONDS. POWER LEVERS WERE RETARDED TO FLIGHT IDLE AND THE TAKEOFF ABORTED, AC RETURNED TO THE GATE. THE PROPELLER WOULD NOT FEATHER NORMALLY SO MANUAL FEATHER WAS SELECTED TO FEATHER AND WHEN THE FUEL CONDITION WAS SET TO SHUTOFF, THE ENGINE DID NOT SHUTDOWN AND THE FIRE T-HANDLE HAD TO BE PULLED TO SHUTDOWN.  MAINT INVESTIGATED AND IT WAS FOUND THAT THE FUEL CONDITION CONTROL ROD HAD SEPARATED, THEREFORE THERE WAS NO FUEL SHUTOFF CONTROL.  THE FUEL CONDITION CONTROL ROD WAS REPLACED (PN 87620134-003 INSTALLED, 72-20-00-05-150) AND THE AC RETURNED TO SERVICE. (TC N2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080221000262008022100026GL  2008       2          21         CA071126002      320071110G61101192            DIAPHRAGM                               NAVIONSTC   STCNAVION              CONT  E225  E2254       17015SO  HARTZLHC12X HC12X207    GL  PROPELLER       SPLIT           W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  DEDESCENT        1                      CA                                                      NAV4779         (CAN) RUBBER ON DIAPHRAM WAS FOUND SPLIT AT INNER SECTION. UNCERTAIN AS TO WHY THE RUBBER APPEARED STIFFER THAN THE PREVIOUS DIAPHRAM. THE DIAPHRAM IS BEING RETURNED TO MFG FOR INSP.  WILL UPDATE WHEN RECEIVE THE INFORMATION BACK FROM THE MFG. (TC NR 20071126002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3O3  O  A782    E267    5  CP845     
20080221000272008022100027EA  2008       2          21         CA071126003      120071123G2750855D1009        BPSU                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              TE FLAP         UNSERVICEABLE   W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA       2    2                                                         (CAN) FLAP FAIL CAUTION MESSAGE ILLUMINATED WHILE IN CRUISE AND FLAPS WERE AT 0 DEG. FLAPLESS LANDING C/O AND A/C LANDED SAFELY. MAINT RANG OUT WIRES AND COULD NOT FIND ANY FAULTS. THE FECU AND THE RT BPSU WERE REPLACED. A TEST FLIGHT WAS C/O TO COLD SOAK TEMPERATURES FOR (2) HOURS AND THE A/C TESTED SERVICEABLE. THERE HAS NOT BEEN A REOCCURRENCE AT THIS TIME.  (TC NR 20071126003)                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
20080221000282008022100028CE  2008       2          21         CA071126006      120071106G801135016R          GEAR                                    CESSNA150   150L        2071826CE  CONT  O200  O200A       17020SO  MCAULY1A101 1A101HCM    GL  STARTER         BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA            360                           814153R                     (CAN) STARTER DRIVE ENGAGES ON TEETH ON GEAR. STARTER WAS SLIPPING, TOOK APART TO EXAMINE AND FOUND 3 BROKEN TEETH. STARTER IS LIGHT WEIGHT. REPLACE STARTER SOLENOID 19 HOURS EARLIER AND BELIEVE FAULTY SOLENOID CAUSE OF PROBLEM. (TC NR 20071126006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  O  3A19    E252    5  NP918     
20080221000292008022100029WP  2008       2          21         CA071126007      220071108G720021190108000     COMPUTER                                BRAERODH125 BAE125800A  1500285EU  GARRTTTFE731TFE7315R    01518WP                              DEEC            INOPERATIVE     W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       7                                                              (CAN) ENGINES FRESH, NEW INSTALLATION OF DEECS ON AC. DEEC PROBLEMS OCCURRED.  THE PROBLEM ENCOUNTERED WITH DIGITAL ENGINE COMPUTERS (DEEC). (TC NR 20071126007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA3EU    E6WE                 
20080221000302008022100030EA  2008       2          21         CA071126008      120071122G2420766283C         GCU                                     CNDAIRCL600 CL6002D24   1390016EA  GE    CF34  CF348C5     30050NE                              NR 2            FAILED          W      A   UNSCHED LANDING                                                                                 H  ELECT. POWER LOSS-50 PC                                                       CRCRUISE         1                      CA                                                                      (CAN) ACCORDING TO THE CREW WRITE UP: NR1- HYD 3A FAILED ( HYP PUMP 3A CAUTION MSG POSTED) ELECTRICALLY POWERED BY AC BUS NR2 - (GEN2 FAILED) WE DID NOT GET A AMBER GEN FAIL INDICATION OR WARNING. AC BUS 2 FAILED AGAIN, NO WARNING. TRU 2 AND ESS TRU FAILED, NO WARNING. GEN AND IDG PINK ON SYNOPTIC PAGE AND PURPLE DASH LINES FOR KVA, V, HZ. GEN1 DID NOT PICK UP AC BUS 2.  MAINTENANCE RAN THE ENGINES, CYCLED THE IDG SW (AUTO/OFF/RESET), COULD NOT DUPLICATE.  PLACED A GCU ON ORDER. BASED ON THE MDC INFORMATION.  GCU  NR 2 REPLACED. (TC NR 20071126008)                                                                                                                                                                    2L72 4F4  FRTA21EA   E00063EN             
20080221000312008022100031EA  2008       2          21         CA071126009      120071123G71102285000808      COWLING                                 CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              NACELLE         BROKEN          W      K   NONE                                                                                            D  INFLIGHT SEPARATION                                                           ININSP/MAINT     1                      CA                                                                      (CAN) UPON LANDING, DURING THE OPERATION OF NR1 THRUST REVERSER THE NR 1 ENGINE UPPER FAN COWL DEPARTED THE AC.  THE PILOTS DID NOT NOTICE THAT THE COWLING WAS MISSING UNTIL THEY DID THEIR POST FLIGHT WALK-AROUND. THE COWLING WAS LATER FOUND BY AIRPORT OPERATIONS ON THE AIRFIELD OFF THE SIDE OF THE RUNWAY. THE COWLING WAS FOUND TO BE BROKEN IN HALF WHEN IT WAS RECOVERED. THE FAA STILL HAS POSSESSION OF THE COWING AT THIS TIME. (WILL ADD COWL SN WHEN THEY ARE MADE AVAILABLE) (TC NR  20071126009)                                                                                                                                                                                                                             2L72 4F4  FRTA21EA   E15NE                
20080221000322008022100032NE  2008       2          21         CA071126010      120071122G6320S613566300      GEARBOX                                 SKRSKYS61   S61N        8142104NE  GE    CT58  CT581402    30011NE                              MAIN ROTOR      MAKING METAL    W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       30833961                                                       (CAN) INTERMEDIATE GEAR BOX CHIP LIGHT ILLUMINATED IN FLIGHT. AFTER LANDING CHIP PLUG INSPECTION CONFIRMED METAL CONTAMINATION, AS WELL AS PAINT DISCOLORATION WAS NOTED IN THE INPUT BRG AREA.  ASSY WILL BE SENT TO OH SHOP FOR INVESTIGATION. (TC NR 20071126010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2G72 4U4  U  1H15    1E3                  
20080221000332008022100033SW  2008       2          21         CA071126011      120071113G6320212030154101    FITTING         BELL                    BELL  205   205A1       1181414SW  LYC   T53   T5317BLYC   41616NE                              LIFT BEAM       BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING THE INSPECTION OF THE LIFT LINK AREA, A CRACK WAS NOTED ON THE LIFT LINK FITTING. UPON FURTHER INVESTIGATION THE AFT EAR WAS COMPLETLY BROKEN FROM THE FITTING. THE BOLT SECURING THE LIFT LINK TO THE FITTING WAS INCORRECT FOR THAT PN OF FITTING. THE BOLT DID FIT THE AFT EAR HOWEVER THERE WAS A .030 INCH GAP BETWEEN THE BOLT AND BUSHING IN THE FWD EAR ALLOWING THE BOLT TO ROCK UP AND DOWN IN THE FITTING. THIS ROCKING MOTION OCCURRED EVERY TIME IT WAS UNDER LOAD, AND STRESSED THE AFT EAR SUBSEQUENTLY CAUSING IT TO CRACK. THE TRANSMISSION WAS INSTALLED IN 2001. ALL ENGINEERS MUST BE CERTAIN WHEN INSTALLING FASTERNERS OR COMPONENTS THAT CORRECT PARTS ARE BEING USED ESPECIALLY WHEN DISASSEMBLY WHEN OFTEN1G71 4U4  U  H1SW    E17EA                
20080221000342008022100034SW  2008       2          21         CA071126012      120071121G5302206030446001    BULKHEAD        BELL                    BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              TAILBOOM        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  BCJN07214                                           (CAN) LT AFT MOUNTING HOLE FOR T/R GEARBOX FOUND CRACKED. (TC NR 20071126012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G71 3U3  U  H2SW    E4CE                 
20080221000352008022100035EU  2008       2          21         CA071127001      120071120G29133508806         PUMP                                    AIRBUS310   A310304     3930339EU  GE    CF6   CF680C2A5        NE                              HYD SYSTEM      CRACKED         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA            180                                                       (CAN) DURING CRUISE, THE YELLOW HYD SYS OVERHEAT ECAM MESSAGE CAME ON. LATER THE HYD RESERVOIR (LO LEVEL) WARNING CAME ON THE ECAM. NORMAL QRH PROCEDURE WAS PERFORMED. DURING INVESTIGATION, MAINT FOUND YELLOW HYD PUMP LEAKING. HYD PUMP CASING WAS CRACKED. PUMP AND FILTERS WERE REPLACED AND AC RETURN TO SERVICE. UNSERVICEABLE PUMP WAS ROUTED TO REPAIR SHOP FOR INVESTIGATION. (TC NR 20071127001)                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA35EU   E13NE                
20080221000362008022100036EU  2008       2          21         CA071127002      120071121G2530HE62190         COFFEEMAKER                             AIRBUS310   A310300     3930305EU  GE    CF6   CF680C2A5        NE                              GALLEY          SPARKS          W      H   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA       207831782                                                      (CAN) DURING FLIGHT, THE F/A REPORTED THE FWD COFFEE MAKER/WATER BOILER OVERHEATING AND NOTICED SOME SPARK COMING FROM THE UNIT. THE UNIT WAS DEACTIVATED. THE UNIT WAS REPLACED BY MAINTENANCE AND ROUTED TO THE REPAIR SHOP FOR INVESTIGATION. (TC NR 20071127002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA35EU   E13NE                
20080221000372008022100037WP  2008       2          21         CA071127003      120071126G6210C1591           BEARING         ROBSIN                  ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              M/R BLADE       SPALLED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       652        5470A                                               (CAN) WHILE CONDUCTING A DI, THE M/R BLADE BOOT WAS FOUND DISTORTED. THE BOOT WAS REPLACED AND A CHECK OF THE SPINDLE BEARINGS WERE FOUND TO BE ROUGH. FURTHER INVESTIGATION REVEALED THE NR 6 BEARING INNER RACE WAS FOUND SPALLING. BEARING REPLACED AND ASSY REINSTALLED. (TC NR 20071127003)                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3O3  O  H11NM   E295                 
20080221000382008022100038WP  2008       2          21         CA071127004      120071120G6730D2121           SERVO                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                                              LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1848                                                           (CAN) WHILE CARRYING OUT A 100 HOUR INSPECTION THE FWD LT SERVO WAS FOUND LEAKING. THE SERVO WAS CHANGED, GROUND RUN AND LEAK CHECK CARRIED OUT WITH OUT FURTHER INCIDENT. (TC NR 20071127004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3O3  O  H11NM   1E4                  
20080221000392008022100039NE  2008       2          21         CA071127005      220071125G7314LW15473         PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL SYS        FAILED          W      C   ABORTED TAKEOFF                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA       355                                                            (CAN) WHEN PILOT TRIED TO PULL THE AC UP IN A HOVER, THE ENGINE DECELERATED (BOGGED DOWN) UNTIL THE COLLECTIVE WAS LOWERED. THIS WAS TRIED SEVERAL TIMES WITH NO SUCCESS. ALL INDICATIONS WERE NORMAL, TEMPS, PRESSURES, MAG DROPS, ETC.  WHILE WAITING FOR THE ENGINEER TO ARRIVE ON SITE, THE PILOT GROUND RAN THE AC FOR 40 MIN TO WARM IT UP AND TRIED TO PULL POWER AGAIN. THIS TIME THE AC LIFTED UP NORMALLY WITH NO SYMPTOMS WHATSOEVER. WHEN THE ENGINEER ARRIVED THE AC WAS INSPECTED AND NO DEFECTS WERE FOUND. A 5 MIN TEST FLIGHT WAS COMPLETED WITH NO ABNORMAL SYMPTOMS. THE AC WAS SHUTDOWN AND REFUELED TO BE REPOSITIONED TO ANOTHER LOCATION.  AFTER RE-STARTING AND WHILE TRANSITIONING FROM A HOVER TO FWD FLIGHT, THE ENGI1G71 3O3  O  H11NM   1E4                  
20080221000402008022100040SW  2008       2          21         CA071127006      120071122G5302                BULKHEAD                                BELL  206   206B        1181511SW  ALLSN 250C  250C20B     03013GL                              TAILBOOM        CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) AFT BULKHEAD P/N 206-030-446-001F CRACKED AT RT GEARBOX MOUNTING HOLE. (TC NR 20071127006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3U3  U  H2SW    E4CE                 
20080221000412008022100041SO  2008       2          21         CA071127007      120071122G8120LW12778         BUTTERFLY VALVE LYC         LTIO540J2BD PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          WARPED          W      C   ABORTED TAKEOFF                                                                                 R  PARTIAL RPM/PWR LOSS                                                          TOTAKEOFF        1                      CA            1487  RL145668A                                           (CAN) THE AC WOULD NOT GET FULL POWER ON THE RT ENGINE. AFTER A RUNUP ALL PARAMETERS WERE NORMAL AND THE TAKEOFF RESUMED. MAINT INSPECTED THE ENGINE AND FOUND THE BUTTERFLY VALVE TUBE THAT GOES OVER THE SHAFT WAS WARPED AND SPLIT. THIS WAS PROBABLY CAUSING AN INTERMITTENT STICKINESS IN THE BUTTERFLY. THE WASTEGATE WAS REPLACED WITH NO FURTHER ISSUES. (TC NR 20071127007)                                                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080221000422008022100042EA  2008       2          21         CA071127008      120071121G5610NP13932114      WINDSHIELD                              CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) F/O WINDSHIELD SHATTERED OUTSIDE LAYERS AT FL340. (TC NR 20071127008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA21EA   E15NE                
20080221000432008022100043EA  2008       2          21         CA071127009      120071120G561013932113        WINDSHIELD                              CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              COCKPIT         CRACKED         W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CLCLIMB          1                      CA                                                                      (CAN) CLIMBING THROUGH 32,400 ON OUR WAY TO 34,000 WE HEARD A POP AND SAW THE PILOTS WINDSHIELD CRACK/ SPLINTER. FOLLOWED QRH AND CONTINUED TO DESTINATION.  (TC NR 20071127009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20080221000442008022100044NM  2008       2          21         CA071127010      120071123G3297                CONNECTOR                               GULSTM200   200         4500308NM                                                               NLG STEERING SYSCONTAMINATED    W      D   RETURN TO BLOCK                                                                                 J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA       878                                                            (CAN) AIRCRAFT LANDED, PILOT REPORTED NO NOSE WHEEL STEERING. PARKED AIRCRAFT AT FBO. LATER A/C WAS TAKEN TO MFG. THE NOSE WHEELING SYSTEM WAS INSPECTED AND MOISTURE WAS FOUND IN THE FEEDBACK POTENTIOMETER CONNECTOR PLUG. CLEANED AND RECONNECTED CONNECTOR PLUG, APPLY SEALANT TO THE CONNECTOR PLUG AND THE COVER FOR THE FEEDBACK POTENTIOMETER.  C/O FUNCTION CHECKS ON SYSTEM OK.   AIRCRAFT RELEASE FOR RETURN TO SERVICE. (TC NR 20071127010)                                                                                                                                                                                                                                                                                        2L72 4F    RTA53NM                        
20080221000452008022100045SW  2008       2          21         CA071127011      120071105G63202120400545      FITTING         BELL                    BELL  205   205A1       1181414SW  LYC   T53   T5317A      41549NE                              M/R GEARBOX     CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            785   ABT301                                              (CAN) ON ROUTINE INSPECTION, A CRACK WAS NOTED IN THE LIFT LINK FITTING. TRANSMISSION WAS REMOVED AND SENT FOR REPAIR. THE TSO FOR THE COMPLETE TRANSMISSION WAS AT 785.1 AND TT 19803.1. NO AVAILABLE INFORMATION FOR TT ON THE SUMP ASSY CASE. (TC NR 20071127011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 4U4  U  H1SW    E17EA                
20080221000462008022100046EU  2008       2          21         CA071128001      120071106G6130                PROP BRAKE                              AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              PROPELLER       DAMAGED         W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                          127023                      (CAN) SHORTLY AFTER ENGINE START, CREW OBSERVED A PROP BRAKE WARNING LIGHT FOLLOWED BY A FIRE WARNING. ENGINE WAS SECURED AND THE AIRCRAFT EVACUATED.  INITIAL INVESTIGATION REVEALED A SEVERELY DAMAGED PROPELLER BRAKE ASSY.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071128001)                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRT        E20NE                
20080221000472008022100047NE  2008       2          21         CA071128002      220071108G753231J285704       TORQUE MOTOR                            CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              BLEED VALVE     DEFECTIVE       W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  DEDESCENT        1                      CA                                          DD0396                      (CAN) DURING DESCENT, CREW NOTED ENGINE NOISE, FOLLOWED BY A REVERSION OF THE EEC TO MANUAL. ENGINE POWER LEVEL REMAINED AT FLIGHT IDLE.  INVESTIGATION REVEALED A DEFECTIVE BLEED VALVE TORQUE MOTOR. (TC NR 20071128002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA22CE   E00059EN             
20080221000482008022100048NE  2008       2          21         CA071128003      220071108G7200                HMU                                     AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  ENGINE          MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CLCLIMB          1                      CA                                          120178                      (CAN) OPERATOR REPORTED UNCOMMANDED ENGINE SHUTDOWN AND EEC REVERSION DURING CLIMB. EEC WAS LATER REPLACED ON GROUND AND OPERATION WAS NORMAL. HMU WAS ALSO REPLACED AS A PRECAUTION. BOTH UNITS WILL BE RETURNED TO MFG FOR INVESTIGATION AND FOLLOW UP. (TC NR 20071128003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080221000492008022100049NE  2008       2          21         CA071128004      220071112G7200                ENGINE                                  BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE                                              SEIZED          W      E   ENGINE SHUTDOWN                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                          93211                       (CAN) CREW REPORT FLASH OF LIGHT FOLLOWED BY SPARKS FROM ENGINE, AND ELECTED TO PERFORM AN INFLIGHT SHUTDOWN. AFTER LANDING AND DURING INITIAL INVESTIGATION, THE PROPELLER COULD NOT BE ROTATED.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR20071128004)                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 4T4  T  A24CE   E4EA                 
20080306002042008030600204NM  2008       3          6          CA071128005      120071020G4920                TURBINE BLADES  PWC                     BOEING747   747400      13848ATNM                                                               APU ENGINE      SEPARATED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  900663                                              (CAN) DURING AC B-CHECK, AIRFRAME APU COMPARTMENT IMPACT DAMAGE WAS OBSERVED CAUSED BY APPARENT TURBINE BLADE LIBERATION AND CASE FLANGE SEPARATION.  THE APU HAD BEEN DECLARED INOPERATIVE BY THE OPERATOR SINCE OCTOBER 20 2007.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071128005)                                                                                                                                                                                                                                                                                                                                                                                                     2L74 4F    RTA20WE                        
20080221000502008022100050EA  2008       2          21         CA071128006      220071103G7200                ENGINE                                  DHAV  DHC6  DHC6100     2802610EA  PWA   PT6   PT6A20      52043EA  HARTZLHCB3T HCB3TN3     GL                  SURGES          W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                          40865                       (CAN) DURING CRUISE, THE CREW OBSERVED ENGINE (SURGES) AND PERFORMED AN INFLIGHT SHUTDOWN. POST FLIGHT INSPECTION REVEALED A SEIZED PROPELLER SHAFT AND POWER TURBINE BLADE DISTRESS.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071128006)                                                                                                                                                                                                                                                                                                                                                                                                                                                  1H72 3T3  TRTA9EA    E4EA    6  CP15EA    
20080221000512008022100051WP  2008       2          21         CA071128007      120071024G5311C04621          FRAME                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUSELAGE        BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1314                                                           (CAN) THE HELICOPTER WAS IN FOR A SCHEDULED 100 HOUR INSPECTION AND THE BROKEN FRAME WAS DISCOVERED BY THE AME. THE AIRCRAFT WAS GROUNDED AND A NEW PART WAS ORDERED AND INSTALLED. (TC NR 20071128007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1G71 3O3  O  H11NM   1E4                  
20080221000522008022100052CE  2008       2          21         CA071128008      120071128G2435                BRUSHES                                 BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCB3T HCB3TN3     GL  STARTER GEN     FAILED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            APAPPROACH       1                      CA            670   12527                                               (CAN) WHILE ON FINAL THE PILOT NOTICED THAT THE LT GENERATOR HAD FAILED. UPON LANDING, AN INSPECTION WAS CARRIED OUT ON THE GENERATOR. IT WAS NOTICED THAT THE BRUSHES WERE ALL BROKEN WHICH WOULD INDICATE AN INTERNAL FAILURE. (TC NR 20071128008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 4T4  T  A24CE   E4EA    6  CP15EA    
20080221000532008022100053NE  2008       2          21         CA071128009      220071116G7261AS3209014       O-RING                                  BRAERO1000  BAE1251000A 1500104EU  PWA   305   PW305B      52128NE                              NR 4 BEARING    LEAKING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          305025                      (CAN) CREW REPORTED OIL PRESSURE FLUCTUATIONS AND ILLUMINATION OF THE LOW OIL PRESSURE WARNING INDICATOR. THE ENGINE WAS SHUTDOWN AND THE FLIGHT DIVERTED.  INVESTIGATION REVEALED DEFECTIVE O-RINGS ON THE  NR4 BEARING TRANSFER TUBES (TC NR 20071128009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA3EU    E35NE                
20080221000542008022100054CE  2008       2          21         CA071128010      120071116G5344051218712       BULKHEAD                                CESSNA172   172M        2072418CE  LYC   O320  O320E2D     41508EA  MCAULY1C160 1C160CTM    GL  DOOR FRAME      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       4714                                                           (CAN) WHILE CARRYING OUT THE SEB 97-1 AFT DOORPOST INSPECTION, CRACKS WERE NOTED AT THE SUBJECT AREAS ON BOTH DOORPOSTS (IPC "CHANNEL-BULKHEAD"). SUBMITTER SUSPECTS THAT TAXIING OVER ROUGH SURFACES, OR POSSIBLY HARD OR CRABBED LANDINGS, CONTRIBUTES TO THE FLEXING OF THE BULKHEAD THAT RESULTS IN THE CRACKING.  CRACKS ARE FOUND BY LOOKING WITH LIGHT AND MIRROR FORWARD NEAR THE AILERON CABLE PULLEY AT THE BOTTOM OF THE AFT DOORPOSTS. THE CRACK RADIATES FROM THE RELIEF CUTOUT WHERE THE INSIDE FLANGE OF THE BULKHEAD CHANGES FROM VERTICAL TO HORIZONTAL.  (TC NR 20071128010)                                                                                                                                                  1H71 3O3  ONT3A12    E274    5  NP910     
20080221000552008022100055NE  2008       2          21         CA071128011      220071031G7321                FUEL CONTROL                            BEECH MU300 400BEECH           CE  PWA   JT15  JT15D5      52112NE                              ENGINE          INOPERATIVE     W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                          JG0033                      (CAN) DURING CRUISE, ENGINE POWER GRADUALLY REDUCED FROM 102 PERCENT N1 INDICATION TO 74 PERCENT. NO RESPONSE TO THROTTLE LEVER MOVEMENT. FLIGHT WAS DIVERTED AND AIRCRAFT LANDED WITH BOTH ENGINES RUNNING.  THE ENGINE FUEL CONTROL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071128011)                                                                                                                                                                                                                                                                                                                                                  2H72 4F4  FRTA16SW   E25EA                
20080320000042008032000004GL  2008       3          20         CA071128012      120071123G2432GE50C           BATTERY                                 NAMER T6    HARVARDMK4  1922828GL  PWA   R1340 R1340*      52016NE  HAMSTD12D   12D40       NE  MASTER          SHORTED         W      A   UNSCHED LANDING                                                                                 H  ELECT. POWER LOSS-50 PC                                                       CLCLIMB          1                      CA       253                                                            (CAN) AC SUFFERED ALMOST AN ENTIRE ELECTRICAL FAILURE DURING CLIMBOUT. AFTER SUBSEQUENT UNSCHEDULED LANDING, IT WAS DETERMINED THAT THE BATTERY HAD ACQUIRED AN INTERNAL SHORT, WHICH DEPLETED THE GENERATOR OUTPUT AND CAUSED THE AVIONICS TO MALFUNCTION.  BATTERY REPLACED WITH A SERVICEABLE SPARE, AND AC ELECTRICAL SYS CONFIRMED OPERATIONAL. (TC NR 20071128012)                                                                                                                                                                                                                                                                                                                                                                        1L71 3R3  R  EXPA1L715E2     5  CP257     
20080221000562008022100056NE  2008       2          21         CA071128013      220071109G7321                FUEL CONTROL                            CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                              ENGINE          FAILED          W      O   OTHER                                                                                           RY PARTIAL RPM/PWR LOSS      ENGINE STOPPAGE                                     NRNOT REPORTED   1                      CA                                          PC0509                      (CAN) ENGINE POWER LOSS AND SUBSEQUENT INFLIGHT SHUTDOWN REPORTED.  MFG IS ATTEMPTING TO RECOVER THE FUEL CONTROL UNIT FOR INVESTIGATION AND WILL ADVISE. (TC NR 20071128013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3T3  T  A37CE   E4EA                 
20080221000572008022100057NE  2008       2          21         CA071128014      220071123G7261                FILTER                                  DHAV  DHC8  DHC8103     1386005NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  ENGINE OIL      FAILED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                          120189                      (CAN) DURING CLIMB, THE CREW OBSERVED ERRATIC OIL PRESSURE INDICATIONS AND ELECTED TO RETURN TO POINT OF DEPARTURE. THE ENGINE OIL PRESSURE CONTINUED TO REDUCE AND THE CREW PERFORMED AN INFLIGHT SHUTDOWN. INVESTIGATION REVEALED A FAULTY MAIN OIL PRESSURE FILTER WITH A REPORTED COLLAPSED INTERNAL ELEMENT.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071128014)                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080221000582008022100058NM  2008       2          21         CA071128015      120071126G3240ZMV811A         VALVE                                   GULSTM200   200         4500308NM  PWC   PW306 PW306A      52165NE                              PARKING BRAKE   MALFUNCTIONED   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA       878                                                            (CAN) PILOT REPORTED PARK BRAKE SET AND INDICATED ON EICAS. STARTED RT ENGINE WITH THE CHOCKS REMOVED, READY FOR DEPARTURE. THE AIRCRAFT ROLL FWD AFTER THE ENGINE WAS STARTED. PILOT CHECKED THE INDICATION ON EICAS AND THE INDICATION WAS STILL ON EICAS PARK BRAKE ON.  PILOT HAD TO USE NORMAL BRAKE TO STOP AIRCRAFT.  MAINT WAS CALLED AND TROUBLESHOOTING REVEALED THAT THE PARK BRAKE VALVE FAILED IN THE CLOSED POSITION. REPLACED PARK BRAKE VALVE AND C/O F/C ON PARK BRAKE SYS AND AC BRAKING SYS ALL FUNCTIONS OK.  AC RELEASED FOR RETURN FOR SERVICE. (TC 20071128015)                                                                                                                                                          2L72 4F4  FRTA53NM   E35NE                
20080221000592008022100059WP  2008       2          21         CA071128017      120071126G6730D2121           SERVO                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                                              LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA            857                                                       (CAN) WHILE CARRYING OUT A 100 HOUR INSP THE FWD LT HYDR SERVO WAS DISCOVERED LEAKING. SERVO WAS REPLACED, GROUND RUN AND LEAK CHECK CARRIED OUT SERVICEABLE (TC NR 20071128017)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3O3  O  H11NM   1E4                  
20080221000602008022100060CE  2008       2          21         CA071128018      120071128G2510505590401       CABLE           AMSAFE      505590401   CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA                              SEAT            BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2                                                              (CAN) COMPLIED WITH SB07-5 PILOT SECONDARY SEAT STOP INSTALLATION. THE AIRCRAFT LEFT OUR SHOP SERVICABLE AND IN COMPLIANCE WITH THE SB.  BROUGHT IT IN THE NEXT DAY TO DO UNSCHEDULED MAINT.  LOOKING OVER THE JOB FOR A SECOND TIME FOUND THE THREADED PLASTIC END OF THE CABLE BROKEN IN HALF AND THE PRODUCT NO LONGER FUNCTIONING CORRECTLY. BELIEVE A POSSIBILITY OF THE PART BRAKING TO BE COOL WEATHER AND THE FACT THAT THE PART IS PLASTIC. (TC NR 20071128018)                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A12    E274                 
20080221000612008022100061WP  2008       2          21         CA071128019      120071006G7810C16932          TAILPIPE                                ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                                              BURNED          W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                                                                      (CAN) PILOT REPORTED ODOR OF EXHAUST IN CABIN. INSPECTION OF EXHAUST COMPLIED WITH AND FOUND BURNED OUT AREA AT TAILPIPE JUNCTION. CF90-03R2 COMPLIED WITH 72.8 HRS PREVIOUS WITH NO DEFECTS FOUND AT THAT TIME. EXHAUST REPLACED. (TC NR 20071128019)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3O3  O  H11NM   1E4                  
20080221000622008022100062    2008       2          21         CA071129001      220071122G7261AS121670        CLEVIS PIN                  PN3004073   DHAV  DHC6  DHC6300     2802606EA                                   HARTZLHCB3T HCB3TN3     GL  OIL TANK DRAIN  MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            22                                                        (CAN) THIS RT ENGINE S/NPCE-50013, WAS IDENTIFIED TO HAVE THE OIL TANK DRAIN PLUG P/N 3004073, MISSING THE LOCKING PIN P/N AS121670. THIS COULD HAD LEAD TO THE COMPLETE LOSS OF ENGINE OIL, RESULTING OF ENGINE SHUTDOWN, IF THE PLUG HAD LOOSEN AND FALLEN AWAY FROM THE ENGINE. (TC NR 20071129001)                                                                                                                                                                                                                                                                                                                                                                                                                                          1H72 3T    RTA9EA            6  CP15EA    
20080221000632008022100063CE  2008       2          21         CA071129002      120071122G57533516505030      BRACKET         BEECH                   BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCE4N HCE4N3      NE  FLAP BRACKET    WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7336       BB1610                                              (CAN) DURING PHASE 1 INSPECTION, LT FLAPS WERE REMOVED TO INSPECT SUPECTED AREA AS RT OB FLAP HAD FAILED IN THE SAME AREA A FEW HOURS PRIOR AND WAS REPORTED UNDER A SEPARATE SDR. WHEN RT OB FLAP BRACKET FAILED, THE FLIGHT CONTROLS WERE AFFECTED. THE CAUSE OF THE WEAR ON THE BRACKET IS FROM BEARING PN BC56985 WEARING OUT CHAFING INTO BRACKET. (TC NR 20071129002)                                                                                                                                                                                                                                                                                                                                                                     1L72 4T4  T  A24CE   E4EA    5  CP10NE    
20080221000642008022100064NM  2008       2          21         CA071130001      120071110G335032145410        POWER SUPPLY                            AIRBUSA319  A319114     3930350NM  CFMINTCFM56 CFM565A3         NE                              EMERGENCY LIGHTSFAILED          W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                                                                      (CAN) IN PROCESS OF DOING AB EMERGENCY LIGHTING TEST, AFTER THE COMPLETION OF THE IN-FLIGHT ENTERTAINMENT MAKEOVER, IT WAS DISCOVERED THAT THE AFT EMERGENCY LIGHTING WAS NOT TESTING. A STRONG BURNING SMELL WAS DETECTED AFTER OPENING A PANEL TO ACCESS THE AFT EMERGENCY POWER SUPPLY UNIT. ONE CORNER OF THE BATTERY UNIT WAS MELTED THROUGH THE CASE AND THE POSITIVE TERMINAL CONNECTION AND CIRCUIT BOARD ON THE ESPU HAD SIGNS OF SEVERE OVERHEATING. THE ESPU AND BATTERY WERE SENT TO THE SHOP FOR EVALUATION.  THE SUSPECTED CAUSE WAS LIQUID INGESTION BUT COULD NOT BE SUBSTANTIATED. (TC NR 20071130001)                                                                                                                         2L72 4F4  FRTA28NM   E29NE                
20080221000652008022100065GL  2008       2          21         CA071130002      120071129G2422GC53100043      INVERTER                                BOMBDRBD100 BD1001A10   1390044GL  RROYCEBR700 BR700710A22009500NE                                              OVERHEATED      W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       257                                                            (CAN) DURING MAINT AND AFTER THE AC HAD BEEN POWERED WITH EXTERNAL GROUND POWER FOR APPROX 4 HOURS, THE CREW NOTICED A BURNING SMELL AROUND THE AC. NO ABNORMAL INDICATIONS WERE DISPLAYED ON THE CREW ALERTING SYS (CAS) MESSAGE AND THE ELECTRICAL MGMT SYS CONTROL AND DISPLAY UNITS (EMSCDU). THE POWER WAS REMOVED FROM THE AC.  THE INVESTIGATION INDICATES THAT THE INTEGRAL LIGHTING INVERTER A179 SHOWN SIGN OF INTERNAL OVERHEATING. THIS RESULTED IN DEPOSITING SOOT TO THE ADJACENT INTEGRAL LIGHTING POWER SUPPLY A176 AND WIRES. BOTH UNITS WERE REMOVED, REPLACE AND SENT TO THE VENDOR TO IDENTIFY THE ROOT CAUSE OF THE FAILURE. THE AC IS BACK IN SERVICE. (TC NR 20071130002)                                                2L72 4F4  FRTT00005NYE00061EN             
20080221000662008022100066CE  2008       2          21         CA071130003      120071128G561010138402522     WINDSHIELD                              BEECH 1900  1900C       1154161CE  PWA   PT6   PT6A65B     52043EA  HARTZLHCB4M HCB4MP3     GL  COCKPIT         CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) COPILOTS WINDSHIELD INNER PANE SHATTERED DURING NORMAL CRUISE FLIGHT. WINDSHIELD REPLACED UPON RETURN TO MAINTENANCE BASE. (TC NR 20071130003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20080221000672008022100067EU  2008       2          21         CA071130004      120071128G2497                WIRE HARNESS                            AEROSPATR42 ATR42300    8680920EU  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF5       NE  CONTROL PANEL   SHORTED         W      D   RETURN TO BLOCK                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA                                                                      (CAN) STANDBY HORIZON CB POPPED. MODERATED ELECTRICAL SMELL/SMOKE.  WIRE BUNDLE UNDER COPILOTS SIDE PANEL ASSY (PNS2511049800300) FOUND CHAFED AND SHORTING TO PANEL. (PANEL IS BELIEVED TO BE MADE OF CARBON FIBER WHICH WILL CONDUCT ELECTRICITY). PANEL ASSY INSPECTED WITH BURNED SPOTS AT WIRE BUNDLE LOCATION AS WELL AS AFT EDGE WHICH WAS CHAFING ON (2) SCREWS. DAMAGED WIRING BUNDLE REPAIRED. PANEL REPAIRED AND REINSTALLED. (TC NR 20071130004)                                                                                                                                                                                                                                                                                    2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080221000682008022100068WP  2008       2          21         CA071130006      120071123G243514924HTH        STARTER                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       155                                                            (CAN) A PILOT ATTEMPTING A START THE AC AND FAILED TO TURN OVER. FURTHER INVESTIAGTION REVEALED STARTER WAS DEFECTIVE. STARTER WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20071130006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3O3  O  H11NM   1E4                  
20080221000692008022100069NM  2008       2          21         CA071130007      120071130G5315146A75031       FLOORBEAM                               BOEING737   737790      13844CNNM                                                               CARGO BAY       CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT CARGO PIT FLOOR SUPPORT RAIL AT BS 767+6 LBL 3 CORRODED AND REPAIRED IAW CUSTOMER EA, LEVEL 2 CORROSION. (TC NR 20071130007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F    RTA16WE                        
20080131002752008013100275NM  2008       1          31         CA071130008      120071130G5315146A75035       FLOORBEAM                               BOEING737   737790      13844CNNM                                                               AFT CARGO PIT   CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT CARGO PIT FLOORBEAM RAIL CORRODED AT BS 767+6 LBL 8 AND REPAIRED IAW CUSTOMER EA LEVEL 2 CORROSION (TC NR 20071130008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RTA16WE                        
20080131002762008013100276NM  2008       1          31         CA071130009      120071130G5315147A55047       FLOORBEAM                               BOEING737   737790      13844CNNM                                                               BS 947          CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT CABIN FLOOR SUPPORT BEAM AT BS 947 LBL 53 CORRODED AND REPAIRED IAW CUSTOMER EA  LEVEL 2 CORROSION (TC NR 20071130009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RTA16WE                        
20080131002772008013100277NM  2008       1          31         CA071130010      120071130G5730112A410210      SKIN                                    BOEING737   737790      13844CNNM                                                               RWS 240         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) RT WING LWR SKIN AT AFT EDGE CHAFFING DAMAGE FROM CONTACT WITH NACELLE STRUT AFT FAIRING INBD BLADE SEAL AT APPROX. WS 240 REPAIRED IAW CUSTOMER EA (TC NR 20071130010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F    RTA16WE                        
20080131002782008013100278NM  2008       1          31         CA071130011      120071130G5730112A41029       SKIN                                    BOEING737   737790      13844CNNM                                                               LWS 260         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) LT WING LWR SKIN CHAFFING DAMAGE FOUND FROM CONTACT WITH NACELLE STRUT AFT FAIRING OB BLADE SEAL AT APPROX WS 260  REPAIRED IAW CUSTOMER EA (TC NR 20071130011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F    RTA16WE                        
20080131002792008013100279EU  2008       1          31         CA071130012      120071130G6321C762C1004103    BRAKE                                   UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              ROTOR           DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1730                                                           (CAN) MECHANICAL DAMAGE TO ROTOR BRAKE GRID ASSEMBLY, DUE TO IMPROPER OPERATION.  TRIGGER WAS NOT DEPRESSED PRIOR TO ENGAGING ROTOR BRAKE HANDLE CAUSING MECHANICAL DAMAGE TO GRID ASSEMBLY.  NEW GRID ASSEMBLY INSTALLED (TC NR 20071130012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G72 3U3  UNCR0001RD E34NE                
20080131002802008013100280NM  2008       1          31         CA071130013      120071130G5730112A410210      SKIN                                    BOEING737   737790      13844CNNM                                                               RWS 260         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) RT WING LWR SKIN CHAFFING DAMAGE FROM CONTACT WITH NACELLE STRUT AFT FAIRING OB BLADE SEAL AT APPROX WS 260 REPAIRED IAW EA.(TC NR 20071130013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F    RTA16WE                        
20080204001282008020400128    2008       2          4          CA071130014      120071126G34113001T60P03      SEAL                                                                       GE    CT58  CT581401    30011NE                                              DEBONDED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                          295291                      (CAN) STATIC DISCHARGE SEAL DEBONDED WHILE ENGINE (SN 295-291) WAS BEING RUN. OUR INTERNAL SQID REPORT NR 07-06724 REFERS. (TC NR 20071130014)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         4  U          1E3                  
20080204001272008020400127    2008       2          4          CA071130015      420071130G3197                WIRE                                    BEECH B300  B300        1159232CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL                  BURNED          W      E   ENGINE SHUTDOWN                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA       393                                                            (CAN) AFTER STARTING ENGINE FOR GROUND RUN, AVIONICS SWITCH WAS SELECTED ON. IMMEDIATELY SMOKE STARTED COMING FROM RT CB PANEL. ENGINES WERE IMMEDIATELY SHUTDOWN AND POWER WAS REMOVED FROM A/C. INVESTIGATION REVEALED THAT A FACE PLATE MOUNTING SCREW HAD SHORTED TO AN AVIONICS FEEDER WIRE P72A10 DUE TO POOR ROUTING OF THE WIRE AT MFG.  (2) 10GAUGE WIRES ARE ATTACHED TO ONE TERMINAL OF CB120 (TCAS), ONE COMING FROM CB92 (AVIONICS POWER LT GEN BUS) WHICH IS A 30AMP BREAKER. ONE OF THE WIRES WAS MOUNTED ALONG THE BACK OF THE PANEL AND HAD BEEN IN HARD CONTACT WITH THE AFT MIDDLE FACE PLATE MOUNTING SCREW. WIRE REPLACED IAW AC43.13-1B PARA 11-98, ROUTED TO AVIOD CONTACT WITH MOUNTING HARDWARE. (TC NR 20071130015)   2L72 4T4  TRTA24CE   E4EA    6  CP56GL    
20080204001262008020400126CE  2008       2          4          CA071202001      120071201G5312                BULKHEAD                                CESSNA206   U206G       2073356CE  CONT  O550  IO550F      17042SO  HARTZLHCJ3Y PHCJ3YF1    GL  FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING COMPLIANCE WITH SEB 93-5 INSP OF LOWER DOOR POST, THE BULKHEAD WAS FOUND CRACKED ON THE LT SIDE, UPPER PART OF LOWER BULKHEAD, JUST IB OF THE WING STRUT ATTACHMENT FITTING. RT SIDE WAS TO BE FREE OF CRACKS AT THIS TIME. MFG SERVICE KIT SK260-42C WAS INCORPORATED TO THE LT LOWER DOOR POST. AC RETURNED TO SERVICE.  THIS INSP IS ALSO CALLED UP IN THE CONTINUED AIRWORTHINESS PROGRAM  INSP NR 53-40-01 INITIAL INSPECTION TO BE DONE AT 12000 HOURS AND REPEAT INSPECTIONS EACH 3000 HOURS THERE AFTER. SEB 95-3R1 CALL FOR THIS INSPECTION AT 4000 HOURS TT AND REPEAT INSPECTIONS EACH 1000 HOURS THERE AFTER.  NOT ALL OPERATORS OF THESE AC ARE IN COMPLIANCE WITH THE C.A.P MANUALS. (TC NR 20071202001)             1H71 3O3  O  A4CE    E3SO    5  CP36EA    
20080131002812008013100281NM  2008       1          31         CA071202002      120071201G5730112A4101209     SKIN                                    BOEING737   737990             NM                                                               RWS 260         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       19198                                                          (CAN) A/C UNDERGOING C-CHECK,HEAVY MAINTENANCE. RT WING, LOWER SKIN PANEL CHAFING DAMAGE FOUND FROM CONTACT WITH NACELLE STRUT AFT FAIRING OB BLADE SEAL AT APPROX WS 260. REPAIRED IAW EA 5720-01345. (TC NR 20071202002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L74 4F    RTA16WE                        
20080131002822008013100282NM  2008       1          31         CA071202003      120071201G5730112A4101209     SKIN                                    BOEING737   737990             NM                                                               LWS 240         CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       19198                                                          (CAN) A/C UNDERGOING C-CHECK HEAVY MAINTENANCE. LT WING LOWER SKIN PANEL CHAFING DAMAGE FOUND DUE TO CONTACT WITH NACELLE STRUT AFT FAIRING IB BLADE SEAL AT APPROX WS 240. REPAIRED IAW EA 5720-01345. (TC NR 20071202003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L74 4F    RTA16WE                        
20080221000702008022100070NM  2008       2          21         CA071202004      120071201G5730112A4101209     SKIN PANEL                              BOEING737   737990             NM                                                               WS 260          CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       19198                                                          (CAN) A/C UNDERGOING C-CHECK HEAVY MAINT. LT WING LOWER SKIN PANEL CHAFING DAMAGE FOUND DUE TO CONTACT WITH NACELLE STRUT AFT FAIRING OB BLADE SEAL AT APPROX WS 260. REPAIRED IAW EA 5720-01346. (TC NR 20071202004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L74 4F    RTA16WE                        
20080221000712008022100071SO  2008       2          21         CA071203001      120071202G3710                VANE            RAPCO       441CC7      PIPER PA31  PA31310     7103103SO  LYC   O540  TIO540A2C   41532EA  HARTZLHCE3Y HCE3YR2A    GL  AIR PUMP        BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            771   125777                                              (CAN) DURING A PRE-MAINTENANCE GROUND RUN, IT WAS NOTED THAT THE RT AIR PUMP WAS INDICATING INOPERATIVE DURING INSPECTION. THE DRIVESHAFT WAS FOUND TO BE SHEARED DUE TO THE CARBON VANES BREAKING AND JAMMING THE PUMP. (TC NR 20071203001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L71 3O3  ORTA20SO   E14EA   5  CP33EA    
20080225000102008022500010SO  2008       2          25         CA071203002      120071202G5340                STRUCTURE                               PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  NLG WW          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1732917329                                                     (CAN) DURING AN EVENT 1 INSP ON THE AC, ENGINEER NOTICED WHAT HE THOUGHT THERE WAS A CRACK ON THE EXTRUSION (LOCATED ABOVE THE NLG WHEEL WELL, JUST AFT OF HYD POWERPACK), TO WHICH THE NOSE LANDING GEAR RETRACTION ACTUATOR ATTACHES TO. AFTER PERFORMING A LIQUID PENETRANT INSP, THE PRESENCE OF A CRACK WAS CONFIRMED. THE EXTRUSION WAS REMOVED FROM THE AIRCRAFT, AT THIS TIME IT WAS ALSO NOTED THAT THE ATTACH POINT (BOLT HOLE) WAS ALSO CRACKED. A NEW EXTRUSION IS BEING INSTALLED. THIS EXTRUSION HAS BEEN INSTALLED SINCE THE AIRFRAME WAS MFG (17328.9 TSN). (TC NR 20071203002)                                                                                                                                                 1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080225000112008022500011NE  2008       2          25         CA071203003      220071203G7314D7341           PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL SYSTEM     FAILED          W      K   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      CA                                                                      (CAN) THE AUXILIARY FUEL PUMP LIGHT CAME, AND WOULD NOT EXTINQUISH. TROUBLESHOOTING REVEALED THAT THE PUMP WAS NO LONGER PUMPING FUEL. THE PUMP WAS CHANGED, LEAK, AND FUNCTION CHECKED SERVICEABLE. (TC 20071203003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3O3  O  H11NM   1E4                  
20080225000122008022500012SW  2008       2          25         CA071203004      120071101G5514400928          SPRING                                  AIRTRCAT802 AT802A      0390308SW  PWA   PT6   PT6A67A     52043NE  HARTZLHCB5M HCB5MA3     GL  TAIL            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       858                                                            (CAN) CRACK FOUND ON TAIL SPRING BEGINNING FROM FWD ATTACH HOLE EXTENDING ALONG SIDE OF SPRING. CRACK THEN EXTENDS TO TOP OF SPRING. LENGTH OF CRACK TOTALS APPROX 6 INCHES. (TC NR 20071203004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20080225000132008022500013EU  2008       2          25         CA071203005      120071203G672011731822A       PITCH LINK                              BOLKMS117   BK117B2     5626013EU  LYC   LTS101LTS101750B1 41560NE                              TAIL ROTOR      MISMARKED       W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                                                                      (CAN) TAIL ROTOR PITCH LINKS P/N 117.31822A.  REPLACED ON 31 OCT/2007, DUE TO BEARING WEAR. ON DEC 3/2007 THE LINKS WERE INSPECTED PRIOR TO BEARING REPLACEMENT AND WERE FOUND TO HAVE AN INCORRECT P/N STAMPED ON THEM. THE NR WAS MISSING THE NR 1. THE STAMP INDICATED P/N 117.3822A. THIS NUMBER IS NOT IN THE IPC MANUAL. THE LINKS ARE THEREFORE SUSPECT. (TC NR 20071203005)                                                                                                                                                                                                                                                                                                                                                             1G72 3U3  UNCH13EU   E5NE10               
20080225000142008022500014SW  2008       2          25         CA071203006      120071203G7120205060105001    MOUNT                                   BELL  205   205A1       1181414SW  LYC   T53   T5313B      41549NE                              ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       7609                                                           (CAN) LT ENGINE TRIPOD AFT TUBING MOUNT FOUND CRACKED DURING 100 HRS INSPECTION JUST BELOW ENGINE MOUNTING PLATE AFT TUBE JUNCTION.  NOTE: THIS MOUNT WAS MODIFIED IAW STC SH99-11, DART ADJUSTABLE MOUNT. (TC NR 20071203006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 4U4  U  H1SW    E17EA                
20080319001662008031900166NE  2008       3          19         CA071203007      220071201G732101645487201     FCU                                     SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              ENGINE          LEAKING         W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      DEDESCENT        1                      CA                                                                      (CAN) THE PILOT WAS DESCENDING WHEN ALL OF A SUDDEN THE CABIN AREA FILLED UP WITH A MIST ORIGINATING FROM THE THE DEFROST VENTS. THE MIST WAS SO STRONG THAT THE PILOT HELD HIS BREATH AND OPENED THE FUSELAGE DOOR SO THE MIST COULD EXIT THE AC.  AFTER A FEW SECONDS THE MIST DISSIPATED SO THE PILOT COULD BREATH NORMALLY. THE PILOT LANDED AT STAGING SITE AND THE AC WAS GROUNDED. THE ENGINEER WAS CALLED TO TROUBLESHOOT THE PROBLEM.  WE BELIEVE IT IS THE FUEL CONTROL THAT CAUSED THIS FUEL MIST IN THE CABIN. THE FUEL CONTROL HAS ABOUT 1400 HOURS SINCE LAST OVERHAUL THE TECH. (3000 HOUR O/H BY MFG) (TC NR 20071203007)                                                                                                       1G71 3U3  U  H9EU    E19EU                
20080225000152008022500015SW  2008       2          25         CA071203008      120071126G3210                BUTTON          FRCHLD                  SWRNGNSA227 SA227AC     8780603SW  GARRTTTPE331TPE33111U   01514WP  MCAULY4HFR344HFR34C652  NE  MLG             SHORT           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  AC714                                               (CAN) UPON DISASSEMBLY OF A MLG FOR OVERHAUL AND SERVICING IT WAS NOTICED THE CYLINDER PISTON TEFLON BUTTONS WERE UNDER FLUSH WITH THE PISTON. THE TEFLON BUTTONS AND PINS ALLOW THE PISTON TO SLIDE INSIDE THE CYLINDER WITHOUT SCORING AND WITHOUT ALLOWING FLUID BLOWBY. UPON INSPECTION OF THE PISTON IT WAS NOTICED THE HOLES WERE TOO DEEP FOR THE TEFLON BUTTONS AND PINS AND ALLOWED FOR SCORING OF THE CYLINDER WALLS. WHEN COMPARED TO A KNOWN CERTIFIED PART, IT DID NOT MEET THE SAME MEASUREMENTS. ACTUAL ENGINEERING DRAWINGS WITH SPECIFIC MEASURMENTS WERE NOT AVAILABLE TO CONFIRM PISTON MEASURMENTS. LIKELY THIS PART IS SUBSTANDARD BUT THE POSSIBILITY OF BEING AN UNAPPROVED PART EXISTS. TOTAL TIME ON THE PISTON IS UNKN2L72 4T4  TRTA8SW    E4WE    6  C3PNE     
20080225000162008022500016GL  2008       2          25         CA071204001      220071129G732323076061        GOVERNOR                                BELL  206   206B        1181511SW  ALLSN 250C  250C20      03013GL                              ENGINE          INOPERATIVE     W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA            456                                                       (CAN) WHILE CARRYING OUT A START, THE ENGINE WAS SLOW TO REACH IDLE, WITH THE N2 INDICATOR STICKING ON START. ONCE DESNAGGED IT WAS DISCOVERED THE GOVENOR WAS THE CAUSE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1G71 3U3  U  H2SW    E4CE                 
20080225000172008022500017SW  2008       2          25         CA071204002      120071101G2450PDLM120         CIRCUIT BREAKER                         AIRTRCAT802 AT802A      0390308SW  PWA   PT6   PT6A67A     52043NE  HARTZLHCB5M HCB5MA3     GL  CB BODY         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5676 5676                                                      (CAN) CB CRACKED.  (TC NR 20071204002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20080225000182008022500018SW  2008       2          25         CA071204003      120071101G5320                NUT                         EISRVAC     AIRTRCAT802 AT802A      0390308SW  PWA   PT6   PT6A67A     52043NE  HARTZLHCB5M HCB5MA3     GL  VACUUM SWITCH   BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5676 5676                                                      (CAN) THE VACUUM SWITCH WAS SUPPLIED BY MFG. PLASTIC ADJUSTING NUT SPLIT, PREVENTING THE VACUUM SWITCH FROM INDICATING A LOW FUEL PRESSURE WARNING. (TC NR 20071204003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20080225000192008022500019NM  2008       2          25         CA071204004      120071204G3230656021132       ACCESSORY UNIT                          BOEING727   727247      138408FNM  PWA   JT8   JT8D15      52051NE                              LANDING GEAR    UNSERVICEABLE   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       9451 7879                                                      (CAN) SHORTLY AFTER TAKEOFF WHEN GEAR WAS BEING RETRACTED, CREW NOTICED THAT THE RT MAIN GEAR RED LIGHT WAS STILL ILLUMINATED. CREW CYCLED THE LANDING GEAR (3) TIMES WITH THE SAME RESULTS. THE CREW ADVISED THAT AIR NOISE COULD BE HEARD. GEAR WAS SELECTED DOWN WITH (3) GREEN AND RETURNED TO THE RAMP. EXTENSIVE TROUBLESHOOTING AND GEAR SWINGS REVEALED LANDING GEAR ASSY UNIT IS AT FAULT. SERVICEABLE UNIT INSTALLED AND GEAR FUNCTION TESTED SERVICEABLE. THE AC HAS FLOWN 4 LEGS SINCE THE REPAIR WITH NO FURTHER PROBLEMS.                                                                                                                                                                                                         2L73 4F4  F  A3WE    E2EA                 
20080225000202008022500020NE  2008       2          25         CA071204006      220071202G7314LW15473         PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              FUEL SYSTEM     FAILED          W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      CA       1013                                                           (CAN) THE AIRCRAFT WAS FLOWN FOR AN HOUR AND THEN SHUTDOWN TO WAIT FOR CUSTOMERS. THE AC WAS RE-STARTED A HALF HOUR LATER AND THE PILOT TRIED TO LIFT OFF, WHEN THE ENGINE LOST PARTIAL POWER AND THE MANIFOLD PRESSURE ROSE ABNORMALLY.  THE POWER SETTINGS CAME BACK TO NORMAL WHEN THE COLLECTIVE WAS LOWERED BUT WOULD DETERIORATE EVERY TIME THE COLLECTIVE WAS RAISED. AFTER SHUTTING DOWN THE ENGINE, FUEL WAS SEEN FLOWING OUT OF THE ENGINE DRIVEN FUEL PUMP DRAIN. THE OAT WAS -30 CELCIUS AND THE ENGINE WAS PRE-HEATED. (TC NR 20071204006)                                                                                                                                                                                         1G71 3O3  O  H11NM   1E4                  
20080225000212008022500021SW  2008       2          25         CA071204007      120071204G6410212010710001    BALANCE WEIGHT                          BELL  212   212         1181420SW  PWA   PT6T  PT6T3       52045EA                              T/R BLADE       INCORRECT       W      K   NONE                                                                                            E  VIBRATION/BUFFET                                                              ININSP/MAINT     1                      CA                                                                      (CAN) INCORRECT WEIGHT FOR PN CAUSED IMBALANCE IN TAIL ROTOR WHICH COULD NOT BE CORRECTED WITHIN BALANCE LIMITS. (TC NR 20071204007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 4U4  U  H4SW    E22EA                
20080225000222008022500022NE  2008       2          25         CA071204008      120071129G6520                BEARING                     S613566300  SKRSKYS61   S61N        8142104NE  GE    CT58  CT581402    30011NE                              GEARBOX         OVERHEATED      W      C   ABORTED TAKEOFF                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA            14    A151024                                             (CAN) ON FIRST FLIGHT OF THE DAY, AIRCRAFT WAS GROUND TAXIING TO TAKE OFF AREA WHEN GROUND CREW NOTICED SMOKE FROM TAIL ROTOR DRIVE INTERMEDIATE GEAR BOX AREA. AIRCRAFT WAS SHUT DOWN, AND INSPECTION REVEALED OVERHEATING IN THE INPUT BEARING AREA. SIKORSKY AND OVERHAUL SHOPS ADVISED, AND ARE INVESTIGATING CAUSE. THIS IS A REOCCURANCE OF PREVIOUS FAILURE. IN BOTH CASES GEAR BOX OIL LEVEL WAS FOUND TO BE SATISFACTORY. (TC# 20071204008)                                                                                                                                                                                                                                                                                            2G72 4U4  U  1H15    1E3                  
20080225000232008022500023GL  2008       2          25         CA071204009      120071130G5551C2TP160A        BRACKET                                 DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HARTZLHCB3R HCB3R304    GL  STAB            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE COMPLETING THE REQUIREMENTS OF CF 91-42R1 IAW SB 2/47 REV (E), THE RT FWD STABILIZER ATTACH BRACKET WAS FOUND TO BE CRACKED. THE CRACK EXTENDED FROM THE TOP OF THE IB EAR OF THE BRACKET, THROUGH THE LOCKWIRE HOLE AND CONTINUED APPROX 75 PERCENT OF THE WAY DOWN THE BRACKET. THIS AIRCRAFT OPERATES EXCLUSIVELY ON FLOATS IN A CORROSIVE ENVIRONMENT.                                                                                                                                                                                                                                                                                                                                                                          1H71 3R3  RRCA806    5E1     5  CP28EA    
20080225000242008022500024NE  2008       2          25         CA071204010      220071123G72611111065         OIL FILTER                              DHAV  DHC8  DHC8103     1386005NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  ENGINE          RESTRICTED      W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA            600                                                       (CAN) INFLIGHT SHUTDOWN AS A PRECAUTION, OIL PRESSURE INDICATION FLUCTUATING IN FLIGHT.  OIL FILTER APPEARED CLEAN BUT WAS RESTRICTING FLOW AS TO WHERE IT WAS CAUSING OIL BYPASS IN THE FILTER HOUSING, WHICH CAUSED THE ERRONEOUS INDICATIONS. (TC NR 20071204010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080225000252008022500025GL  2008       2          25         CA071204011      120071123G5343                ATTACH FITTING                          TCRAFTBC    BC12D       8850316GL  CONT  A65   A658        17003SO  UNIVAC72    72A         GL  MLG             BROKEN          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) WHILE INSTALLING NEW STRUTS IAW APPLICABLE STC, THE LT REAR ATTACH FITTING SEPERATED (BROKE IN HALF) AS VERY SLIGHT DOWNWARD PRESSURE WAS APPLIED TO THE LIFT STRUT.  INSPECTION OF THE FAILED PART SHOWED A PRE EXISTING CRACK UNDER THE LOCKNUT. (TC NR 20071204011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  O  A696    E205    5  N802      
20080225000262008022500026EA  2008       2          25         CA071205001      120071205G2820215T640836      FITTING                                 CNDAIRCL215 CL2156B11215       EA  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  TANK DRAIN      BROKEN          W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) MAJOR FUEL LEAK BY THE BROKEN NR 3 COLLECTOR TANK DRAIN FITTING, SOLENOID SIDE. PIPE DRAIN 215T64083-6 REPLACED.   (TC NR 20071205001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRTA14EA   E20NE   6  CP7NE     
20080225000272008022500027EU  2008       2          25         CA071205002      120071203G56103501262334      WINDSHIELD                              SNIAS 350   AS350*             EU  TMECA ARRIELARRIEL1B    6OO30NE                              COCKPIT         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                              2295                                    (CAN) DURING PREFILGHT INSP, CRACKS WERE DISCOVERED ON LT WINDSHIELD TECH TOOLS PLASTICS P/N 350126231 AND RT WINDSHIELD TECH TOOLS PLASTICS P/N 3501-2623-1. BOTH LT AND RT WINDSHIELDS WERE CRACKED 4.5 TO 5 INCHES LONG ON BOTTOM EDGE. THE AIRCRAFT HAND FLOWN THE PREVIOUS DAY IN TEMPERATURES OF -30 DEGREES C AND HAD BEEN HANGERED OVERNIGHT. (TC NR 20071205002)                                                                                                                                                                                                                                                                                                                                                                       1G71 3U3  U  H9EU    E19EU                
20080225000282008022500028EA  2008       2          25         CA071205003      220071205G732262226           STOP PIN                                AMTR  ELITE ELITE532    13027GGGL  LYC   O360  O360A2F     41514EA  SNSNCH76E   76EM8S5     EA  AIR METERING    MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            105                                                       (CAN) AN INTERMITTENT, MINOR ROUGHNESS IN THE ENGINE WAS OBSERVED TO TAKE PLACE JUST BEFORE LANDING. NOTHING OUT OF THE ORDINARY WAS OBSERVED DURING LANDING, TAXI AND SHUTDOWN (I.E. NO ABNORMAL CHT, EGT OR RPM). INSP OF ENGINE REVEALED NOTHING, EXTERNALLY.   CARB WAS REMOVED FROM ENGINE AND SENT IN TO INSTALL AN OPTIONAL ENRICHMENT KIT TO CONVERT THE P/N 10-3878 CARB TO A P/N 10-3878M FOR IMPROVED PERFORMANCE AND BETTER COLD WEATHER OPS. WHEN DISASSEMBLED, IT WAS DISCOVERED THAT THE CARB AIR METERING STOP PIN HAD VIBRATED LOOSE AND HAD FALLEN OUT. ALLOWING SPRING LOADED AIRBLEED NEEDLE TO POP OUT AND FALL INSIDE CARB, JAMMING THE THROTTLE. PILOT DID NOT DETECT ANY JAMMING OF THROTTLE OR MALFUNCTION OF MECHANICA1G71 3I3  ONTEXPA1G71E286    5  NP4EA     
20080225000312008022500031NE  2008       2          25         CA071205004      220071128G7300                UNKNOWN                                 CESSNA560   560XL       2076702CE  PWC   545   PW545B           NE                                              UNKNOWN         W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) DURING CLIMB, THE EEC REVERTED TO MANUAL WITH LOSS OF THRUST LEVER, RESPONSE NOTED. THRUST DECREASED INITIALLY TO 54 PERCENT AND LATER TO 25 PERCENT. FLIGHT WAS DIVERTED AND AN UNSCHEDULED LANDING PERFORMED. AFTER TROUBLESHOOTING, AC WAS CLEARED TO RETURN TO BASE. ADDITIONAL TROUBLESHOOTING FOCUSED ON FUEL SYS COMPONENTS.  AC HAS RETURNED TO SERVICE AFTER REPLACEMENT OF SUSPECT COMPONENTS.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071205004)                                                                                                                                                                                                                         2L72 4F4  FRTA22CE   E00059EN             
20080225000352008022500035EU  2008       2          25         CA071205005      120071202G7110                COWLING                                 UROCOPEC135 EC135P1     8680990EU  PWA   PW206 PW206B      0    NE                              ENGINE          BURNED          W      E   ENGINE SHUTDOWN                                                                                 A  FLAME/FIRE                                                                    TXTAXI/GRND HDL  1                      CA                                                                      (CAN) DURING START, AN ENGINE COMPARTMENT FIRE WAS NOTED. DAMAGE IS EVIDENT TO COWLING, ENGINE AND ENGINE COMPARTMENT.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071205005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G72 3U3  UO H88EU   E42NE                
20080225000372008022500037NE  2008       2          25         CA071205006      220071130G7261                ENGINE                                  DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE                                              OIL CONSUMPTION W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA                                          AE0084                      (CAN) OIL MIST WAS NOTED IN THE CABIN AFTER LANDING. INITIAL TROUBLESHOOTING REVEALED THAT 2 LITRES OF OIL WERE CONSUMED DURING THE PREVIOUS FLIGHT. ENGINE WAS REMOVED FOR INVESTIGATION.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071205006)                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA13NM   E20NE                
20080225000392008022500039EA  2008       2          25         CA071205007      220071130G7200                ENGINE                                  BELL  412   412         1182202SW  PWA   PT6T  PT6T6       52045EA                                              MAKING METAL    W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         EJ VIBRATION/BUFFET          WARNING INDICATION                                  CRCRUISE         1                      CA                                          72459                       (CAN) CREW HEARD A METALLIC BANG FROM THE ENGINE AREA, FOLLOWED BY CAUTION LIGHTS. ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED. SUBSEQUENT INITIAL INSPECTION REVEALED DEBRIS ON THE OIL FILTER. ENGINE IS BEING REMOVED FOR INVESTIGATION. P&WC WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071205007)                                                                                                                                                                                                                                                                                                                                                                                                1G72 4U4  U  H4SW    E22EA                
20080225000412008022500041NE  2008       2          25         CA071205008      220071128G7314                PUMP                                    AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              FUEL SYSTEM     MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE, THE CREW REPORTED THAT ENGINE TORQUE WAS (UNSTABLE).   POST FLIGHT INVESTIGATION REVEALED THAT ENGINE POWER WAS LIMITED TO 86 PERCENT VS. 90 PERCENT TARGET. FUEL PUMP AND FUEL CONTROL WERE REPLACED. FUEL PUMP IS SUSPECT AND WILL BE SENT FOR INVESTIGATION.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071205008)                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRT        E20NE                
20080225000682008022500068EA  2008       2          25         CA071205009      220071130G7200                ENGINE                                  BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA                                              FOD             W      O   OTHER                                                                                           RXJPARTIAL RPM/PWR LOSS      ENGINE FLAMEOUT           WARNING INDICATION        CRCRUISE         1                      CA                  FA0279                                              (CAN) ENGINE (FLAMED OUT) AND AUTO RECOVERED WITHIN TEN SECONDS TIME FRAME WITH NO CREW INTERVENTION.  FADEC DATA INDICATES POSSIBLE WATER/ICE INGESTION. (TC NR 20071205009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA13NM   E00062EN             
20080225000692008022500069EU  2008       2          25         CA071205010      120071126G2160342B030000AMDTA THERMOSTAT                              AIRBUS320   A320211     3930320EU  CFMINTCFM56 CFM565A1         NE                              TEMP CONTROL    FAILED          W      BA  EMER. DESCENT           UNSCHED LANDING                                                         J  WARNING INDICATION                                                            CRCRUISE         1                      CA       5970                                                           (CAN) WHILE IN CRUISE AT FL 390, THE CREW HAD A BLEED AIR SUPPLY NR 2 FAILURE, AND DURING A DESCENT WHILE REFERING TO THE QRH, ALSO HAD NR 1 BLEED FAIL. CREW LOST BOTH PACKS, AND INITIATED EMERGENCY DESCENT TO 10,000 FT. FLT DIVERTED TO NEARBY AIRPORT.  TEMP CONTROL THERMOSTAT (TCT) AND FAN AIR VALVE WERE CHANGED. IT IS TO BE NOTED THAT THE TCT IS POST MOD TO ENABLE IT TO OPERATE UNDER SINGLE BLEED CONDITIONS. (TC NR 20071205010)                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA28NM   E29NE                
20080225000712008022500071CE  2008       2          25         CA071206001      120071205G3230508103237       TORQUE LINK                             BEECH 100   A100        1152915CE  PWA   PT6   PT6A28           EA  MCAULY4HFR344HFR34C762  NE  MLG             CRACKED         W      L   ABORTED APPROACH                                                                                O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING A SPECIAL LPI INSPECTION OF THE MLG TORQUE LINKS DUE TO THE FAILURE OF A LINK ON ANOTHER AIRCRAFT (SDR 20071024010 AND 20071122002), 3 OF THE 4 LINKS WERE FOUND CRACKED.  THE LINKS FROM 3 ADDITIONAL AIRCRAFT WERE REPLACED IN ORDER TO COMPLETE THE LPI OFF AIRCRAFT, THE LPI WAS COMPLETED AND 4 OF THE 12 LINKS WERE FOUND TO HAVE VERY SMALL CRACKS, ALL THE CRACKS ARE IN THE SAME RADIUS AREA,  (TC# 20071206001)                                                                                                                                                                                                                                                                                                          1L72 3T4  T  A14CE   E4EA    6  C3PNE     
20080225000732008022500073CE  2008       2          25         CA071206003      120071203G35101183840093      CONTROL CABLE                           BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  OXYGEN MASK     STIFF           W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       10075                                                          (CAN) WHILE PERFORMING AN INTERIOR PREFLIGHT CHECK THE F/O PULLED THE CONTROL KNOB FOR THE OXYGEN SYS. THE KNOB WAS DIFFICULT TO PULL BUT THE PILOT CONFIRMED THAT THERE WAS FLOW AT THE MASKS. DURING THE FLIGHT THE PILOT AND CO-PILOT DONNED THE OXYGEN MASKS AND FOUND THERE WAS NO OXYGEN FLOW.  UPON RETURN TO BASE MAINT CHECKED THE SYS AND FOUND IT SERVICEABLE. DURING THE NEXT FLIGHT THE PILOTS FOUND THE SAME PROBLEM WITH THE CONTROL KNOB. DURING TROUBLESHOOTING THE AC WAS COLD-SOAKED AND THE KNOB FOUND DIFFICULT TO PULL. THE CONTROL CABLE ASSY WAS REMOVED AND REPLACED. (TC NR 20071206003)                                                                                                                              2L72 4T4  TRTA24CE   E26NE   5  CP10NE    
20080225000752008022500075CE  2008       2          25         CA071206004      120071205G3260MS25237327      BULB                                    CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              MLG ANNUNCIATOR BURNED OUT      W      L   ABORTED APPROACH                                                                                P  NO WARNING INDICATION                                                         APAPPROACH       1                      CA                                                                      (CAN) PILOTS REPORT, ON FINAL TO LANDING RUNWAY, SELECTED THE GEAR DOWN HOWEVER THE RT MAIN GEAR GREEN LIGHT FAILED TO ILLUMINATE. THE RED (GEAR UNLOCKED) LIGHT WAS EXTINGUISHED. ADVISED TOWER AND CONDUCTED A MISSED APPROACH WITH REQUEST FOR VECTORS TO REMAIN IN AREA. WE COULD VISUALLY SEE THE WHEEL DOWN, AND THE GEAR HORN WOULD NOT SOUND WITH FULL FLAPS HOWEVER EXECUTED THE MANUAL EXTENSION PROCEDURE REGARDLESS, ASKED FOR THE EMERGENCY VEHICLES TO BE STANDING BY ON LANDING AS A PRECAUTION. BRIEFED OURONLY PASSENGERS AND LANDED WITH OUT FURTHER INCIDENT. CLEARED THE RUNWAY, ASKED FOR EMERGENCY CREWS TO VIEW OUR RT WHEEL FOR ANY OBVIOUS DAMAGED. THEY REPORT NOTHING APPARENT TO THEM AND SINCE THE AC LANDED, ROLLE1L72 4F4  F  A22CE   E1NE                 
20080225000782008022500078CE  2008       2          25         CA071206005      120071203G2120                UNKNOWN                                 BEECH 200   200BEECH    1152920CE  PWA   PT6   PT6A67D          NE  HARTZLHCE4A HCE4A3I     NE  COCKPIT         ODOR            W      A   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                              UE63                                    (CAN) UPON REACHING LEVEL FLIGHT BOTH THE CAPT AND F/O SMELLED SMOKE IN THE COCKPIT, WHICH SHORTLY AFTER COULD ALSO BE SEEN IN THE COCKPIT. AFTER LESS THAN A MINUTE THE SMOKE DISSIPATED AND THE CAPTAIN MADE THE DECISION TO RETURN TO THE DEPARTURE POINT. AFTER CONTACT WITH ATC THE SMOKE AND SMELL HAD COMPLETELY DISAPPEARED. MAINT PERFORMED GROUND RUNS AND COULD NOT DUPLICATE THE DEFECT. SYS TESTED AND INSPECTED, FWD NOSE AVIONICS, INSTRUMENT PANEL WIRING, COOLING FANS, CABIN AND COCKPIT LIGHTING, CIRCUIT BREAKERS, PC BOARDS, INVERTER AND DC BUS CHECKS, ENVIRONMENTAL SYSTEM, ACM, LT AND RT ENGINES, AND WINDSHIELD HEAT ALL CHECKED SERVICEABLE WITH NO FAULT FOUND. (TC NR 20071206005)                                1L72 4T4  T  A24CE   E26NE   5  CP10NE    
20080225000792008022500079NM  2008       2          25         CA071206006      120071126G271082700518001     CONTROL CABLE                           DHAV  DHC8  DHC8106     2809020NM  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF7       NE  AILERON         WORN            W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             DEDESCENT        1                      CA                                                                      (CAN) PILOTS REPORTED THAT THE AILERON CONTROLS WERE STIFF (OAT -20C). INSPECTION OF THE AIRCRAFT WAS CARRIED OUT AND THE AILERON CABLE WAS FOUND TO BE WORN WHERE IT CROSSED A ROLLER FAIRLEAD AT APPROX STN YW189.00. THE ROLLER FAIRLEAD WAS NEARLY SEIZED. THE OB AILERON QUADRANT BEARINGS WERE ALSO FOUND TO BE STIFF WHEN COLD. THE CABLES IN BOTH WINGS WERE REPLACED AS WELL AS THE ROLLER FAIRLEAD. THE BEARINGS WERE REPLACED IN THE AILERON QUADRANTS AND THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (TC NR 20071206006)                                                                                                                                                                                         2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080225000832008022500083NM  2008       2          25         CA071206007      120071203G2797                WIRE HARNESS    LUCAS                   DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  AILERON ACTUATORWORN            W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             CLCLIMB          1                      CA       1855018550 0084                                                (CAN) AFTER ROTATION, HEAVY LT AILERON INPUT NEEDED IN FLIGHT. AILERON TRIM WAS CENTERED BUT HAD NO EFFECT. FLIGHT RETURNED TO DEPARTURE AIRPORT SAFELY WITH NO NEED TO DECLARE AN EMERGENCY. MAINT TROUBLESHOOTING, FOUND WIRE HARNESS ON AILERON TRIM ACTUATOR WORN WHERE WIRES ENTER BODY OF ACTUATOR CAUSING CIRCUIT BREAKER TO POP WHEN TRIM IMPUT WAS SELECTED. AILERON TRIM ACTUATOR REPLACED AND SYSTEM TESTED SERVICEABLE. (TC NR 20071206007)                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080319001672008031900167NE  2008       3          19         CA071206008      220071129G732070BM032010      MODULE                                  SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                              ENGINE FUEL     DAMAGED         W      A   UNSCHED LANDING                                                                                 XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA       2975                                                           (CAN) IN A CRUISE FLIGHT OR CLIMB POWER, THE AC ENGINE WOULD SURGE. THE AC WAS REMOVED FROM SERVICE FOR INSP.  A CLOSE INSPECTION OF THE COVER THAT IS LOCATED OVER THE COMPRESSOR IMPELLOR, REVEALED A HOLE APPX. 4-5MM IN DIAMETER. THE MODULE 3 WAS REMOVED AND REPLACED WITH A DIFFERENT MODULE AND THE AIRCRAFT WAS RE CERTIFIED.                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3U3  U  H9EU    E00054EN             
20080225000852008022500085SO  2008       2          25         CA071207002      120071120G323140327000        TRUNNION                                PIPER PA31  PA31350     7103110SO  LYC   O540  LTIO540J2BD 41533EA  HARTZLHCE3Y HCE3YR2A    GL  MLG DOOR        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                              317552130                               (CAN) DURING INSPECTION, A CRACK WAS FOUND IN THE RT UPPER TRUNNION, MOVING FROM THE BOTTOM OF THE TRUNNION UPWARDS TOWARD THE ATTACHMENT POINT, THE GEAR DOOR ROD.  THIS IS THE SECOND ONE THIS YEAR. (TC NR 20071207002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3O3  O  A20SO   E14EA   5  CP33EA    
20080225000862008022500086NM  2008       2          25         CA071207003      120071104G3230483023          SOLENOID VALVE                          BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  RT MLG          INOPERATIVE     W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) UPON TAKEOFF AND GEAR RETRACTION RT MLG DOOR REMAINED OPEN WITH RT GEAR DOOR UNSAFE INDICATION.  MAINT REPLACED RT MLG SOLENOID SEQUENCE VALVE. (TC NR 20071207003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080319001682008031900168EA  2008       3          19         CA071207004      220071130G8500                ENGINE                                  GULSTM500   500B        0141106SW  LYC   O540  IO540B1A5   41532EA  HARTZLHCC3Y HCC3YR2     NE                  POWER LOSS      W      B   EMER. DESCENT                                                                                   RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      (CAN) AFTER 45 MINUTE FLIGHT BOTH ENGINES BEGAN LOSING PWR WITH NO FUEL FLOW INDICATIONS OR FUEL PRESSURE INDICATIONS. ENGINES WOULD ONLY DEVELOP IDLE PWR. PILOT MADE A FORCED LANDING WITH MINOR INJURIES. FOLLOW UP INVESTIGATION TO FOLLOW. FOLLOW UP REPORT ON FINDING TO FOLLOW. (TC NR 20071207004)                                                                                                                                                                                                                                                                                                                                                                                                                                      1H72 3O3  O  6A1     1E4     5  CP25EA    
20080319001692008031900169NE  2008       3          19         CA071208001      220071205G732001644448430     FCU                                     SNIAS 350   AS350BA     8680817EU  TMECA ARRIELARRIEL1B    6OO30NE                              ENGINE          SURGES          W      K   NONE                                                                                            X  ENGINE FLAMEOUT                                                               ININSP/MAINT     1                      CA                                                                      (CAN) FCU WAS SURGING DURING A GROUND RUN LEAK CHECK, BLEED VALVE TACH BOX HAD BEEN CHANGED FOR TROUBLESHOOTING, SURGING CONTINUED. FCU CHANGED OUT AND SURGING PROBLEM WAS RESOLVED.  AC RETURN TO SERVICE. (TC NR 20071208001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1G71 3U3  UNCH9EU    E19EU                
20080225000872008022500087NM  2008       2          25         CA071210001      120071206G213320224806        ACTUATOR                                BOEING767   7673Y0             NM  GE    CF6   CF680C2B6F  30025NE                              OUTFLOW VALVE   MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) ON DEPARTURE FLIGHT, LOST BOTH AUTO PRESSURIZATION SYS. FLIGHT CLIMBED TO FL190, AND RETURNED TO AIRPORT. CABIN PRESS WAS APPROX 2000 FT. THE STATUS MESSAGES RECEIVED: CABIN ALT AUTO 1 AND CABIN ALT AUTO 2. QRH CARRIED OUT, AND FLIGHT RETURNED TO DEPARTURE. NO FAULT FOUND, SYSTEM RESET, BUT THE VALVE ACTUATOR IS SUSPECTED,  (TC NR 20071210001)                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA1NM    E13NE                
20080324004212008032400421EU  2008       3          24         CA071210003      120071206G3250AIR860020       SELECTOR VALVE                          BAG   JETSTMJETSTM3212  1500217EU                                                               NLG STEERING    UNSERVICEABLE   W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                  BADL48                                              (CAN) ON TAXI, PILOT FOUND THAT HE HAD REDUCED STEERING CONTROL OF THE AC USING THE NOSE WHEEL STEERING SYS. PILOT RETURNED TO BLOCKS, UNABLE TO CONTINUE HIS FLIGHT. UPON TROUBLESHOOTING, IT WAS FOUND THAT THE STEERING SELECTOR WAS NOT OPERATING PROPERLY, CAUSING A STEERING SYS FAILURE. THE STEERING SELECTOR WAS INSTALLED 03/10/2007 AND HAS ACCUMULATED 513 CYCLES SINCE O/H AND 38.2 WEEKS IN SERVICE. THE O/H INTERVAL FOR THIS PART IS 10 000 CYCLES OR 72 MONTHS. THE STEERING SELECTOR WAS REMOVED AND AN O/H UNIT WAS INSTALLED AND THE NOSE WHEEL STEERING SYS FUNCTION CHECKED WITH NO FAULTS FOUND. AC RETURNED TO SERVICE. THIS STEERING SELECTOR WAS PURCHASED THROUGH TURBINE ENGINE CONSULTANTS INCORPORATED AFTER HAVIN2L72 4T    RTBA15CAA                      
20080225000892008022500089CE  2008       2          25         CA071210004      120071209G5753351650503031    HINGE                                   BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCE4N HCE4N3      NE  TE FLAP         WORN            W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9534                                                           (CAN) LT AND RT OB FLAPS IB HINGES WORN DUE TO ROLLER DIGGING INTO OB BRACKETS P/N 35-165050-30 AND 35-165050-31. THE AFT BEARINGS/ROLLERS HAVE TO BE REMOVED TO GET A GOOD INSPECTION OF THIS AREA. IT SHOULD NOT BE DONE (IN-SITU). THIS IS THE 3RD AIRCRAFT IN THIS COMPANY FLEET THAT HAS HAD WEAR IN THIS AREA. IF LET GO TOO FAR, A FLIGHT CONTROL ISSUE MAY BE ENCOUNTERED. (TC NR 20071210004)                                                                                                                                                                                                                                                                                                                                          1L72 4T4  T  A24CE   E4EA    5  CP10NE    
20080225000902008022500090WP  2008       2          25         CA071210005      120071204G6310369A53515       HOUSING         DOUG                    HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              CLUTCH          CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA            1758                                                      (CAN) CLUTCH HOUSING RECEIVED FOR OVERHAUL AFTER PAINT STRIPPING HOUSING SENT OUT FOR NDT INSPECTION AND CAME BACK FOUND CRACKED ON ENGINE SIDE OF HOUSING. (TC NR 20071210005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3U3  U  H3WE    E4CE                 
20080225000912008022500091EU  2008       2          25         CA071210006      120071207G2917RPR2B           CONTROLLER                              SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              HYD ACCUMULATOR MALFUNCTIONED   W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       8813                                                           (CAN) DURING FIRST GROUND RUN FOLLOWING A MAJOR 12 YEAR INSP, THERE WAS SIGNIFICANT HYDR FLUID LOSS IN THE AREA OF THE MAIN ROTOR ACCUMULATORS. THE HELICOPTER HAD BEEN AT 70 PERCENT GROUND IDLE FOR APPROX 3-4 MINUTES. THE HELICOPTER WAS SHUTDOWN IMMEDIATELY AND INSPECTED. ALL (3) ACCUMULATORS UNDERWENT VARYING DEGREES OF DEFORMATION (EXPANSION) DUE EXCESSIVE HYDR PRESSURE. HYDR FLUID LOSS WAS ISOLATED TO THE AREA OF THE COLLECTOR ASSEMBLIES MOUNTED ON THE SIDES OF THE SERVOS, SPECIFICALLY AT THE ACCUMULATOR AND ELECTRO VALVE JOINTS. IT IS SUSPECTED THE PRESSURE REGULATING VALVE OF THE HYDR MANIFOLD STUCK, PREVENTING FLUID FROM RETURNING TO TANK. THIS ALLOWED PRESSURE TO BUILD BEYOND REGULATED PRESSURE. FURTHER 1G71 3U3  U  H9EU    E19EU                
20080225000922008022500092NM  2008       2          25         CA071211001      120071108G273182760174005     JACKSCREW                               DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF23      NE  ELEVATOR TRIM   CONTAMINATED    W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             CRCRUISE         1                      CA       7816                                                           (CAN) ADVISORY MESSAGE DISPLAY INDICATED (MISTRIM NOSE DN) WITH AUTOPILOT ENGAGED. DISENGAGED AUTOPILOT - FWD CONTROL COLUMN FORCE REQUIRED TO MAINTAIN LEVEL FLIGHT, ATTEMPTED TO TRIM FWD BUT TRIM WHEEL WAS JAMMED WITH TRIM INDICATOR AT FWD OF THE TAKEOFF RANGE. TRIM MOVED REARWARDS OF THAT POSITION BUT NOT FWD OF IT. PAN DECLARED AND SERVICES REQUESTED, NORMAL APPROACH AND LANDING COMPLETED. FUNCTIONAL CHECK OF THE ELEVATOR TRIM SYS CARRIED OUT ON THE GROUND.  UNABLE TO REPLICATE REPORTED CONDITION. BOTH THE LT AND RT HAND SCREW JACK ASSEMBLIES, ELEVATOR TRIM WERE INSPECTED AND FOUND TO HAVE SUFFICIENT GREASE LUBRICATION, BUT THE GREASE WAS DETERMINED TO BE WATER CONTAMINATED DUE TO THE DISCOLORATION OF THE GR2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080225000932008022500093EU  2008       2          25         CA071211002      120071210G2750Z4243130000     CONTROL CABLE                           ZLIN  242   Z242L       9970204EU  LYC   O360  AEIO360A1B6 41514EA  MUHBR MTV   MTV9*       EU  TE FLAPS        FRAYED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       404                                                            (CAN) THE FLAP CENTER CABLE WAS FOUND FRAYED DURING REGULARLY SCHEDULED MAINTENANCE. (TC NR 20071211002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L71 3O3  O0 A76EU   1E10    5  CP24NE    
20080225000942008022500094    2008       2          25         CA071211003      420071208G34178220372497      ADC                                     CNDAIRCL600 CL6002B16   1900305EA  GE    CF34  CF348C5     30050NE                                              MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 H  ELECT. POWER LOSS-50 PC                                                       NRNOT REPORTED   1                      CA       616  616                                                       (CAN) THE FO REPORTED AN AIRSPEED OVER-SPEED TAPE ILLUMINATED AND COVERED THE ENTIRE SPEED TAPE ON THE AIRSPEED INDICATOR. AN AMBER (STALL FAIL) EICAS MESSAGE AND STICK SHAKER ENSUED. THE STALL PTCT SWITCH WAS SELECTED OFF HOWEVER THE STICK SHAKER CONTINUED. QRH PROCEDURE C/O, REVERTED TO NR1 ADC AND SHAKER STOPPED, ALTHOUGH STALL FAIL, SPOILER FAIL AND MANY OTHER EICAS MESSAGES DISPLAYED. OPERATED SINGLE ADC AND ELECTED TO TURN BACK TO DEPARTURE. MDC FAULT HISTORY DISPLAYED ADC 2 NR OUT PUT MESSAGE B1-005863, STALL FAIL B1-008073 AND LABEL 350 BIT 27 SET INCONSISTENT ADC DATA. NR2 ADC AND NR2 AOA SENSOR AT FAULT. NR2 ADC AND NR2 AOA SENSOR REPLACED AND FUNCTION TEST OF ADC-OVERSPEED WARNING AND ALTIMETER SCALE2L72 4F4  FRTA21EA   E00063EN             
20080225000952008022500095EA  2008       2          25         CA071211004      120071205G2750865D1007        PDU                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAPS        FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       7610 7610                                                      (CAN) AFTER LANDING WITH FLAPS AT 45 DEGREES, FLAPS SELECTED TO 0 DEGREES. CREW RECEIVED A FLAP FAIL AMBER MESSAGE AT FLAPS 41 DEGREES. MAINTENANCE TROUBLESHOOTING REVEILED FECU FAULT CODES FOR ASYMMETRY, BINDNG AND FLAPS NOT IN POSITION LEADING TO REPLACEMENT OF THE FLAP POWER DRIVE UNIT IAW AMM 27-52-01-400.  WILL UPDATE WHEN TEAR DOWN RESULTS BECOME AVAILABLE. (TC NR 20071211004)                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20080225000962008022500096EA  2008       2          25         CA071211005      120071205G27501104SD10020     FLEX DRIVE                              CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAPS        TWISTED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFTER LANDING WITH FLAPS AT 45 DEGREES, FLAPS SELECTED TO 0 DEGREES. CREW RECEIVED A FLAP FAIL AMBER MESSAGE AT FLAPS 41 DEGREES. DURING MAINTENANCE TROUBLESHOOTING OF FLAPS THE NR 2 RT FLEX DRIVE SHAFT ASSY WAS FOUND TWISTED. UPON REMOVAL PART LENGHTH WAS DISCOVERED TO BE 40 INCHES INSTEAD OF 39 INCHES IAW MFG SPECIFICATIONS. NO RECORD OF PREVIOUS REPLACEMENT SINCE AC NEW. IPC 27-53-00 FIG 1, ITEM 10B.  (TC NR 20071211005)                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20080225000972008022500097NE  2008       2          25         CA071211006      220071130G7314LW15473         PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENG FUEL        LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA            746                                                       (CAN) DURING A 50 HOUR INSPECTION THE ENGINE DRIVE FUEL PUMP WAS FOUND LEAKING FROM SEAL.  (INNER DIAPHRAM) (TC NR 20071211006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3O3  O  H11NM   1E4                  
20080225000982008022500098NE  2008       2          25         CA071211007      220071211G7314LW15473         PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENG FUEL        LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       822                                                            (CAN) DURING GROUND RUN, PUMP WAS FOUND LEAKING FROM DRAIN. PUMP REPLACED, NO FURTHER DEFECT. (TC NR 20071211007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3O3  O  H11NM   1E4                  
20080225000992008022500099EU  2008       2          25         CA071211008      120071210G2820                WYE PIPE                                SNIAS 350   AS350BA     8680817EU  LYC   LTS101LTS101600A2 41560NE                              FUEL SYSTEM     LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) THE AC WAS BEING REFUELED OUT SIDE WHEN FUEL STARTED POURING ON THE GROUND FROM SOMEWHERE IN THE FUEL TANK AREA. FURTHER INVESTIGATION REVEALED THE (Y) CONNECTION OF THE FUEL SUPPLY LINE FROM THE 2 BOOST PUMPS HAD SIMPLY FALLEN OUT OF THE FUEL LINE GOING UP TO THE FUEL FILTER ON THE TRANSMISSION DECK. THE 2 GEAR CLAMPS THAT SECURE THE HOSE TO THE (Y) FITTING WERE SECURED TIGHT ENOUGH THAT THE CLAMPS FELT TIGHT AND COULD NOT BE ROTATED ON THE HOSE BUT WHEN CHECKED WITH A SCREWDRIVER, THEY COULD BE TIGHTENED BY A FEW TURNS.  DUE THE NATURE OF THE ROUTING AND CLAMPING OF THE HOSE, THERE WAS A NATURAL TENDENCY FOR THE Y FITTING TO PULL DOWN ON THE UPPER HOSE. THE HOSE WAS REPOSITIONED AND CLAMPED PROPERLY TO 1G71 3U3  UNCH9EU    E5NE                 
20080225001012008022500101CE  2008       2          25         CA071212002      120070921G571195B55           SPAR                                    BEECH 95    95B55       1152729CE  CONT  O470  IO470L      17026SO  HARTZLHCC2Y BHCC2YF2    GL  WING            CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9896                                                           (CAN) DURING ANNUAL INSPECTION, VISUAL INSPECTION OF AREA REVEALED A SUSPECTED CRACK. NOT OF DYE PENETRANT AND EDDY CURRENT CONFIRMED. MFG SERVICE KIT TO INSTALLED. PART LAST NDT INSPECTED 22.1 HRS PREVIOUS AND NO INDICATIONS. (TC NR 20071212002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3O3  ORT3A16    3E1     5  CP920     
20080225001022008022500102    2008       2          25         CA071212003      420070510G3416152734          RING                                    ISRAEL1125  1125               NM  GARRTTTFE731TFE7313A    01518WP                              STBY ALTMETER   INCORRECT       W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                  8091                                                (CAN) MODIFICATION OF LOCKING PIN SLOT OF ITEM (PN 152734). RING SUPPORT FOUND ON THIS STBY ALTIMETER (TC NR 20071212003).                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA16NM   E6WE                 
20080225001032008022500103GL  2008       2          25         CA071212004      320071110G6114B1192           DIAPHRAGM                               NAVIONSTC   STCNAVION              CONT  E185  E1853       17014SO  HARTZLHC12V HC12V20*    GL  PROP HUB        CRACKED         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       34                                                             (CAN) OIL LEAK AROUND PROP HUB AND SPRAYED ONTO WINDSHIELD.  PROP REMOVED. JACK PLATE ASSY REMOVED. DIAPHRAGM REMOVED. INNER SURFACE AROUND CENTER ATTACH RING ALMOST TOTALLY SPLIT AROUND CIRCUMFERENCE. THE DIAPHRAGM WAS INSTALLED JUNE 15, 2007 AND FAILED IMMEDIATELY.  (TC NR 20071212004)                                                                                                                                                                                                                                                                                                                                                                                                                                                1L71 3O3  O  A782    E246    5  CP46GL    
20080225001052008022500105CE  2008       2          25         CA071212005      120071127G5344051701912       HINGE PIN                               CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA  MCAULY1A170 1A170E      GL  DOOR HINGE      CORRODED        W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA                                                                      (CAN) DOOR HINGE PINS APPEAR TO BE WELDING RODS OR STEEL PINS CUT LONG AND BENT OVER TO SERVE FROM FALLING OUT. REPLACED WITH PROPER PARTS. CAUSED DISSIMILAR METAL CORROSION TO HINGE MATERIAL AS BOGUS PINS RUSTED.  THE ENTIRE FLEET HAS THESE SAME BOGUS PINS (10 AIRCRAFT IN TOTAL). INSTALLED BY PREVIOUS MAINTAINER, AMO 73-03. (TC NR 20071212005)                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O3  ONT3A12    1E10    5  NP857     
20080225001062008022500106EA  2008       2          25         CA071212006      320071127G6111                BLADE           SNSNCH                  DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       265        AG1827                              AG1827          (CAN) LONGITUDINAL CRACK AT BLADE TIP NR 1 BLADE.  CRACK APPROX 1.5 INCH LONG AT APPROX .75 CHORD.  FOUND DURING INSPECTION (ROUTINE). APPEARS TO BE CAUSED BY IMPACT DAMAGE FROM FOD. (TC NR 20071212006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20080225001082008022500108EA  2008       2          25         CA071212007      320071127G6111                BLADE                                   DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  PROPELLER       CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         ININSP/MAINT     1                      CA       330        AG3920                              AG3920          (CAN) LONGITUDINAL CRACK AT BLADE TIP, NR 1 BLADE.  CRACK APPROX 0.75 INCH LONG AT .25 CHORD.  FOUND DURING INSPECTION (ROUTINE). NO APPARENT CAUSE, NO IMPACT DAMAGE FROM FOD. (TC NR 20071212007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20080225001102008022500110NE  2008       2          25         CA071212009      220071114G7200                ENGINE                                  DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE                                              CONTAMINATED    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          123216                      (CAN) CREW RECEIVED A LOW OIL PRESSURE WARNING AND ELECTED TO SHUTDOWN THE ENGINE. INITIAL POST FLIGHT INVESTIGATION REVEALS CONTAMINATION OF THE CHIP DETECTORS AND OIL FILTERS. THE ENGINE WILL BE SENT FOR INVESTIGATION.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071212009)                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E20NE                
20080225001112008022500111NE  2008       2          25         CA071212010      220070613G7250                TURBINE                                 AEROSPATR72 ATR72201    8680943EU  PWA   PW120 PW124B           NE                              ENGINE          DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                          124515                      (CAN) REPORTED TO MFG ON DEC 07 2007.  ENGINE REPORTED TO HAVE SUFFERED AN INFLIGHT SHUTDOWN DURING TAKEOFF/CLIMB. NO OTHER DETAILS PROVIDED. POST FLIGHT INSPECTION INDICATES SEVERE DAMAGE TO THE TURBINE SECTION.   MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071212010)                                                                                                                                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA53EU   E2ONE                
20080225001132008022500113NE  2008       2          25         CA071212011      220071021G7261                TUBE                                    AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE                              ENGINE OIL      FRACTURED       W      FEA ACTIVATE FIRE EXT.      ENGINE SHUTDOWN         UNSCHED LANDING                                 KAJFLUID LOSS                FLAME/FIRE                WARNING INDICATION        CRCRUISE         1                      CA                                          120746                      (CAN) FIRE WARNING DURING CRUISE. CREW ACTIVATED THE FIRE SUPPRESSION SYSTEM AND SECURED THE ENGINE. POST FLIGHT INITIAL INSPECTION REVEALED A FRACTURED NR 6 AND NR 7 BEARING OIL TRANSFER TUBE. SOME FIRE DAMAGE WAS OBSERVED ON THE AFT PORTION OF THE ENGINE. THE ENGINE HAS BEEN REMOVED AND FORWARDED FOR FUTHER INVESTIGATION.   MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071212011)                                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA53EU   E20NE                
20080225001142008022500114CE  2008       2          25         CA071212012      120071211G2720MS35206228      SCREW                                   CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              RUDDER PEDAL    MISSING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) SL 550-27-14 FOUND 2 SCREWS, P/N MS350206-228, MISSING FROM PILOTS LT RUDDER SUPPORT BRACKET AND 2 LOOSE SCREWS P/N MS 350206-228 ON THE CO-PILOTS RT RUDDER SUPPORT BRACKET.CARRY OUT ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 1THRU 4. (TC NR 20071212012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 4F4  F  A22CE   E1NE                 
20080225001152008022500115EU  2008       2          25         CA071212014      120071211G2922704A34629013    STRAINER                                SNIAS 350   AS350BA     8680817EU  TMECA ARRIELARRIEL1B    6OO30NE                              HYD SYSTEM      CONTAMINATED    W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) STRAINER WAS INSPECTED AND FOUND CONTAMINATED WITH PARTICLES FOREIGN MATTER AND SLIVERS OF MATERIAL FROM THE O-RING, P/N MS28775-016, WHICH WAS HARD AND BRITTLE.  THE MFG MM REQUIRES INSPECTION AND CLEANING OF THE STRAINER ONLY WHEN THE MANIFOLD IS REPLACED DURING A HYDRAULIC PUMP REPLACEMENT, THERE IS NO SCHEDULED INTERVAL FOR CLEANING.  ALL AC IN THE COMPANY FLEET WILL BE INSPECTED ON OR BEFORE THE NEXT 100 HOUR INSPECTION AND THIS TASK WILL BE ADDED TO 500 HOUR T-INSPECTION.  THE MFG TECH REP HAS BEEN INFORMED OF THE FINDINGS OF THIS INSPECTION. (TC NR 20071212014)                                                                                                                                            1G71 3U3  UNCH9EU    E19EU                
20080225001182008022500118EA  2008       2          25         CA071212024      120071026G78103009090         EXHAUST DUCT                            DHAV  DHC6  DHC6100     2802610EA  PWA   PT6   PT6A20      52043EA  HARTZLHCB3T HCB3TN3     GL  ENGINE          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5861                                                           (CAN) WHILE INSPECTING THE POWER SECTION FOR REASSEMBLY AFTER HSI, CIRCUMFERENTIAL CRACKS WERE DISCOVERED ALONG THE WELDS OF THE EXHAUST DUCT JUST FWD OF THE PT VANE MOUNTING FLANGE. (4) CRACKS RANGED IN LENGTH FROM .75 INCH TO 4.75 INCH. THE POWER SECTION WAS REPLACED. (TC NR 20071212024)                                                                                                                                                                                                                                                                                                                                                                                                                                              1H72 3T3  TRTA9EA    E4EA    6  CP15EA    
20080225001192008022500119GL  2008       2          25         CA071212025      320071212G611487292           HUB             MCAULY                  CESSNA180   180J        2072622CE  CONT  O470  O470R       17026SO  MCAULY2A34C 2A34C203    GL  PROPELLER       CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1481       022853                              022853          (CAN) AT OVERHAUL PROPELLER HUB WAS STRIPPED OF PAINT FINISH. ENTIRE OUTER SURFACE OF HUB AND BLADE O-RING GROOVES WERE CORRODED BEYOND LIMITS. HUB WAS RETURNED TO MFG FOR EVALUATION. (TC NR 20071212025)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3O3  O  5A6     E273    5  CP3EA     
20080225001222008022500122GL  2008       2          25         CA071212026      320071211G6110                FLANGE          MCAULY                  CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  PROPELLER       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            1516  SR773463                            SR773463        (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION IAW AD 2003-12-05. A SMALL CRACK WAS LOCATED RADIALLY AT THE EDGE OF ONE MOUNTING BOLT HOLE.  TIME SINCE LAST INSPECTED FOR AD 2003-12-05 WAS 409.2 HOURS. (TC NR 20071212026)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                1H71 3O3  ONT3A19    E223    5  NP50GL    
20080225001232008022500123CE  2008       2          25         CA071212027      120071207G3244TU29110010      TIRE                                    CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  MLG             FLAT            W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) TIRE WENT FLAT. (TC NR 20071212027)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20080225001242008022500124CE  2008       2          25         CA071212028      120071128G3244TU29110010      TIRE                                    CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  MLG             FLAT            W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA       920                                                            (CAN) TIRE WENT FLAT. (TC NR 20071212028)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20080225001262008022500126NE  2008       2          25         CA071213001      220071212G72616087T04P09      SCAVENGE PUMP   GE                      CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              ENGINE          FAILED          W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA       29540367   807240                  807240                      (CAN) DURING CRUISE FLIGHT, THE CREW RECEIVED RED NR 2 ENG LOW OIL PRESS MESSAGE AND GAUGE INDICATION FOR NR 2 ENGINE SHOWED (0) PSI, CREW ELECTED TO SHUTDOWN ENGINE AND RETURN TO DEPARTURE AIRPORT, NORMAL LANDING. MAINTENANCE FOUND NR 2 ENGINE, OIL LUBE/SCAVENGE PUMP ROTATES FREELY WITH NO PRESSURE OUTPUT.  PUMP TO BE SENT OUT TO VENDOR FOR INVESTIGATION.  OIL PUMP INFORMATION: MFG CO P/N 99207SOCN6087T04P09, CODE IDENT 86329, REF 4406-9 S/N NMAAD498 TSN 29540HR / 24208CY , TSO 367HR / 309CY.(TC NR 20071213001)                                                                                                                                                                                                           2L72 4F4  FRTA21EA   E15NE                
20080225001272008022500127CE  2008       2          25         CA071213002      120071212G2121                BRUSHES                                 BEECH 90    C90A        1152911CE  PWA   PT6   PT6A21      52043EA  HARTZLHCB3T HCB3TN3     GL  BLOWER MOTOR    BURNED          W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA            1357                                                      (CAN) CREW DECLARED EMERGENCY DUE TO SMOKE IN COCKPIT AND LANDED SAFELY. REPAIR PARTY LT FROM ANOTHER BASE. FOUND CAUSE WAS CABIN VENT BLOWER. DISABLED SYSTEM. AIRCRAFT FERRIED TO AIRPORT.  MAINTENANCE WILL REPLACE VENT BLOWER. (TC NR 20071213002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3T4  TRT3A20    E4EA    6  CP15EA    
20080225001282008022500128NM  2008       2          25         CA071213003      120071213G5321CMKD8400FP540   FLOOR PANEL                             BOMBDRDHC8  DHC8400            NM                                                               CABIN           DELAMINATED     W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       2595                                                           (CAN) FORWARD CABIN FLOOR PANEL WHERE PURSER STANDS TO GIVE PRE-FLIGHT BRIEFING STARTING TO DELAMINATE. MATERIAL IS COMP 28 WHICH IS BUILT TO STAND STRESS OF 75 LB/FT SQUARED. (TC NR 20071213003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2H72 4T    RTA13NM                        
             20080520     CE  2008       5          20         CA071213004      120070725G272007600323        SHAFT                                   CESSNA180   180J        2072622CE  CONT  O470  O470S       17026SO  MCAULY2A34C 2A34C203    GL  RUDDER PEDALS   CRACKED         W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       14983                                                          (CAN) RUDDER BAR ASSY CRACKED AT SPIGOT ATTACH POINT WHERE RUDDER PEDAL STUB SHAFT (PN 0411307) CONNECTS TO RUDDER BAR ASSY.  PILOTS REPORTED A SOFT PEDAL ON WATER OPERATIONS, INVESTIGATION REVEALED A SPHERICAL CRACK ON THE RUDDER PEDAL TORQUE TUBE. (TC NR 20071213004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H71 3O3  O  5A6     E273    5  CP3EA     
20080225001292008022500129CE  2008       2          25         CA071214001      120071204G5220                HANDLE                                  BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  HARTZLHCE4N HCE4N3      NE  EMERGENCY EXIT  JAMMED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       200                                                            (CAN) DURING THE INITIAL PHASE ONE INSPECTION THE EMERGENCY EXIT COULD NOT BE OPENED FROM THE OUTSIDE AND THE EXIT COULD NOT BE LOCKED FROM THE INSIDE. (TC NR 20071214001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1L72 4T4  T  A24CE   E4EA    5  CP10NE    
20080225001302008022500130GL  2008       2          25         CA071214002      120071214G5751C2WA126A        HINGE BRACKET   DHAV                    DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985*       52008NE                              AILERON         BROKEN          W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA                  SA721                                               (CAN) FAILURE NOTICED DURING WALK AROUND BY MECHANIC. THE SPIGOT (INTEGRAL PART OF THE HINGE BRACKET) HAD FAILED COMPLETELY, JUST BELOW THE UPPER EDGE OF THE BALANCE WEIGHT ARM. JUDGING BY THE SURFACES THE SPIGOT HAD BEEN BROKEN FOR SOME TIME. EXTREMELY DANGEROUS SITUATION. NO LOG BOOKS OR RECORDS AVAILABLE. (TC NR 20071214002)                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3R3  RRCA806    5E1                  
20080131002832008013100283EA  2008       1          31         CA071214003      120071214G2823C2CE523A        CABLE                                   DHAV  DHC2  DHC2MK1     2800102EA  PWA   R985  R985*       52008NE                              FUEL SELECTOR   CORRODED        W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA                                                                      (CAN) FUEL SELECTOR CABLE VERY BADLY CORRODED, CABLE FAILED WHEN REMOVED.  NO LOG BOOKS OR RECORDS AVAILABLE. (TC NR 20071214003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3R3  R  A806    5E1                  
20080131002842008013100284EA  2008       1          31         CA071214004      120071213G2752852D10019       ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              TE FLAPS        UNSERVICEABLE   W      O   OTHER                                                                                           J  WARNING INDICATION                                                            DEDESCENT        1                      CA                                                                      (CAN) FLAP FAIL ON DESCENT, WHEN FLAP SELECTED FROM 0 DEG TO 8 DEG. FLAPLESS LANDING CARRIED OUT WITHOUT FURTHER INCIDENT. TROUBLESHOOTING IN PROGRESS. WILL UPDATE WHEN MORE INFORMATION IS AVAILABLE (TC NR 20071214004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA21EA   E15NE                
20080131002852008013100285GL  2008       1          31         CA071214005      120071004G5344C2FS1253A       HINGE BRACKET                           DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  CARGO DOOR      CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       11888                                                          (CAN) TOP HINGE BRACKET CRACKED ON FWD FACE OF HINGE.  (TC NR 20071214005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3R3  RRCA806    5E1     5  CP206     
20080131002872008013100287    2008       1          31         CA071214006      420071212G61223011847         LINE                                    BEECH 100   100BEECH    1152916CE  PWA   PT6   PT6A28           EA  HARTZLHCD4N3HCD4N3A     GL  ENGINE          CRACKED         W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CLCLIMB          1                      CA                                          PCE51194                    (CAN) AFTER DEPARTURE DURING CLIMB, THE PILOT NOTICED SLIGHT POWER LOSS ON THE LT ENGINE WHICH SLOWLY DECAYED UNTIL TORQUE WAS AT 100LBS AT WHICH TIME THE PROP WAS FEATHERED. THE CREW ELECTED TO LEAVE THE ENGINE RUNNING AS ALL OTHER INDICATIONS WERE GREEN AND THEY WANTED THE GENERATOR RUNNING AS ICING CONDITIONS WERE FORECAST.  UPON INSPECTION BY MAINTENANCE, IT WAS DISCOVERED THE PY LINE FROM THE PROP GOVERNOR TO THE FCU WAS CRACKED. THE LINE WAS REPLACED GROUND RUNS CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20071214006)                                                                                                                                                                              1L72 3T4  T  A14CE   E4EA    5  CSTC      
20080204001252008020400125EU  2008       2          4          CA071214007      120071210G3411257SF2099       PITOT TUBE                              BRAERODH125 HS125700A   4230170EU  GARRTTTFE731TFE7313R1H  29001WP                                              CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6664                                                           (CAN) FOLLOWING A FAILED PITOT STATIC TEST, AN INSPECTION OF THE PITOT STATIC TUBING WAS CARRIED OUT AND MAINT FOUND THAT ONE OF THE TUBES (P/N 25-7SF209-9) HAD A PIN HOLE, WHICH APPEARS TO HAVE BEEN CAUSED BY INTERGRANULAR CORROSION. THE LINE WAS REPAIRED AND THE PITOT STATIC SYSTEM TESTED SERVICEABLE.  REFERENCE:  PARTS CATALOG 34-10-00-22 ITEM 24 (P/N 25-7SF209-9), PIPE ASSY-STATIC 5 FEED, TEE-PIECE TO TEE-PIECE, 3/8 INS O/D, L56, 22 SWG (MOD252870) (TC NR 20071214007)                                                                                                                                                                                                                                                    2L72 4F4  F  A3EU    E6WE                 
             20080520     CE  2008       5          20         CA071214008      120071213G3230CAC99126259     VALVE                                   CESSNA560   560XL       2076702CE  PWC   545   PW545B           NE                              MLG             FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         APAPPROACH       1                      CA       585                                                            (CAN) AT LANDING GEAR SELECTION, THE LANDING GEAR DID NOT COME DOWN AND NONE OF THE FOLLOWING INDICATIONS WERE OBSERVED:  HYD PUMP OPERATION GEAR MOVEMENT / NOISE GEAR DOWN LIGHTS INDICATION ON THE CONTROLLER,  NOTE: ALL OTHER HYD CONSUMERS WERE OPERATIONAL THE GEAR WAS RECYCLED WITH NO SUCCESS. A GO-AROUND WAS INITIATED THEN THE ABNORMAL/EMERGENCY CHECKLIST WAS REVIEWED AND CARRIED OUT, GEAR CAME DOWN AND LOCKED . VALVE REPLACED GEAR SYS, OK (TC NR 20071214008)                                                                                                                                                                                                                                                              2L72 4F4  FRTA22CE   E00059EN             
20080204001242008020400124SW  2008       2          4          CA071214009      120071210G7120205060106001    MOUNT                                   BELL  205   205A1       1181414SW  LYC   T53   T5317A      41549NE                              RT ENGINE       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9047                                                           (CAN) RT ENGINE BIPOD INSPECTED FOR SUSPICIOUS CRACK IN FRONT TUBING DURING 100 HRS INSPECTION. NDT REVEALED CRACK MOUNT AT WELDED JOINT.  NOTE: THIS MOUNT WAS MODIFIED IAW STC SH99-11, DART ADJUSTABLE MOUNT. (TC NR 20071214009)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 4U4  U  H1SW    E17EA                
20080204001232008020400123WP  2008       2          4          CA071214010      120071214G7603A9333           ROD END                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              THROTTLE CONTROLSEPARATED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ENGINE HAD HIGH IDLE, TRYED TO ADJUST AND WAS UNABLE TO BRING IDLE BELOW 64 PERCENT ENG RPM. INSPECTED THROTTLE LINKAGE AND FOUND ROD END BRG OUTER HOUSING SEPARATED FROM STAKED IN SPHERICAL BEARING. POSSIBLE LOST OF ENGINE CONTROL UNDER QUICK POWER CHANGES. REPLACED ROD END AND RECTIFIED DEFECT. (TC NR 20071214010)                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3O3  O  H11NM   1E4                  
20080204001222008020400122CE  2008       2          4          CA071214011      120071214G528016911003421     BOLT            BEECH                   BEECH 76    76          1153005CE  LYC   O360  O360A1G6D        EA  HARTZLHCM2Y HCM2YR      GL  MLG DOOR        MISSING         W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA                                                                      (CAN) PILOT NOTICED ON PRE-FLIGHT, ABNORMAL ANGLE OF GEAR DOOR. IT WAS DISCOVERED THAT THE BOLT SECURING THE DOOR WAS MISSING. THIS STRESSED THE AFT BRACKET TO THE POINT OF CRACKING WHICH ALSO CAUSED THE DOOR TO CRACK ALONG THE BOLT HOLES. (TC NR 20071214011)                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1L72 3O3  O  A29CE   E286    5  CP43GL    
20080204001212008020400121NE  2008       2          4          CA071217001      220071205G7230                FAN BLADE                               CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              RT ENGINE       DAMAGED         W      A   UNSCHED LANDING                                                                                 CE F.O.D.                    VIBRATION/BUFFET                                    CRCRUISE         1                      CA                                          807658                      (CAN) CREW REPORTED N2 VIB ICON (RT ENG) POSTED DURING CRUISE AT FL320. CREW FOLLOWED QRH AND COULD NOT CONTROL VIB IFSD AND DIVERTED.  MAINTENANCE OBSERVED FOD DAMAGE TO FAN BLADES. ENGINE REMOVED AND REPLACED (TC NR 20071217001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
20080204001202008020400120NM  2008       2          4          CA071217003      120071205G2910DSC252B40124    FLEX LINE                               DHAV  DHC8  DHC8202     2809007NM  PWA   120   PW123D      52152NE  HAMSTD14SF  14SF23      NE  HYD SYSTEM      LEAKING         W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  DEDESCENT        1                      CA                                                                      (CAN) TOTAL FAILURE OF NR 2 HYD SYS OCCURRED AFTER GEAR EXTENSION (NORMAL). LOSS OF PRESSURE WITH ASSOCIATED CAUTION LIGHTS QUICKLY FOLLOWED BY TOTAL LOSS OF ALL NR 2 HYD QUANTITY (FLUID). UPGRADED CALL TO PAN WITH REQUEST FOR LOCAL SERVICES ON STANDBY. AFTER ALTERNATE GEAR EXTENSION, THE NR 2 HYD PRESSURE ROSE TO NORMAL AT 3000 PSI. AFTER LANDING WITH NORMAL HYD PRESSURE, AC TAXIED CLEAR OF RUNWAY.   ENGINEERING INVESTIGATION REVEALED A FAILURE OF THE NLG DRAG BRACE ACTUATOR (DOWN) FLEXIBLE HOSE. HOSE REPLACED AND FOLLOWING APPROPRIATE CHECKS IAW THE MM.  THE AIRCRAFT WAS RELEASED BACK TO SERVICE WITHOUT FURTHER INCIDENT.   THIS IS A KNOWN ISSUE PREVIOUS SDR 20031030005. (TC NR 20071217003)                    2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080225001362008022500136EA  2008       2          25         CA071217004      120071212G76003052970         CONTROL CABLE                           DHAV  DHC7  DHC7102     2802708EA  PWA   PT6   PT6A50      52043EA  HAMSTD24PF  24PF305     GL  CONDITION LEVER DISCONNECTED    W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             NRNOT REPORTED   1                      CA                                                                      (CAN) AFTER FLIGHT, THE NR 2 CONDITION LEVER WOULD NOT MOVE TO FEATHER OR CUTOFF, THE ENGINE HAD TO BE SHUTDOWN USING THE T-HANDLE.  FURTHER INVESTIGATION REVEALED THAT THE NR 2 TELEFLEX CABLE HAD BECOME UNSCREWED NEAR THE BEARING.  WE WERE UNAWARE THAT THE CABLE COULD BE UNSCREWED AT THIS LOCATION, WHEN THE CABLE IS ASSEMBLED THERE IS NO VISUAL INDICATION THAT THE CABLE CAN BE DISASSEMBLED. THERE ARE NO PROVISIONS FOR THE CABLE TO BE LOCK WIRED AT THIS LOCATION. TIME SINCE NEW UNKNOWN.  FURTHER INVESTIGATION FOUND ONE OTHER UNSCREWED CABLE ON THE AIRCRAFT. WE WILL BE INSPECTING OUR FLEET TO ASSURE NO OTHER CABLES ARE LOOSE. (TC NR 20071217004)                                                                    2H74 4T4  T  A20EA   E4EA    6  CP1NE     
20080225001372008022500137EA  2008       2          25         CA071217005      120071214G2752852D100         ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              TE FLAPS        FROZEN          W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  DEDESCENT        1                      CA                                                                      (CAN) FLAP FAIL DURING DESCENT. FLAPS WOULD NOT EXTEND WHEN SELECTED, FLAP 0 APPROACH AND LANDING CONDUCTED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.  FAULT CODES SENT TO TECH OPS, AIRCRAFT WILL BE FERRIED WHEN CREW AVAILABLE. FAULT CODES ARE AS FOLLOWS: EVENT 1 FLIGHT LEG 4555  JAM/ LT BPSU/ PDU DIFFERENTIAL/ 5 1B/ 5 2B/ 9 1A/ 9 2A/ 17 1A/ 17 2A/ 25 BC. EVENT 2 FLIGHT LEG 4555 JAM/ ADC SIGNALS/ LH BPSU FAIL/ 5 2B. FAULT INDICATION IS POINTING A FREEZE EVENT. MORE INFORMATION WILL BE ADDED AS SOON AS BECOME AVAILABLE. (TC NR 20071217005)                                                                                                                                                                                2L72 4F4  FRTA21EA   E15NE                
20080225001382008022500138WP  2008       2          25         CA071217006      220071214G7321NAS1351C3LL6    BOLT            WOODWARD                BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33110UG  01514WP  ROTOL R333  R333482F12  GL  FUEL CONTROL    BACKED OUT      W      A   UNSCHED LANDING                                                                                 RF PARTIAL RPM/PWR LOSS      FLT CONT AFFECTED                                   CLCLIMB          1                      CA                  2137501                                             (CAN) ON CLIMB OUT, THE PILOT REPORTS NR 1 ENG RPM DROPPED TO 97 PERCENT AND HE WAS NOT ABLE TO RESTORE THE ENG TO 100 PERCENT RPM.  PROCEEDED TO MAKE AN UNSCHEDULED LANDING AT DEPARTURE AIRFIELD. UPON INVESTIGATION IT WAS FOUND THAT THE BOLT ATTACHING THE SPEED LEVER TELEFLEX CABLE TO SPEED INPUT SHAFT OF THE FCU HAD BACKED OUT COMPLETELY AND THE CABLE HAD SEPARATED FROM THE INPUT ROD. THE BOLT IN QUESTION WAS RE-USED ON AN ENGINE CHANGE THAT TOOK PLACE 33.6 HOURS PRIOR TO THIS EVENT, ON 11/28/2007. AT THAT TIME THE BOLT MET THE RUN-DOWN TORQUE REQUIREMENTS FOR SELF LOCKING HARDWARE IAW MM STANDARD PRACTICES. THE BOLT WAS REPLACED, THE ENGINE RE-RIGGED WITH NO FAULTS FOUND AND THE AC RETURNED TO SERVICE. (TC N2L72 4T4  TRTBA15CAA E4WE    6  CP61GL    
20080225001402008022500140NE  2008       2          25         CA071217007      220071217G7314D7431           PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              AUX FUEL        FAILED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       1564                                                           (CAN) PILOT ATTEMPTED TO START AIRCRAFT, BUT FAILED. FURTHER INVESTIGATION REVEALED THE AUX FUEL PUMP DID NOT SUPPLY FUEL TO START AIRCRAFT.  PUMP WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. (TC NR 20071217007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1G71 3O3  O  H11NM   1E4                  
20080225001412008022500141EA  2008       2          25         CA071217008      120071212G27505275200         DRIVE ASSY                              CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAPS        FAULTY          W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       9151 9145                                                      (CAN) FLAPS FAILED AT 30 DEG WHEN 45 DEG SELECTED.  FLAP ACTUATORS, PDU AND FECU REPLACED TEST FLIGHT CARRIED OUT CHECKED SUSPECT POWER FLAP DRIVE AT FAULT DUE TO HISTORY. (TC NR 20071217008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
20080225001422008022500142EA  2008       2          25         CA071217009      120071214G2752854D10019       ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAP         MALFUNCTIONED   W      L   ABORTED APPROACH                                                                                JF WARNING INDICATION        FLT CONT AFFECTED                                   APAPPROACH       1                      CA       7255                                                           (CAN) ON APPROACH THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER SELECTING THE FLAP LEVER TO 8 DEGREES. THE EICAS FLIGHT CONTROL PAGE WAS SHOWING THE FLAP POSITION AT 2 DEGREES. THE CREW REQUESTED EMERGENCY SERVICES AND LANDED WITHOUT FURTHER INCIDENT.   AC WAS INSPECTED AND FERRIED. ADCF 2007-10 AND SB601R-27-150 WERE COMPLETED. THE LT NR4 AND RT NR3 FLAP ACTUATORS FAILED THE -60 DEGREES CELSIUS TORQUE CHECK AT A VALUE OF 35 AND 30 INCHES/POUND RESPECTIVELY.   LT NR4, P/N 854D100-19, S/N 2312, TSN 7255:58, CSN 5839, TSR 1971:52 RT NR3, P/N 853D100-20, S/N 3377, TSN 8268:20, CSN 6104, TSR 1971:52  BOTH ACTUATORS WERE REPLACED. THE LT NR3, RT NR1 AND NR4 FLAP ACTUATORS WERE FOUND NEAR SERVICE LIMIT AND WERE2L72 4F4  FRTA21EA   E15NE                
20080225001432008022500143EA  2008       2          25         CA071217010      120071213G2750                FCU                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAPS        FAULTED         W      L   ABORTED APPROACH                                                                                F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA                                                                      (CAN) FLAP FAIL ON APPROACH WHEN FLAPS SELECTED TO 20 FROM 8.  SYS RESET AND CHECKED SERVICEABLE, MAINT EMPLOYEE ON SITE GOT FAULT CODES FROM FECU.  SKEW BITE RESET AND FLAP CONTROL AND POWER DRIVE UNIT RESETS CARRIED OUT.  FLAP FAULT CLEARED. FLAPS CYCLED SEVERAL TIMES NO FAULTS NOTED. SYSTEM FUNCTION CHECKED SERVICEABLE FOR FLIGHT. (TC NR 20071217010)                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA21EA   E15NE                
20080225001452008022500145EU  2008       2          25         CA071218001      220071208G7261FC3401B01B01B029HOSE                                    DIAMONDA20  DA20A1      2990000GL  ROTAX 912   ROTAX912    55555EU  HOFMANHOV352HOV352F     NE  ENGINE OIL      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       2000                                                           (CAN) PILOT LANDED NORMALLY AND SHUTDOWN AFTER NOTICING FALLING OIL PRESSURE INDICATION. THIS WAS ON INITIAL TEST FLIGHT OF A NEW ENGINE INSTALLATION, ON INSPECTION THE OIL PRESSURE HOSE FITTING AT THE OIL PUMP WAS FOUND TO BE LEAKING, THIS WAS TIGHTENED AND AN INSPECTOR OF THE ENGINE COMPLETED. A SEPARATE MECHANIC VERIFIED THE OIL LINE FITTING AND FOUND IT TO BE LOOSENED OFF AGAIN. A TWIST IN THE HOSE AND A WEAK THREAD ENGAGEMENT WERE SUSPECTED. A NEW HOSE WAS INSTALLED AND THE ENGINE TEST RUN AND CHECKED WITH NO PROBLEMS NOTED, A TEST FLIGHT WAS COMPLETED AND ANOTHER INSPECTION OF THE ENGINE REVEALED NO PROBLEMS. THE AC WAS RETURNED TO SERVICE. (TC NR 20071218001)                                              1L71 3O3  INTTA4CH   EXPE3I  5  CTP5BO    
20080225001472008022500147CE  2008       2          25         CA071218002      120071214G711010191011947     VANE                                    BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  RT INTAKE DUCT  DEBONDED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       744                                                            (CAN) ON THE RT ENGINE COWLING INTAKE DUCT THERE IS A VANE ASSY TO REDIRECT INTAKE AIRFOW. THE VANE ASSY WAS FOUND TO HAVE DEBONDED ITSELF FROM THE ATTACH BRACKETS. THE VANE WAS ALSO CRACKED COMPLETELY ALONG THE TRAILING EDGE AND A 4 INCH CRACK LOCATED ON THE LT SIDE LEADING EDGE OF THE VANE. IT LOOKS LIKE POOR WELDING AND BONDING WERE THE CAUSE OF FAILURE. (TC NR 20071218002)                                                                                                                                                                                                                                                                                                                                                     2L72 4T4  T  A24CE   E4EA    6  CP56GL    
20080225001492008022500149NE  2008       2          25         CA071218003      220071217G732078639110        HMU                                     DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  ENGINE          UNSERVICEABLE   W      E   ENGINE SHUTDOWN                                                                                 F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA            26832                         120644                      (CAN) NR2 ENGINE EXPERIENCED AN IN FLIGHT SHUTDOWN, SHORT FINAL (500FT AGL) AND WAS IN ECU MODE. CREW DID NOT HAVE THE TIME TO TRY MANUAL MODE. AS THEY WERE FEATHERING THE ENGINE (PROPELLER), THEY NOTICED THE TORQUE INCREASING, AS IT HIT AROUND 90 PERCENT AND THE CREW SHUT THE ENGINE DOWN.  FDR WAS REMOVED AND YYC AVIONICS SHOP HAS BEEN RESERVED TO READ THE FDR.  ANALYSIS OF THE FDR INDICATES THAT THERE IS AN UNCOMMANDED INPUT OF FUEL TO NR2 ENGINE. THERE IS NO INDICATION THAT THE PROPELLER IS OVER TORQUED AND IS THEREFORE SERVICEABLE FOR FURTHER USE. THE FOLLOWING MAINTENANCE ACTIONS WERE CARRIED OUT: NR2 HMU CHANGED. NR2 ENGINE RIGGING CHECK CARRIED OUT FROM THE COCKPIT OUT TO THE ENGINE.  NR 2 SPRING STRUT I2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080225001512008022500151CE  2008       2          25         CA071218004      120071217G3246                WHEEL                                   CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              MLG             DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) ON PILOTS WALK AROUND THEY FOUND METAL AROUND NOSE WHEEL TIRE. AIRCRAFT WAS TOWED INTO A HEATED HANGER AND PILOT PHONED MAINTENANCE . ENGINEER JACKED NOSE WHEEL AND INSPECTED NOSE WHEEL SPIN-UP KIT AND FOUND LT TURBINE AND LT SPIN-UP COVER WERE DAMAGED. REMOVED NOSE WHEEL SPIN-UP KIT AND INSTALLED ANOTHER TIRE/WHEEL ASSY AND RETURNED AIRCRAFT TO SERVICE (TC NR 20071218004)                                                                                                                                                                                                                                                                                                                                                   1L72 4F4  F  A22CE   E1NE                 
20080225001522008022500152NE  2008       2          25         CA071218005      220071216G7261                SEAL                                    AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF5       NE  NR 1 ENGINE     FAILED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                          PCE120670                   (CAN) AFTER DEPARTURE AND ENROUTE TO DESTINATION, THE CREW OBSERVED A LOW OIL PRESSURE WARNING LIGHT AND NOTED FLUCTUATING OIL PRESSURE ON THE NR 1 ENGINE. THE ENGINE WAS SHUTDOWN AND RESTARTED IAW THE OPERATING PROCEDURES MANUAL, THE OIL PRESSURE WAS NOTED TO BE NEAR ZERO. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE DETERMINED THAT THE NR 1 GENERATOR SEAL FAILED RESULTING IN THE LOSS OF OIL FROM THE NR 1 ENGINE. (TC NR 20071218005)                                                                                                                                                                                                                        2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080225001532008022500153SW  2008       2          25         CA071218006      120071214G56102719442004      WINDSHIELD                              SWRNGNSA226 SA226TC     8780404SW  GARRTTTPE331TPE33110UA  01514WP  HARTZLHCE4N HCE4N3      NE  COCKPIT         CRACKED         W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       4884                                                           (CAN) UPON ENGINE START AND TAXI THE F/O HEATED WINDSCREEN CRACKED. THE GLASS CRACKED FROM THE BOTTOM UP. THE CREW TURNED AROUND AND SHUTDOWN. MAINT REMOVED AND REPLACED THE WINDOW. OUR COMPANY CONTINUES TO HAVE PROBLEMS WITH THESE HEATED WINDSHIELDS AND IN SPEAKING WITH OTHER OPERATORS IN THE RECENT PAST THEY HAVE HAD SIMILAR FAILURES OF THESE WINDSHIELDS. MOST OF THE FAILURES ARE IN FLIGHT FAILURES. THE TOTAL TIME ON THE WINDSHIELD WAS DETERMINED TO BE 4884.1 BUT MAY BE SLIGHTLY HIGHER AS THIS WINDSHEILD WAS INSTALLED ON THE AC PRIOR TO PURCHASE. REGARDLESS OF TOTAL TIME THE FAILURE MODE OF THESE WINDOWS IS A SAFFTY CONCERN. (TC NR 20071218006)                                                                  2L72 4T4  TRTA8SW    E4WE    5  CP10NE    
20080225001552008022500155EA  2008       2          25         CA071218007      120071214G5320CA447           SHROUD                                  CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              BS 559          CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       29474                                                          (CAN) DURING HEAVY CHECK INSP, THE FUEL DISTRIBUTION PRESSURE BOX ASSY, P/N 601R62676-5 WAS FOUND CRACKED AND BOTH THE FUEL SHROUD AND FUEL LINES HAVE CHAFFING DAMAGE BEYOND LIMITS. THESE COMPONENTS ARE LOCATED AT FUSELAGE STATION FS559.  PARTS ARE ON ORDER AND DAMAGED FUEL SHROUD AND THE FUEL BOX WILL BE REPLACED BEFORE AIRCRAFT IS RELEASED FROM HEAVY CHECK. NOTE:- PLEASE REFER TO PREVIOUS SDR NR 20071005001 (TC NR20071218007)                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
20080225001562008022500156EU  2008       2          25         CA071218008      120071213G256022719TK060052X  PIN                                     SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              SEAT BELT       LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) DURING THE PROCESS OF AN ICC FOLLOWING HEAVY MAINT, THE ENGINEER NOTICED THAT THE RETAINING PIN P/N 22719TK060052X FOR THE PILOT`S SEAT BELT OB FITTING WAS LOOSE OR ABOUT TO FALL OUT OF THE FLOOR SUPPORT. UPON INVESTIGATION IT WAS FOUND THAT THE RIVET THAT NORMALLY HOLDS THE SEAT BELT PIN IN PLACE HAD BEEN REPLACED, POSSIBLE DURING A VERTICAL REFERRENCE WINDOW INSTALLATION. THE RIVET WAS REPLACED WAS BUCKED TO THE NORMAL SIZE IAW STANDARD PRACTICES AND DID NOT PROTRUDE LONG ENOUGH TO HOLD THE PIN IN PLACE. UPON NOTICING THIS OCCURANCE WE CHECKED (4) OTHER AIRCRAFT ON SITE AND FOUND 2 MORE WITH THE SAME PROBLEM.  IN THE IPC 53.10.20.000 (04-06) PAGE 02.00 FIGURE 1 SHOWS THE PIN AS DRILLED AT THE END MAYBE 1G71 3U3  U  H9EU    E19EU                
20080225001572008022500157NM  2008       2          25         CA071219001      120071216G32346131001001      SELECTOR VALVE                          BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  MLG             FAILED          W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA                                                                      (CAN) AFTER TAKEOFF, LANDING GEAR SELECTOR LEVER SELECTED UP, BOTH LT AND RT MAIN GEAR DOOR CAUTION LIGHTS ILLUMINATED, BOTH MAIN GEARS FAILED TO RETRACT BUT NOSE GEAR HAD RETRACTED.  AC RETURNED TO BASE FOR FURTHER INVESTIGATION. FLIGHT SNAG COULD BE DUPLICATED ON GROUND. DURING TROUBLESHOOTING AND REMOVAL OF THE MLG SELECTOR VALVE, IT WAS NOTICED THAT FILTER HAD SEPARATED IN VALVE CAUSING BLOCKAGE. (TC NR 20071219001)                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080225001592008022500159NE  2008       2          25         CA071219002      220071218G7230BRH20419        BLADE           RROYCE                  BOEING717   717200      1383700NM  RROYCEBR700 BR700715A130     NE                              HP COMPRESSOR   FAILED          W      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          APAPPROACH       1                      CA       1744       M33121                                              (CAN) ENGINE SURGE ON LANDING. ENGINE RETURNED TO SHOP FOR SUSPECTED HPC STG 1 BLADES DAMAGE. DURING ENGINE DISSASEMBLY HPC ROTOR WAS FOUND WITH HEAVY DAMAGE, SUSPECT DAMAGE CAUSED BY A BLADE FAILURE AT PLATFORM. ALL FAILED PARTS WILL BE RETURNED TO THE OEM FOR INVESTIGATION. (TC NR 20071219002)                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FTRA6WE    E00061EN             
20080225001602008022500160NE  2008       2          25         CA071219003      220071219G7250FW35594         TURBINE BLADES                          BOEING717   717200      1383700NM  RROYCEBR700 BR700715A130     NE                              ENGINE          FAILED          W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA       8994                                                           (CAN) ENGINE WILL BE INDUCTED IN JANUARY, 2008 FOR INVESTIGATION FOR HPT STG 1 BLADE FAILURE.  BLADES WERE FITTED NEW AT LAST SHOP VISIT AT 14773 CYCLES. SUSPECT FAILURE SIMILAR TO PREVIOUS SDR SUBMITTED 20070911004, 20071001001. FURTHER DETAILS WILL BE SUBMITTED AT ENGINE DISASSEMBLY. (TC NR 20071219003)                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FTRA6WE    E00061EN             
20080225001612008022500161NE  2008       2          25         CA071219004      220071219G7250FW35544         TURBINE BLADES                          BOEING717   717200      1383700NM  RROYCEBR700 BR700715A130     NE                              ENGINE          FAILED          W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA       7723                                                           (CAN) ENGINE CURRENTLY IN SHOP FOR REPAIR DUE TO HP 1 TURBINE BLADE FAILURE, ENGINE DISASSEMBLY REVEALED FAILURE OF BLADE AT PLATFORM. FAILED PART WILL RETURNED TO THE OEM FOR INVESTIGATION. PREVIOUS SDR RAISED FOR SAME EVENT 2007091104, 20071001001,20071219003. ENGINES SHOP VISITS DOCUMENTATIONS HAS BEEN REQUESTED BY THE OEM FOR ALL SIMILAR EVENT FOR THE INVESTIGATION (TC NR 20071219004)                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FTRA6WE    E00061EN             
20080225001622008022500162NE  2008       2          25         CA071219005      220070905G8530127599          SCREW                                   DHAV  DHC2  DHC2MKI     2801830GL  PWA   R985  R985AN14B   52008NE  HAMSTD2D    2D30        NE  INTAKE ROCKER   SEVERED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA            869                                                       (CAN) DURING AN UNRELATED INSPECTION, THE INTAKE VALVE ROCKER ARM ADJUSTMENT SCREW (127599) WAS FOUND SEVERED INSIDE THE LOCKING JAM NUT.  POSSIBLE METAL FATIGUE.  (TC NR 20071219005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3R3  RRCA806    5E1     5  CP206     
20080225001642008022500164EA  2008       2          25         CA071219006      120071217G5414                SKIN                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              NACELLE         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       29474                                                          (CAN) BOTH THE LT AND RT REPAIR DOUBLERS THAT ARE IDENTIFIED AS ITEM -1 ON THE ATTACHED REO601R-53-61-358, REVISION A, WERE FOUND CRACKED DURING AN INSPECTION OF THE ENGINE SUPPORT BEAMS AT A HEAVY CHECK VISIT.  THIS AC CAME INTO OUR AIRLINE OPERATION AT APPROX 20859 CYCLES. WE ARE UNABLE TO CONFIRM THE EXACT TIME THIS REPAIR WOULD HAVE BEEN INCORPORATED ON THIS AC.  WE HAVE CONTACTED THE MFG TECHNICAL HELP DESK WITH OUR FINDING AND ARE AWAITING FURTHER REPAIR INSTRUCTIONS FROM THEM. (TC NR 20071219006)                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
             20080520     CE  2008       5          20         CA071219008      120071213G2497AAPA4CHAFED     WIRE                                    CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  NR 2 BUS BAR    CHAFED          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) DURING CRUISE FLIGHT ALL (3) BUS, NR 2 CIRCUIT BREAKERS POPPED AND THE STANDBY POWER CIRCUIT BREAKER ON BUS, NR 2 POPPED. THE AC LANDED WITHOUT FURTHER INCIDENT. UPON ARRIVAL MAINT PERSONNEL INSPECTED THE WIRING ON THE DISTRIBUTION PANEL AND FOUND WIRE AAPA4 CHAFED TO THE NR 2 BUS BAR. THE CHAFED WIRE WAS REPAIRED IAW STANDARD PRACTICES AND THE AC WAS GROUND RUN AND CHECKED SERVICEABLE. (TC NR 20071219008)                                                                                                                                                                                                                                                                                                                 1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20080225001672008022500167NM  2008       2          25         CA071219009      120071218G3230535201          SEQUENCE VALVE                          DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  MLG             MALFUNCTIONED   W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA       28240925                                                       (CAN) THE GEAR WAS SELECTED UP, IT RETRACTED NORMALLY. THROUGH 2000 FT THUMPING NOISE IN NOSE WAS HEARD FOLLOWED BY AN AMBER LIGHT IN THE SELECTOR KNOB FLASHING ON.  OCCASIONALLY A RED NOSE GEAR LIGHT CAME ON. MAINT REPLACED NLG DOOR WARN PROX SWITCH AND SWAPPED THE NOSE GEAR SEQ VALVE RELAY WITH THE RT MLG DOOR SEQ VALVE. AFTER FURTHER T/S IT WAS SUSPECTED THAT MLG SELECTOR HANDLE WAS AT FAULT. AT THIS TIME THE MLG SELECTOR HANDLE WAS REPLACED FOR T/S AND WILL UPDATE FURTHER WHEN AVAILABLE. GEAR SWINGS WERE C/O WITH THE NEW SELECTOR HANDLE AND THE A/C WAS CHECKED SERVICEABLE.  (TC NR 20071219009)                                                                                                                    2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080225001692008022500169WP  2008       2          25         CA071219010      220071214G726131081331        TUBE                                    BAG   JETSTMJETSTM3212  1500217EU  GARRTTTPE331TPE33110UG  01514WP  MCAULY4HFR344HFR34C652  NE  ENGINE OIL      CHAFED          W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                          P63333                      (CAN) DURING A SCHEDULED FLIGHT BETWEEN, A WARNING INDICATION OF OIL PRESSURE LOSS ON THE NR 1 ENGINE APPEARED ON THE ANNUNCIATOR PANEL. THE CREW VERIFIED THE WARNING BY OBSERVING THE OIL PRESSURE GAUGE. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. THE CREW LANDED THE AC WITHOUT INCIDENT. UPON INSPECTION IT WAS FOUND THAT THE STEEL TUBE BETWEEN THE PROPELLER GOVERNOR AND A T-FITTING WAS LEAKING FROM THE FLARED END WHERE IT ATTACHED TO THE T-FITTING. THE TUBE WAS REPLACED WITH A NEW ONE AND HIGH POWER GROUND RUNS WERE PERFORMED. NO LEAKS WERE PRESENT. THE OIL WAS CLEANED FROM THE ENGINE COMPARTMENT AND THE AC RETURNED TO BASE. DURING REPLACEMENT OF THE TUBE IT WAS NOTED THAT IT HAD BEEN CHAFFING ON AN 2L72 4T4  TRTBA15CAA E4WE    6  C3PNE     
20080225001702008022500170NM  2008       2          25         CA071220001      120071219G3297                GROUND STUD                             DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE  HAMSTD14SF  14SF*       NE  MLG             LOOSE           W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      CA       3943239432                                                     (CAN) AFTER SELECTING GEAR UP, LT AND RT MAIN GEAR DOOR AMBER WARNING AND NLG RED WARNING. GEAR SELECTED DOWN AND NORMAL EXTENSION, AFTER GEAR DOWN (AMBER) NLG LIGHT REMAINED ILLUMINATED. MAINT INSPECTION/ TROUBLE SHOOTING REPLACED LANDING GEAR SELECTOR VALVE AND NLG DOOR SEQUENCE VALVE, DURING GEAR SWINGS GEAR FAILED TO RETRACT AFTER SECOND CYCLING . FURTHER INVESTIGATION FOUND NLG DOOR SEQUENCE VALVE GROUND STUD (WIRE DIAGRAM 32-30-00 SHEET 4 OF 4 PAGE 1 WIRE IDENTIFIER 93A22N , STUD IDENTIFIER 3251-GS-1) LOOSE. STUD LOCATED ON BULKHEAD FWD OF FWD PRESSURE BULKHEAD. STUD TIGHTENED, GEAR SWINGS COMPLETED SUCCESSFULLY. AC RETURNED TO SERVICE. (TC NR 20071220001)                                                  2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080319001702008031900170EU  2008       3          19         CA071220002      220071108G7320057610E000201   ECU             THIELT                  DIAMONDA42  DA42        2990004EU  THIELTTAE125TAE12502114      EU                              FADEC           MALFUNCTIONED   W      O   OTHER                                                                                           XJ ENGINE FLAMEOUT           WARNING INDICATION                                  CRCRUISE         1                      CA       608        3544                                                (CAN) DURING FLIGHT TRAINING MANEUVERS, SIMULATED SINGLE ENG OPS AT 5000 FT ASL, THE LT ENGINE WAS THROTTLED BACK TO FLIGHT IDLE (5 PERCENT PWR, THROTTLE RETARDED).  UPON RETURN TO NORMAL PWR OPS THE LT ENG BEGAN TO SURGE FROM 20-100 PERCENT PWR, REGARDLESS OF THROTTLE POSITION, ENG WAS UNCONTROLLABLE.  THE LT ENGINE FADEC WAS SELECTED FROM ECU A TO ECU B AND CONTROL OF LT ENGINE WAS REGAINED. THE AC RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT.  MAINT ACTIONS:  DISCREPANCY COULD NOT BE DUPLICATED DURING GROUND TESTS. LT ENGINE OPERATED NORMALLY ON BOTH ECU A AND ECU B OF THE LT FADEC.  LT HAD FADEC REPLACED AND AC RELEASED FOR TEST FLIGHT. NO FURTHER ENG SURGING NOTED. (TC NR 20071220002)         1L72 3I3  BRTA57CE   E00069EN             
             20080520     CE  2008       5          20         CA071220004      120071215G2910AE2463531G0460  HOSE                                    CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              HYDRAULIC PUMP  CRACKED         W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) ALL GEARS DOWN AND LOCK WITH (3) GREEN LIGHTS.  WHEN PILOT SELECTED FLAPS DOWN, LT HYD FLOW LIGHT COMES ON AND FOLLOW THE RT SIDE. FINALLY, HYD FLUID LEVEL LIGHT COMES ON.  AC LANDED SAFELY WITH NO HYD SYS AVAILABLE. FOUND LT ENG HYD PRESSURE HOSE CRACKED. BOTH HYD PRESSURE HOSE REPLACED WITH AE2463531G0460 ON LT SIDE AND AE2463531G0226 ON RT AND BOTH ENG DRIVEN HYD PUMP REPLACED WITH 9912062-4. HYD FILTER INSPECTED AND REPLACED WITH NEW FILTER KIT CPDPHF-1. FUNCTIONAL CHECK C/O AND AC RETURN TO SERVICE. (TC NR 20071220004)                                                                                                                                                                                         2L72 4F4  FRTA22CE   E25EA                
20080225001722008022500172EU  2008       2          25         CA071221001      120071219G2997                WIRE                                    SNIAS 350   AS350BA     8680817EU  TMECA ARRIELARRIEL1     60030NE                              HYD CONTROL     INCORRECT       W      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      CA                              2076                                    (CAN) DURING AN AC CONVERSION IAW SB 01.00.50 THE HYD CONTROL WIRE WAS FOUND NOT CRIMPED PROPERLY IN SPLICE CONNECTOR.  WIRE DH5E PULLED OUT OF SPLICE DURING HANDLING.  WIRE CONNECTOR SHOW NO SIGN OF PROPER CRIMP.  THE INSTALLATION OF THIS SPLICE IS MANDATED BY EASA AD F-2004-089 (ASB 29.00.07).  WIRE CONNECTION FAILURE RENDERS THE PILOT UNABLE TO PERFORM EMERGENCY PROCEDURES LISTED IN THE FLIGHT MANUAL SECTION 3.3  (HYD FAILURE) AND SECTION 3.1 PARA 5 (TAIL ROTOR CONTROL FAILURE) THE LACK OF PROPER CRIMPING WAS ALSO FOUND ON AC.  (TC NR 20071221001)                                                                                                                                                                    1G71 3U3  UNCH9EU    E19EU                
20080225001742008022500174NE  2008       2          25         CA071221002      220071209G7200                ENGINE                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              SEIZED          W      A   UNSCHED LANDING                                                                                 EJ VIBRATION/BUFFET          WARNING INDICATION                                  CLCLIMB          1                      CA                                          17384                       (CAN) SHORTLY AFTER TAKEOFF, CREW FELT VIBRATION FOLLOWED BY AN INDICATION OF LOW OIL PRESSURE.  AC LANDED IN A FIELD AWAY FROM THE DEPARTURE POINT AND CREW SHUTDOWN ENGINE.  POST FLIGHT INSP REVEALED THAT NEITHER ENGINE ROTOR COULD BE TURNED AND THE OIL FILTER AND CHIP DETECTORS WERE CONTAMINATED BY DEBRIS.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071221002)                                                                                                                                                                                                                                                                                                                 1H71 3T3  T  A37CE   E4EA                 
20080225001752008022500175NE  2008       2          25         CA071221003      220071212G753231J285704       MOTOR                                   CESSNA560   560XL       2076702CE  PWC   545   PW545B           NE                              BLEED VALVE     DEFECTIVE       W      E   ENGINE SHUTDOWN                                                                                 EFJVIBRATION/BUFFET          FLT CONT AFFECTED         WARNING INDICATION        DEDESCENT        1                      CA                                          DD0323                      (CAN) VIBRATION, (RUMBLE) AND EEC REVERSION WAS EXPERIENCED DURING DESCENT. THE CREW ELECTED TO PERFORM AN INFLIGHT SHUTDOWN OF THE ENGINE AND CONTINUE TO DESTINATION. TROUBLESHOOTING REVEALED A DEFECTIVE BLEED VALVE TORQUE MOTOR CAUSING THE COMPRESSOR SURGES/STALLS. THE UNIT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC 20071221003)                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA22CE   E00059EN             
20080225001762008022500176EU  2008       2          25         CA071221004      120071212G7930                OIL SYSTEM                              AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              ENGINE          LOW PRESSURE    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          127176                      (CAN) DURING CRUISE, THE CREW OBSERVED FLUCTUATIONS IN THE OIL PRESSURE, FOLLOWED BY A DROP TO ZERO. THE ENGINE WAS SHUTDOWN ACCORDINGLY.  TROUBLESHOOTING IS ONGOING, MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071221004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2H72 4T4  TRT        E20NE                
20080225001772008022500177NE  2008       2          25         CA071221005      220071214G7200                ENGINE                                  BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                                              MAKING METAL    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      CA                                          1140211142                  (CAN) DURING FINAL APPROACH, THE LOW OIL PRESSURE WARNING ACTIVATED. THE CREW SHUTDOWN THE ENGINE. POST FLIGHT INVESTIGATION REVEALED THAT THE ENGINE ROTORS WERE DIFFICULT TO TURN AND THAT METAL SHAVINGS WERE DEPOSITED ON THE OIL FILTER. THE ENGINE IS BEING SENT FOR INVESTIGATION.  MFG  WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071221005)                                                                                                                                                                                                                                                                                                                                             2L72 4T4  TRTA24CE   E26NE                
20080225001812008022500181NE  2008       2          25         CA071221006      220071217G7200                ENGINE                                  DHAV  DHC8  DHC8301     1386003NM  PWA   PW120 PW123            NE                                              SEIZED          W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                          123019                      (CAN) OPERATOR REPORTED THAT THERE WAS AN INFLIGHT SHUTDOWN OF THE ENGINE AND THAT POST FLIGHT INSPECTION REVEALED THAT THE POWER TURBINE ASSY COULD NOT BE ROTATED. NO OTHER DETAILS PROVIDED AT THIS TIME.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071221006)                                                                                                                                                                                                                                                                                                                                                                                                                           2H72 4T4  TRTA13NM   E20NE                
20080225001822008022500182NE  2008       2          25         CA071221007      220071202G7250                TURBINE BLADES                          CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                              ENGINE          DISTRESSED      W      A   UNSCHED LANDING                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                          PC503                       (CAN) OPERATOR REPORTED (TECHNICAL PROBLEMS) WHICH RESULTED IN A FORCED LANDING ON A PUBLIC MOTORWAY. INITIAL INVESTIGATION REVEALED COMPRESSOR TURBINE BLADE DISTRESS. THE ENGINE IN BEING RETURNED TO MFG FOR INVESTIGATION. UPDATES WILL BE PROVIDED WHEN AVAILABLE. (TC NR 20071221007)                                                                                                                                                                                                                                                                                                                                                                                                                                                     1H71 3T3  T  A37CE   E4EA                 
20080225001832008022500183NE  2008       2          25         CA071221008      220071216G7261                ENGINE                                  AEROSPATR42 ATR42320    8680930EU  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF5       NE                  LEAKING         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA                                          120670                      (CAN) DURING CLIMB, THE OIL PRESSURE STARTED TO FLUCTUATE AND THE LOW OIL PRESSURE WARNING WAS ACTIVATED. THE CREW SHUT THE ENGINE DOWN AND RETURNED TO THE POINT OF ORIGIN. 5 MIN PRIOR TO LANDING, THE ENGINE WAS RE-STARTED AND ALL PARAMETERS WERE NORMAL EXCEPT THAT THERE WAS NO OIL PRESSURE INDICATION AND THE LOW OIL PRESSURE WARNING.  THEY KEPT THE ENGINE RUNNING TILL LANDING. POST FLIGHT INSP REVEALED THAT THE OIL TANK WAS EMPTY AND A SIGNIFICANT OIL LEAK WAS OBSERVED AT THE STARTER GENERATOR PAD.   THE ENGINE WILL BE REMOVED AND SENT FOR REPAIRS.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071221008)                                                            2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080225001842008022500184EA  2008       2          25         CA071221009      220071129G7261                FITTING                                 DHAV  DHC8  DHC8*              NM  PWC   150   PW150A           EA  ROTOL R408  CR4086123F17EU  ENGINE OIL      LOOSE           W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA                                          FA0302                      (CAN) DURING CRUISE, THE OIL PRESSURE WAS OBSERVED TO DECREASE AND AND A WARNING SOUNDED. THE ENGINE WAS SHUTDOWN AND THE AC RETURNED TO BASE. INITIAL INVESTIGATION REVEALED AN AIRFRAME SUPPLIED OIL COOLER HOSE FITTING HAD PULLED FREE OF THE ENGINE AND CAUSED A MASSIVE LEAKAGE. THE ENGINE HAS BEEN REMOVED AND WILL BE SENT FOR INVESTIGATION.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20071221009)                                                                                                                                                                                                                                                                                 2H72 4T4  TRTA13NM   E00062EN6  CP17BO    
20080225001852008022500185NE  2008       2          25         CA071221010      220071129G7250                TURBINE BLADES                          BEECH 99    C99         1154006CE  PWA   PT6   PT6A36      52043NE                              ENGINE          DAMAGED         W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                          38152                       (CAN) DURING CRUISE A LOUD BANG WAS HEARD AND ENGINE OPERATION CEASED WITHOUT CREW INVOLVEMENT.  POST FLIGHT INPECTION DISPLAYED COMPRESSOR AND POWER TURBINE BLADE DAMAGE. THE COMPRESSOR ROTOR IS SEIZED THE ENGINE WILL BE REMOVED AND FORWARDED TO MFG FOR INVESTIGATION. UPDATES WILL BE PROVIDED WHEN AVAILABLE. (TC NR 20071221010)                                                                                                                                                                                                                                                                                                                                                                                                      1L72 3T4  T  A14CE   E4EA                 
20080225001862008022500186NM  2008       2          25         CA071221011      120071215G7712                SIGNAL COND UNIT                        DHAV  DHC8  DHC8*              NM  PWA   120   PW123D      52152NE                              ENGINE TORQUE   MALFUNCTIONED   W      C   ABORTED TAKEOFF                                                                                 J  WARNING INDICATION                                                            TOTAKEOFF        1                      CA                                          AG0044                      (CAN) TAKEOFF WAS ABORTED DUE TO NOISES SIMILAR TO ENGINE SURGE OR PROPELLER MALFUNCTION. INSPECTION REVEALED THAT THE ENGINE HAD REACHED 136 PERCENT TORQUE FOR A PERIOD LESS THAN 20 SECONDS. THE PROPELLER, TORQUE PROBE AND TORQUE SIGNAL CONDITIONER WERE REPLACED. ROOT CAUSE HAS NOT BEEN ESTABLISHED. UPDATES WILL BE PROVIDED WHEN AVAILABLE. (TC NR 20071221011)                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRTA13NM   E20NE                
20080225001872008022500187NE  2008       2          25         CA071221012      220070820G7250                TURBINE BLADES                                                             PWA   PW120 PW127            NE                              ENGINE          CLOGGED         W      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  NRNOT REPORTED   1                      CA                                                                      (CAN) THIS SDR IS BEING RAISED TO ADVISE OF A QUALITY ESCAPE REPORTED. DUE TO THE USE IMPROPER MATERIALS AND PROCEDURES, THE COOLING PASSAGES OF SOME HP TURBINE BLADES WERE INADVERTANTLY BLOCKED BY BLASTING MEDIA DURING THE CLEANING PROCESS AT SHOP VISIT. THESE BLADES WERE THEN INSTALLED ON A NR OF ENGINES AND RELEASED TO THE FIELD FOR SERVICE.  THERE HAVE BEEN (2) CASES OF THESE BLADES SUBSEQUENTLY FRACTURING IN SERVICE DUE TO OVERHEATING, ENGINES AV0063 AND 120308.   HAVE ACKNOWLEGED THE QUALITY ESCAPE AND TAKING REMEDIAL ACTION TO ADDRESS OTHER AFFECTED ENGINES.  WILL BE ADVISED OF FURTHER OCCURANCES IN THE FIELD. (TC NR 20071221012)                                                                                   4  T          E20NE                
20080225001882008022500188NM  2008       2          25         CA071222001      120071222G5315146A75032       FLOORBEAM                               BOEING737   737790      13844CNNM                                                               BS 767          CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT CARGO PIT FLOOR SUPPORT RAIL AT BS 767+5 RBL 3 FOUND CORRODED DURING CPCP INSPECTION. LEVEL 2 CORROSION. REPAIRED IAW CUSTOMER E.A. (TC NR 20071222001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F    RTA16WE                        
20080225001892008022500189NM  2008       2          25         CA071222002      120071222G5315146A75031       FLOORBEAM                               BOEING737   737790      13844CNNM                                                               BS767           CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT CARGO PIT FLOOR SUPPORT RAIL AT BS 767+14, LBL 3 FOUND CORRODED DURING CPCP INSPECTION. LEVEL 2 CORROSION. REPAIRED IAW CUSTOMER EA. (TC NR 20071222002)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F    RTA16WE                        
20080225001902008022500190NM  2008       2          25         CA071222003      120071222G5320146A75035       FLOOR SUPPORT                           BOEING737   737790      13844CNNM                                                               BS767           CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT CARGO PIT FLOOR SUPPORT RAIL AT BS 767+5, LBL8 FOUND CORRODED DURING CPCP INSPECTION. LEVEL 2 CORROSION. REPAIRED IAW CUSTOMER EA. (TC NR 20071222003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RTA16WE                        
20080225001912008022500191NM  2008       2          25         CA071222004      120071222G5315141A550519      FLOORBEAM                               BOEING737   737790      13844CNNM                                                               BS 344          CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) PASSENGER CABIN FLOORBEAM AT BS 344, RBL4 TO LBL56 FOUND CORRODED DURING CPCP INSPECTION. LEVEL 2 CORROSION. REPAIRED IAW CUSTOMER EA. (TC NR 20071222004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RTA16WE                        
20080225001932008022500193NM  2008       2          25         CA071222005      120071222G5315147A55048       FLOORBEAM                               BOEING737   737790      13844CNNM                                                               BS 947          CORRODED        W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) AFT CABIN FLOORBEAM AT BS 947, LBL53 FOUND CORRODED DURING CPCP INSPECTION. LEVEL 2 CORROSION FOUND. REPAIRED IAW CUSTOMER EA. (TC NR 20071222005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F    RTA16WE                        
20080225001942008022500194WP  2008       2          25         CA071224001      120071223G2897WIRE1544        WIRE HARNESS                            ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              AUX FUEL PUMP   CHAFED          W      K   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      CA                                                                      (CAN) AC HAD AN INTERMITTENT PROBLEM WITH ITS FUEL PUMP WARNING LIGHT. INTERMITTENTLY THE AUX FUEL PUMP WARNING LIGHT WOULD FLICKER ON AND OFF AT APPROX. 60 PERCENT BRIGHTNESS DURING A LONG FLIGHT. AN ENGINEER CHANGED THE AUX FUEL PUMP AND THE FUEL PRESSURE SWITCH. THE PROBLEM DID NOT REOCCUR DURING TESTING. HOWEVER, THE AC WAS BROUGHT BACK TO BASE TO ENSURE THERE WAS NO OTHER PROBLEM. UPON FURTHER INSPECTION, FOUND ONE OF THE WIRES FOR THE FUEL PUMP WAS CHAFING ON A VENT TUBE NEAR THE FIREWALL. REPLACED A SECTION OF WIRE AND COVERED IT IN SPIRAL WRAP, TO PREVENT CHAFING IN THE FUTURE. (TC NR 20071224001)                                                                                                            1G71 3O3  O  H11NM   1E4                  
20080225001952008022500195EU  2008       2          25         CA071224002      120071213G2710                AILERON                                 BRAERODH125 HS125700A   4230170EU  GARRTTTFE731TFE7313R1H  29001WP                                              ICED            W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      CA       9523                                                           (CAN) PILOTS REPORTED ON APPROACH INTO AIRPORT, COULD NOT GET ANY ROLL ON AC CONTROLS. IT APPEARED THAT AILERONS WERE FROZEN. SHORTLY BEFORE TOUCHDOWN THEY WERE ABLE TO GAIN CONTROL OF THE AILERON MOVEMENT. THE AC LANDED WITHOUT INCIDENT. MAINT WAS CALLED AND ON INSPECTION OF THE AC FOUND ICE BUILD UP ON LT AND RT AILERON HORNS, LT AND RT WINGS AND WING TIPS. SOME AREAS OF THE LEADING EDGE HAD SOME ICE BUILD UP. CHECKED AC CONTROLS AND VERIFIED CORRECT MOVEMENT. AILERON CONTROLS OPERATED WITHOUT ANY BINDING. CONTACTED MFG AND REPORTED INCIDENT. FURTHER TROUBLESHOOTING WILL BE CARRIED OUT ON THE AC AILERONS TO AS CERTAIN THE CAUSE OF THE AILERON FREEZING UP. (TC NR 20071224002)                                  2L72 4F4  F  A3EU    E6WE                 
20080225002252008022500225NE  2008       2          25         CA071224003      220071220G7314D74311          PUMP                                    ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              AUX             FAILED          W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       828                                                            (CAN) WHILE ATTEMPTING TO START THE AIRCRAFT, THE AUX FUEL PUMP FAILED TO RUN. FURTHER INVESTIGATION REVEALED THE PUMP AND AUX FUEL PUMP PRESSURE SWITCH (P/N B426-6) HAD FAILED. PUMP AND SWITCH WERE REPLACED AND NO FURTHER DEFECTS WERE NOTED. (TC NR 20071224003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1G71 3O3  O  H11NM   1E4                  
20080225002262008022500226NM  2008       2          25         CA071224004      120071219G7920305726501       ADAPTER                                 BOMBDRDHC8  DHC8400            NM  PWC   150   PW150A           EA                              LP COMPRESSOR   LOOSE           W      E   ENGINE SHUTDOWN                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CLCLIMB          1                      CA       2628                                                           (CAN) WHILE INVESTIGATING AN OIL LEAK, DISCOVERED THAT WHEN REMOVING THE OIL COOLER LINE FROM THE LP COMPRESSOR CASE, AFTER CUTTING THE LOCKWIRE FROM 1 OF THE 3 BOLTS, THE REMAINING 2 BOLTS CAME OUT WITH THE LOCKWIRE STILL ATTACHED. BOLTS SECURE THE OIL COOLER LINE AND ADAPTOR OIL TUBE TO THE LP COMPRESSOR. (TC NR 20071224004)                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E00062EN             
20080225002272008022500227EA  2008       2          25         CA071226001      120071222G3020300013000003    ANTI-ICE VALVE                          CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              LT NACELLE      UNSERVICEABLE   W      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA       7709 7709                                                      (CAN) WHILE ENROUTE, AC DEVELOPED A COWL ANTI ICE SNAG. THE AC RETURNED TO FOR REPAIRS. MAINTENANCE FOUND THE COWL ANTI ICE VALVE TO BE AT FAULT ONCE REPLACED OPERATIONAL CHECKS WERE C/O SERVICEABLE. A/C WAS RETURNED TO SERVICE.  (TC NR 20071226001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA21EA   E15NE                
20080225002282008022500228EA  2008       2          25         CA071227001      120071224G2752854D1001921     ACTUATOR                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAPS        UNSERVICEABLE   W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AFTER LANDING, CREW WERE UNABLE TO RETRACT FLAPS, STUCK AT 41 DEGREES. FLT CANCELLED AS A RESULT. EXPECT TO FERRY AC. CODES RETRIEVED: 1)FECU/BPSU 2)ETHER BPSU 3)WIRING,  AC RETRIEVED CODES, FORWARDED TO TECH. CARRIED OUT ACTION PLAN 168 AND ALL WIRING RANG OUT OK. FLAPS WERE CYCLED 5 TIMES IN HANGAR WITH NO FAULTS NOTED.  PERFORMED A LOW TEMP TORQUE CHECK OF THE ACTUATORS AND REPORT FAILED UNITS. TAIL 168 FLAP ACTUATOR FREEZE TORQUE CHECK COMPLETED AND RESULTS AS FOLLOWS: LT IB FLAP, IB ACT FAILED, C NR 5275305  LT IB FLAP, OB ACT PASSED  LT OB FLAP, IB ACT FAILED, C NR 5275306 LT OB FLAP, OB ACT FAILED, C NR 5275308  RT IB FLAP, IB ACT PASSED RT IB FLAP, OB ACT FAILED, C NR 5275305 RT OB FLAP, IB ACT FA2L72 4F4  FRTA21EA   E15NE                
20080225002292008022500229NE  2008       2          25         CA071227002      220071223G7230355924400       SENSING ELEMENT                         CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              14TH STAGE DUCT CHAFED          W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA                                                                      (CAN) RT 14TH STAGE DUCT MESSAGE DURING CLIMBOUT. FLIGHT RETURNED TO AIRFIELD.  MAINTENANCE INSPECTION DISCOVERED 14TH STAGE COWL DUCT INSULATION BROKEN AND CHAFING ON SENSING LOOP. BOTH SENSING LOOP AND DUCT WERE REPLACED AND ENGINE RUNS WERE C/O AND THE AC WAS CHECKED SERVICEABLE.  (TC NR 20071227002)                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
             20080520     CE  2008       5          20         CA071227003      120071015G3220NAS464P5A42     BOLT                                    CESSNA210   2105        2073404CE  CONT  O470  IO470S      17026SO  MCAULYD3A36 D3A36C410   GL  NLG DRAG STRUT  BROKEN          W      D   RETURN TO BLOCK                                                                                 O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       8203                                                           (CAN) WHILE TAXING ON BUSH STRIP, NOSE GEAR AFT DRAG STRUT BOLT BROKE AND WORKED OUT CAUSING NOSE GEAR TO FOLD FWD. (TC NR 20071227003)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  O  3A21    3E1     5  CP47GL    
             20080520     CE  2008       5          20         CA071227004      120070909G531212128582        BULKHEAD                                CESSNA206   TU206A      2073318CE  CONT  O520  TSIO520C    17040SO  HARTZLHCC3Y PHCC3YF1    GL  FUSELAGE        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5803                                                           (CAN) CRACK IN REAR BULKHEAD PIN DURING MANDATORY NDT INSPECTION OF THE ARGA. (TC NR 20071227004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  O  A4CE    E8CE    5  CP25EA    
20080225002302008022500230EA  2008       2          25         CA071227006      120071213G2421M2750010SP3U00  WIRE HARNESS                            CNDAIRCL600 CL600*      1900302EA  GE    CF34  CF348E5A1   30062NE                              RAT             CHAFED          W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       15541                                                          (CAN) DURING INCORPORATION OF SB601-0591 (SPECIAL CHECK/MODIFICATION  AIR-DRIVEN GENERATOR SYS REPLACEMENT OF CHAFING ADG POWER FEED WIRE) FOUND THE WIRING CHAFED BARE AND CLAMPS BURNED AFT OF THE FWD PRESSURE BULKHEAD AT THE FIRST STANDOFF AFT OF THE FEED THROUGH AT APPROX  FS 210. WIRES HAVE BEEN REPLACED IAW SB601-0591 INSTRUCTIONS. (TC NR 20071227006)                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA21EA   E00063EN             
20080225002322008022500232GL  2008       2          25         CA071227007      220071218G72616793065         CAP             ALLSN       23035102    HUGHES369   369D        4470706WP  ALLSN 250C  250C20B     03013GL                              OIL PUMP        CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                  SER26317                                            (CAN) DURING ROUTINE INSPECTION AND FILTER CHANGE, A CRACK AROUND THE EAR OF THE CAP WAS NOTED. THE STUD WAS ALSO STRIPPED. MFG COVERED THIS TOPIC IN THEIR CSL-1251. TORQUEING IS THE POSSIBLE CAUSE FOR THIS DEFECT, THE LETTER RECOMMENDS 30-40 LBS-IN. IT IS IMPORTANT TO FOLLOW MFG PROCEDURES IN ASSEMBLY AND REPAIR. (TC NR  20071227007)                                                                                                                                                                                                                                                                                                                                                                                                1G71 3U3  U  H3WE    E4CE                 
20080225002332008022500233EA  2008       2          25         CA071227008      120071220G3260895304          PSEU                                    CNDAIRCL600 CL600*      1900302EA  GE    CF34  CF348C5     30050NE                              MLG             FAILED          W      A   UNSCHED LANDING                                                                                 N  FALSE WARNING                                                                 CLCLIMB          1                      CA       2275                                                           (CAN) A/C EXPERIENCED A PROX SYS FAULT DURING CLIMB OUT MESSAGE BECAME INTERMITTENT AFTER 8-10 MINUTES. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINT REPLACED THE PSEU AND CHECKED THE SYS THROUGH THE MFG SERVICEABLE. GEAR SWINGS C/O, NFF. A/C RETURNED TO SERVICE. (TC NR 20071227008)                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E00063EN             
20080225002352008022500235EU  2008       2          25         CA071228001      120071224G76037898435010      ECU                                     AEROSPATR42 ATR42300    8680920EU  PWA   120   PW120            NE  HAMSTD14SF  14SF5       NE  POWER LEVER     FAILED          W      D   RETURN TO BLOCK                                                                                 J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                                                      (CAN) POWER LEVER SPLIT AT HIGH POWER SETTINGS. FAULT ISOLATED TO FAULTY LT ENGINE ECU. ECU REPLACED. TESTED SERVICEABLE. (TC NR 20071228001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2H72 4T4  TRTA53EU   E20NE   6  CP7NE     
20080225002372008022500237EA  2008       2          25         CA071228002      120071227G2421720845E         IDG                                     CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              NR 2            DAMAGED         W      O   OTHER                                                                                           HJ ELECT. POWER LOSS-50 PC   WARNING INDICATION                                  NRNOT REPORTED   1                      CA       3922 3922  4258                                                (CAN) AT ALTITUDE CREW RECEIVED AN IDG CAUTION MESSAGE. THE NR 2 IDG WAS DEFERRED UNTIL MAINT COULD BE ACCOMPLISHED. AC WAS BROUGHT TO THE HANGER TO HAVE REPAIRS C/O, REMOVAL OF THE IDG REVEALED THAT THE INTERNAL SHAFT OF THE IDG PUNCHED THROUGH THE OUTER CASING AND METAL SHAVINGS COLLECTED AT BOTTOM OF IDG/AGB MATING FLANGE PLUGGING DRAIN HOLE. ALL METAL DEBRIS WAS CLEANED FROM THE FLANGE AND DRAIN AND NEW CARBON SEAL AND IDG INSTALLED AND CHECKED SERVICEABLE. (TC NR 20071228002)                                                                                                                                                                                                                                           2L72 4F4  FRTA21EA   E15NE                
20080225002382008022500238    2008       2          25         CA071228003      420071227G83003008779         COLLAR                                  DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  ACCESSORY G/B   DISLODGED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                          PCE40510                    (CAN) DURING AN ENGINE NR 2 SCHEDULE OIL CHANGE WHILE REMOVING OIL AT THE ACCESSORY GB DRAIN PLUG PORT HOLE, A METALLIC COLLAR HALF (P/N 3008779) FELL OUT. SUSPECTED THAT THIS COLLAR HALF HAD FALLEN OFF THE SCAVENGE OIL PUMP DRIVESHAFT.  ENGINE REMOVED FROM AIRCRAFT AND SENT TO MFG FOR INVESTIGATION. (TC NR 20071228003)                                                                                                                                                                                                                                                                                                                                                                                                               1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
20080225002392008022500239EA  2008       2          25         CA071231001      120071228G2750855D10011       BPSU                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              TE FLAPS        UNSERVICEABLE   W      O   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  APAPPROACH       1                      CA                                                                      (CAN) FLAP FAIL ON APPROACH. FLAP ZERO APPROACH AND LANDING CARRIED OUT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. RT FLAP BRAKE SENSOR UNIT, SKEW DETECTION UNIT AND RT OB FLEX DRIVE SHAFT REPLACED. FLAP SYS FUNCTION CHECKED SERVICEABLE. (TC NR 20071231001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA21EA   E15NE                
20080225002402008022500240SO  2008       2          25         CA071231002      120071228G33972067081         CONNECTOR                               PIPER PA31  PA31350     7103110SO  LYC   O540  TIO540J2BD  41532EA                              CONTROL PANEL   BURNED          W      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      CA                                                                      (CAN) STROBE CB POPPED AND WILL NOT RESET. FAULT T/S TO DAMAGED WIRE IN RT WING. WIRE (L161FF) REPLACED IAW AC43-13-1B AND SECURED. WIRES FOR AILERON TRIM, STALL WARNING, POSITION LIGHTS AND FUEL QUANTITY SENDERS DISTURBED. ALL CONNECTIONS OF THESE SYSTEMS WERE RETERMINATED AND OPERATION CHECKED OK. DURING T/S CONNECTOR E312(TAXI AND LANDING LIGHTS) IN THE OVERHEAD PANEL WAS NOTED DAMAGE. (SEVERAL BURNED PINS) INSULATION TEST OF THE SYS CARRIED OUT AND ADDITIONAL DAMAGE FOUND AT CONNECTOR E302. BOTH CONNECTORS REPLACED AS REQUIRED. TAXI AND LANDING LIGHT LINES MEGGERED OUT WITH NO FURTHER FAULTS INDICATED. SYSTEM OPN TESTED SERVICEABLE. (TC NR 20071231002)                                                        1L72 3O3  O  A20SO   E14EA                
20080225002532008022500253NM  2008       2          25         CA080102004      120071227G3310                LAMP                                    DHAV  DHC8  DHC8102     2809003NM  PWA   120   PW120A           NE  HAMSTD14SF  14SF7       NE  COCKPIT LIGHTS  BURNED          W      K   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      CA                                                                      (CAN) SIDEWALL LAMP HOLDER AT SEAT AREA 3DF FOUND BURNED WHILE TROUBLESHOOTING SAME POSITION. DEFECT FOUND DURING LAND SERVICE CHECK. LAMP HOLDER/BALLAST ASSY REPLACED. (TC NR 20080102004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
20080225002542008022500254CE  2008       2          25         CA080102005      120071231G542010191001641     COVER                                   BEECH 200   B200        1152922CE  PWA   PT6   PT642A           NE  HARTZLHCD4N3HCD4N3A     GL  NACELLE         CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) FOUND EXHAUST SOOT IN COWLS. CLOSER INSPECTION FOUND THE BUTTERFIELD STC COVER PLATE LEAKING AND THE HEATED INLET CRACKED IN MULTIPLE LOCATIONS ON BOTH COWLS. (TC NR 20080102005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 4T4  T  A24CE   E4EA    5  CSTC      
20080225002572008022500257EA  2008       2          25         CA080102007      120071230G2150                A/C PACK                                CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              RIGHT           SMOKE           W      A   UNSCHED LANDING                                                                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CLCLIMB          1                      CA                                                                      (CAN) (AC RETURNED TO THE FIELD DUE TO SMOKE TOILET WARNING. THERE WAS A HAZE IN THE CABIN. THEY DECLARED AN EMERGENCY)  FOUND THAT THE RT PACK WAS SMOKING UP THE CABIN.  DEFERRED THE RT PACK.  ADDITIONAL INFORMATION REQUESTED TO THE FSR, AC STILL UNDER MMEL (TC NR 20080102007)                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA21EA   E15NE                
             20080522     SW  2008       5          22         CA080102008      120071227G26123219027001      MODULE          FRCHLD      2782797001  FRCHLDSA227 SA227DC     3377521SW  GARRTTTPE331TPE33112UHR      WP  MCAULY4HFR344HFR34C652  NE  FIRE EXTINGUISH DAMAGED         W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         N  FALSE WARNING                                                                 CLCLIMB          1                      CA       5472                                                           (CAN) DURING CLIMB-OUT THE PILOTS NOTICED THE ENGINE FIRE DETECTION INDICATION LIGHT CAME ON. THE ENGINE WAS SHUTDOWN AND THE ENGINE FIRE EXTINGUISHING BOTTLE WAS ACTIVATED. THE PILOTS DECLARED AN EMERGENCY, LANDED SAFELY AT THE AIRPORT OF ORIGIN AND EVACUATED THE AIRCRAFT. NO ENGINE FIRE WAS OBSERVED. MAINTENANCE INSPECTED THE FIRE EXTINGUISHING SYSTEM AND FOUND THAT THE FIRE LOGIC CONTROL BOX HAD HEAT DAMAGE AT AN ELECTRICAL CONNNECTOR. (TC NR 20080102008)                                                                                                                                                                                                                                                                  2L72 4T4  TRTA18SW   E4WE    6  C3PNE     
20080225002582008022500258NE  2008       2          25         CA080103001      220071224G7414E06KA245        MAGNETO                                 ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              ENGINE          INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA       224                                                            (CAN) AFTER ROUTINE START ENGINE RPM AND OR GOVENOR BEGAN TO HUNT. PROBLEM PERSISTED EVEN AFTER ENGINE WARMED UP. ENGINE SHUTDOWN AND RT MAGNETO REPLACED. GROUND RUN CARRIED AND NO DEFECTS FOUND WITH NEW MAGNETO. (TC NR 20080103001)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1G71 3O3  O  H11NM   1E4                  
20080225002592008022500259WP  2008       2          25         CA080103004      120071223G2910D2121           SERVO                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              HYD SYSTEM      LEAKING         W      K   NONE                                                                                            KJ FLUID LOSS                WARNING INDICATION                                  ININSP/MAINT     1                      CA       1213                                                           (CAN) DURING A POST FLIGHT INSPECTION THE HYDRUALIC SERVO WAS FOUND LEAKING AT THE PILOT VALVE. SERVO CHANGED AND LEAK CARRIED OUT SERVICEABLE. (TC NR 20080103004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3O3  O  H11NM   1E4                  
20080225002612008022500261CE  2008       2          25         CA080103005      120071228G77978975294         WIRE HARNESS    GARRTT      TPE3316252  BEECH 100   100BEECH    1152916CE  GARRTTTPE331TPE3316252B 01514WP  HARTZLHCB4T HCB4TN5     GL  ENGINE          FAILED          W      E   ENGINE SHUTDOWN                                                                                 N  FALSE WARNING                                                                 TXTAXI/GRND HDL  1                      CA       1000       P27038                  P27038                      (CAN) AFTER A STOPOVER THE AIRCREW WENT TO START THE NR 2 ENGINE, AT THIS TIME IT WAS NOTED THAT THE ITT GAUGE WAS NOT WORKING. MAINTENANCE PERSONNEL FLEW TO THE AIRCRAFT LOCATION AND THROUGH TROUBLESHOOTING DETERMINED THAT THE ITT HARNESS HAD FAILED. A FERRY PERMIT WAS USED TO RETURN THE AIRCRAFT BACK TO THE MAIN BASE. ENGINE WAS REMOVED AND A NEW HARNESS INSTALLED. (TC NR 20080103005)                                                                                                                                                                                                                                                                                                                                           1L72 3T4  T  A14CE   E2WE    6  CP40EA    
20080225002622008022500262EA  2008       2          25         CA080103006      220071227G7414BL6006163       MAGNETO                                 ROBSINR44   R44         7640120WP  LYC   O540  O540F1B5    41532EA                              ENGINE          UNSERVICEABLE   W      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      CA            961                                                       (CAN) ENGINE WOULD NOT START.  LT MAGNETO FOUND UNSERVICEABLE.  MAGNETO CHANGED, GROUND RUN AND FUNCTIONAL CHECKS CARRIED OUT SERVICEABLE. (TC NR 20080103006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3O3  O  H11NM   E295                 
20080225002642008022500264WP  2008       2          25         CA080103008      120071222G8011                COVER                                   ROBSINR44   R44RAVENII  7640122WP  LYC   O540  IO540AE1A5  41530NE                              STARTER         LOOSE           W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       173                                                            (CAN) DURING A 50/100 HOUR INSPECTION, THE STARTER COOLING COVER WAS FOUND LOOSE. THE 3 SCREWS HOLDING IT IN PLACE HAD LOOSENED OFF. THE STARTER WAS REPLACED, GROUND RUN CHECKED SERVICEABLE. (TC NR 20080103008)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1G71 3O3  O  H11NM   1E4                  
             20080520     CE  2008       5          20         CA080104002      120071229G7603SL60112SL6011   KNOB                                    CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE  MCAULY3AF34C3GFR34C703  GL  POWER LEVER     SEPARATED       W      A   UNSCHED LANDING                                                                                 O  OTHER                                                                         CRCRUISE         1                      CA       6101 6101                                                      (CAN) (2) KNOBS ON EITHER SIDE OF THE POWER LEVER ARE USED TO RAISE A GATE TO ALLOW REVERSE THRUST. THE KNOBS ARE SCREWED TOGETHER. DURING FLIGHT THE KNOBS SEPARATED (UNSCREWED) AND FELL OFF. THIS ALLOWED THE GATE TO PIVOT IF THE POWER LEVER WAS RETARDED ALLOWING THE ENGINE/PROP TO ENTER THE REVERSE MODE OF OPERATION. (TC NR 20080104002)                                                                                                                                                                                                                                                                                                                                                                                             1H71 3T3  T  A37CE   E4EA    5  CP60GL    
20080225002662008022500266EU  2008       2          25         CA080104003      120071231G6410355A12003114    TRIM TAB                                SNIAS 350   AS350B      8680801EU  TMECA ARRIELARRIEL1B    6OO30NE                              TAIL ROTOR      UNSERVICEABLE   W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3104                                                           (CAN) WHILE PERFORMING A BRIDGING INSPECTION ON AN A/C PREVIOUSLY LEASED TO A DIFFERENT COMPANY, AD 2007-0138-E WAS BEING C/O. SECTION OF MISSING PAINT NOTED ON AREA REQUIRING INSPECTION IAW ASB 05-00.40( IB ATTACHMENT POINT OF T/E TAB). A CRACK WAS NOTED THROUGH VISUAL INSP, AND THE T/R ASSY REMOVED FROM A/C FOR FURTHER EVALUATION. AD HAD BEEN SIGNED OUT BY PIC PRIOR TO PERFORMING FERRY FLIGHT TO OUR BASE. T/R ASSY WAS INSTALLED ON THIS AIRCRAFT 19.7 HRS PRIOR TO DISCOVERY OF DEFECT. BLADE ASSY SENT TO MFG FOR FURTHER EVALUATION (TC NR 20080104003)                                                                                                                                                                     1G71 3U3  U  H9EU    E19EU                
20080319001722008031900172EA  2008       3          19         CA080105001      120071224G2497VS643           RELAY                                   CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343A1     30068NE                              ELECTRICAL PWR  FAILED          W      O   OTHER                                                                                           B  SMOKE/FUMES/ODORS/SPARKS                                                      TXTAXI/GRND HDL  1                      CA                                                                      (CAN) UPON ARRIVAL, GROUND PWR APPLIED TO AC BUT SHUTOFF IMMEDIATELY. GROUND PWR RESTARTED AND AFTER ABOUT A MINUTE CREW NOTED NUMEROUS CIRCUIT BREAKERS POPPED, HEARD A LOUD BANG FROM THE NOSE SECTION AND A LIGHT SMELL OF SMOKE IN THE COCKPIT. CIRCUIT BREAKERS POPPED INCLUDED CENT TRU 1, NAV LIGHTS, TRU 1, TRU2, STCU, TRU SERVICE, SENSOR TOILET, CEILING LIGHTS, SIDEWALL LIGHTS AND STAB CHAN HSTCU. MAINT TROUBLESHOOTING, TRACED FAULT TO AN AC SERVICE BUS FAULT. PWR SENSE RELAY K5XD ( P/N VS-643) IN JB6 REPLACED (SHORTED WIRING ALSO REPAIRED). NUMEROUS OTHER PARTS REPLACED DUE TO DOWN LINE FAILURES. ( HSTCU P/N 7060-10, S/N 213.)  LT AND RT WINDSHIELD HEAT CONTROLLERS P/N 601R59006-5, S/NS 5131 & 3475(SOME BURNE2L72 4F4  FRTA21EA   E15NE                
20080319001742008031900174    2008       3          19         CA080106002      420071228G3418501177003       ACTUATOR                                CNDAIRCL600 CL6002D24   1390016EA  GE    CF34  CF348C5B1   30052NE                              STICK PUSHER    FOD             W      O   OTHER                                                                                           F  FLT CONT AFFECTED                                                             LDLANDING        1                      CA                                                                      (CAN) THE CABLE RUNS HAVE BEEN INSPECTED IN THE FWD ELECTRONICS BAY AND THE FWD QUADRANTS HAVE BEEN INSPECTED AND NO DEFECTS NOTED. THE FWD PULLEYS AND CABLES WERE LUBED AND AC SENT FOR A TEST FLIGHT. IN ALL OTHER MODES OF FLIGHT THE AC OPERATES NORMALLY. ONLY ON LANDING WHEN THE PILOTS HAVE FLARED THE NOSE UP AND THE MLG HITS THE GROUND DOES IT SEEM TO LOCK UP PREVENTING THE PILOTS FROM PRESSING THE NOSE DOWN TO LAND.         WITH THE AC ON THE GROUND AND THE PITCH DISCONNECTED YOU CAN FEEL WHAT IS DESCRIBED AS A ROUGH SPOT IN THE FOS YOKE AS YOU MOVE HALF WAY FROM FULLY AFT TO CTR AND HALF WAY FROM CENTER POSITION TO FULLY FWD POSITION.  PROBLEM WAS SOLVED BY REPLACING THE STICK PUSHER ASSY. STICK PUSHER WAS2L72 4F4  FRTA21EA   E00063EN             
20080320000052008032000005NE  2008       3          20         CA080108001      220071218G7261                SUMP                                    CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              NR 1 ENGINE     LEAKING         W      C   ABORTED TAKEOFF                                                                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  TOTAKEOFF        1                      CA                                                                      (CAN)  SMOKE CARGO MESSAGE SHORTLY AFTER T/O AND ODOR OF SMOKE ON FLIGHT DECK. LANDED, & TAXI TO PARKING AND DEBARKING OF PAX, CABIN INSPECTED BY FIRE BRIGADE. CABIN CREW REPORTED NO SMOKE IN CABIN AND TOILET DURING FLT AND TAXI BACK. DURING TROUBLESHOOTING, FOUND A-SUMP OIL LEAK ON ENGINE NR 1. A-SUMP CARBON SEAL NR 1 AND NR 3 ON ENGINE NR 1 ON WING ACC. SEI 756 SPECIAL PROCEDURE 41 REPLACED. INSP AND ENGINE RUNS SATISFACTORY. NO MORE SMOKE OBSERVED. REF OS WO 5524048. AIRCRAFT RELEASED TO SERVICE.                                                                                                                                                                                                                        2L72 4F4  FRTA21EA   E15NE                
             20080520     CE  2008       5          20         CA080108008      120071217G323055275042        VALVE SEAT      CESSNA      55275042    CESSNA500   550         2076604CE  PWA   JT15  JT15D4      52112NE                              UPLOCK ACTUATOR DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       6025                                                           (CAN) WHEN PRESSURE IS APPLIED TO THE UPLOCK ACTUATOR THE ACTUATOR MUST TRAVEL FULL STROKE BEFORE ALLOWING FLUID TO THE GEAR ACTUATOR. IN THIS ACTUATOR THE DAMAGED SEAT ALLOWED FLUID TO THE GEAR ACTUATOR BEFORE THE UPLOCK HAD RELEASED THE GEAR.  WE HAVE HAD A COUPLE INCIDENTS WHERE THE GEAR WOULD NOT EXTEND WHEN THE GEAR ACTUATOR APPLIED DOWN FORCE TO THE GEAR BEFORE THE UPLOCK COULD RELEASE AND THE UPLOCK COULD NOT OVERCOME THE FORCE. UPLOCK ACTUATOR WAS REPLACED. (TC NR 20080108008)                                                                                                                                                                                                                                       1L72 4F4  F  A22CE   E1NE                 
             20080520     NE  2008       5          20         CA080109007      220071227G7261MS955610        BOLT                                    EMB   ERJ190ERJ190100IGW3260408NM  GE    CF34  CF3410E5A1  30022NE                              PUMP            LOOSE           W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) AC WAS ON MONITOR FOR LOW OIL QTY SNAGS SINCE THE 21ST OF DEC. TODAY (27TH) ALL OF THE EDP MIDDLE CASING BOLTS WERE FOUND LOOSE.  CMM 29-12-10, ITEM 300: BOLT P/N MS9556-10 AND ITEM 305: WASHER NAS620C10L. (TC NR 20080109007)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA57NM   E00070EN             
20080225002742008022500274NM  2008       2          25         CA080110004      120070831G29136617303         PUMP                                    BOMBDRDHC8  DHC8400            NM                                                               HYD SYSTEM      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       1497                                                           (CAN) MFG HAD ISSUED SB 84-29-15A/ SB 66173-29-349 DUE TO LEAKING OF THE ENGINE DRIVEN HYD PUMP. THE SB WAS CARRIED OUT ON THE ABOVE MENTIONED COMPONENT AT TSN: 834.0 AND CSN OF 874. COMPONENT REMOVED DUE TO LEAKAGE IN THE FLANGE AREA THAT HAD BEEN RETORQUED IAW THE SB. HAVE ADDED THE RETORQUING OF THIS COMPONENT IAW THE ABOVE MENTIONED SB INTO THE AC MAINT PROGRAM. (TC NR 20080110004)                                                                                                                                                                                                                                                                                                                                            2H72 4T    RTA13NM                        
20080225002752008022500275CE  2008       2          25         CA080110005      120070108G711010191001651     COWLING                                 BEECH 200   200BEECH    1152920CE  PWA   PT6   PT642A           NE  MCAULY3G34C73GFR34C701  GL                  CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) BACK WALL OF HEATED LIP ASSY FOUND CRACKED.  DEFECT INTRODUCES HOT EXHAUST GASES INTO COWL ASSY, CONTAMINATING ENGINE INTAKE, CABIN PRESSURIZATION, ENGINE CONTROL, AIR.  DEFECT CAUSES INCREASED CORROSION OF COWL ASSY.  DEFECT IS DIFFICULT TO SEE UPON INSP DUE TO LOCATION. (TC NR 20080110005)                                                                                                                                                                                                                                                                                                                                                                                                                                      1L72 4T4  T  A24CE   E4EA    5  CP60GL    
20080320000082008032000008EU  2008       3          20         CA080114004      120071212G2497                WIRE                                    GROB  120   G120A       1660208EU                                                               ALTERNATOR      CHAFED          W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA       632                                                            (CAN) ALTERNATOR CB POPPED IN FLIGHT WITH MINOR SMELL OF SMOKE.  AC RETURNED TO BASE WITHOUT FURTHER INCIDENT. MAINT FOUND THE ALTERNATOR PWR WIRE HAD CHAFED THROUGH THE OIL COOLER HSG AND GROUNDING CONTACT WAS MADE THROUGH CARBON FIBER LOWER COWLING AND HARDWARE ATTACH POINTS SEVERING THE GROUND CABLE FROM THE ALTERNATOR. THIS WAS THE THIRD INCIDENT (FOR FLEET) INVOLVING THE ALTERNATOR WIRES MAKING CONTACT WITH THE OIL COOLER SHROUD. MFG ADDRESSED THE PROBLEM BY ISSUING SB 1121-093, WHERE THE ALTERNATOR WIRES WERE SHORTENED AND SECURED AWAY FROM THE OIL COOLER SHROUD. (TC NR 20080114004)                                                                                                                             1L71 3O    RTA49CE                        
20080306002202008030600220EA  2008       3          6          CA080115011      120071217G2910AE4186G0210000  LINE                                    CNDAIRCL600 CL6002B16   1900305EA  GE    CF34  CF343A1     30068NE                              HYDRAULIC SYS   RUPTURED        W      O   OTHER                                                                                           KJ FLUID LOSS                WARNING INDICATION                                  LDLANDING        1                      CA       4495                                                           (CAN) PRESSURE LINE ON NR 3A PUMP RUPTURED AND SYS FLUID WAS LOST. GEAR WAS ALTERNATELY EXTENDED AND LANDED WITHOUT INCIDENT. THE HOSE WAS REPLACED AND THE AC WAS FERRIED. THE GEAR WAS SWUNG AND THE HYDRAULICS BLED, TESTED SERVICEABLE. THERE ARE CURRENTLY NO LIFE LIMIT ON THESE LINES. (TC NR 20080115011)                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA21EA   E15NE                
20080306002222008030600222NE  2008       3          6          CA080116004      220071220G7200                ENGINE                                  AEROSPATR42 ATR42500    8680948EU  PWA   PW120 PW127            NE                                              MAKING METAL    W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         EJ VIBRATION/BUFFET          WARNING INDICATION                                  CLCLIMB          1                      CA                                          AM0076                      (CAN) VIBRATION WAS FELT ACCOMPANIED BY 3 LOUD NOISES AND FIRE WARNING. ENGINE WAS SHUTDOWN AND AC RETURNED TO POINT OF DEPARTURE. POST FLIGHT INSPECTION REVEALED NO EVIDENCE OF FIRE, HOWEVER PROPELLER COULD NOT BE ROTATED AND THE TURBOMACHINE CHIP DETECTOR WAS FOUND TO BE HEAVILY CONTAMINATED WITH METALIC DEBRIS. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20080116004)                                                                                                                                                                                                                                                                                                             2H72 4T4  TRTA53EU   E20NE                
20080306002232008030600223NE  2008       3          6          CA080116005      220071212G7200                ENGINE                                  AEROSPATR42 ATR42500    8680948EU  PWA   PW120 PW127            NE                                              SHUTDOWN        W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            NRNOT REPORTED   1                      CA                                          AM0110                      (CAN) CREW ELECTED TO SHUTDOWN ENGINE DURING FLIGHT DUE TO LOW/NO OIL PRESSURE INDICATION.  ENGINE WAS SUBMITTED TO REPAIR SHOP FOR INVESTIGATION AND REPAIR.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20080116005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2H72 4T4  TRTA53EU   E20NE                
20080306002252008030600225NE  2008       3          6          CA080116008      220071220G7200                FITTING                                 AGUSTAA109  A109E       0260119EU  PWC   PW206CPW206C           NE                              P3              CONTAMINATED    W      EA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA                                          BC0503                      (CAN) DURING CRUISE, THE ENGINE POWER DECREASED UNCOMMANDED TO IDLE SETTING, FOLLOWED BY LOSS OF OIL PRESSURE. THE CREW ELECTED TO SHUTDOWN THE ENGINE AND RETURN TO BASE. INVESTIGATION FOUND THE P3 FITTING TO BE CONTAMINATED WITH FOREIGN DEBRIS. FITTING AND SYS WAS CLEANED AND THE AC RETURNED TO SERVICE. (TC NR 20080116008)                                                                                                                                                                                                                                                                                                                                                                                                           1G72 3U3  URTH7EU    E42NE                
20080306002272008030600227NE  2008       3          6          CA080116010      220071221G7200                ENGINE                                  BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A67D          NE                                              MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 JB WARNING INDICATION        SMOKE/FUMES/ODORS/SPARKS                            CRCRUISE         1                      CA                                          114478114162                (CAN) DURING CRUISE, THE MASTER CAUTION ILLUMINATED AND ENGINE SURGES WERE NOTED FOLLOWED BY LOSS OF POWER AND OIL HAZE IN THE CABIN. THE CREW ELECTED TO SHUT THE ENGINE DOWN. THE ENGINE IS TO BE RETURNED TO MFG FOR INVESTIGATION, UPDATES TO FOLLOW. (TC NR 20080116010)                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4T4  TRTA24CE   E26NE                
20080306002282008030600228NE  2008       3          6          CA080116011      220071226G7320                FUEL CONTROL                            CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              ENGINE          INOPERATIVE     W      O   OTHER                                                                                           RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  APAPPROACH       1                      CA                                          JC0550                      (CAN) DURING APPROACH, THE ENGINE DID NOT RESPOND TO THRUST LEVER INPUTS AND REMAINED AT IDLE. AFTER LANDING GROUND TESTS INDICATED THAT THE ENGINE WOULD NOT ACCELERATE ABOVE 46 PERCENT, N2. THE FUEL CONTROL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20080116011)                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA22CE   E25EA                
20080306002292008030600229NE  2008       3          6          CA080116012      220071231G7320                FUEL CONTROL                            CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              ENGINE          MALFUNCTIONED   W      O   OTHER                                                                                           YJ ENGINE STOPPAGE           WARNING INDICATION                                  APAPPROACH       1                      CA                                          DB0324                      (CAN) DURING APPROACH AT 3000 FEET, THE LOW FUEL FLOW WARNING CAME ON, FOLLOWED BY ENGINE SHUTDOWN. THE FUEL CONTROL HAS BEEN REMOVED AND SUBMITTED FOR INVESTIGATION. UPDATES WILL BE PROVIDED WHEN AVAILABLE. (TC NR 20080116012)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             2L72 4F4  FRTA22CE   E00059EN             
20080306002302008030600230EU  2008       3          6          CA080116013      120071230G7931                OIL SYSTEM                              AEROSPATR72 ATR72              EU  PWA   PW120 PW127            NE                              ENGINE          LOW PRESSURE    W      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                          EB0078                      (CAN) DURING CRUISE, THE ENGINE OIL PRESSURE FLUCTUATED INTERMITTENTLY, THEN DROPPED DURING DESCENT. THE CREW ELECTED TO SHUTDOWN THE ENGINE.  ENGINE IS TO BE INVESTIGATED BY MFG, UPDATES TO FOLLOW. (TC NR 20080116013)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2H72 4T4  TRT        E20NE                
20080306002332008030600233EA  2008       3          6          CA080116016      220071126G7250                TURBINE BLADES                          DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA                              ENGINE          FRACTURED       W      CED ABORTED TAKEOFF         ENGINE SHUTDOWN         RETURN TO BLOCK                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  TOTAKEOFF        1                      CA                                          PG0179                      (CAN) DURING TAKEOFF ROLL, THE ENGINE LOST POWER. TAKEOFF WAS ABORTED AND AC RETURNED TO THE RAMP. INVESTIGATION BY MFG REVEALED FRACTURED COMPRESSOR TURBINE BLADES AND A FRACTURED FUEL BYPASS LINE. (TC NR 20080116016)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      1H72 3T4  TRTA9EA    E4EA                 
20080306002352008030600235NM  2008       3          6          CA080116018      120071225G4920                STARTER         PWC                     BOEING747   747400      13848ATNM                                                               APU ACC G/B     FAILED          W      F   ACTIVATE FIRE EXT.                                                                              BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  TXTAXI/GRND HDL  1                      CA                  900077                                              (CAN) WHILE DEPLANING PASSENGERS, AN OIL SMELL WAS NOTED IN THE CABIN ACCOMPANIED BY A FIRE WARNING. THE FIRE BOTTLES WERE DISCHARGED. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGATION. INITIAL INSP INDICATES A MALFUNCTION OF THE STARTER MOTOR LEADING TO ACCESSORY GEARBOX DISTRESS.  UPDATES WILL BE PROVIDED AS AVAILABLE. (TC NR 20080116018)                                                                                                                                                                                                                                                                                                                                                                                          2L74 4F    RTA20WE                        
20080324004272008032400427GL  2008       3          24         CA080116019      220071230G723023064613        IMPELLER        ALLSN                   BELL  407   407         1182206SW  ALLSN 250C  250C47B          GL                              COMPRESSOR      SATURATED       W      O   OTHER                                                                                           K  FLUID LOSS                                                                    LDLANDING        1                      CA       5708       CAC44047                                            (CAN) AFTER UNEVENTFUL AND NORMAL SHUTDOWN, PILOT NOTICED A POOL OF OIL UNDER THE AC AND OIL ALL OVER THE ENGINE COWLS AS WELL AS SOAKING THE IB .2500 OF THE MAIN ROTOR BLADES. THERE WERE NO OIL TEMP OR PRESSURE CAUTION WARNINGS OR ENGINE CHIP LIGHT INDICATIONS. TO THE PILOT SHUTDOWN WAS NORMAL AND PLANNED, EXCEPT FOR A NOTICEABLE ODOR IN THE COCKPIT.  SUBSEQUENT INSP SHOWED OIL EMANATING FROM COMPRESSOR FRONT SUPPORT AREA WITH OIL DISCHARGING FROM BLEED VALVE (VENTED INTO EXHAUST COLLECTOR) AND COMPRESSOR VENT. INITIALLY SUSPECTED NR1 BEARING OIL SEAL FAILURE OR CRACK IN THE COMPRESSOR FRONT SUPPORT OIL PRESSURE/RETURN STRUT. ENGINE SERVICE TECH WAS CALLED IN TO DISASSEMBLE AND REPLACE THE FRONT SUPPORT OR SEA1G71 3U3  UO H2SW    E1GL                 
             20081104     CE  2008       11         4          CA080121006      120071218G32220543011         CAP                                     CESSNA172   172D        2072410CE  CONT  O300  O300D       17022SO                              NLG STRUT       CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       3346                                                           (CAN) DURING ANNUAL INSP OF THE NOSE GEAR ASSY AND OLEO, THE OLEO CAP WAS FOUND TO BE CRACKED. THE CRACK WAS LOCATED .1875 IN FROM THE RADIUS OF THE END FLANGE. THE CAP WAS FOUND TO BE BROKEN THROUGH AND WAS REMOVED IN 2 PIECES. REVIEW OF THE TECHNICAL RECORDS INDICATED THAT THE ACFT HAD BEEN SUBJECT TO SIGNIFICANT DAMAGE LATE IN 1979 AT 2479.9 HRS TTAF. (TC NR 20080121006)                                                                                                                                                                                                                                                                                                                                                        1H71 3O3  ONT3A12    E253                 
             20081105         2008       11         5          CA080122006      120071107G7810PN2031          COLLECTOR                               NAVIONSTC   STCNAVION              CONT  E185  E1853       17014SO  HARTZLHC12V HC12V20*    GL  EXHAUST         DAMAGED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) FOUND WHEN CF90-03R2 WAS DONE. THERE WERE NO VISIBLE SIGNS OF EXHAUST LEAKS. WHEN PRESSURE TESTED WITH AIR AND SOAPY WATER, 4 LEAKS WERE EVIDENT. IT HAS BEEN STANDARD PRACTICE IN THIS AMO TO DO SOAPY WATER TESTS ONLY. OVER THE LAST 8 TO 10 YEARS WE HAVE FOUND 4 OR 5 EXHAUST UNITS THAT SHOW NO VISIBLE SIGNS OF LEAKS, BUT FAIL THE SOAPY WATER TEST. ALL WERE LEAKS AROUND EXISTING WELDS. ONE CRACK THAT STARTED MY POLICY OF SOAPY WATER ONLY TESTING, WAS ALONG THE EDGE OF A WELDED PIPE. THAT CRACK WAS ABOUT .6250 INCH LONG. THERE WERE NO SIGNS OF LEAKS. IT WAS THE RATHER SURPRISED RESPONSE FROM MY TC. THAT PROMPTED THIS REPORT. THE QUESTION IS, HOW MANY OTHERS ARE OUT THERE THAT PASS THE VISUAL TEST, BUT FAIL T1L71 3O3  O  A782    E246    5  CP46GL    
20080220000372008022000037CE  2008       2          20         CA080122011      120071225G2497                WIRE                                    BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  DC GENERATOR    CHAFED          W      D   RETURN TO BLOCK                                                                                 J  WARNING INDICATION                                                            TXTAXI/GRND HDL  1                      CA                                                                      (CAN) MAINT HAD TROUBLESHOT A GENERATOR PROBLEM. THE GENERATOR WOULD GO OFF LINE OCCASIONALLY.  REPLACED PC CARD, REPLACED THE GENERATOR. THE PROBLEM WAS GONE FOR 3 WEEKS. IT RETURNED, MAINT REPLACED THE PC CARD, WITH A HARD FAULT. TESTED SERVICEABLE. NEXT MORNING ON TAXI THE GENERATOR FAILED AGAIN. DISCOVERED A WIRE FROM THE PC CARD TO THE GENERATOR BUS TIE RELAY CHAFED IN THE NACELLE. THE BUNDLE WAS PROPERLY SECURED AND PROTECTED, HOWEVER, THE ONE WIRE WAS ON THE EDGE OF THE BUNDLE AND CHAFED ON A RIVET HEAD. REROUTED THE BUNDLE, SPLICED THE WIRE AND RETURNED THE AC TO SERVICE. (TC NR 20080122011)                                                                                                                  2L72 4T4  T  A24CE   E4EA    6  CP56GL    
20080220000382008022000038CE  2008       2          20         CA080122012      120071128G361013182E40600     TUBE                                    BEECH 300   300BEECH    1152930CE  PWA   PT6   PT6A60A     52043NE  HARTZLHCB4M HCB4MP3     GL  BLEED AIR       LEAKING         W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                                                                      (CAN) CREW REPORTED A BLEED AIR FAIL ANNUCIATOR IN FLIGHT. TROUBLESHOOT AND FOUND A PIN HOLE IN THE BLEED AIR WARNING LINE. HOLE WAS NOT CAUSED BY A BLEED AIR LEAK, NOR BY MECHANICAL DAMAGE. LINE WAS ADEQUATELY SUPPORTED AND NO CHAFING WAS EVIDENT. SPLICED IN REPAIR SECTION IAW MFG SIRM AND TESTED SERVICEABLE. SECOND AC TO HAVE A FALSE FAILURE RECENTLY. (TC NR 20080122012)                                                                                                                                                                                                                                                                                                                                                         2L72 4T4  T  A24CE   E4EA    6  CP56GL    
20080220000412008022000041EU  2008       2          20         CA080123004      120071009G6220704A33633208    SPHERICAL STOP                          SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                              MAIN ROTOR HEAD CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5209                                                           (CAN) PROTRUDING RUBBER FOUND COMING OUT, IN THE MIDDLE OF STOP. (TC NR 20080123004)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1G71 3U3  U  H9EU    E00054EN             
20080220000422008022000042EU  2008       2          20         CA080123005      120071009G6220350431182703    FREQ ADAPTER                            SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B    60037NE                              MAIN ROTOR HEAD BLISTERED       W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       5208                                                           (CAN) ON INSP OF MAIN ROTOR HEAD AT THE END OF THE DAY ENGINEER FOUND BLISTERS ON THE SIDE OF ONE FREQUENCY ADAPTER. BLISTERS WHERE FOUND TO BE BEYOND LIMITS:  REPLACED ALL (3) ADAPTERS. (TC NR 20080123005)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1G71 3U3  U  H9EU    E00054EN             
20080220000762008022000076SO  2008       2          20         CA080128003      120070527G2912460635          FILTER                                  PIPER PA42  PA42720     7104212SO  PWA   PT6   PT6A61      52043EA  HARTZLHCB3T HCB3TN3     GL  HYD SYSTEM      CRACKED         W      O   OTHER                                                                                           K  FLUID LOSS                                                                    LDLANDING        1                      CA       10144                                                          (CAN) DURING APPROACH TO LANDING, FLIGHT CREW EXPERIENCED DIFFICULTY EXTENDING THE LANDING GEAR VIA NORMAL MEANS AND SUBSEQUENTLY MANUALLY LOWERED THE GEAR. INVESTIGATION SHOWED SUBSTANTIAL HYD FLUID LOSS THROUGH CRACKED THREADS OF THE LT ENG HYDR FILTER BOWL. MAINT TO REPLACE THE DAMAGED BOWL WITH NEW, AND TO OVERHAUL THE HYDR PUMPS AND FLUSH THE HYD SYS PRIOR TO FURTHER FLIGHT. (TC NR 20080128003)                                                                                                                                                                                                                                                                                                                              1L72 4T4  T  A23SO   E4EA    6  CP15EA    
20080220000772008022000077SW  2008       2          20         CA080128006      120071215G6320214040118001    BEARING         BELL        205040001101BELL  205   205A1       1181414SW  LYC   T53   T5317BLYC   41616NE                              TRANSMISSION    MAKING METAL    W      O   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      CA                  ABT00760                                            (CAN) TSO OF THE TRANSMISSION ASSY 1186.6 HOURS.  THE AC HAD TAKEN OFF AND WAS IN CRUISE WHEN A TRANSMISSION METAL DETECTOR LIGHT ILLUMINATED. THE PILOT LANDED AC BACK AT CAMP FOR THE ENGINEER TO INVESTIGATE THE DEFECT.  THE BEARING IS AN ON CONDITION BEARING.  THE MAST ASSY AND TRANSMISSION ASSY WERE REMOVED.  THE COMPONENT SHOP FOUND THAT THE TRANSMISSION INPUT TRIPLEX BEARING, P/N 214-040-118-001, WAS THE FERROUS METAL MAKER.  THE MAST BEARING WAS ALSO INSPECTED AND NO DEFECT WAS FOUND. (TC NR 20080128006)                                                                                                                                                                                                              1G71 4U4  U  H1SW    E17EA                
20080319001832008031900183SW  2008       3          19         CA080204006      120070614G2497                WIRE                                    BELL  205   205A1       1181414SW  LYC   T53   T5313B      41549NE                              COCKPIT         SHORTED         W      K   NONE                                                                                            B  SMOKE/FUMES/ODORS/SPARKS                                                      ININSP/MAINT     1                      CA                                                                      (CAN) PILOT REPORTED SPARKS AND A SMALL AMOUNT OF SMOKE FROM THE OVERHEAD CONSOL. UPON INVESTIGATION IT WAS FOUND THAT THE LT OVERHEAD CONSOL PANEL HAD CHAFED THROUGH SEVERAL WIRES COMING UP THE CENTER POST OF THE WINDSHIELD CAUSING THE WIRES TO SHORT TO GROUND.   AFFECTED WIRES REPLACED AND THE WIRING BUNDLE REPOSITIONED. (TC NR 20080204006)                                                                                                                                                                                                                                                                                                                                                                                        1G71 4U4  U  H1SW    E17EA                
20080319001922008031900192EU  2008       3          19         CA080206007      120071217G6123                PROPELLER                               CASA  C212  C212CC      2410204EU  PWA   PW120 PW127            NE                                              MALFUNCTIONED   W      E   ENGINE SHUTDOWN                                                                                 R  PARTIAL RPM/PWR LOSS                                                          APAPPROACH       1                      CA                                          AX0043                      (CAN) DURING APPROACH, CREW REPORTED TORQUE AND PROP SPEED REDUCTION. THE PROPELLER FEATHERED AND AC LANDED. TROUBLESHOOTING IS FOCUSING ON AUTOFEATHER UNIT.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.  INSTALLATION IS CASA 295M. FLEET PRESENTLY GROUNDED AND TROUBLESHOOTING ON HOLD DUE TO CRASH OF SISTER AC. (TC NR 20080206007)                                                                                                                                                                                                                                                                                                                                                             2H72 4T4  T  A43EU   E20NE                
             20081222     CE  2008       12         22         CA080207001      120071214G2160IE502           ACTUATOR VALVE                          CESSNA560   560XL       2076702CE  PWC   545   PW545B           NE                              HEAT EXCHANGER  STICKING        W      C   ABORTED TAKEOFF                                                                                 MJ OVER TEMP                 WARNING INDICATION                                  TOTAKEOFF        1                      CA       88   88                                                        (CAN) RT BLEED AIR OVERTEMP WARNING LITE CAME ON DURING T/O. TWICE IN 42 T/O. THE HEAT EXCHANGER VALVE WAS STICKING IN CLOSED POSITION - VALVE ACTUATOR PIN IE50-2 WAS REPLACED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA22CE   E00059EN             
             20081222     CE  2008       12         22         CA080207002      120071214G783064ND782047      ACTUATOR                                CESSNA560   560XL       2076702CE  PWC   545   PW545B           NE                              THRUST REVERSER LEAKING         W      D   RETURN TO BLOCK                                                                                 K  FLUID LOSS                                                                    TXTAXI/GRND HDL  1                      CA       88   88                                                        (CAN) LT THRUST REVERSER INBD ACTUATOR. WEEPING HYDRAULIC FLUID. NOTE: THIS ACTUATOR WEEPED FLUID FROM DAY ONE ON 560 S/N 0648 HAD 2 ACTUATORS I/B LT REPLACED FOR HYDRAULIC FLUID LEAKS OVER APPROX 1800 HRS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA22CE   E00059EN             
             20081222     CE  2008       12         22         CA080207003      120070920G2433RR18            CONVERTER                               CESSNA525   525         2076601CE  WILINTFJ44  FJ44        66000GL                                              INOPERATIVE     W      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      CA       69   69                                                        (CAN) MFD FAIL TO COME ON WHEN ACFT MASTER SWITCH TURNED ON. DC-DC CONVERTER REPLACED - SAME PROBLEM OCCURED AT 102.6 AIRFRAME HRS. - 66 AIRFRAME CYLES, AND DC-DC CONVERTER REPLACED AGAIN (33 HRS + 19 CYCLES) MFG IS AWARE OF THE POOR QUALITY OF THE RR18 DC-DC CONVERTERS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 4F4  FRTA1WI    E3GL                 
             20081222     CE  2008       12         22         CA080207004      120071005G324649290           PLUG                                    CESSNA560   560XL       2076702CE  PWC   545   PW545B           NE                              RT WHEEL        LEAKING         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       30   30                                                        (CAN) TIRE/WHEEL ASSY LOOSING AIR PRESSURE. SL560XL32-19 PROVIDES IMPROVED THERMAC PLUG. PIN 542-7 WHICH WAS TO BE INSTALLED IN THIS SERIAL NR ACFT AND WHEEL S/N- THE OLD PIN 49-290 PLUG IS MAGNETIC. THE NEW PIN 542-7 IS NO MAGNETIC. CHECKING OF NEW SPARE WHEEL AND BOTH ACFT MAIN WHEELS FOUND OLD PIN PLUGS INSTALLED.                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA22CE   E00059EN             
20080319002102008031900210NM  2008       3          19         CA080208006      120071230G7160658536912       NOSE BULLET                             BOEING737   737275      1384485NM  PWA   JT8   JT8D17      52049NE                              ENGINE          SEPARATED       W      A   UNSCHED LANDING                                                                                 DR INFLIGHT SEPARATION       PARTIAL RPM/PWR LOSS                                CLCLIMB          1                      CA                                                                      (CAN) FOLLOWING DEPARTURE, THE CREW REPORTED COMPRESSOR STALLING OF THE NR 1 ENG AT CLIMB PWR. THE ENGINE PWR WAS REDUCED AND COMPRESSOR STALLS STOPPED. THE AC RETURNED TO DEPARTURE WITH NO FURTHER INCIDENT. INSP OF THE ENGINE IDENTIFIED THAT THE NR 1 ENGINE NOSE DOME HAD SEPARATED FROM THE ENGINE DURING FLIGHT AND MINOR DAMAGE TO THE INTAKE ACOUSTIC LINER AND FIRST STAGE COMPRESSOR BLADES. A BOROSCOPE INSP SHOWED NO INTERNAL ENGINE DAMAGE. THE FIRST STAGE COMPRESSOR BLADES WERE BLENDED, ENGINE INTAKE WAS REPLACED ALONG WITH THE NOSE DOME AND THE A/C WAS RETURNED TO SERVICE. (TC NR 20080208006)                                                                                                                       2L72 4F4  F  A16WE   E2EA                 
20080319002162008031900216NM  2008       3          19         CA080211016      120070224G3260H10101534       DOWNLOCK SWITCH                         BOEING727   727243      138408DNM  PWA   JT8   JT8D9A      52048NE                              MLG             FAILED          W      O   OTHER                                                                                           N  FALSE WARNING                                                                 DEDESCENT        1                      CA                                                                      (CAN) DURING APPROACH INTO AIRPORT, THE LANDING GEAR WAS EXTENDED AT WHICH TIME THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AND THE DOWN AND LOCKED LIGHT REMAINED EXTINGUISHED. THE GEAR WAS RECYCLED WITH THE SAME RESULT AND SOON AFTERWARD, THE UNSAFE LIGHT EXTINGUISHED AND THE DOWN AND LOCKED LIGHT ILLUMINATED AND THE AC LANDED WITHOUT FURTHER INCIDENT. THE GEAR UNSAFE AND DOWN AND LOCKED SWITCHES WERE REPLACED AND THE AC WAS RETURNED TO SERVICE. (TC NR 20080211016)                                                                                                                                                                                                                                                      2L73 4F4  FRTA3WE    E2EA                 
             20080520     SO  2008       5          20         CA080213009      120071101G2752B5195           WORM DRIVE      EMB         D22466      EMB   110   EMB110P1    3260122SO  PWA   PT6   PT6A34      52043EA  HARTZLHCB3T HCB3TN3     GL  FLAP ACTUATOR   STRIPPED        W      A   UNSCHED LANDING                                                                                 F  FLT CONT AFFECTED                                                             LDLANDING        1                      CA            1872                                                      (CAN) AFTER LANDING, THE WING FLAPS OF AN AC COULD NOT BE RETRACTED. THE ASYMMETRY WARNING SYSTEM HAD BEEN TRIPPED. THE LT AND RT FLAP ACTUATORS WERE REPLACED WITH OVERHAULED UNITS AND THE AC WAS DISPATCHED. UPON DISASSEMBLY OF THE ACTUATOR AT THE OVERHAUL SHOP THE BRASS WORM WHEEL THAT DRIVES THE SCREW JACK WAS FOUND STRIPPED.  AWD 82-07-04R3 PART 2 HAD BEEN COMPLETED FEBRUARY 19, 2007. THE PART HAD ONLY 2202 CYCLES AND 1871.8 HOURS SINCE OVERHAUL AND THE ACCOMPLISHMENT OF THE AWD. (TC NR 20080213009)                                                                                                                                                                                                                     1L72 4T4  T  A21SO   E4EA    6  CP15EA    
             20080521     EA  2008       5          21         CA080213011      120070919G3250712761          STUD                                    DHAV  DHC6  DHC6300     2802606EA  PWA   PT6   PT6A27      52043EA  HARTZLHCB3T HCB3TN3     GL  NLG STEERING    SHEARED         W      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      CA                                                                      (CAN) DURING TAXI, A SNAP WAS HEARD BY THE FLIGHT CREW AND HYDRAULIC STEERING CONTROL WAS LOST. THE AC WAS TAXIED TO THE RAMP USING DIFFERENTIAL PWR AND BRAKING.  THE STUD SECURING THE HYD STEERING ACTUATOR WAS FOUND SHEARED. THE NOSE GEAR ASSY WAS REPLACED AND AC WAS RETURNED TO SERVICE. THE CAUSE OF THE BROKEN STUD COULD NOT BE DETERMINED. (TC NR 20080213011)                                                                                                                                                                                                                                                                                                                                                                     1H72 3T4  TRTA9EA    E4EA    6  CP15EA    
             20080521     GL  2008       5          21         CA080214006      220071219G72506847100         SHAFT                                   CVAC  440   440         2422902WP  ALLSN 501D  501D13D     03004GL  ALLSN A6441 A6441FN606  GL  ENGINE          DAMAGED         W      EF  ENGINE SHUTDOWN         ACTIVATE FIRE EXT.                                                      RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CA            445                                                       (CAN) IN CRUISE AT 22,000 FEET, THE CREW OBSERVED A DROP IN RPM FOLLOWED BY A FIRE WARNING IN ENGINE NR1. THE FLIGHT CREW PULLED THE (E) HANDLE AND DISCHARGED THE (2) FIRE EXTINGUISHER BOTTLES. THE FLIGHT CREW THEN PROCEEDED, AFTER DECLARING AN EMERGENCY. THE AC LANDED SAFELY AND NO OTHER INCIDENT REPORTED. THE COMPRESSOR AND TURBINE INTERCONNECT SHAFT AND COUPLING FOUND DAMAGED CAUSING FREE TURBINE ROTATION. THE QEC WAS REMOVED, SPLIT, INSPECTED AND ALL THE PARTS SENT TO THE ENGINE SHOP FOR INVESTIGATION. (TC NR 20080214006)                                                                                                                                                                                             2L72 4R4  T  6A6     E282    6  CP898     
             20081230     CE  2008       12         30         CA080219003      120070914G555104320049        ATTACH BRACKET                          CESSNA150   152         2071835CE  LYC   O235  O235L2C     41505EA  MCAULY1A103 1A103TCM    GL  HORIZONTAL STAB CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       12749                                                          (CAN) DURING INSP OF FIN ATTACH BRACKET NUT PLATES IAW AD 80-11-04 CRACKS WERE DISCOVERED RUNNING ALONG THE BEND RADIUS OF THE WELDED BRACKET. THE AD ALLOWS FOR REMOVING REPETATIVE INSP REQUIREMENTS IF THE NUT PLATES ARE DRILLED OFF AND REPLACED WITH FIBERLOCKING NUTS. ALTHOUGH THE AD MAY NO LONGER MAY BE APPLIABLE IN SOME ACFT THE ENTIRE WELDED BRACKET SHOULD BE INSPECTED CLOSELY EVERY 100-HRS.                                                                                                                                                                                                                                                                                                                                  1H71 3O3  ONT3A19    E223    5  NP50GL    
             20081104     WP  2008       11         4          CA080221006      120071214G6330369H5105        BOLT                                    HUGHES369   369A        4470503WP  ALLSN 250C  250C20B     03013GL                              M/R TRANSMISSIONCRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA                                                                      (CAN) MAIN ROTOR TRANSMISSION RECEIVED FOR OVERHAUL AFTER NDT INSPECTION 31 OF THE 32 RING GEAR BOLTS P/N 369H5105 WERE FOUND CRACKED UNDER THE BOLT HEADS. (TC NR 20080221006)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1G71 3U3  U  H3WE    E4CE                 
200805141    200805141    EA  2008       5          14         CA080304008      220070322G8530LW13622         INTAKE VALVE    LYC         05K21108    PIPER PA31  PA31325     7103105SO  LYC   O540  TIO540F2BD  41532EA  HARTZLHCE3Y HCE3YR2A    GL  ENGINE          FAILED          W      BA  EMER. DESCENT           UNSCHED LANDING                                                         ER VIBRATION/BUFFET          PARTIAL RPM/PWR LOSS                                CRCRUISE         1                      CA       136                                                            (CAN) WHILE IN CRUISE, THE PILOT HEARD A BANG AND EXPERIENCED A LOSS IN POWER ON THE LT ENGINE. AS THE ENGINE REMAINED RUNNING AND THERE WAS NO IMMEDIATE CONCERN FOR SAFETY THE PILOT CHOSE TO LEAVE THE ENGINE RUNNING AND SET DOWN AT THE NEAREST AIRPORT. UPON EXAMINATION OF THE ENGINE IT WAS DISCOVERED THAT THE NR1 CYLINDER INTAKE VALVE HAD FAILED AT THE TIP KEEPER LOCATION. THE DECISION WAS MADE TO REMOVE THE ENTIRE ENGINE ASSY AND RETURN IT TO THE OVERHAUL SHOP DUE TO THE LOW TIME SINCE OVERHAUL (TSO).   I WOULD LIKE TO MAKE NOTE THAT THE ENGINE PARTS MANUAL IS NOT CLEAR AS TO THE STYLE OF KEEPER REQUIRED FOR THE INTAKE VALVE POSITION AND, THOUGH IT WAS NOT A CONCERN IN THIS CASE, IT COULD BECOME AN ISSUE FOR 1L72 3O3  O  A20SO   E14EA   5  CP33EA    
             20090102     CE  2009       1          2          CA080305006      120071130G2197OR551           RESISTOR                                CESSNA340   340A        2076405CE  CONT  O520  TSIO520NB   17040SO  MCAULY3AF32C3AF32C505   GL  HEATER BLOWER   OVERHEATED      W      B   EMER. DESCENT                                                                                   B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      CA                                                                      (CAN) RESISTOR LOCATED UNDER CO-PILOT SEAT(CONTROLS HIGH LOW OPERATION OF HEATER BLOWER MOTOR.  THERE ARE 3 RESISTORS OF THE SAME TYPE IN THIS LOCATION, IN THIS CASE HEATER RESISTOR-OR55-1 OVERHEATED CAUSING THE TY-RAP LOCATED ON THE UPPER PORTION OF RESISTOR TO MELT AND CATCH FIRE, THERE IS A SMALL SHIELD OF FLAME RESISTANCE MATERIAL ON THIS TERMIAL WHICH THE TY-RAP KEEPS IN PLACE.  RECOMMEND THIS AREA BE CHECK TO THE HEAT BUILD UP OF THIS RESISTOR AS THIS WILL INDIACATE THE NEED TO BE CHANGED. RESISTOR WAS CHANGED AND THE NEW RESISTOR HL55-08-Z-1-OHM WAS FOUND AFTER A 30 MINUTE RUN THE TEMP WAS 123 FDEGREES AND THE OLD RESISTOR WAS 187F DEGRESS IN FREE AIR WITH THE SAME LOAD FACTOR,IN THE ENCLOSED SPACE I ASS1L72 3O3  O  3A25    E8CE    5  CP22EA    
             20080602     NE  2008       6          2          CA080305014      220071220G7200                ENGINE                                  CESSNA208   208B        2073701CE  PWA   PT6   PT6A114A    52043NE                                              STOPPED         W      A   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      CA                                                                      DURING FLIGHT AT 12000 FEET ENGINE POWER WAS LOST.  THE AIRCRAFT WAS FORCED TO DITCH 25 MILES OFF COAST.  CREW WAS RESCUED.  INVESTIGATION REVEALED THAT THE ENGINE WAS MAKING NO POWER AT TIME OF IMPACT.  THE FUEL PUMP DRIVE SHAFT REVEALED WORN AND FRACTURED DRIVE SPLINES.  INVESTIGATION IS ONGOING, UPDATES WILL BE PROVIDED.                                                                                                                                                                                                                                                                                                                                                                                                           1H71 3T3  T  A37CE   E4EA                 
             20080521     NE  2008       5          21         CA080305015      220071027G7200                ENGINE                                  BELL  212   212         1181420SW  PWA   PT6T  PT6T3B      52045NE                                              FAILED          W      A   UNSCHED LANDING                                                                                 ET VIBRATION/BUFFET          ENGINE CASE PENETRATION                             APAPPROACH       1                      CA                                                                      (CAN) DURING APPROACH, VIBRATION WAS NOTED BY THE CREW THROUGH THE FLIGHT CONTROLS. LANDING WAS ABORTED AND AC RETURNED TO BASE. NEARING BASE, VIBRATION LEVEL INCREASED ABD CREW DECLARED AN EMERGENCY. DURING LANDING FLARE, (2) LOUD NOISES WERE HEARD. POST FLIGHT INSP REVEALED NON-CONTAINMENT OF ENGINE POWER TURBINE SECTION HARDWARE WHICH HAD PENETRATED THE AIRFRAME DECK, COWLING AND BELLY.  MFG WAS NOTIFIED OF THIS BY THE OVERHAUL AGENCY CONDUCTING THE INVESTIGATION. THE DAMAGED HARDWARE WILL BE RETURNED TO MFG FOR FURTHER ANALYSIS.  MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 20080305015)                                                                             1G71 4U4  U  H4SW    E22EA                
             20081104     EU  2008       11         4          CA080305018      120071017G2822P94B12209       PUMP                                    SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              FUEL BOOST      FAILED          W      K   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      CA            162                                                       (CAN) PILOT HAD INDICATION OF A FUEL BOOST PUMP FAILURE. ACFT PERFORMED A NORMAL PLANNED LANDING AND THE PUMP WAS SUBSEQUENTLY REPLACED, NO FURTHER INCIDENT. (TC NR 20080305018)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1G71 3U3  U  H9EU    E19EU                
             20080521     NE  2008       5          21         CA080305019      220071010G7310419110003       MANIFOLD                                SNIAS 350   AS350B2     8680813EU  LYC   LTS101LTS101*          NE                              FUEL SYSTEM     UNSERVICEABLE   W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA                                                                      (CAN) DURING POST MAINT INSP GROUND RUN, A FUEL LEAK WAS DISCOVERED AT THE FUEL MANIFOLD, IT WAS DETERMINED THE MANIFOLD WAS THE CAUSE, THE PART WAS REPLACED WITHOUT FURTHER INCIDENT. (TC NR 20080305019)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     1G71 3U3  U  H9EU    E5NE                 
             20081105     EU  2008       11         5          CA080318005      120071120G2916                RESERVOIR                               UROCOPEC120 EC120B      8680987EU  TMECA ARRIUSARRIU2F          NE                              HYD SYSTEM      LEAKING         W      K   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      CA       3193                                                           (CAN) THE RESERVOIR SECTION OF THE HYDRAULIC PUMP ASSEMBLY BEGAN TO LEAK HYDRAULIC FLUID. THE LEAK WAS NOTED ON A PREFLIGHT INSPECTION WHERE THERE WAS A PUDDLE OF HYDRAULIC FLUID ON THE TRANSMISSION DECK OF THE HELICOPTER. THE FLIGHT WAS CANCELLED. THE LEAK WAS TRACED TO A LARGE PLUG WHICH IS SWAGED OR STAKED INTO THE BOTTOM OF THE RESERVOIR. THE HYDRAULIC PUMP ASSEMBLY WAS REMOVED AND IT WAS FOUND THAT THE PLUG WAS LOOSE IN THE BOSS, AND COULD ROTATE FREELY. THERE IS NO REPLACEABLE SEAL OR METHOD TO RESEAL THE PLUG. THE HYDRAULIC PUMP ASSEMBLY WAS RETURNED TO THE MANUFACTURER.                                                                                                                                        1G72 3U3  UNCR0001RD E34NE                
             20081229         2008       12         29         CA080404003      420070807G83002140402141      LINER           BELL                    BELL  214   214B1       1182105SW  LYC   T55   T5508D      41555NE                              RGB BEARING     SHEARED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CA       9203 1345                                                      (CAN) DURING THE COURSE OF A 100 HR INSP, AME FOUND A LARGE AMOUNT OF NON-FERROUS METAL PARTICLES IN THE REDUCTION GEARBOX OIL FILTER AND THE OIL DRAINED FROM THE GEARBOX. CHIP PLUG WAS INSPECTED AND FOUND CLEAN. REDUCTION GEARBOX WAS REMOVED AND REPLACED WITH A SERVICEABLE GEARBOX. LATER TEARDOWN OF THE GEARBOX FOUND THE INPUT BEARING LINER P/N 214-040-214-1 HAD SHEARED ITS 3 RETAINING PINS AND SPUN WITHIN THE MAGNESIUM CASE P/N 214-040-211-005.                                                                                                                                                                                                                                                                              2G71 4U4  U  H6SW    E4NE                 
             20081107     NE  2008       11         7          CA080714002      220070806G7250304915201       TURBINE BLADES                          DHAV  DHC8  DHC8106     2809020NM  PWA   PW121 PW121       52124NE  HAMSTD14SF  14SF7       NE  TURBINE SECTION FRACTURED       W      A   UNSCHED LANDING                                                                                 EY VIBRATION/BUFFET          ENGINE STOPPAGE                                     CRCRUISE         1                      CA       7628                                                           (CAN) ON AUGUST 6/2007 SHORTLY AFTER TAKEOFF, MX HAD A REPORT FROM THE CREW OF A SMELL OF OIL IN THE CABIN. THIS WAS FOLLOWED BY A NR 2 ENGINE FIRE WARNING AND THE CREW PROCEEDED TO CARRY OUT THEIR SOP`S AND THE ENGINE WAS SHUT DOWN. THE ACFT PROCEEDED BACK TO YYT WHERE IT LANDED WITHOUT INCIDENT.  THE ENGINE WAS REMOVED AND SENT FOR EVALUATION. IT WAS DETERMINED THAT 1 OF THE LOW PRESSURE TURBINE BLADES HAD FRACTURED AT THE BLADE ROOT. THE BLADES WERE SENT TO P&W FOR EVALUATION. IT WAS DETERMINED THAT 1 FRACTURED LPT BLADE AT .050 INCH FROM THE BLADE PLATFORM OCCURRED AS A RESULT OF FATIGUE ORIGINATING FROM THE TRAILING EDGE. DAMAGE TO THE REMAINING LPT BLADE AIRFOILS WAS CAUSED BY SUBSEQUENT MECHANICAL IMPACT2H72 4T4  TRTA13NM   E20NE   6  CP7NE     
             20081112     EU  2008       11         12         CA080729005      120070620G29131259A           MOTOR                                   DORNERDO228 DO228202    2992030EU  GARRTTTPE331TPE3315251K      NM  HARTZLHCB4T HCB4TN5     GL  HYD SYSTEM      INTERMITTENT    W      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                NRNOT REPORTED   1                      CA            1153                                                      (CAN) UPON SELECTED GEAR DOWN NOTHING HAPPENED. PILOT THEN CYCLED THE GEAR DOWN AGAIN ALL FUNCTION NORMALLY, 3 GREEN DOWN AND LOCKED. ACFT WAS THEN INSPECTED, NO FAULTS FOUND, MAINT CREWS AND EQUIPMENT WERE FLOWN IN AND PUT A/C ON JACKS GEAR SWUNG NO FAULTS ACFT WAS THEN FLOWN BACK, FOR FURTHER TROUBLESHOOTING. AFTER SEVERAL GEAR SWING HYDR MOTOR WAS FOUND TO OPERATE INTERMITTENTLY. IT IS ALSO BELIEVED THAT COLD WEATHER POSSIBLY COULD OF HAD A INFLUENCE, BELIEVED TO BE -40.                                                                                                                                                                                                                                                  2H72 4T4  TRTA16EU   E2WE    6  CP40EA    
             20081119     EA  2008       11         19         CA080805004      120070901G307011020140T       HEAT TAPE                               CNDAIRCL600 CL6002B19   1900309EA  GE    CF34  CF343B1     30070NE                              WATER HEATER    BURNED          W      K   NONE                                                                                            M  OVER TEMP                                                                     ININSP/MAINT     1                      CA                                                                      (CAN) THE AFT WATER SUPPLY HEATER TAPE OVERHEATED AND BURNED. INVESTIGATION REVEALED WATER HEATER WAS RUNNING WITHOUT TEMP REGULATION.  HEATER WAS REPLACED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA21EA   E15NE                
             20081112     NM  2008       11         12         CA080815008      120071224G3240                BRAKE                                   EMB   ERJ170ERJ170200SU NIR    NM  GE    CF34  CF348E5A1   30062NE                              MLG             STICKING        W      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                TXTAXI/GRND HDL  1                      CA                                                                      (CAN) AS REPORTED BY FLIGHT CREW: ON LANDING IAH BRAKES WORKED WELL. DURING TAXI OFF RUNWAY FELT BRAKES GRABBING. WALKAROUND NORMAL, BRAKE TEMP NORMAL. HAD REPORT OF SMOKE FROM RT SIDE. NO EVIDENCE OF DAMAGE. ON TAXI OUT RT OTBD FAILED. BRAKE WAS REMOVED AND CONFIRMED CARBON FAILURE                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA56NM   E00063EN             
             20081230         2008       12         30         CA081118009      420071101G2300                TRANSPONDER                             BOMBDRBD100 BD1001A10   1390044GL  HNYWL AS907 AS90711A    33908WP                              NAV/COMM        MALFUNCTIONED   W      O   OTHER                                                                                           N  FALSE WARNING                                                                 CRCRUISE         1                      CA                                                                      (CAN) LOSS OF COMM/NAV/ TRANSPONDER OCCURRED BACK IN NOV 2007. NOT REPORTED UNTIL 9/11/08 AFTER CUSTOMER HAD HEARD OF A SIMILAR OCCURRENCE ON ANOTHER CHALLENGER 300 (20016) THROUGH ADV COMMITTEE CONFERENCE CALL. IN FLIGHT CREW NOTED THAT TRANSPONDER CODE CHANGING FREQ.  LT AND RT RADIOS INDICATED YELLOW ON C/P MFD. ALSO ON C/P MFD, HAD AMBER BOXED DCP FLASHING ON AND OFF. IAW RECOMMENDATION FROM REP, THE C/P DCP CHANGED OUT. TECHS UNABLE TO DUPLICATE PROBLEM.                                                                                                                                                                                                                                                                 2L72 4F4  FRTT00005NYE00010LA             
             20081230     GL  2008       12         30         CA081121008      120071109G29101005354220N50192LINE                                    BOMBDRBD100 BD1001A10   1390044GL                                                               HYDRAULIC SYS   CHAFED          W      A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      CA       4000                                                           (CAN) CREW REPORTED DURING CRUISE FLIGHT THEY LOST ALL RT SIDE HYD FLUID. NUMEROUS CAS MESSAGES. RT SYS SHOWS 2 PERCENT QUANTITY AND 0 PSI. TEMP 36 C.  ACFT DIVERTED IN FLIGHT. AFTER LANDING CREW NOTED HYD FLUID RUNNING OUT OF THE LR FUSELAGE BY THE MAIN WHEEL WELL AREA. FOUND NR 2 ENGINE HYD SUPPLY LINE WITH CLAMP THAT HAD CHAFED INTO THE TUBE ASSY AND WORN A HOLE.                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RTT00005NY                     
20080108003612008010800361EA  2008       1          8          CHI08CA035       220071101G8520                NUT             LYC                     MOONEYM20   M20E        5870212SW  LYC   O360  IO360A1A    41514EA  HARTZLHCC2Y HCC2YK1     GL  CONNECTING ROD  BACKED OUT      G      BAH EMER. DESCENT           UNSCHED LANDING         DEACTIVATE SYST/CIRCUITS                        RYTPARTIAL RPM/PWR LOSS      ENGINE STOPPAGE           ENGINE CASE PENETRATION   CRCRUISE         1                      GL115912Q1800 818               821         L227651A    CA385           NR 3 PISTON CONNECTING ROD SEPARATED FROM THE CRANKSHAFT. PISTON SHEARED MOUNTING STUDS OF CYLINDER HOUSING AT ENGINE CASING. CYLINDER HOUSING SEPARATED FROM ENGINE CASING. ENGINE SHUTDOWN.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  O  2A3     1E10    5  CP920     
20070504001312007050400131CE  2007       5          4          CM2R747K         120070501G273053608014        BELLCRANK                               CESSNA340   340A        2076405CE  ALLSN 250C  250C28B     03013GL                              ELEVATOR        BROKEN          B  CM2RO   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      SW15397R 6383 127               0009                                    BEARING AND BOLT FAILED IN THE ELEVATOR BELLCRANK P/N 5360801-4.  CENTER BEARING THAT SUPPORTS THIS BELLCRANK FAILED.  BEARING IS P/N MS27640-4.   BOLT P/N AN4-14 WAS SEVERELY WORN AND BROKEN IN TWO.  IF EITHER END OF THE BOLT SLIPPED OUT OF THIS BELLCRANK, THE A/C WOULD HAVE LOST PRIMARY ELEVATOR CONTROL.  THE ELEVATOR TRIM SYSTEM WOULD STILL FUNCTION.                                                                                                                                                                                                                                                                                                                                                                             1L72 3O3  U  3A25    E1GL                 
20070808000652007080800065CE  2007       8          8          CNQ2918C         120070726G3010M1200180244     THERMAL SWITCH                          CESSNA680   680CE       2076811CE                                                               ANTI ICE SYSTEM WARNING MESSAGE B      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      GL25350QS1725                   6800036                                 IN-FLIGHT AT FL 300, LT IB WING ANTI-ICE MSG ILLUMINATED, FOLLOWED BY ILLUMINATION OF THE LT WING ANTI-ICE COLD CAS MSG AND THE LT WING BLEED LEAK CAS MSG. FLIGHT CREW FOLLOWED CHECKLIST PROCEDURES; COULD NOT EXTINGUISH ANY AMBER CAS MSGS.  FLIGHT CREW DIVERTED AIRCRAFT FOR MAINTENANCE.  TECHNICIANS FOUND THE (2) ELECTRICAL LEAD WIRES BROKEN AT SL006 SWITCH, SOLDER CONNECTIONS.  REPAIRED WIRES AND PERFORMED OPERATIONAL CHECKS; ALL OPERATIONAL CHECKS WERE SATISFACTORY.  AIRCRAFT RETURNED TO SERVICE 07/19/07.                                                                                                                                                                                                                2L72 4F    RCT00012WI                     
20070824003102007082400310NM  2007       8          24         CO1Y200700001    120070818G5313A6A71211        LONGERON                                DOUG  MD11  MD11        3023602NM                                                               ZONE 100        CRACKED         B  CO1YK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA33702BC                       48504                                   CAC COMPARTMENT AT STA 6-100 ON LONGHERON NR 37LT SIDE FOUND CRACK 1 INCH.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L73 4F    RTA22WE                        
20070824003112007082400311NM  2007       8          24         CO1Y200700002    120070818G5330AEA75732        DOUBLER                                 DOUG  MD11  MD11        3023602NM                                                               BS 1321-1341    CORRODED        B  CO1YK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA33702BC                       48504                                   MAIN CABIN FROM STA 1321 TO STA 1341 FROM L NR 13 TO L NR 14 RT SIDE ON DOUBLER FOUND CORROSION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L73 4F    RTA22WE                        
20070917000022007091700002NM  2007       9          17         CO1Y200700003    120070901G5730                SKIN                                    DOUG  MD11  MD11        3023602NM                                                               LT WING         CORRODED        B  CO1YK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA33702BC                       48504                                   LT WING UPPER SURFACE ON SKIN FROM XORS 130 TO XORS 738 FOUND EXFOLIATION CORROSION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L73 4F    RTA22WE                        
20070917000012007091700001NM  2007       9          17         CO1Y200700004    120070901G5730                SKIN                                    DOUG  MD11  MD11        3023602NM                                                               RT WING         CORRODED        B  CO1YK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA33702BC                       48504                                   RT WING UPPER SURFACE FROM XORS 345 TO XORS 828 FOUND 15EA EXFOLIATION CORROSION POINTS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L73 4F    RTA22WE                        
20071204001042007120400104NM  2007       12         4          CO1Y200700009    120071105G5330ACA3108503      SKIN                                    DOUG  MD11  MD11        3023602NM                                                               BS 535          CRACKED         B  CO1YK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA33702BC                       48504                                   AT RT AIR CONDITIONING COMPARTMENT AFT DOOR JAMB FOUND 0.25 INCH CRACK ON EXTERNAL SKIN STA 535 L NR32RH.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L73 4F    RTA22WE                        
20070202000152007020200015SO  2007       2          2          CWQD200702       120070130G32511159LM305489    SCISSORS                                GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6118          EU                              MLG STEERING    CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05411QS9576                   1311                                    DURING CHECKLIST FOUND UPPER TORQUE LINK CRACKED P/N 1159LM30548-9 AT CONNECTING LOWER TORQUE LINK P/N 1159LM30553-3.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           2L72 4F4  FRTA12EA   E25NE                
20070131001402007013100140CE  2007       1          31         CWQR200701       120070122G273055653426        PUSHROD                                 CESSNA500   550         2076604CE                                                               ELEVATOR        MISMANUFACTURED B  DXTAK   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      GL05                                                                    DURING THE REPAIR STATION PRELIMINARY INCOMING PARTS INSPECTION, IT WAS OBSERVED THAT ONE OF THE NEW ELEVATOR PUSHROD CLEVIS ENDS WERE ATTACHED WITH ALUMINUM RIVETS. ANOTHER NEW UNIT AND THE OLD PUSHRODS USED MONEL RIVETS. A CALL TO MFG CONFIRMED THAT MONEL RIVETS SHOULD BE INSTALLED. THE PART WAS REJECTED, TAGGED AND RETURNED TO MFG.  ASKED MFG TO CHECK THEIR STOCK FOR THIS CONDITION. AN SCR HAS BEEN SUBMITTED TO MFG UNDER NR 271980.                                                                                                                                                                                                                                                                                          1L72 4F      A22CE                        
20070417001342007041700134CE  2007       4          17         CWQR200702       120070416G541065526022        FLANGE                                  CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              NACELLE         CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05820QS2627                   5600650                                 DURING A PHASE 1-4 INSPECTION A 2.5 INCH CRACK WAS FOUND ON THE ENGINE INLET FLANGE, THIS CRACK PASSES THROUGH (2) FASTENERS THAT ATTACH THE INLET TO THE FLANGE. AND ARE AT THE 3 O'CLOCK POSITION ON BOTH THE LT AND RT ENGINES.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA22CE   E00053EN             
20070712001342007071200134CE  2007       7          12         CWQR200703       120070706G5340556560821       ATTACH BRACKET                          CESSNA500   560CESSNA   2076750CE                                                               MASTER CYLINDER CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05347QS7855                   5600357                                 DURING A PHASE 1-4 INSPECTION, FOUND THE MASTER CYLINDER ATTACH BRACKET MOUNT HOLES GOUGED DURING INSTALLATION AT THE FACTORY, UPON FURTHER INSPECTION FOUND A .7500 INCH CRACK IN THE FLANGE ATTACH LEG RADIUS. REPLACED WITH NEW BRACKET ASSY. SUBMITTED SCR TO MFR UNDER SCR NR 301844.                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F    RTA22CE                        
20070808000452007080800045CE  2007       8          8          CWQR200704       120070716G571266211511        CLOSEOUT PANEL                          CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              LEFT WHEEL WELL CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05694QS                       5605194                                 DURING A PHASE 5 INSPECTION, FOUND LT WHEEL WELL AFT SPAR CLOSE OUT PANEL CRACKED.  (3) CRACKS WERE FOUND BEGINNING FROM THE LOWER SKIN ATTACH FLANGE AND GOES STRAIGHT UP THE PANEL.  AN SDR HAS BEEN SUBMITTED TO AIRCRAFT UNDER NR 303303.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA22CE   E00059EN             
20070808000462007080800046CE  2007       8          8          CWQR200705       120070716G571266211511        CLOSEOUT PANEL                          CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              LEFT WHEEL WELL CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05694QS                       5605194                                 DURING A PHASE 5 INSPECTION, FOUND LT WHEEL WELL AFT SPAR CLOSE OUT PANEL CRACKED.  (3) CRACKS WERE FOUND BEGINING FROM THE LOWER SKIN ATTACH FLANGE AND GOES STRAIGHT UP THE PANEL.  AN SCR HAS BEEN SUBMITTED TO MFG AIRCRAFT UNDER NR 303303.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA22CE   E00059EN             
20070808001012007080800101CE  2007       8          8          CWQR200706       120070725G5540663322513       PLATE                                   CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              RUDDER          RUSTED          B  CWQRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05801QS                       5600601                                 DURING A PHASE 1-4 INSPECTION, NOTICED A RUST STAIN COMING FROM THE LOWER RUDDER BEARING PLATE ASSY (LOWEST HINGE POINT). UPON DISASSEMBLE, FOUND THE DRAIN HOLE FROM THE RUDDER TORQUE TUBE WAS DRAINING INTO THE LOWER BEARING PLATE ASSY. THIS IS DUE TO A NEW DESIGN OF THE PLATE ASSY, THE NEW ONE IS BEEFED UP AND HAS A BUILT UP AREA AROUND THE BEARING, THAT DIRECTS WATER TO THE BEARING, UNLIKE THE PREVIOUS DESIGN THAT WAS A FLAT PLATE AND ALLOWED WATER TO DRAIN AWAY FROM THE BEARING.  SERVICE CONDITION REPORT HAS BEEN FILED WITH MFG UNDER NR 305034.                                                                                                                                                                       2L72 4F4  FRTA22CE   E00053EN             
20070824003042007082400304CE  2007       8          24         CWQR200707       120070821G554066331508        BALANCE WEIGHT                          CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              RUDDER          MISINSTALLED    B  DXTAK   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      GL05698QS                       5605653                                 DURING A PHASE 1-4 INSPECTION, FOUND THE RUDDER BALANCE WEIGHT WAS TRIMMED DOWN AND ATTACHED WITH ONLY (2) BOLTS.THE IPC SHOWS (4) BOLTS TO ATTACH THIS WEIGHT. CONTACTED MFG ENGINEERING, THEY STATED THE WEIGHT REQUIRES (4) BOLTS TO MEET THE 100 (G) STANDARD. APPEARS THE RUDDER BALANCE WEIGHT WAS TRIMMED DOWN AND INSTALLED AT THE FACTORY. REPLACED RUDDER BALANCE WEIGHT IAW SRM 51-60-03, RUDDER BALANCING.  SUBMITTED SERVICE CONDITION REPORT TO MFG UNDER NR 310349.                                                                                                                                                                                                                                                              2L72 4F4  FRTA22CE   E00059EN             
20070824003122007082400312CE  2007       8          24         CWQR200708       120070731G3110556560914       SUPPORT CHANNEL                         CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              INST PANEL      CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05371QS                       5600471                                 DURING MAINTENANCE FOUND THE RUDDER UPPER SUPPORT CHANNEL CRACKED WHERE IT ATTACHES TO THE INSTRUMENT PANEL.  THIS AIRCRAFT HAD SL560-27-13 COMPLIED WITH 826.6 HOURS PRIOR TO FINDING THE CRACKED CHANNEL. THIS SL UPGRADED THE ATTACHING HARDWARE BUT DOES NOT CHANGE THE BRACKET.  REPLACED BRACKET AND HARDWARE WITH NEW.  AN SCR HAS BEEN SUBMITTED TO MFG UNDER NR 306488.                                                                                                                                                                                                                                                                                                                                                                2L72 4F4  FRTA22CE   E25EA                
20070824003132007082400313CE  2007       8          24         CWQR200709       120070808G541565526022        MOUNT                                   CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              NACELLE         CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05810QS                       5600625                                 DURING AN INSPECTION FOUND THE ENGINE NACELLE ATTACH FLANGE EARS CRACKED IN (2) LOCATIONS. SENT TO MFG FOR EVALUATION AND REPAIR. SUBMITTED SCR TO MFG UNDER NR 308174.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA22CE   E00053EN             
20070824003152007082400315CE  2007       8          24         CWQR200710       120070808G322055423002        FORK                                    CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              NLG             LOOSE           B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05804QS                       5600610                                 DURING A MAINTENANCE TAXI CHECK NOTICED SHIMMY FROM NOSE GEAR. UPON DISASSEMBLY FOUND FORK LOOSE ON NOSE GEAR PISTON, THIS SHOULD BE A PRESS FIT FROM THE FACTORY.  SENT UNIT RELIABILITY GROUP FOR EVALUATION.   A SCR HAS BEEN SUBMITTED TO MFG UNDER NR 308107.                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4F4  FRTA22CE   E00053EN             
20070824003162007082400316CE  2007       8          24         CWQR200711       120070813G716065526057        INTAKE DUCT                             CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              LT ENGINE       CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05804QS                       5600610                                 DURING A PHASE INSPECTION FOUND LT ENGINE INLET DUCT ASSY CRACKED. CRACKS WERE FOUND ON THE AFT PORTION OF THE INLET DUCT ASSY THROAT. THIS UNIT HAD TO BE RETURNED TO THE MFG FOR REPAIR. AN SCR WAS SUBMITTED TO MFG UNDER NR 308858.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA22CE   E00053EN             
20070824003172007082400317CE  2007       8          24         CWQR200712       120070813G716065526057        INTAKE DUCT                             CESSNA500   560CESSNA   2076750CE  PWA   530   PW535A           NE                              RT ENGINE       CRACKED         B  DXTAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05804QS                       5600610                                 DURING A PHASE INSPECTION FOUND RT ENGINE INLET DUCT ASSY CRACKED. CRACKS WERE FOUND ON THE AFT PORTION OF THE INLET DUCT ASSY THROAT. THIS UNIT HAD TO BE RETURNED TO THE MFG FOR REPAIR. AN SCR WAS SUBMITTED TO MFG UNDER NR 308873.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA22CE   E00053EN             
20070209001012007020900101CE  2007       2          9          DEBD624B0207     120070202G3246GYS186C21       BOLT            GOODYEARAERO            BEECH MU300 400A        1155402CE                                                               MLG WHEEL       BROKEN          B  DEBDK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL19624B 1169       NOV991386   RK369                                   A WHEEL THRU BOLT BROKE WHILE BEING TORQUED DURING WHEEL REASSEMBLY AFTER A TIRE CHANGE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4F    RTA16SW                        
20070125001402007012500140CE  2007       1          25         DELR200700001    120070104G71202652002         BOLT                                    LEAR  55    55LEAR      5170702CE  ALIDSGTFE731TFE7313AR        WP                              ZONE 400        SHEARED         B  DELRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE03345RJ7248 6267              078         P85197                      AFTER REMOVAL OF SAFTY WIRE TO REMOVE BOLT, THE MOUNT BOLT WAS FOUND SHEARED AT THE NECK OF THE BOLT. THREADED SECTION OF BOLT WAS REMOVED WITH AN EASYOUT IAW CHAPTER 5 THIS ITEM IS LIFE LIMITED AT 20,000.00 HOURS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  F  A10CE   E6WE                 
20070504001502007050400150GL  2007       5          4          DJS041707        120070417G770035C155103       SENSOR                                  AMTR  500   ECLIPSE500  05614K5GL                                                               ENGINE          FAULTY          C      E   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      EA27110DJ42                     000007                                  INFLIGHT SHUTDOWN IAW AFM DUE TO LOSS OF OIL TEMPERATURE. TROUBLESHOT TO A FAULTY MOT/MOP SENSOR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 3F    RTEXPA1L72                     
20070425002482007042500248GL  2007       4          25         DJS110DJ         120070416G324440440A          TIRE                                    AMTR  500   ECLIPSE500  05614K5GL                                                               LT MLG          BLOWN           C      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      EA27110DJ41                     000007                                  LT MAIN WHEEL AND TIRE ASSEMBLY BLEW OUT DURING TAXI.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           1L72 3F    RTEXPA1L72                     
20070302000352007030200035NM  2007       3          2          DU4R2007060      120070227G5710                VENT                                    DOUG  MD80  MD83        3023681NM                                                               LT WING         CORRODED        B  BWIAK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15789BV                       49789                                   S/O 244001 N/R 22938 N/R 22839 CORROSION ON I/B END OF EXISTING REPAIR ON AFT L/H WING VENT BOX REPAIRED BY REMOVING EXISTING DOUBLER, FLAP PEENED CORROSION IAW BWIA DWG BW-D9-57-A/5120 AND MD-80 MM 20-10-10. FABRICATED AND INSTALLED DOUBLER 41.9 X 3.5, FILLER 1.5 X .9 FROM 2024-T3 0.100 IAW BWIA DWG BW-D9-57-A/5120 AND MD-80 SRM 51-30-2 AND 51-30-1.                                                                                                                                                                                                                                                                                                                                                                                2L72 4F    RT                             
20071101001922007110100192CE  2007       11         1          EA25070193       120071019G32203400            LANDING GEAR                            CESSNA182   182P        2075816CE  CONT  O470  O470S       17026SO                              FWD RT          DEPARTED        G      O   OTHER                                                                                           D  INFLIGHT SEPARATION                                                           CLCLIMB          1                      EA256506M30                     18263735                                AIRCRAFT ALTERED IAW STC SA02031NY INSTALLATION OF 3400 AMPHIBIOUS FLOATS APPROXIMATELY 36 HOURS PRIOR TO OCCURRENCE. ON TAKEOFF FROM HARD SURFACE RUNWAY, RT FORWARD WHEEL AND SUPPORT ASSY DEPARTED LANDING GEAR STRUT. WHEEL AND SUPPORT ASSY LT GEAR STRUT CLEANLY AND ONLY DAMAGE APPEARED TO BE FROM GROUND IMPACT.  AIRCRAFT MADE SUBSEQUENT WATER LANDING WITHOUT INCIDENT. INSPECTION OF AIRCRAFT SHOWS THAT WHEEL AND SUPPORT ARE ATTACHED TO GEAR STRUT THROUGH USE OF A SPRING AND PAWL MECHANISM.  IMPOSSIBLE TO TELL IF SPRING OR PAWL FAILED WITHOUT FURTHER DISASSEMBLY. POSSIBLE THAT ASSEMBLY WAS OVER-GREASED OR GREASED TOO QUICKLY, AS PLACARD NEAR GREASE FITTING WARNS TO (APPLY GREASE SLOWLY).  WILL FORWARD THIS INFOR1H71 3O3  ONTTA13    E273                 
20080110001302008011000130SO  2008       1          10         EA25200802753    120071218G534062522000        FITTING                                 PIPER PA34  PA34200     7103405SO  LYC   O360  IO360A1A    41514EA                              FUSELAGE        CORRODED        G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA251031U9840                   347250012                               DURING WINDSHIELD REPLACEMENT, NOTED STEEL FITTINGS AND ATTACHING HARDWARE WERE SUBSTANTIALLY CORRODED. FUNCTION OF FITTINGS IS ATTACHMENT OF FUSELAGE OVERHEAD (A) PILLAR TO FUSELAGE STRUCTURE PROPER. OTHER THAN SOME RIVETS THROUGH THE SKINS, THESE FITTINGS ARE THE MAJOR STRUCTURAL ATTACHMENTS OF THE CABIN OVERHEAD TO THE FUSELAGE STRUCTURE. CAUSE OF CORROSION APPEARS TO BE FOAM INSULATION, HELD IN CONSTANT CONTACT WITH THE FITTINGS, BECOMING AND REMAINING WET THROUGH LEAKING WINDSHIELDS. COMPANY MECHANIC RECOMMENDS REMOVING PORTION OF INSULATION IN CONTACT WITH FITTINGS AND INSPECTING THIS AREA AT EACH 100 HOUR/ANNUAL INSPECTION. ACCESS IS GAINED THROUGH SIMPLE REMOVAL OF INTERIOR WINDSHIELD PILLAR TRIM PANELS1L72 3O3  O  A7SO    1E10                 
20080122000112008012200011SO  2008       1          22         EA25200803022    120071218G534068257000        FITTING                                 PIPER PA34  PA34200     7103405SO  LYC   O360  IO360A1A    41514EA                                              CORRODED        G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA251031U9840                   347250012                               DURING WINDSHIELD REPLACEMENT, MECHANIC NOTED STEEL FITTINGS AND ATTACHING HARDWARE WERE SUBSTANTIALLY CORRODED. FUNCTION OF FITTINGS IS ATTACHMENT OF FUSELAGE OVERHEAD A PILLAR TO FUSELAGE STRUCTURE PROPER. OTHER THAN SOME RIVETS THROUGH THE SKINS, THESE FITTINGS ARE THE MAJOR STRUCTURAL ATTACHMENTS OF THE CABIN OVERHEAD TO THE FUSELAGE STRUCTURE. CAUSE OF CORROSION APPEARS TO BE FOAM INSULATION, HELD IN CONSTANT CONTACT WITH THE FITTINGS, BECOMING AND REMAINING WET THROUGH LEAKING WINDSHIELDS. MECHANIC RECOMMENDS REMOVING PORTION OF INSULATION IN CONTACT WITH FITTINGS AND INSPECTING THIS AREA AT EACH 100 HOUR/ANNUAL INSPECTION. ACCESS IS GAINED THROUGH SIMPLE REMOVAL OF INTERIOR WINDSHIELD PILLAR TRIM PANELS.1L72 3O3  O  A7SO    1E10                 
20070625000042007062500004EU  2007       6          25         EBVR200700000    120070609G274212342           MOTOR           AMD                     AMD   FALC10FALCON10    2730101EU                                                               BRAKE UNIT      FAILED          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL0955DG      863   103         207                                     FAILED NORMAL MOTOR TRAVEL TIME CHECKS. SUSPECT NORMAL MOTOR BRAKE WAS PREVIOUSLY ASSEMBLED INCORRECTLY CAUSING DAMAGE TO MOTOR.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F      A33EU                        
20070712001262007071200126NE  2007       7          12         EWCR070700002    220070703G7200                ENGINE                                  CESSNA500   560CESSNA   2076750CE  PWA   JT15  JT15D5      52112NE                              LEFT            UNKNOWN         B  EWCAEA  ENGINE SHUTDOWN         UNSCHED LANDING                                                         XYTENGINE FLAMEOUT           ENGINE STOPPAGE           ENGINE CASE PENETRATION   CLCLIMB          1                      EA39757CK                       5600028     108055                      FOLLOW UP REPORT AFTER PILOT REPORT TO FSDO OF (LARGE) BIRD STRIKE TO INLET AND INGESTION INTO LT ENGINE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F4  FRTA22CE   E25EA                
20070821002812007082100281    2007       8          21         EY2R0097613      320070718G61107826761         BEARING                                 EMB   120   EMB120      3260201SO                                                               BLADE           CORRODED        B  EY2RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL03                                                                    PROPELLER BLADE BEARING CORRODED.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4T    RTA31SO                        
20071130001112007113000111SO  2007       11         30         FA20071025001    220071025G7414655845          GEAR            SLICK       4309        DIAMONDA20  DA20C1      2990001GL  CONT  O240  IO240B      17063SO  SNSNCHW69EK W69EK63     EA  MAGNETO         BROKEN          D      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      WP25629DC1134 490   99052002    C0129       806243      AE4420          IN CRUISE,  NOTICED DROP IN OIL PRESSURE BELOW YELLOW ARC NOT INDICATED DURING RUN UP & TAKEOFF.  MADE PRECAUTIONARY RETURN TO HOME BASE & LANDED APPROX 7-8 MINUTES AFTER NOTICING DROP IN OIL PRESSURE.  OIL PRESSURE INDICATED ZERO PSI DURING TAXI BACK TO HANGER.  PRELIMINARY INSP &MAINT PERFORMED.  REMOVED OIL FILTER, CUT OPEN  AND INSPECTION SATISFACTORY, NO METAL PRESENT.  REPLACED OIL PRESSURE TRANSDUCER WITH NEW AND RAN ENGINE.  LOW OIL PRESSURE STILL INDICATED.  CHECKED OIL PRESSURE WITH CALIBRATED SHOP GAGE.  LOW OIL PRESSURE INDICATED.  REMOVED AND CHECKED OIL PRESSURE RELIEF VALVE, FOUND FERROUS METAL CHUNK APPROX SIZE .060 DIA AT VALVE SEAT.  RAN ENGINE & OIL PRESSURE IN INDICATED IN THE GREEN ARC.  IN1L71 3O3  ONTTA4CH   E7SO    5  NTA4CH    
20080111002322008011100232GL  2008       1          11         FAA010208001     120071130G2497                UNKNOWN                                 CIRRUSSR    SR22        2130001GL  CONT  O550  IO550*           SO                              PFD             MALFUNCTIONED   D      O   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      SW99123DV                       1313                                    PFD AND GPS/NAV1 BOTH REBOOTED AT THE SAME TIME.  RESTARTED WITHOUT GOING THROUGH EITHER ITS STANDARD INITIALIZATION OR ITS FAST START ROUTINE.  THE AUTOPILOT SEEMED TO BE STILL ENGAGED BUT THE VS SELECTION, QNH, ALTITUDE PRE-SELECT AND HEADING WERE RESET AND THESE RESET VALUES APPEARED TO BE PASSED TO THE AUTOPILOT.  THIS OCCURRED AT LOW LEVEL, IN THE CLIMB, IN IMC WITH HEADING AND ALTITUDE ACQUIRE SET ON THE AUTOPILOT.  THERE WAS SOME ELECTRICAL ACTIVITY  WITHIN 10 MILES.  THE AIRCRAFT WAS FLOWN SAFELY BACK TO THE DEPARTURE FIELD USING BACKUP INSTRUMENTS.  ENGINEERS SUSPECT EITHER A SPIKE FROM ALTERNATOR 2 OR MFG BELIEVES THIS COULD BE A BONDING ISSUE AND WAS CAUSED BY STATIC.  MFG INCIDENT REF: 871500HQ.  EN1L71 3O3  ONTA00009CHE3SO                 
20080111002332008011100233CE  2008       1          11         FAA010208002     120071102G3233MS28775218      O-RING                                  CESSNA425   425         2076018CE  PWA   PT6   PT6A60A     52043NE                              NLG ACTUATOR    DISINTEGRATED   B  YN8RA   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            LDLANDING        1                      CE071262K                       4250234                                 AN EMERGENCY LANDING MADE, DID NOT GET A GREEN DOWN AND LOCK INDICATION FOR MLG.  MADE SAFE LANDING.  FOUND RT MLG NOT DOWN AND FULLY LOCKED.  DISCOVERED BLOW DOWN BOTTLE FULLY DISCHARGED,  DISCOVERED HYDRAULIC RESERVOIR EMPTY.  JACKED ACFT & ATTEMPTED TO MANUAL EXTEND RT MLG BY HAND.  DISCOVERED THAT RT MLG WAS HYDRO-LOCKED.  BLED OFF HYDRAULIC PRESSURE FROM ACTUATOR, ABLE TO ENGAGE DOWNLOCK.  , JACKED ACFT AND TRIED TO CYCLE GEAR SYSTEM.  GEAR WOULD NOT CYCLE UP OR DOWN.  TROUBLESHOT AND DISCOVERED NLG ACTUATOR, PISTON O-RINGS HAD COME APART AND WENT THRU THE ENTIRE MLG AND PLUGGED SYSTEM.  PRIOR TO FLIGHT, FWD SEALS ON ACTUATOR HAD BEEN REPLACED DUE TO EVIDENCE OF HYD LEAK.  AFTER SEALS HAD BEEN REPLACED, PE1L72 3T4  TRTA7CE    E4EA                 
20080111002352008011100235SO  2008       1          11         FAA010208003     220071219G8550SAS6250         VALVE                                   BBAVIA7     7EC         2110120SW  CONT  O200  O200A       17020SO                              OIL TANK        DAMAGED         G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL13274AC1                      10142007    256377                      INSTALLED OIL QUICK DRAIN VALVE PN SG250 ON NEW AIRCRAFT/ ENGINE.  AIRCRAFT FLEW APPROX 1 HOUR.  OIL LEAK NOTICED FROM DRAIN VALVE.  REMOVED VALVE TO FIND VALVE SNAP RING IN OIL DRAINED FROM ENGINE AND VALVE O-RING DAMAGED.  ONE CUT THROUGH AND THE OTHER NICKED.  INVESTIGATION REVEALED OIL DRAIN VALVE CONTACTED THE EDGE OF THE OIL PICK-UP TUBE CAUSEING DAMAGE.  SUBJECT VALVE IS NOT COMPATABLE WITH THE O200A66B ENGINE.  (K)                                                                                                                                                                                                                                                                                                      1H71 3O3  O  A759    E252                 
20070703000482007070300048EU  2007       7          3          FAA070628001     120070628G6320350A32031002    GEARBOX                                 SNIAS 350   AS350B3     8680954EU  TMECA ARRIELARRIEL2B1   60056NE                              MAIN ROTOR      MAKING METAL    B      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      EA17808CP161                    4151        23335                       MGB CHIP LIGHT CAME ON IN FLIGHT. REMOVED CHIP PLUGS FROM THE MGB AND THE MAST FOUND PARTICALS ON THE MGB PLUG LESS THAN LIMITS CALLED OUT IN AEC AS350B3 SPM 20.08.01.601 NOTHING ON THE MAST PLUG.PERFORMED 10 MIN. HOVER AND RECHECKED CHIP PLUGS AS PER AEC AS350B3 MWC 05.53.00.608 NO MORE PARTICALS FOUND AND NO RE-ACCURANCE OF THE CHIP LIGHT.                                                                                                                                                                                                                                                                                                                                                                                         1G71 3U3  U  H9EU    E00054EN             
20080111001442008011100144EA  2008       1          11         FAA122707001     220071111G8530AEL65102SN041   CYLINDER HEAD                           CESSNA172   172P        2072436CE  LYC   O320  O320D2J     41508EA                              ENGINE          CRACKED         D      B   EMER. DESCENT                                                                                   YJ ENGINE STOPPAGE           WARNING INDICATION                                  CLCLIMB          1                      SO19622811083                   17275242    L1236139A                   HEAD CAME OFF BARRELL OF CYLINDER P/N AEL65102 SN0.41 S/N 20255-13 1083.3 HOURS ON CYLINDER SINCE INSTRUCTION OF 10/5/04 (HEAD, BARRELL SEPARATED).                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H71 3O3  ONT3A12    E274                 
20080111002222008011100222CE  2008       1          11         FAA122808001     120071228G3220AN7520          BOLT                                    BEECH 18    H18         1151012CE  PWA   R985  R985*       52008NE                              NLG             SHEARED         G      O   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      SO19117ME                       BA638                                   DURING THE INVESTIGATION.  IT WAS DISCOVERED THAT THE REMAINDER OF THE BOLT FOR NOSE GEAR RETRACT PUSH PULL TUBE TO CANTILEVER ARM FOR DRAG BRACE HAD SHEARED ON (2) DIFFERENT OCCASIONS FOR REASONS UNDETERMINED.  THE OPERATOR ALSO OPERATES (2) OTHER VOLPAR TRICYCLE GEARED AC, A BOLT FROM ONE OF THOSE AC WAS REMOVED TO FIND SCORE MARKS IN THE SHANK OF THE BOLT IN THE SAME VICINITY OF THE SHEAR POINTS OF THE INCIDENT AIRCRAFT BOTH AIRCRAFT HAVE SIMILAR AIRFRAME TT.  IT WAS DISCUSSED WITH THE OPERATOR ON TECHNIQUES AND MISTAKES MADE DURING LANDING AND IT WAS DISCOVERED THAT IF THE AIRCRAFT IS EMPTY/LIGHT AND THE PILOT ALLOWS THE NOSE TO SETTLE TOO SOON IF COULD INDUCE A PORPOSING EFFECT THAT COULD PUT LARGE SHEAR L1L72 3R3  R  A765    5E1                  
20070703000062007070300006GL  2007       7          3          FAA20070618001   320070618G6114                HUB                                     PIPER PA34  PA34200     7103405SO                                   HARTZLHCC2Y HCC2Y*      GL  PROPELLER       FAILED          D      A   UNSCHED LANDING                                                                                 D  INFLIGHT SEPARATION                                                           CRCRUISE         1                      SO1515156                       347350028                               ON JUNE 6,2007 PIPER SENECA N15156 WHILE IN CRUSE ON A TRAINING FLIGHT HAD A CATROSTRIFIC FAILRUE OF THE PROPELLER HUB CAUSING THE LOSS INFLIGHT OF ONE OF THE PROPELLER BLADES. THE FAILURE OF THE HUB WAS OF THE SAME KIND ADDRESSED IN AD2006-18-15 EXCEPT THE FAILURE IN THIS CASE PROPAGATED FROM THE AFT HALF OF THE HUB WHICH IS NOT PART OF THE AD'S REQUIRED INSPECTION. EDDY CURRENT INSPECTION IN ACCORDANCE WITH THE AD HAD BEEN PREFORMED 17 HOURS PRIOR TO THE FAILURE. INSPECTOR FOR HARTZELL PROPS CONFIRMED THIS INFORMATION AFTER INSPECTING THE HUB ALONG WITH FAA AND NTSB INVESTIGATORS ON JUNE 9TH, 2007.                                                                                                                 1L72 3O      A7SO            5  CP920     
20080104002392008010400239SO  2008       1          4          FAA2007121001    120071210G2130SYLC518361      ACTUATOR                                EMB   135   EMB135BJ    3260306SO  ALLSN AE300 AE3007A          GL                              RAM AIR         SHORTED         B      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      SO11124LS                       14500948                                WHILE IN FLIGHT THE AIRCRAFT EXPERIENCED AND NR1 PAC OVLD INDICATION WITH SUBSEQUENT NR1 PAC AUTO SHUTDOWN AS A RESULT THE FLIGHT CREW MADE AN IN-FLIGHT DIVERSION AND UNSCHEDULED LANDING.  PERFORMED DOWNLOAD OF THE CENTRAL MAINTENANCE COMPUTER WHICH REVEALED 1 OCCURRENCE OF NR1 PAC OVERTEMP AND 63 OCCURRENCES OF NR2 PAC OVERTEMP.  TROUBLESHOOTING REVEALED THAT THE LT AND RT PAC OVERTEMP SWITCHES FAILED BENCH CHECK.  BOTH SWITCHES WERE REPLACED WITH NEW SWITCHES.  DURING THE PERFORMANCE OF THE PAC SYSTEM OPERATIONAL TEST IT WAS DISCOVERED THAT THE RT RAM AIR ACTUATOR HAD AN ELECTRICAL SHORT CAUSING THE CIRCUIT BREAKER TO (POP).  REPLACED THE RT RAM AIR ACTUATOR AND PERFORMED PAC SYSTEM OPERATIONAL TESTS.  DURING2L72 4F4  FRT        TE6CH                
20070125002542007012500254    2007       1          25         FCPR20070001     420070105G34165934PA1         ALTIMETER                                                                                                                               COCKPIT         BROKEN          B  FCPRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM09                                                                    BAROMETRIC SCALE DOES NOT MOVE WITH DIAL INDICATION RESULTING IN INACCURATE READINGS THROUGH OUT THE ENTIRE RANGE.  ALLOWS GEARS TO DISENGAGE INTERNALLY.  PART IS REMOVED FROM AIRCRAFT AT DISCOVERY.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    
20070214001432007021400143SO  2007       2          14         FCPR20070003     220070131G8520655516          GEAR                                    BEECH 36    A36         1151604CE  CONT  O550  IO550B           SO                              CAMSHAFT        BROKEN          B  FCPRA   UNSCHED LANDING                                                                                 YJ ENGINE STOPPAGE           WARNING INDICATION                                  CRCRUISE         1                      NM0918391200                    E1113       685492                      ENGINE FAILED IN FLIGHT.  FOUND 13 TEETH MISSING FROM CAMSHAFT GEAR P/N 655516.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L71 3O3  O  3A15    E3SO                 
20080110000572008011000057    2008       1          10         FCPR200700118    220071227G732210603511        CARBURETOR                                                                                                                              ENGINE          NO TEST         B  FCPRO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM09                                                                    CARBURETOR FAILED THE STUMBLE TEST, FOUND TO BE ACCELERATOR CIRCUIT.  PART RETURNED TO MFG FOR FURTHER EVALUATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   
20080114000852008011400085    2008       1          14         FCPR200700125    220071227G732210603511        CARBURETOR                                                                                                                              ENGINE          NO TEST         B  FCPRK   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      NM09                                                                    CARBURETOR FAILED THE STUMBLE TEST, FOUND TO BE ACCELERATOR CIRCUIT.  PART RETURNED TO MFG FOR FURTHER EVALUATION.  (K)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   
20080108003512008010800351EA  2008       1          8          FCPR20070110     220071208G7314RB15985         DIAPHRAGM       ROMEC       RG179801M   PIPER PA23  PA23250     7102308SO  LYC   O540  TIO540C1A   41532EA                              FUEL PUMP       FAILED          B  FCPRK   NONE                                                                                            O  OTHER                                                                         UKUNKNOWN        1                      NM09          294   C5518       277754126   L853261A                    PUMP VALVE REGULATOR DIAPHRAGM FAILED AT GUIDE PIN, PUMP WOULD NOT FUNCTION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1L72 3O3  O  1A10    E14EA                
20070412000062007041200006CE  2007       4          12         FMOR20070001     120070409G323057412025        UPLOCK HOOK                             CESSNA414   414A        2075907CE  CONT  O520  TSIO520*    17040SO                              ZONE 700        CRACKED         B      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                CRCRUISE         1                      SO156161Z7024                   414A0019                                PILOT REPORTED THAT THE LANDING GEAR CAME UNHOOKED FROM THE UP POSITION IN FLIGHT.  THE GEAR WAS EXTENDED AND THE AIRCRAFT LANDED.  THE AIRCRAFT WAS JACKED AND THE GEAR CYCLED TO THE UP POSITION.  WHEN ALL (3) UPLOCK SWITCHES WERE MADE THE RT MAIN GEAR FELL FROM THE WHEEL WELL.  A DISTORTED AND CRACKED UPLOCK HOOK WAS FOUND.  THE CRACK WAS FROM THE CENTER OF THE HOOK TO THE HOLE FOR THE UPLOCK SWITCH.                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  A7CE    E8CE                 
20070413001112007041300111CE  2007       4          13         FMOR20070002     120070410G2731NAS302665170    CONTROL CABLE                           BEECH 90    C90A        1152911CE  PWA   PT6   PT6*        52043EA                              FS 216          FRAYED          B      O   OTHER                                                                                           S  AFFECT SYSTEMS                                                                CRCRUISE         1                      SO15120TT5072                   LJ1073                                  THE ELEVATOR TRIM CABLE BEGAN UNRAVELING JUST FORWARD OF THE CABIN DOOR.  FROM THERE THE CABLE BEGAN BINDING IN A PULLEY UNDERNEATH THE PILOT'S SIDE FORWARD FACING PASSENGER CHAIR CAUSING STIFFNESS OF OPERATION BY HAND AND THE MALFUNCTION OF THE ELECTRIC TRIM SYSTEM LEADING TO THE EVENTUAL INOPERATION OF THE ELEVATOR TRIM.  THE ISSUE MOST LIKELY AROSE DUE TO AGE.  WHILE UNDER THE SCHEDULED INSPECTION PROGRAM OUTLINED BY MFG THE INSPECTION OF THESE AREAS OCCURS ONCE EVERY (2) YEARS OR 800 HOURS.                                                                                                                                                                                                                             1L72 3T3  TRT3A20    E2NE                 
20070906000822007090600082CE  2007       9          6          FMOR20070003     120070828G2731NAS302665170    CONTROL CABLE                           BEECH 90    C90         1152913CE  PWA   PT6   PT6A60A     52043NE                              FS 216          FRAYED          B  FMORK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO15725AR6415 310               LJ879                                   THE ELEVATOR TRIM CABLE WAS FOUND TO HAVE SEVERAL BROKEN STRANDS AND BEGINNING TO UNRAVEL WHERE IT GOES AROUND THE ELEVATOR TRIM ACTUATOR CAPSTAND. THIS CONDITION WAS MOST LIKELY CAUSED BY AGE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L72 3T4  T  3A20    E4EA                 
20070425002602007042500260CE  2007       4          25         FMOR477K         120070409G323057412025        UPLOCK HOOK                             CESSNA414   414A        2075907CE  CONT  O520  TSIO520*    17040SO                              MLG             DISTORTED       B      O   OTHER                                                                                           O  OTHER                                                                         CRCRUISE         1                      SO156161Z7024                   414A0019                                PILOT REPORTED THAT THE LANDING GEAR CAME UNHOOKED FROM THE UP POSITION IN FLIGHT.  THE GEAR WAS EXTENDED AND THE AIRCRAFT LANDED.  THE AIRCRAFT WAS JACKED AND THE GEAR CYCLED TO THE UP POSITION.  WHEN ALL (3) UPLOCK SWITCHES WERE MADE THE RT MAIN GEAR FELL FROM THE WHEEL WELL.  A DISTORTED AND CRACKED UPLOCK HOOK WAS FOUND.  THE CRACK WAS FROM THE CENTER OF THE HOOK TO THE HOLE FOR THE UPLOCK SWITCH.                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  A7CE    E8CE                 
20080111001342008011100134    2008       1          11         FPFC20070113     220071226G732210603511        CARBURETOR                                                                                                                                              NO TEST         B  FCPRK   NONE                                                                                            L  NO TEST                                                                       ININSP/MAINT     1                      NM09                                                                    CARBURETOR FAILED THE STUMBLE TEST, FOUND DEFECTIVE ACCELERATOR CIRCUIT. PART RETURNED TO PRECISION FOR FURTHER EVALUATION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               
20070824003242007082400324CE  2007       8          24         GC4N200700001    120070824G3233                ACTUATOR                                RAYTHN390   390         7150030CE  WILINTFJ44  FJ442A           GL                              NLG             FAULTED         D      O   OTHER                                                                                           J  WARNING INDICATION                                                            LDLANDING        1                      GL077088S                       RB188                                   AFTER COMPLAINT FROM THE PILOT OF NOT GETTING A NOSE LANDING GEAR DOWN LIGHT STRAIT AWAY, PLACED THE AIRCRAFT ON JACKS AND CARRIED OUT 4 RETRACTIONS WHICH RESULTED IN 100 PERCENT FAILURE OF THE NOSE LANDING GEAR FULLY EXTENDING, AFTER FAULT FINDING WE BELIEVE THE NOSE LANDING GEAR ACTUATOR TO BE FAULTY, A PART IS ON ORDER FROM MFG.                                                                                                                                                                                                                                                                                                                                                                                                   1L72 3F4  FRTA00010WIE3GL                 
20080111002842008011100284SO  2008       1          11         GW4R200700001    120071210G2130SYLC518361      ACTUATOR                                EMB   135   EMB135BJ    3260306SO  ALLSN AE300 AE3007A          GL                              RAM AIR         FAILED          B  CWQAA   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      SO11124LS                       14500948                                DURING FLIGHT, AIRCRAFT EXPERIENCED AND NR 1 PACK OVLD INDICATION WITH SUBSEQUENT NR 1 PACK AUTO SHUTDOWN AS A RESULT MADE AN IN-FLIGHT DIVERSION AND UNSCHEDULED LANDING.  PERFORMED DOWNLOAD OF THE CENTRAL MAINTENANCE COMPUTER WHICH REVEALED 1 OCCURRENCE OF NR 1 PACK OVERTEMP AND 63 OCCURRENCES OF NR 2 PACK OVERTEMP.  TROUBLESHOOTING REVEALED THE LT AND RT PACK OVERTEMP SWITCHES FAILED BENCH CHECK.  BOTH SWITCHES WERE REPLACED.  DURING PERFORMANCE OF PACK SYSTEM OPS TEST, IT WAS DISCOVERED THAT THE RT RAM AIR ACTUATOR HAD AN ELECTRICAL SHORT CAUSING THE CIRCUIT BREAKER TO TRIP.  REPLACED THE RT RAM AIR ACTUATOR AND PERFORMED PAC SYSTEM OPS TESTS.  DURING THE ABOVE CENTRAL MAINTENANCE COMPUTER DOWNLOAD, 17 OCCUR2L72 4F4  FRT        TE6CH                
20080108003262008010800326SO  2008       1          8          GW4R237272       120071129G2130SYLC518361      ACTUATOR                                EMB   135   EMB135BJ    3260306SO  ALLSN AE300 AE3007A          GL                              RT RAM AIR      SHORTED         B      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      SO11124LS                       14500948                                WHILE IN FLIGHT THE AC EXPERIENCED AND NR1 PAC OVLD INDICATION WITH SUBSEQUENT NR1 PAC AUTO SHUTDOWN AS A RESULT THE FLIGHT CREW MADE AN IN-FLIGHT DIVERSION AND UNSCHEDULED LANDING.  DOWNLOAD OF THE COMPUTER REVEALED 1 OCCUR OF NR1 PAC OVERTEMP AND 63 OF NR2 PAC OVERTEMP.  LT AND RT PAC OVERTEMP SWITCHES FAILED BENCH CHECK.  BOTH SWITCHES WERE REPLACED.  DURING THE PAC SYSTEM OPS TEST, THE RT RAM AIR ACTUATOR HAD AN ELECTRICAL SHORT CAUSING THE CIRCUIT BREAKER TO POP.  REPLACED THE RT RAM AIR ACTUATOR AND PERFORMED PAC SYSTEM OPERATIONAL TESTS.  DURING THE COMPUTER DOWNLOAD, 17 OCCURRENCES OF A NR1 PRECOOLER TEMP CONTROL SYSTEM FAIL MESSAGE WAS NOTED.  ACCESSED FAN AIR TEMPERATURE THERMOSTATS FOR TROUBLESHOOTIN2L72 4F4  FRT        TE6CH                
20080108003332008010800333SO  2008       1          8          GW4R237272NR1    120071129G2150SYLC518361      SWITCH                                  EMB   135   EMB135BJ    3260306SO  ALLSN AE300 AE3007A          GL                              A/C PACK        FAILED          B      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            UKUNKNOWN        1                      SO11124LS                       14500948                                IN FLIGHT AC EXPERIENCED AND NR1 PAC OVLD IND WITH NR1 PAC AUTO SHUTDOWN.  FLT CREW MADE AN IN-FLIGHT DIVERSION AND UNSCHEDULED LANDING.  DOWNLOAD OF THE COMPUTER REVEALED 1 OCCUR OF NR1 PAC OVERTEMP AND 63 NR2 PAC OVERTEMP.  LT AND RT PAC OVERTEMP SWITCHES FAILED BENCHCHECK.  BOTH SWITCHES WERE REPLACED.  DURING THE PAC SYSTEM OPS TEST DISCOVERED THE RT RAM AIR ACTUATOR HAD AN ELEC SHORT CAUSING THE CB TO POP.  REPLACED THE RT RAM AIR ACTUATOR AND PAC SYSTEM OPS TESTS.  DURING THE COMPUTER DOWNLOAD, 17 OCCURRENCES OF A NR1 PRECOOLER TEMP CONTROL SYSTEM FAIL MESSAGE WAS NOTED.  ACCESSED FAN AIR TEMPERATURE THERMOSTATS FOR TROUBLESHOOTING AND UPON REMOVAL IT WAS NOTED THAT THE AMBIENT AIR TEMPERATURE PORTS ON EA2L72 4F4  FRT        TE6CH                
20070227000542007022700054CE  2007       2          27         HAG07001         120070223G57532322330177      SUPPORT BRACKET GARKENYON   26044       LEAR  60    60LEAR      5170707CE  PWA   305   PW305            NE                              FLAP ACTUATOR   FAILED          B  H51RO   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      NM03252FX5936       0295        196                                     DURING FLAP OPERATION, FLAP ACTUATOR SUPPORT BRACKETS FAILED CAUSING FLAP ACTUATOR TO DAMAGE LT WING RIB SEGMENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA10CE   E35NE                
20070309000012007030900001CE  2007       3          9          HAG07002         120070222G55324555030001804   PANEL                                   LEAR  45    45LEAR      5170805CE  GARRTTTFE731TFE7312B         WP                              VERTICAL STAB   CRACKED         B  H51RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM03451WM5571                   091                                     DURING INSPECTION, FOUND RT SIDE VERTICAL STABILIZER CENTER BULLET FAIRING PANEL CRACKED IN 5 LOCATIONS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F4  FRTT00008WIE6WE                 
20070312000582007031200058CE  2007       3          12         HAG2007001       120070223G57402322330177      SUPPORT BRACKET GARKENYON   26044       LEAR  60    60LEAR      5170707CE  PWA   305   PW305A      52128NE                              ZONE 500        FAILED          B  H51RO   OTHER                                                                                           FJ FLT CONT AFFECTED         WARNING INDICATION                                  APAPPROACH       1                      NM03252FX5936       0295        196                                     DURING FLAP OPERATION, FLAP ACTUATOR SUPPORT BRACKETS FAILED CAUSING FLAP ACTUATOR TO DAMAGE LT WING RIB SEGMENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA10CE   E35NE                
20070226001642007022600164CE  2007       2          26         HAGGAN07001      120070223G57402322330177      SUPPORT BRACKET GARKENYON   26044       LEAR  60    60LEAR      5170707CE                                                               ZONE 500        FAILED          B  H51RO   OTHER                                                                                           F  FLT CONT AFFECTED                                                             APAPPROACH       1                      NM03252FX5936       0295        196                                     DURING FLAP OPERATION, FLAP ACTUATOR SUPPORT BRACKETS FAILED CAUSING FLAP ACTUATOR TO DAMAGE LT WING RIB SEGMENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F    RTA10CE                        
20070613001712007061300171NE  2007       6          13         IG0R200743437    220070508G73222526385         BELLOWS         ALIDSG      DPF2                                           PWA   PT6   PT6A135     52043NE                              FUEL CONTROL    FAILED          B      O   OTHER                                                                                           R  PARTIAL RPM/PWR LOSS                                                          TXTAXI/GRND HDL  1                      NM03          92    A59386                  PCE92578                    THE FUEL CONTROL (FCU) P/N 3244777-4-3-2, S/N A59386 DIRECTED THE ENGINE TO MIN FLOW SHORTLY AFTER LANDING WITHOUT ANY FURTHER POWER LEVER RESPONSE.  THE CONTROL TSO IS 92.8.  THIS CONTROL WAS LAST SERVICED BY INTERNATIONAL GOVERNOR SERVICES (IGS) IN NOV 2006. THE AS RECEIVED TEST REVEALED FUEL FLOWS HAD DROPPED BELOW SCHEDULE AT ALL TEST POINTS EXCLUDING MIN FLOW AND MAX FLOW (THESE ARE BOTH PHYSICAL HARD STOPS).  FURTHER INVESTIGATION REVEALED THAT THE EVACUATED SECTION OF THE BELLOWS (HONEYWELL P/N 2526385) WAS BREACHED (LOST THE VACUUM). THE INSPECTION CRITERIA FOR THE EVACUATED SECTION OF THE BELLOWS INVOLVES MEASURING THE BELLOWS HEIGHT AND COMPARING THE READING WITH THAT RECORDED DURING ORIGINAL MANUFACT       4  T          E4EA                 
20070613002032007061300203EA  2007       6          13         IG0R200743667    220070509G73212523973         BEARING         ALIDSG      DPF2                                           PWA   PT6   PT6*        52043EA                              FCU             FAILED          B      K   NONE                                                                                            O  OTHER                                                                         NRNOT REPORTED   1                      NM03                C75067                  PCEPH0218                   ALLIED SIGNAL AEROSPACE (HONEYWELL) FUEL CONTROL UNIT (FCU)P/N 4138008-3, S/N C75067 RECEIVED FOR OVERHAUL AT INTERNATIONAL GOVERNOR SERVICES (IGS) CRS IG0R976N EXPERIENCED A SPOOL BEARING (P/N 2523973) FAILURE.  THE FCU WAS REMOVED FROM PT6A ENGINE S/N PCE-PH0218.  CONTROL APPEARS TO BE FIRST RUN OVERHAUL, HOWEVER, WE ARE UNABLE TO OBTAIN TIME SINCE NEW. IGS WILL FORWARD THE BEARING TO HONEYWELL FOR REVIEW.  NOTE: THIS IS THE 5TH OR 6TH BEARING WE HAVE SEEN FAIL IN THE PAST 6 MONTHS OR SO.                                                                                                                                                                                                                                        3  T          E2NE                 
20070615001722007061500172EA  2007       6          15         IG0R200746139    220070518G73222523629         HOUSING         HONEYWELL   DPF2                                           PWA   PT6   PT6*        52043EA                              FUEL CONTROL    CORRODED        B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM03          2452  309482                                              CORROSION ON FLOW BODY METERING VALVE OPERATING LEVER COVER, EXCEEDS LIMITS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           3  T          E2NE                 
20080110001332008011000133EA  2008       1          10         IG0R200751070    220071219G73212523631         BELLOWS         HNYWL       DPF2        BEECH 90    C90         1152913CE  PWA   PT6   PT6A21      52043EA                              FCU             DAMAGED         B      E   ENGINE SHUTDOWN                                                                                 RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      NM03          54    A33630                                              ENGINE WENT TO IDLE IN FLIGHT. FAILED BELLOWS BENCH TEST. BELLOWS BREACHED. UPON FURTHER INSPECTION THERE WAS NO PHYSICAL DAMAGE TO THE BELLOWS HOWEVER THERE WAS CORROSION ON THE TOP OF THE BELLOWS AND AT THE FIRST CONVOLUTION. REPLACED BELLOWS AND RECALIBRATED FUEL CONTROL UNIT.                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3T4  T  3A20    E4EA                 
20071205000612007120500061CE  2007       12         5          IWP2720085003    120071123G3230608100961       SPRING          BEECH                   BEECH 60    B60         1153605CE                                                               MLG DOWNLOCK    MISINSTALLED    G      O   OTHER                                                                                           G  MULTIPLE FAILURE                                                              LDLANDING        1                      WP27408FA                       P434                                    THIS AIRCRAFT EXPERIENCED A BENT /DAMAGED RT MAIN GEAR RETRACT ROD ASSEMBLY P/N 60-810057-617. A CURRENT OVERLOAD OF THE LANDING GEAR MOTOR CIRCUIT. THE RT MAIN GEAR FAILED TO EXTEND. THE EMERGENCY GEAR FAILED TO ALSO EXTEND THE RETRACTED MAIN. AC WAS FORCED TO LAND GEAR UP.  INVESTIGATION REVEALED AN IMPROPERLY INSTALLED TORSION SPRING (IN QUESTIONABLE CONDITION) ON THE RT MAIN DOWN-LOCK CABLE (JURY STRUT). INVESTIGATION REVEALED THAT THE IMPROPER INSTALLATION OF THIS SPRING RESULTED IN THE RT DOWN LOCK CABLE MOVING INTO AND ENTANGLING WITH THE DRAG BRACE KNEE JOINT AND UPLOCK DOWNLOCK PIVOT POINT DURING RETRACTION. HOWEVER- IT HAS NOT BEEN PROVEN BY FAA INSPECTORS, THAT THE IMPROPER INSTALLATION OF THIS SPRIN1L72 3O      A12CE                        
20070312000222007031200022CE  2007       3          12         J0UR200700001    120070218G2121EM6039          MOTOR                                   BEECH 90    C90A        1152911CE  PWA   PT6   PT6*        52043EA                              BLOWER          FAILED          B  J0URA   UNSCHED LANDING                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      CRCRUISE         1                      SO091103G                       LJ1475                                  AIR CONDITIONING / VENT BLOWER MOTOR ASSEMBLY FAILED CAUSING SMOKE IN COCKPIT. PILOT DECLARED EMERGENCY AND LANDED AT CLOSEST AIRPORT WITHOUT FURTHER INCIDENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 3T3  TRT3A20    E2NE                 
20070226001262007022600126    2007       2          26         JZBR710K21907    220070219G73229867500500      NUT                                     SKRSKYS76   S76C        8143008NE                                                               FILTER CAP ASSY MISSING         B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      EA25165ML           121B        760471      20026                       DURING COMPLIANCE WITH MANDATORY SB 292-73-2824, (REPLACEMENT OF FUEL FILTER DRAIN SCREW ON HMU FILTER BOWL COVER ASSEMBLY), UPON COVER REMOVAL IT WAS DISCOVERED THAT THE NUT (P/N 9867500500) AND STOP WASHER (P/N 0319910870) WERE NOT INSTALLED, MISSING FROM DRAIN SCREW THREADS ON THE INSIDE OF THE COVER ASSEMBLY. FILTER WAS REMOVED FOR FURTHER INSPECTION OF FILTER BOWL LOWER RECESSES WITH NO EVIDENCE OF MISSING PARTS INSIDE.                                                                                                                                                                                                                                                                                                    1G72 3U    NCH1NE                         
20080108003252008010800325EU  2008       1          8          LJER12102007     220071206G7414106825515       CONTACTOR                               PIPER PA44  PA44180     7104402SO  ROTAX       ROTAX*           EU                              MAGNETO         DEBONDED        B  LJERA   UNSCHED LANDING                                                                                 R  PARTIAL RPM/PWR LOSS                                                          CRCRUISE         1                      NM092163 1                                                              CONTACT POINT MATERIAL DEBONDED, POINTS WILL NOT CLOSE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3O3  I  A19S0   EXPE3I               
20070918001102007091800110EA  2007       9          18         LX5R200700006    220070913G7200                ENGINE                                  SKRSKYS76   S76B        8143007NE  PWA   PT6   PT6B36      52043EA                              RIGHT           MAKING METAL    B  LX5RA   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      GL19761LL3685                   760379      PS36144                     DURING CRUISE, SHORTLY AFTER T/O NR 2 ENG CHIP LIGHT ILLUMINATED.  APPROPRIATE CB WAS PULLED TO TRY AND (BURN) OFF FUSS, BUT LIGHT REMAINED ILLUMINATED. IAW FLIGHT MANUAL, CREW LANDED WITHOUT INCIDENT AT NEAREST AIRPORT TO INVESTIGATE CHIP LIGHT. FLIGHT CONDITIONS WERE DAY VFR, NO CLOUDS, UN-RESTRICTED VISABILITY, WIND CALM, 65 DEGREE F, AND CRUISE SPEED WAS 145KTS.   AFTER LANDING CREW CALLED HOME MAINT BASE. A MECHANIC TALKED TO OUR HOME BASE AND INSPECTED AFFECTED CHIP DETECTOR. IT WAS DETERMINED, THE SMALL SLIVERS OF METAL WERE ACCEPTABLE IAW MM. ENG WAS CLOSED UP AND THE CREW PERFORMED A GROUND RUN AND CHIP LIGHT DID NOT COME BACK ON. FLGT CONTINUED TO DESTINATION, WITHOUT OTHER INDICATIONS.  (K)          1G72 4U4  U  H1NE    E4EA                 
20070226000312007022600031SO  2007       2          26         M1144            220070208G8530                EXHAUST VALVE                           CESSNA421   421C        2076016CE  CONT  O520  GTSIO520*   17032SO                              NR 5 CYLINDER   BROKEN          B      B   EMER. DESCENT                                                                                   RJ PARTIAL RPM/PWR LOSS      WARNING INDICATION                                  CRCRUISE         1                      CE03540CA1776 612               421C0144                                PILOT REPORTED THAT RT ENGINE WAS RUNNING ROUGH IN FLIGHT. HE DID NOT SHUTDOWN ENGINE. FOUND NO COMPRESSION IN NR 5 CYLINDER ON RT ENGINE. REMOVED CYLINDER AND FOUND EXHAUST VALVE WAS BROKEN. INSTALLED OVERHAULED CYLINDER ASSEMBLY.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3O3  O  A7CE    E7CE                 
20070402001352007040200135CE  2007       4          2          M40675           120070320G274045AS610023139   ACTUATOR                                BEECH MU300 400A        1155402CE  PWA   JT15  JT15D5      52112NE                              PITCH TRIM      INOPERATIVE     C  R71AO   OTHER                                                                                           F  FLT CONT AFFECTED                                                             DEDESCENT        1                      WP05790SS1550                   RK363                                   DIFFICULTY OCCURRED UPON DESCENT. PILOT RECEIVED A WARNING PITCH TRIM WAS NOT SYNCHRONIZED WITH AUTOPILOT SYSTEM AND TO PREPARE FOR RESISTANCE WHEN AUTOPILOT IS DISCONNECTED. PITCH TRIM ACTUATOR WAS FOUND INOPERATIVE IN THE EMERGENCY MODE/AUTOPILOT MODE. REPLACED PITCH TRIM UNIT AND RETURNED AIRCRAFT TO SERVICE. THIS AIRCRAFT WAS LAST INSPECTED ON 11-9-06 AT 1408.6 TT.                                                                                                                                                                                                                                                                                                                                                             2H72 4F4  FRTA16SW   E25EA                
20070504001512007050400151GL  2007       5          4          MDR041607        120070416G3244                TIRE                                    AMTR  500   ECLIPSE500  05614K5GL                                                               LT MLG          FAILED          C      O   OTHER                                                                                           O  OTHER                                                                         TXTAXI/GRND HDL  1                      EA27110DJ41                     000007                                  LT MAIN LANDING GEAR WHEEL AND TIRE ASSEMBLY BLEW OUT DURING TAXI. WHEEL HAS BEEN QUARANTINED AND WILL BE FORWARDED TO AN INDEPENDENT INSPECTION LAB FOR FURTHER REVIEW.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        1L72 3F    RTEXPA1L72                     
20071002000292007100200029SO  2007       10         2          MINR2007918A     120070918G781040B19974        EXHAUST PIPE                            PIPER PA46  PA46350P    7104602SO  LYC   O540  TIO540AE2        EA                              ENGINE          BULGED          B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM05498MM1349                   4636149                                 THE EXHAUST CROSSOVER EXHAUST PIPE WAS FOUND SEVERELY BULGED IN THE AREA COVERED BY THE HEAT SHROUD. THE DAMAGE WAS TO THE POINT, ISSUES WERE FORMING THAT WOULD HAVE LED TO RUPTURE. IF AN EXHAUST LEAK OCCURS IN THIS AREA, THE HEAT WILL AFFECT THE MAGNETO, FUEL AND OIL LINES. IT IS HIGHLY RECOMMENDED BY MAINTENANCE PERSONNEL THAT THE HEAT SHROUD BE REMOVED AT EACH 100 HOUR INSPECTION FOR AIRCRAFT WITH MORE THAT 500 HOURS.  NR 3 CYLINDER EXHAUST RISER PN 40B19827 WAS ALSO FOUND SEVERELY BULGED. THIS CAN BE SEEN WITH THE ENGINE COWLING REMOVED WITHOUT FURTHER DISASSEMBLY.  THE LT EXHAUST TRANSITION PN 47C19848 WAS FOUND BULGED AND CRACKED. THIS CAN BE SEEN WITH A MIRROR AND FLASHLIGHT.  IF ANY DAMAGE IS FOUND ON T1L71 3O3  ORTA25SO   E14EA                
20071023000922007102300092CE  2007       10         23         N843E12007       120070801G24329036102331      HED                                     BEECH 1900  1900D       1154162CE  PWA   PT6   PT6A6       52043EA                              BATTERY         FAULTED         C      A   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      NE03843E 7178                   UE339                                   CREW LEFT STATION.  TWENTY MINUTES IN FLIGHT "BATT TIE OPEN" ANNUNCIATOR ILLUMINATED.  CREW RETURNED TO STATION WITHOUT ISSUE.  REMOVED AND REPLACED BATTERY HED.  OPS CHECK GOOD.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              2L72 4T3  TRTA24CE   E4EA                 
20080114000582008011400058CE  2008       1          14         ODAA121907001    120071219G5510                ACCESS PANEL                            RAYTHNDH125 HAWKER800XP 7150012CE  GARRTTTFE731TFE731*     01518WP                                              OUT OF ADJUST   E  ODAAO   OTHER                                                                                           F  FLT CONT AFFECTED                                                             TXTAXI/GRND HDL  1                      EA212G                          258354                                  PILOT REPORTED RUDDER PEDALS BINDING FOUND DURING PREFLIGHT, WITH RT PEDAL FORWARD AND LT PEDAL AFT.  AFTER APPLYING PRESSURE TO PEDALS WITH FEET, PEDALS BECAME UNBOUND WITH POPPING NOISE HEARD.  INSPECTED RUDDER SYSTEM.  FOUND RUDDER BINDING AT PANEL SCREW FOR LOWER CONTROL COLUMN ACCESS, FORWARD, DUE TO BEND IN PANEL.  REMOVED SCREWS AND ADJUSTED PANEL FOR BETTER CLEARANCE.  REPLACED SCREWS WITH SHORTER VERSION OF SAME.  RUDDER SYSTEM OPERATED NORMALLY.  REFERENCE MM, CHAPTER 27.                                                                                                                                                                                                                                          2L72 4F4  FRTA3EU    E6WE                 
20071214003482007121400348GL  2007       12         14         ODAR15DR1        120070411G2421BC4101          ALTERNATOR                              CIRRUSSR    SR22        2130001GL  CONT  O550  IO550*           SO                              NR 2            DESTROYED       B  ODARO   OTHER                                                                                           J  WARNING INDICATION                                                            NRNOT REPORTED   1                      EA2115DR                        0394                                    OWNER REPORTED NR2 ALTERNATOR LIGHT ILLUMINATED.  REMOVED TOP COWLING TO INSPECT NR2 ALTERNATOR.  FOUND NR2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS.  ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE.  REMOVED P/N BC410-1, S/N 0921403.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  ONTA00009CHE3SO                 
20070417000302007041700030GL  2007       4          17         ODAR3            120070411G2421BC4101          ALTERNATOR                              CIRRUSSR    SR22        2130001GL  CONT  O550  IO550*           SO                              NR 2            DESTROYED       B  ODARK   NONE                                                                                            J  WARNING INDICATION                                                            ININSP/MAINT     1                      EA2115DR                        0394                                    OWNER REPORTED NR 2 ALTERNATOR LIGHT ILLUMINATED.  REMOVED TOP COWLING TO INSPECT NR 2 ALTERNATOR.  FOUND NR 2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS.  ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE.  REMOVED P/N BC410-1, S/N 0921403. PICTURES AVAILABLE AT THIS FACILITY.                                                                                                                                                                                                                                                                                                                                                                                                                                                      1L71 3O3  ONTA00009CHE3SO                 
20070501000852007050100085CE  2007       5          1          OMKR20071        120070331G323008420003        DRAG LINK                               CESSNA310   310C        2074210CE  CONT  O470  IO470*      17026SO                              NLG             BROKEN          B  OMKRO   OTHER                                                                                           O  OTHER                                                                         LDLANDING        1                      NM034411                        39024                                   UPON LANDING, THE NOSE LANDING GEAR DRAG LINK ASSEMBLY P/N 0842000-3 BROKE AT THE STRUT ATTACH POINT, ALLOWING THE NOSE GEAR TO COLLAPSE REARWARD, CAUSING THE AIRCRAFT TO SLIDE ON ITS NOSE UNTIL IT STOPPED.  THE DRAG LINK ASSEMBLY APPEARS TO HAVE BROKEN THROUGH THE FORWARD ATTACH HOLE. TOTAL TIME OF THE PART AND TOTAL TIME OF THE AIRCRAFT ARE UNKNOWN AT THIS TIME DUE TO ABSENCE OF LOG BOOKS.  CURRENT HOBBS TIME IS 118.4.                                                                                                                                                                                                                                                                                                        1L72 3O3  O  3A10    E1CE                 
20071205000572007120500057CE  2007       12         5          OMKR200711211    120071121G2500443030401       ADJUSTER                                CESSNA206   U206G       2073356CE  CONT  O520  IO520*      17032SO                              HARNESS ADJUSTERIMPROPER PART   B  OMKRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM039957R                       U20606999                               AD 2004-19-01C CALLS FOR A SPRING TO BE REMOVED FROM SHOULDER HARNESS ADJUSTER P/N443030-401, THAT WAS INADVERTENTLY INSTALLED ON A CERTAIN BATCH OF ACCESSORY KITS SHIPPED FROM MFG 1984 THROUGH 1986.  THIS RESULTED IN AD 86-26-04 BEING ISSUED.  CURRENTLY HAVE (2) AIRCRAFT IN THE HANGAR WITH THIS PN ADJUSTER WITH SPRINGS INSTALLED.  THEY DO NOT FALL INTO THE AFFECTIVITY RANGE OF THE AD OR SB.  CONTACTED THE ENGINEER ON THE BACK OF THE AD, AND HE INSISTS I DO NOT HAVE AN AFFECTED ADJUSTER.  HE HAD A MFG REP. WHO WAS FAMILIAR WITH THE AD CONTACT ME AND I FOUND OUT THE AD RESULTS FROM (INCORRECTLY) INSTALLED SPRINGS.  I SUBMIT THE AD REQUIRES CLARITY AS TO THE DIFFERENCE BETWEEN (INADVERTENTLY INSTALLED) AND (INCOR1H71 3O3  O  A4CE    E5CE                 
20070131001712007013100171SO  2007       1          31         PAI52007S4448    220070130G8520                STUD                                    CESSNA414   414A        2075907CE  CONT  O520  TSIO520NB   17040SO                              NR 4 CYLINDER   BROKEN          B  PAI5K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO05414CJ     1403              414A0432    519053                      DURING ANNUAL INSPECTION FOUND 5 BROKEN HOLD DOWN STUDS ON NR 4 CYLINDER.  ENGINE WAS MODIFIED IAW RAM STC SE3630SW AND SE3631SW AT PREVIOUS OVERHAUL.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3O3  O  A7CE    E8CE                 
20070326000982007032600098CE  2007       3          26         PAI52007S4508    120070322G760010052417717     CONDITION LEVER                         BEECH B300  B300        1159232CE  PWA   PT6   PT6A6       52043EA                              COCKPIT         LOOSE           B  PAI5K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO05507EB4957                   FL81                                    PILOT NOTED RT ENGINE CONDITION LEVER CONTROL FELT LOOSE AND IDLE N1 SPEED LOW.  UPON INSPECTION, MAINTENANCE FOUND ALL SCREWS ATTACHING CONDITION LEVER TO QUADRANT LOOSE TO THE POINT OF ALMOST FALLING OUT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4T3  TRTA24CE   E4EA                 
20070614001422007061400142CE  2007       6          14         PAI52007S4573    120070515G573000011013333     SKIN                                    BEECH B300  B300        1159232CE                                                               WING            CRACKED         B  PAI5K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO05507EB5010 196               FL81                                    WHILE PERFORMING PHASE 2 INSPECTION NOTED AN 8 INCH LONG SPANWISE CRACK ON LOWER SURFACE OF WING LEADING EDGE SKIN P/N 000-110133-33.  ALSO FOUND CHANNEL P/N 101-910119-147 INSIDE THE ABOVE MENTIONED SKIN BROKEN IN TWO.  REPLACED BOTH PARTS WITH NEW PARTS FROM BEECH.                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4T    RTA24CE                        
20071003000162007100300016EU  2007       10         3          PAI52007S4724    120070926G301080232118401     DUCT                                    PIAGIOP180  P180        6960204EU  PWA   PT6   PT6*        52043EA                              WING LE         CRACKED         B  PAI5K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO05145SL2994                   1093                                    DURING 3000 HOUR D-CHECK FOUND 3 OF 4 WING OB LEADING EDGE PANELS WITH CRACKED HEATING DUCTS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1H72 3O3  TRTA59EU   E2NE                 
20071105000042007110500004SW  2007       11         5          PAI52007S4751    120071024G2910T610488109      LINE                                    GULSTM690TP 690B        7630516SW                                                               HYD SYSTEM      RUPTURED        B  PAI5A   UNSCHED LANDING                                                                                 KJ FLUID LOSS                WARNING INDICATION                                  CRCRUISE         1                      SO0591CT                        11428                                   HYDRAULIC PRESSURE FLEX LINE AT RT ENGINE DRIVEN HYDRAULIC PUMP RUPTURED IN FLIGHT CAUSING LOSS OF HYDRAULIC FLUID.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1H72 3T      2A4                          
20070501001172007050100117CE  2007       5          1          PAZR200700001    120070416G5551663110215       ATTACH FITTING                          CESSNA560   560XL       2076702CE  PWA   545   PW545A           NE                              ZONE 300        CRACKED         B  PAZRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE03186XL2179                   5605186                                 DURING A SCHEDULED INSPECTION, A 1.5 INCH CRACK WAS FOUND IN THE LOWER RADIUS OF THE HORIZONTAL STABILIZER AFT ATTACH FITTING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA22CE   E00059EN             
20070206000502007020600050    2007       2          6          QKPR07001        120070202G493038828406        FCU             HONEYWELL   GTCP36150RR                                                                                                 APU             LEAKING         B  QKPRO   OTHER                                                                                           L  NO TEST                                                                       NRNOT REPORTED   1                      SO05                                                                    THERE IS A PIN HOLE IN THE FCU HOUSING. IN THIS CASE THERE WAS 4 STREAMS OF FUEL AND HEAVY MISTING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       
20070410000682007041000068NM  2007       4          10         QXEANM09402      120070315G4920164161100       DRAIN VALVE     SUNDSTRANDEM            BOMBDRDHC8  DHC8402     1390042NM  PWC   150   PW150A           EA                              APU             MISINSTALLED    G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      NM09402QX                       4032                                    BALL ON WRONG SIDE OF SPRING, WHICH ALLOWS IT TO REST IN CLOSED POSITION, NOT ALLOWING PROPER DRAINAGE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T4  TRTA13NM   E00062EN             
20070409001252007040900125NM  2007       4          9          QXEANM09417      120070314G4920164161100       DRAIN VALVE                             BOMBDRDHC8  DHC8402     1390042NM  PWC   150   PW150A           EA                              APU             PLUGGED         G  QXEAO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      NM09417QX                       4086                                    BALL ON WRONG SIDE OF SPRING ALLOWING IMPROPER DRAINAGE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2H72 4T4  TRTA13NM   E00062EN             
20070131001852007013100185NE  2007       1          31         R021692          320070117G6111D7745           BEARING                                 BEECH 1900  1900D       1154162CE  PWA   PT6   PT6*        52043EA  HARTZLHCE4A HCE4A3A     NE  PROPELLER BLADE BROKEN          B  SJ3RO   OTHER                                                                                           E  VIBRATION/BUFFET                                                              ININSP/MAINT     1                      GL05SJ3R 3115                                           HJ1819          ON 12/14/06 REPORTED AIRCRAFT VIBRATIONS FROM STBD ENGINE. INSPECTION OF PROPELLER ON GROUND REVEALED EXCESSIVE RADIAL PLAY OUT OF LIMIT OF NR 3 BLADE.  PROPELLER REMOVED FROM AIRCRAFT FOR FURTHER INVESTIGATION. SERVICE CENTER NOTES: BLADE NR 3 CAM FOLLOWER BROKEN, PRELOAD PLATE GOUGED, BLADE SIDE D-7745 BEARING CRACKED RADIALLY AND PIECE MISSING. RETAINING WASHER ATTACHED TO PC KNOB. BLADE NR 3 FORK SLOT WORN 0.028, OTHER 3 SLOTS WORN 0.015-0.021, CIRCUMFERENTIAL WEAR IN FORK SEAT. BLADE NR 3 RETENTION SHOULDER HEIGHT MEASURED 0.914 - 0.974, UNABLE TO PERFORM OPTICAL COMPARATOR INSPECTION OF RADIUS DUE TO SHOULDER HEIGHT DIMENSION BELOW 0.972. SEE S/B 287.                                                       2L72 4T3  TRTA24CE   E2NE    5  CP10NE    
20070322000912007032200091GL  2007       3          22         R022366          320070316G6110A20742          SEAL RING                               CIRRUSSR    SR22        2130001GL  CONT  O550  IO550F      17042SO  HARTZLHCJ3Y PHCJ3YF1    GL  PROPELLER BLADE DEBONDED        B  SJ3RK   NONE                                                                                            E  VIBRATION/BUFFET                                                              ININSP/MAINT     1                      GL05     81                                             FP5296B         TEFLON (BLADE SEAL) DEBONDED FROM THE SHANK OF BLADE SN A0336 CAUSING GREASE LEAK.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              1L71 3O3  ONTA00009CHE3SO    5  CP36EA    
20070821002332007082100233GL  2007       8          21         R0240301         320070814G6110B3493           BRACKET                                 MTSBSIMU2   MU2B60      5780460CE                                   HARTZLHCB4T HCB4TN5     GL  PROPELLER       CRACKED         B  SJ3RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL05                                                                    FIVE B-3493 START LOCK BRACKETS WERE FOUND DURING PENETRANT INSPECTION TO BE CRACKED AT THE SAME LOCATION. CRACKS ARE LOCATED ON THE EXTERIOR START PIN BORE NEXT TO THE SPINNER MOUNTING BOLT RELIEF CUT-OUT. THIS BRACKET IS PART OF THE 830-34L START LOCK UNIT INSTALLED ON 4-BLADED MU-2S.                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H72 3T    RTA10SW           6  CP40EA    
20071002000242007100200024CE  2007       10         2          RDA092407        120070924G284205235571        TRANSMITTER                             CESSNA175   175         2072502CE  CONT  O300  GO300*      17022SO                              FUEL QTY        CRACKED         G      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL239456B2440                   55256                                   WHILE CALIBRATING THE FUEL QUANTITY SYSTEM THE LT FUEL GAUGE WOULD SHOW AN INCREASE IN QUANTITY THEN START DECREASING.  WHILE TROUBLESHOOTING THE LT TANK FUEL QUANTITY SENDER, FOUND 2 CRACKS APPROXIMATELY 1 INCH LONG IN THE BRASS FLOAT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1H71 3O3  ONT3A17    E298                 
20070627000052007062700005CE  2007       6          27         RUAGACC61007     120070610G321016410077        SPRING                                  CESSNA188   T188C       2073012CE  CONT  O520  TSIO520*    17040SO                              LT MLG          FAILED          G  RUAGO   OTHER                                                                                           O  OTHER                                                                         CLCLIMB          1                      NM052535J7163 181               T18803471T                              AIRCRAFT ACCIDENT.  LT MLG (SPRING) FAILED DURING TAKEOFF ATTEMPT, APPROXIMATELY 6 INCHES ABOVE AXLE.  NO EVIDENCE OF PREVIOUS FRACTURE (CRACK) COULD BE DETECTED.  LT WING BUCKLED AND AIRCRAFT NOSED OVER.  SUBSTANTIAL DAMAGE, NO INJURIES.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L71 3O3  O  A9CE    E8CE                 
20071213003782007121300378EU  2007       12         13         S0700432         120071203G2435                COMMUTATOR      BFGOODRICH              PILATSPC12  PC1245      7090551EU                                                               STARTER GEN     FAILED          B      BA  EMER. DESCENT           UNSCHED LANDING                                                         HE ELECT. POWER LOSS-50 PC   VIBRATION/BUFFET                                    CRCRUISE         1                      CE07462PC           97102       462                                     DURING CRUISE FLIGHT, LOUD NOISE FROM ENGINE COMPARTMENT FOLLOWED BY VIBRATION AND LOSS OF PRIMARY ELECTRICAL POWER.  UPON INSPECTION, ONE SEGMENT FROM COMMUTATOR WAS MISSING AND AFT END OF GENERATOR AND BRUSHES HAD SUSTAINED HEAVY DAMAGE.  AFTER REPLACEMENT WITH OVERHAULED UNIT, NO ABNORMALITIES WERE NOTED.                                                                                                                                                                                                                                                                                                                                                                                                                           1L71 3T    RTA78EU                        
20070227000712007022700071SO  2007       2          27         SDR0701          120070123G53121159B2156227    ANGLE                                   GULSTMG1159 GIV         3980115SO  RROYCETAY   TAY6108          NE                              BS 793          CRACKED         W      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA29254GA11823                  1032                                    DURING SCHEDULED 5000 LANDING FS793 BULKHEAD CAP ANGLE NDT INSPECTION, DETECTED A 1.25 INCH LONG CRACK IN RT BULKHEAD CAP ANGLE. MANUFACTURER HAS RECOMMENDED REPLACEMENT OF LT AND RT FS793 BULKHEAD CAP ANGLES.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               2L72 4F4  FRTA12EA   E25NE                
20070213000802007021300080CE  2007       2          13         SO19200712477    120070126G3297                WIRE                                    CESSNA177   177RG       2073709CE  LYC   O360  IO360A1B6   41514EA                              WARNING HORN    BROKEN          C      O   OTHER                                                                                           P  NO WARNING INDICATION                                                         LDLANDING        1                      SO19177RR                       177RG0937                               DURING THIRD NIGHT CURRENCY LANDING PILOT FAILED TO EXTEND GEAR AND DIDN'T HEAR THE GEAR UP WARNING HORN.  SHOWING A BROKEN WIRE AT THE GEAR WARNING HORN SWITCH.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1H71 3O3  O  A20CE   1E10                 
20070125001572007012500157NM  2007       1          25         SROM200700001    120070105G212065544709        DUCT                                    BOEING737   737201      1384454NM  PWA   JT8   JT8D15      52051NE                              A/C PACK        RUPTURED        I  SROMH   DEACTIVATE SYST/CIRCUITS                                                                        B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      AL03245US                       22751                                   UPON TAKEOFF A POP WAS WAS HEARD FOLLOWED BY PERCEIVED SMOKE (DUST) IN THE CABIN.  PACS WERE SELECTED TO OFF AND A IMMEDIATE LANDING MADE AT THE DEPARTURE AIRPORT.  ALL COCKPIT INDICATIONS NORMAL.  FOUND LT AIR CONDITIONING PAC MIXING CHAMBER AND HOT AIR SUPPLY DUCT SEPARATED/ DAMAGED ALLOWING HOT CONDITIONED AIR TO ENTER CABIN THROUGH RETURN GRILLS, THUS CREATING DUST.  APPEARS TO HAVE EXPERIENCED INTERNAL DAMAGE RESULTING IN BACK PRESSURE WHICH CAUSED THE DUCT/FLANGE FAILURE.  NO OTHER DAMAGE NOTED.  REPLACED MIXING AND HOT AIR DUCTS.                                                                                                                                                                                  2L72 4F4  F  A16WE   E2EA                 
20070614001432007061400143NM  2007       6          14         SROM200700002    120070516G5280                DOOR                                    BOEING737   737205      1384456NM                                                               NLG             BINDING         C  SROMA   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      AL03736BP                       23465                                   LOUD VIBRATION AFTER TAKEOFF.  VIBRATION INCREASED WITH SPEED AND DECREASED AT LOWER SPEEDS.  RETURNED TO DEPARTURE AIRPORT.  PERFORMED VIBRATION CONDITIONAL INSPECTION.  FOUND NLG DOORS ON GRAVEL SKI EQUIPPED AIRCRAFT TO BE BINDING ON EACH OTHER.  ADJUSTED PER AMM 32-22-12.  AIRCRAFT RELEASED AN OPERATIONAL CHECK FLIGHT NORMAL.  NO REPORT OF VIBRATION ON SUBSEQUENT FLIGHTS.                                                                                                                                                                                                                                                                                                                                                       2L72 4F    RTA16WE                        
20070613002442007061300244NM  2007       6          13         SROM200700003    120070522G5753                BEARING                                 BOEING737   737205      1384456NM                                                               ROD END         LOOSE           C  SROMA   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      AL03736BP                       23465                                   AIRFRAME BUFFET NOTED AFTER GEAR UP ON TAKEOFF & BEFORE FLAP RETRACTION & POWER REDUCTION DURING CLIMB.  THIS IS THE 2ND WRITE UP OF THIS CONDITION.  PERFORMED AIRFRAME CONDITIONAL INSPECTION.  REPLACED NLG GRAVEL SKI DEFLECTOR ACTUATOR DUE TO LOOSE ROD END AND REPLACED BEARING IN LEFT INBOARD GROUND SPOILER OUTBOARD ACTUATOR LINKAGE DUE TO LOOSENESS.  AIRCRAFT RELEASED FOR OPERATION CHECK FLIGHT WITH NO REPORTS OF VIBRATION ON TWO TAKEOFFS DURING CHECK FLIGHT.                                                                                                                                                                                                                                                               2L72 4F    RTA16WE                        
20070614001792007061400179NM  2007       6          14         SROM200700004    120070531G212028410           VALVE                                   BOEING737   737205      1384456NM                                                               FLOW CONTROL    FLUTTER         C  SROMA   UNSCHED LANDING                                                                                 E  VIBRATION/BUFFET                                                              CLCLIMB          1                      AL03736BP     7463              23465                                   AFTER TAKEOFF AT AROUND 1000 FEET VIBRATION STARTED IN FWD PART OF AIRCRAFT AND TRAVELED TO REAR OF AIRCRAFT.  AFTER SHUTTING OFF ALL PACKS AND BLEEDS IT SLOWLY WENT AWAY.  AIRCRAFT RETURNED TO DEPARTURE AIRPORT.  AIRCRAFT INSPECTED WITH NO FAULTS FOUND AND RELEASED FOR FLIGHT TO MAINTENANCE BASE WITH SLIGHT VIBRATION NOTED IN FLOOR.  FURTHER INSPECTION FOUND CRACKED E&E BAY COOLING DUCT AND CHATTERING E&E BAY FLOW CONTROL VALVE.  REPLACED DUCTS AND VALVE.  NO REPORTS OF VIBRATION ON SUBSEQUENT FLIGHT.                                                                                                                                                                                                                     2L72 4F    RTA16WE                        
20070824003232007082400323NM  2007       8          24         SROM200700006    120070801G5311                FRAME                                   BOEING737   737205      1384456NM  PWA   JT8   JT8D17      52049NE                              BS 616          CRACKED         C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR63-CRACK ON BODY FRAME INNER CHORD BS616 RT SIDE AT STUB BEAM LOWER CHORD ATTACH (ABOVE WING BOX BL64R). DAMAGE OF BODY FRAME INNER CHORD STA 616 RT SIDE AT STUB BEAM LOWER CHORD ATTACH REMOVED IAW MFG SB 737-53-1182R1. REPAIR ANGLE INSTALLED IAW MFG SB 737-53-1182R1 AND MFG MSG NR: 1-508321689-2.                                                                                                                                                                                                                                                                                                                                                                                                                                    2L72 4F4  FRTA16WE   E2EA                 
20070906000682007090600068NM  2007       9          6          SROM200700007    120070807G5315                FLOORBEAM                               BOEING737   737205      1384456NM  PWA   JT8   JT8D17A     52049NE                              BS 660          CRACKED         C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR228-CRACK IN FLOORBEAM AND WEB STA 660 BL0. CRACKED FLOORBEAM AND WEB AT STA 660 BL0 REPAIRED IAW MFG SB 737-57-1210, REV 1, DATED AUG 27/07.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F4  FRTA16WE   E2EA                 
20070917000052007091700005NM  2007       9          17         SROM200700008    120070808G5330                SKIN                                    BOEING737   737205      1384456NM  PWA   JT8   JT8D17      52049NE                              BS 900 S17-18L  DENTED          C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR247- DENT FOUND STA 900 LT BETWEEN STRINGERS 17 AND 18. REPAIRED IAW MFG SRM 53-30-3, PAGES 253-320 AND 51-30-3, PAGE 7 AND 51-30-02.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA16WE   E2EA                 
20070913000622007091300062NM  2007       9          13         SROM200700009    120070808G3211                SUPPORT FITTING                         BOEING737   737205      1384456NM                                                               RT MLG          DAMAGED         C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR269 - WEAR DAMAGE RIGHT MAIN LANDING GEAR FUSE TO TRUNNION SUPPORT BEAM ATTACH FITTING.  REPAIRED IN ACCORDANCE WITH BOEING APPROVED FAA FORM 8100-9 MESSAGE 1-515849678-6, DATED AUGUST 23, 2007.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            2L72 4F    RTA16WE                        
20070913001462007091300146NM  2007       9          13         SROM200700010    120070808G574365C313326       SUPPORT BEAM                            BOEING737   737205      1384456NM                                                               RT MLG          CORRODED        C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR270 - PITTING RIGHT MAIN LANDING GEAR TRUNNION SUPPORT BEAM UPPER SURFACE.  REPLACED RIGHT MLG SUPPORT BEAM IN ACCORDANCE WITH BOEING 737 AMM 57-15-0.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        2L72 4F    RTA16WE                        
20070913001472007091300147NM  2007       9          13         SROM200700011    120070808G5743658276415       SUPPORT BEAM                            BOEING737   737205      1384456NM                                                               LT MLG          CORRODED        C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR279 - PITTING LEFT MAIN LANDING GEAR TRUNNION SUPPORT BEAM UPPER SURFACE (LIGHT).  REPLACED LEFT MLG SUPPORT BEAM IN ACCORDANCE WITH BOEING 737 AMM 57-15-0.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F    RTA16WE                        
20070917000212007091700021NM  2007       9          17         SROM200700012    120070808G5343                TRUNNION                                BOEING737   737205      1384456NM  PWA   JT8   JT8D17      52049NE                              LT MLG          WORN            C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   WEAR DAMAGE, LT MLG FUSELAGE TO TRUNNION SUPPORT BEAM ATTACH FITTING. BLEND REPAIRED IAW MFG, FORM 8100-9, MESSAGE NR 1-515849678-6, DATED AUGUST 23, 2007.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F4  FRTA16WE   E2EA                 
20070913000632007091300063NM  2007       9          13         SROM200700013    120070808G5315                FLOORBEAM                               BOEING737   737205      1384456NM                                                               FUSELAGE        CORRODED        C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR291 - CORROSION ON FLOORBEAM UPPER FLANGE STA 344 LBL 48-60.  REPAIRED IN ACCORDANCE WITH BOEING SRM 53-10-9, FIGURE 1.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       2L72 4F    RTA16WE                        
20070906000852007090600085NM  2007       9          6          SROM200700014    120070810G5315                FLOORBEAM                               BOEING737   737205      1384456NM  PWA   JT8   JT8D17A     52049NE                              ZONE 100        CORRODED        C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR296-CORROSION ON FLOORBEAM UPPER FLANGE AT STA 294 AND RBL 43 TO 53. FLOORBEAM UPPER FLANGE FROM RBL 6 (EXISTING SPLICE) TO RBL 60, STA 294 REMOVED AND REPLACED IAW WITH MFG SRM 53-10-9, FIG 5, SHEET 1-5.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA16WE   E2EA                 
20070914001012007091400101NM  2007       9          14         SROM200700015    120070810G5512                SKIN                                    BOEING737   737205      1384456NM                                                               HORIZONTAL STAB GOUGED          C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR378 - RT STABILIZER LOWER SURFACE FOUND WITH A GOUGE IN THE SKIN ON THE RIB ATTACH LOCATION AT 138.7 DEPT IS 0.037 WHICH IS OVER 50 PERCENT.  DAMAGED SECTION OF SKIN ON RT STABILIZER LOWER SURFACE LOCATION 138.7 REMOVED.  REPAIR DOUBLER FABRICATED AND INSTALLED IN ACCORDANCE WITH DER APPROVED DRAWING NR 73R55116228.                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F    RTA16WE                        
20070913001482007091300148NM  2007       9          13         SROM200700016    120070810G5330                SKIN                                    BOEING737   737205      1384456NM                                                               FUSELAGE        CRACKED         C  SROMK   NONE                                                                                            Z  SIGNIFICANT FAILURE REPORT                                                    ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR393 - FUSELAGE SKIN CRACKED AT AIRSTAIR CONTROL HANDLE CUTOUT AT BS 378 BETWEEN STRINGERS 21-L AND 22-L.  REPAIR DOUBLER FABRICATED AND INSTALLED IN ACCORDANCE WITH BOEING SB 737-53-1093.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F    RTA16WE                        
20070913001492007091300149NM  2007       9          13         SROM200700017    120070810G5343                SUPPORT BEAM                            BOEING737   737205      1384456NM                                                               NLG             CRACKED         C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR419 - CRACK ON NLG ACTUATOR SUPPORT BEAM AT BS 227-0 UPPER RIGHT SIDE.  REPLACED NLG ACTUATOR UPPER RIGHT SIDE SUPPORT BEAM IN ACCORDANCE WITH BOEING 737 SRM 51-10-1, 53-10-2 AND 51-30-2.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F    RTA16WE                        
20070906000752007090600075NM  2007       9          6          SROM200700018    120070818G5330                SKIN                                    BOEING737   737205      1384456NM  PWA   JT8   JT8D17A     52049NE                              BS 907          NICKED          C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NICK STA 907 STR 22 LT. NICK AT STA 907, STR 22L REPAIRED IAW SRM 53-30-3, FIG 48. NICK BEYOND LIMITS AND DAMAGE REMOVED. HFEC IAW NDT PART 6, 53-30-00, FIG 4 OF REPAIR AT FUSELAGE SKIN STA 907 STR 22L. NO CRACKS EVIDENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F4  FRTA16WE   E2EA                 
20070906000012007090600001NM  2007       9          6          SROM200700019    120070818G5330                SKIN                                    BOEING737   737205      1384456NM  PWA   JT8   JT8D17A     52049NE                              ZONE 100        NICKED          C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NICK STA 887 STR 24L-25L LT.  DAMAGED AREA OF SKIN REMOVED AND REPAIR PLATES FABRICATED IAW SRM 53-30-3, FIG 48. INSTALLED REPAIR IAW 51-30-2.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  2L72 4F4  FRTA16WE   E2EA                 
20070906000712007090600071NM  2007       9          6          SROM200700020    120070818G5330                SKIN                                    BOEING737   737205      1384456NM  PWA   JT8   JT8D17A     52049NE                              ZONE 100        NICKED          C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NICK STA 847 STR 21 LT.  NICK AT STA 847 STR 21L FOUND TO BE BEYOND LIMITS. NICK REMOVED AND AREA AT STA 847 STR 21L REPAIRED IAW SRM 53-30-3, FIG 48.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          2L72 4F4  FRTA16WE   E2EA                 
20070906000792007090600079NM  2007       9          6          SROM200700021    120070810G5315                FLOORBEAM                               BOEING737   737205      1384456NM  PWA   PT6   PT6A114A    52043NE                              BS 328          CORRODED        C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR392-CORROSION ON UPPER CHORD OF FLOORBEAM STA 328 RBL 52. FLOORBEAM REPAIRED IAW SRM 53-10-9, FIG 5, PAGE 21.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 2L72 4F3  TRTA16WE   E4EA                 
20070906000662007090600066NM  2007       9          6          SROM200700022    120070803G5311                FRAME                                   BOEING737   737205      1384456NM  PWA   JT8   JT8D17A     52049NE                              BS 783 S25R     CORRODED        I  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR145-LIGHT CORROSION ON FRAME AT STA 783 STR 25R. REPAIRED FRAME IAW MFG MESSAGE NR 1-518342007-2, DATED AUG 1, 2007 AND PRODUCTION DRAWINGS FOR PN 65-47959-47 STRAP AND PN 65C31240-1 FRAME DOUBLER.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         2L72 4F4  FRTA16WE   E2EA                 
20070917000462007091700046NM  2007       9          17         SROM200700023    120070807G5524                NUT PLATE       BOEING                  BOEING737   737205      1384456NM  PWA   JT8   JT8D17      52049NE                              ELEVATOR        STRIPPED        C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP982        457         23465                                   NR122-LT ELEVATOR TRIM TAB IB HINGE FITTING MISSING BOLT.  NEW ELEVATOR INSTALLED 12/06/06, 982 TT, 717 TC.  (2) OUT OF (4) HINGE ATTACH FITTING NUTPLATES STRIPPED FROM THE FACTORY. REPLACED NUTPLATES IAW SRM 51-30-2, FIGURES 3 AND 7.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      2L72 4F4  FRTA16WE   E2EA                 
20070913000642007091300064NM  2007       9          13         SROM200700024    120070815G4910                INTAKE DUCT                             BOEING737   737205      1384456NM                                                               APU             CORRODED        C  SROMK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      AL03736BP38551                  23465                                   NR481 - CORROSION AROUND AIR INLET DUCT FLANGE APU TORQUE BOX WEB BS 1064 RIGHT HAND SIDE.  REPLACED AIR INLET DUCT FLANGE IN ACCORDANCE WITH BOEING SRM 51-10-1, PAGE 8, 51-30-2, FIGURES 11, 12, 13, AND 51-30-6, FIGURE 3.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   2L72 4F    RTA16WE                        
20071016000512007101600051NM  2007       10         16         SROM200725       120071005G8097                WIRE                                    BOEING737   737205      1384456NM  PWA   JT8   JT8D17A     52049NE                              START SWITCH    BURNED          C  SROMAH  UNSCHED LANDING         DEACTIVATE SYST/CIRCUITS                                                B  SMOKE/FUMES/ODORS/SPARKS                                                      CLCLIMB          1                      AL03736BP38641      NSN         23465                                   DURING CLIMB SPARKS AND SMOKE EMITTED FROM THE AREA OF THE NR 1 START SWITCH. LOW IGNITION CB POPPED AT WHICH TIME THE SPARKS AND SMOKE CEASED. FLIGHT CREW RETURNED TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL LANDING. REPLACED SWITCH DUE TO ARCING ON CASE AND REPAIRED WIRING. INSPECTED OTHER AIRCRAFT IN FLEET NO OTHER CHAFED WIRES FOUND IN VICINITY OF THE START SWITCHES.                                                                                                                                                                                                                                                                                                                                                            2L72 4F4  FRTA16WE   E2EA                 
20070918000962007091800096    2007       9          18         STS001           420070914G25641116FAUL33011   LIFE RAFT                                                                                                                                               ACTIVE          B      K   NONE                                                                                            L  NO TEST                                                                       NRNOT REPORTED   1                      SO15WL7R                                                                LIFE RAFT (APPLIANCE, CAT II) SERVICED 10/19/2005 (SMER451X) THE 406 MHZ ELT NOT TIED TO BOARDING LADDER IAW MANUAL.  ELT WOULD NOT HAVE SELF-DEPLOYED TO ALERT SAR, AS REQUIRED BY CMM 25-60-101, REVISION E                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             
200805141    200805141    NE  2008       5          14         SWDG20080016     220070318G7250310718501       GAS GENERATOR                           AIRTRCAT802 AT802A      0390308SW  PWC   PT6   PT6A67AG    52211NE  HARTZLHCB5M HCB5MA3     GL  ENGINE          ERODED          D  SWDGK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW11803DG4731 550               802A0077    PCERD0016                   BROKEN 'T' HEAD BOLT SHANK FOUND IN COWLING.  MANUFACTURER REP VISITED AND TOOK PICTURES OF ERODED GAP IN THE 'C' FLANGE AT THE SCAVENGE TUBE COUPLING LOCATION WHERE THE BOLT HAD BEEN SEVERED.  THE DAMAGE TO THE BOLT, FLANGE MATING SURFACES AND COUPLING ARE CLEARLY NOT THE RESULT OF CORROSION BECAUSE THE SURFACES IN THE AREAS OF DAMAGE ARE CLEAN AND HAVE AN ALMOST POLISHED APPEARANCE.  SIMILAR ENGINES HAVE A SEALING RING INCORPORATED INTO THE FLANGE APPARENTLY FOR THIS VERY REASON.  THE MANUFACTURER REPS HAVE STATED THAT THIS EROSION IS UNEXPLAINED AND THEREFORE IS NOT A SAFETY OF FLIGHT ISSUE.  THE MACHINING OF THE FLANGES AND INSTALLATION OF SEALING RING WOULD BE A START FOR REPAIRS, AND THE SOLUTION WOULD BE1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
200805141    200805141    NE  2008       5          14         SWDG20080024     220070319G7250310718501       GAS GENERATOR                           AIRTRCAT802 AT802A      0390308SW  PWC   PT6   PT6A67AG    52211NE  HARTZLHCB5M HCB5MA3     GL  ENGINE          ERODED          D  SWDGK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW11804DG3129 3129              802A0089    PCERD0024                   ENGINE REMOVED FOR OVERHAUL EVALUATION. DUE TO THE FINDING OF SEVERE EROSION DAMAGE TO THE 'C' FLANGE AND NUMEROUS BROKEN 'T' BOLTS ON 3 OTHER ENGINES, THE DISSASSEMBLED EXHAUST DUCT AND GAS GENERATOR CASE FLANGES HAVE BEEN PHOTOGRAPHED AND FOUND THAT THIS 4TH ENGINE SUFFERS FROM SIMILAR DAMAGE.  IT SHOULD BE NOTED THAT THE MANUFACTURER HAS BEEN NOTIFIED AND THAT THEIR REP HAS TAKEN PICTURES OF THE DAMAGED ENGINES AND HAS TOLD US THAT THE BROKEN BOLTS, 'C' FLANGE DAMAGE, AND P3 AIR LEAKAGE ONTO THE OIL TUBES ARE NOT SAFETY OF FLIGHT ISSUES.  IT IS SUGGESTED THAT THE MANUFACTURER IMPLEMENT WARRANTY PROVISIONS FOR THE INCORORATION OF A SEALING RING ON THE -67AG JUST LIKE SIMILAR ENGINES IN THE FAMILY.            1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
200805141    200805141    NE  2008       5          14         SWDG20080077     220070319G7250310718501       GAS GENERATOR                           AIRTRCAT802 AT802A      0390308SW  PWC   PT6   PT6A67AG    52211NE  HARTZLHCB5M HCB5MA3     GL  ENGINE          ERODED          D  SWDGK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW11803DG1800 1800              802A0077    PCERD0077                   AS THE 'T' HEAD BOLTS WERE BEING REMOVED FOR HSI, ONE NUT DETACHED FROM THE BOLT SHANK WITH THE THREAD INSIDE THE NUT.  CLOSE INSPECTION OF THE ADJACENT BOLT REVEALED SEVERE EROSION (NOT CORROSION OR STRETCH DAMAGE) TO THE BOLT SHANK.  IT WAS FURTHER NOTED AND PHOTOGRAPHED BY THE MANUFACTURER REP THAT THE EXHAUST DUCT FLANGE AND GAS GENERATOR FLANGE IN THE BROKEN BOLT AREA HAD MATERIAL LOSS THAT WAS ALLOWING P3 AIR LOSS THAT MAY BE ATTRIBUTED TO THE HIGHER THAN NORMAL OIL TEMP INDICATION ON THE GROUND.  THE AIR LEAK IS VENTING ONTO THE SCAVENGE OIL TUBE COUPLING.  MANUFACTURER REPS SAY THAT THIS IS AN ISOLATED CASE AND IS NOT A SAFETY OF FLIGHT ISSUE AS THAT THERE ARE MANY MORE BOLTS THAT HOLD 'C' FLANGE TOGETH1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
200805141    200805141    NE  2008       5          14         SWDG20080113     220070319G7250310718501       GAS GENERATOR                           AIRTRCAT802 AT802A      0390308SW  PWC   PT6   PT6A67AG    52211NE  HARTZLHCB5M HCB5MA3     GL  ENGINE          ERODED          D  SWDGK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SW11804DG346  346               802A0089    PCERD0113                   ENGINE PARAMETERS ABNORMAL AND SUBSIQUENT INSPECTION FOUND T5 HARNESS DAMAGED AT ASSEMBLY.  IT WAS FURTHER NOTED THAT SUBSTANTIAL MATERIAL LOSS IN THE CENTER BOLT HOLE @ THE SCAVENGE TUBE COUPLING WAS ALLOWING COMPRESSOR AIR TO ERODE THE 'T' BOLT SHANK.  MANUFACTURER REP TOOK PICTURES OF DAMAGE AS NOTED ON NOVEMBER 22, 2006 AND HAS YET TO OFFER SUGGESTED CAUSE OR REPAIR SCHEME.  THE "WITNESS" MARK OF SURFACE CONTACT OF THE 'C' FLANGES INDICATE NON-UNIFORM ALIGNMENT AXIALY OF THE FLANGE WELDED TO THE CASE.  THE MANUFACTURER REPS HAVE FURTHER COMMENTED THAT P3 AIR LEAKAGE IS NOT A SAFETY OF FLIGHT ISSUE AND THAT FLANGE DAMAGE AND BOLT DAMAGE OR LOSS IS NOT A SAFETY OF FLIGHT ISSUE.                                1L71 3T4  TNCA19SW   E26NE   6  CP44GL    
20080114000422008011400042CE  2008       1          14         T4OR4765001      120071221G52105043004315      LEVER                                   BEECH 200   B200        1152922CE  PWA   PT6   PT6A42      52043NE                              CABIN DOOR      TWISTED         B  T4ORK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA63240CT7199                   BB1063                                  WHILE TRYING TO RIG THE CABIN DOOR UPPER LATCH HOOKS FOR PROPER OVERCENTER, IT WAS FOUND PROPER OVERCENTER COULD NOT BE OBTAINED WITHOUT THE ADJUSTING ROD END WITNESS HOLES BEING EXPOSED.  CLOSER EXAMINATIONS SHOWED THE FWD AND AFT DOOR ACTUATION LEVER ASSEMBLIES, PN 50-430043-15 (FWD) AND 50-430043-17 (AFT) WERE TWISTED, CHANGING THE RELATIVE ANGLE BETWEEN THE LATCH HOOK AND ROD END ATTACH POINT.  NORMALLY THE ANGLES BETWEEN THE LATCH HOOK AND LATCH ROD ATTACH POINT IS ABOUT 90 DEGREES.  THE PARTS IN THIS DOOR WERE SOMEWHAT LESS THAT 90 DEGREES, CLOSER TO 75 DEGREES DUE TO THE TWIST.  WITH THIS CONDITION, THE PUSHROD FOR THE UPPER HOOK OVERCENTER ADJUSTMENT WOULD NEED TO BE EXTENDED FARTHER THAN DESIGNED, EXPO1L72 4T4  T  A24CE   E4EA                 
20071204002342007120400234EU  2007       12         4          T9NR200700001    120071106G3246315182          WHEEL                                   AEROSPATR42 ATR42*      8680900EU                                                               MLG             CRACKED         B  TL9RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO19                                                                    OUR SHOP REPORTS THE PRESENCE OF AN UNUSUAL CRACK ON THIS WHEEL. IT LIES BETWEEN THE WHEEL'S LIGHTING HOLES (WEB), AND IS COMPLETELY CRACKED BETWEEN ADJACENT LIGHTING HOLES. THE WHEEL ASSEMBLY PN IS NOTED BELOW, BUT THE CRACK EXHIBITED ITSELF ON THE WHEEL HALF PN 300-824/10-1606                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T    RTA53EU                        
20071204002352007120400235EU  2007       12         4          T9NR200700002    120071106G3246315182          WHEEL                                   AEROSPATR42 ATR42*      8680900EU                                                               ZONE 700        CRACKED         B  T9NRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO19                                                                    OUR SHOP REPORTS THE PRESENCE OF AN UNUSUAL CRACK ON THIS WHEEL. IT LIES BETWEEN THE WHEEL'S LIGHTING HOLES (WEB), AND IS COMPLETELY CRACKED BETWEEN ADJACENT LIGHTING HOLES. THE WHEEL ASSEMBLY PN IS NOTED BELOW, BUT THE CRACK EXHIBITED ITSELF ON THE WHEEL HALF PN 300-824/10-1606                                                                                                                                                                                                                                                                                                                                                                                                                                                         2H72 4T    RTA53EU                        
20080111001582008011100158CE  2008       1          11         TAS07003         120071116G32331FA100433       CAP                                     BEECH 1900  1900        1154160CE                                                               MLG ACTUATOR    CRACKED         B      K   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO05     11943      1209B                                               MLG ACTUATOR WAS RECEIVED DUE TO INDICATIONS FOUND IN THE END CAP DURING ULTRASONIC TESTING.  ACTUATOR WENT THROUGH A PRELIMINARY INSPECTION AND A COMPLETE FUNCTIONAL TEST WITH NO EXTERNAL EVIDENCE OF LEAKING OR CRACKING.  AFTER DISASSEMBLY, A CRACK IN THE INTERNAL RADIUS OF THE END CAP WAS CONFIRMED BY A FLUORESCENT PENETRANT INSPECTION.                                                                                                                                                                                                                                                                                                                                                                                            2L72 4T    RTA24CE                        
20070412000242007041200024EU  2007       4          12         THMN4346176      120070410G5340                ATTACH BRACKET                          AMD   FALC10FALCON10    2730101EU                                                               RT NLG DOOR     CRACKED         B  T0DRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE03101HS                       82                                      RT NOSE LANDING GEAR DOOR ATTACH POINT IN THE RT NOSE COMPARTMENT HAS 2 EA CRACKS AT FRAME C.  MADE AIRWORTHY REPAIR IAW SRM 51-20-02-0, 51-40-11, AND 51-40-13.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F      A33EU                        
20070412000252007041200025EU  2007       4          12         THMN4346177      120070410G5340                ATTACH BRACKET                          AMD   FALC10FALCON10    2730101EU                                                               LT NLG DOOR     CRACKED         B  T0DRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE03101HS                       82                                      LT NOSE LANDING GEAR DOOR ATTACH POINT IN THE LT NOSE COMPARTMENT HAS 2 EA CRACKS AT FRAME C.  MADE AIRWORTHY REPAIR IAW SRM 51-20-02-0, 51-40-11, AND 51-40-13.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                2L72 4F      A33EU                        
20070412000262007041200026EU  2007       4          12         THMN4346179      120070410G5320                SPLICE PLATE                            AMD   FALC10FALCON10    2730101EU                                                               FUSELAGE        CRACKED         B  T0DRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      CE03101HS                       82                                      SPLICE PLATE ON RT SIDE OF CABIN AT FRAME 13 JUST BELOW WINDOW LINE CRACKED.  MADE AIRWORTHY REPAIR IAW SRM 51-00-01 FIG. 201 AND 51-40-11.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F      A33EU                        
20070614001442007061400144CE  2007       6          14         TIMR20070003     120070521G3233998201233       ACTUATOR                                BEECH 99    B99         1154004CE                                                               NLG DOOR        SEPARATED       E  TIMAA   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      NM07950AA388                    U159                                    DURING CRUISE, PILOT HEARD A CLUNK AND THE -GEAR IN TRANSIT- LIGHT CAME ON.  RETURNED TO AIRPORT, PERFORMED FLY-BY WHICH CONFIRMED NOSE GEAR HANGING OUT BUT NOT FULLY EXTENDED.  NOSE GEAR COLLAPSED ON LANDING.  INVESTIGATION REVEALED THAT THE ACTUATOR SHAFT HAD SHEARED JUST ABOVE THE CLEVIS BOLT CONNECTING TO THE DRAG BRACE.                                                                                                                                                                                                                                                                                                                                                                                                          1L72 3T      A14CE                        
20071130001792007113000179CE  2007       11         30         TIMR20070008     120071031G3230                SWITCH                                  BEECH 99    99A         1154003CE  PWA   PT6   PT6*        52043EA                              POWER LEVER     INOPERATIVE     B  TIMAA   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            CLCLIMB          1                      NM07899CA                       U104                                    GEAR-IN-TRANSIT LIGHT DID NOT EXTINGUISH AFTER TAKE-OFF AND GEAR UP. PILOT CYCLED GEAR AGAIN WITH SAME RESULT.  PILOT RETURNED TO DEPARTURE AND LANDED.  MECHANIC FOUND THAT THE LT POWER LEVER SWITCH HAD FAILED.  REPLACING THE SWITCH RESOLVED THE PROBLEM.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                  1L72 3T3  T  A14CE   E2NE                 
20071204002972007120400297CE  2007       12         4          TIMR20070009     120070928G3233993880011       ACTUATOR                                BEECH 99    99          1154002CE  PWA   PT6   PT6*        52043EA                              MLG             CRACKED         B  TIMAA   UNSCHED LANDING                                                                                 J  WARNING INDICATION                                                            APAPPROACH       1                      NM074381Y     961               U71                                     AFTER SELECTING GEAR DOWN ON APPROACH, THE PILOT NOTICED THAT HE DID NOT HAVE A GREEN (SAFE) INDICATION FOR THE NOSE GEAR.  HE FOLLOWED THE EMERGENCY PROCEDURE TO PUMP THE GEAR DOWN BUT WAS UNABLE TO BUILD UP PRESSURE OR GET A GREEN LIGHT. PILOT THEN LANDED AND THE NOSE GEAR COLLAPSED.  INVESTIGATION FOUND THAT THE LT MAIN GEAR ACTUATOR END CAP HAD CRACKED AND ALLOWED THE EMERGENCY SYSTEM FLUID TO VENT OVERBOARD, PREVENTING THE NOSE ACTUATOR FROM EXTENDING FULLY.                                                                                                                                                                                                                                                             1L72 3T3  T  A14CE   E2NE                 
20070507001902007050700190EU  2007       5          7          TL9R200700001    120070501G3240C200601004      BRAKE                                   AIRBUS330   A300*              EU                                                               MLG             MAKING METAL    B  TL9RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      GL13                                                                    BRAKE ROTORS DE-LINED (STARTED TO FALL APART) IN OPERATION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                     2L72 4F    RTA26NM                        
20070712001332007071200133NE  2007       7          12         UE5R02           220070705G7210310825401       GEARBOX                                 AIRTRCAT602 AT602       0390309SW  PWA   PT6   PT6A60      52043NE                                              CORRODED        B  UE5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA61                                        PSRG0056                    PT6A-60AG REDUCTION GEAR REAR HOUSING P/N 3106854-01 HAS SEVERE CORROSION ON OUTER SURFACE OF HOUSING. DEEP PITTING, SOME AREAS UP TO .125 INCH DEEP. CORRODED AREAS EXTEND THE ENTIRE CIRCUMFERENCE OF HOUSING, PRIMARILY NEXT TO MATING FLANGE FOR FWD HOUSING.                                                                                                                                                                                                                                                                                                                                                                                                                                                                               1L71 3T4  TNCA19SW   E4EA                 
20070917000712007091700071EA  2007       9          17         UE5R04           220070911G7250T102401100      BLADES                                  BEECH 99    99          1154002CE  PWA   PT6   PT6A28           EA                              TURBINE SECTION CRACKED         B  UE5RO   OTHER                                                                                           O  OTHER                                                                         NRNOT REPORTED   1                      EA61                                                                    DURING STRETCH CHECK OF TURBINE BLADES P/N T102401-100, FLUORESCENT PENETRANT INSPECTION WAS PERFORMED.  THIS INSPECT REVEALED SEVERAL BLADES WITH CRACKS ALONG TRAILING EDGE. THESE CRACKS IN THE DIRECTION OF THE CHORD OF THE BLADE.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1L72 3T4  T  A14CE   E4EA                 
20070416000522007041600052NE  2007       4          16         UE5R1            220070402G72303023401         BLADE           PWC                     BEECH 100   100BEECH    1152916CE  PWC   PT6   PT6A67AG    52211NE                              COMPRESSOR DISC CRACKED         B  UE5RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      EA61                7P070                                               COMPRESSOR TURBINE DISC BLADE FAILURE. SINGLE BLADE IN COMPRESSOR TURBINE DISC CRACKED IN FUR TREE AREA OF BLADE. CAUSED MISALIGNMENT OF CT BLADE AND SUBSEQUENT RUB ON SHROUD SEGMENTS. THE CRACK IN FIR TREE WAS NOT VISIBLE WITH ENGINE SPLIT IF PERFORMING A ROUTINE INSPECTION, HOWEVER BLADE MISALIGNMENT AND RUB WERE VISIBLE. THE BLADE CRACK BECAME VISIBLE WHEN CT DISC ASSY WAS REMOVED FROM ENGINE.                                                                                                                                                                                                                                                                                                                                 1L72 3T4  T  A14CE   E26NE                
20070817000962007081700096SW  2007       8          17         WGEA200700001    120070803G2752EM41165         ACTUATOR                                ECLIPSEA500 ECLIPSEEA5003350000SW                                                               T/E FLAPS       MALFUNCTIONED   C  WGEAK   NONE                                                                                            F  FLT CONT AFFECTED                                                             DEDESCENT        1                      EA27109DJ205  205               000006                                  FLAP FAIL CAS MESSAGE IN FLIGHT.  REMOVED AND REPLACED LT AND RT INBOARD FLAP ACTUATORS PER EA 500 AM CH 27-51-11.  RIGGED FLAP`S AND COMPLIED WITH SATISFACTORY FUNCTIONAL/OPERATIONAL CHECKS.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1L72 4J    RTA00002AC                     
20080111001362008011100136CE  2008       1          11         WSA12262007      120071226G1400998100611       BOLT                                    BEECH 200   200BEECH    1152920CE                                                               MLG             MISMANUFACTURED B      K   NONE                                                                                            W  INADEQUATE Q C                                                                ININSP/MAINT     1                      SW171558                        BC20                                    HAVE ORDERED FROM MFG THE LANDING GEAR DRAG LEG BOLTS TWICE AND HAVE RECEIVED (2) DEFECTIVE BOLTS EACH TIME. THE COTTER PIN HOLE WAS MISDRILLED AND WOULD COULD NOT GET THE HOLES TO LINE UP WITH THE NUT CASTELLATION. (2) OF THE BAD BOLTS WERE DATE TAGGED 12/2/2006. THE ACTUAL BOLT MANUFACTURER IS UNKNOWN ALTHOUGH THEY WERE SOURCED FROM AC MFG. IT IS BELIEVED THAT AC MFG HAS PULLED THESE FROM THEIR INVENTORY AFTER OUR PROBLEM.                                                                                                                                                                                                                                                                                                    1L72 4T      A24CE                        
20070808000632007080800063EU  2007       8          8          WTU0701          120070719G2435150SG122Q       STARTER GEN                             SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              ENGINE          SEIZED          B  R8RRA   UNSCHED LANDING                                                                                 BJ SMOKE/FUMES/ODORS/SPARKS  WARNING INDICATION                                  CRCRUISE         1                      WP075204Y10   10                3101        9782                        WHILE CONDUCTING A SEARCH OVER MOUNTAINOUS TERRIAN AT NIGHT UTILIZING AN SX-5 SEARCHLIGHT, TEN MINUTES INTO THE SEARCH LIGHT QUIT WORKING.  APPROXIMATELY 30 SECONDS LATER THE GENERATOR FAIL LIGHT ILLUMINATED AND THE CREW SMELLED SMOKE IN THE COCKPIT.  APPROXIMATELY 30 SECONDS LATER THE FIRE LIGHT ILLUMINATED.  THE PILOT IMMEDIATELY EXCEUTED EMERGENCY PROCEDURES BY TURNING OFF THE GENERATOR AND LAND AS SOON AS PRACTICAL.  AFTER THE PILOT LANDED AND SHUTDOWN THE AIRCRAFT THEY EXITED AND SAW SMOKE COMING OUT OF THE STARTER GENERATOR COOLING DUCT TUBE.  THE CREW OPENED THE ENGINE COWLING AND THERE WAS NO FIRE BUT EVIDENCE THAT THERE MAY HAVE BEEN ONE INSIDE THE S/G.  UPON REMOVAL THE S/G HAD A SHEARED SHAFT IT WAS 1G71 3U3  U  H9EU    E19EU                
20070906000202007090600020EU  2007       9          6          WTU0702          120070828G2435150SG122Q       STARTER GEN                             SNIAS 350   AS350B2     8680813EU  TMECA ARRIELARRIEL1D1   60053NE                              ENGINE          INOPERATIVE     B  R8RRA   UNSCHED LANDING                                                                                 HJ ELECT. POWER LOSS-50 PC   WARNING INDICATION                                  CRCRUISE         1                      WP07455AE15   15                3509        9576                        WHILE CONDUCTING A ROUTINE PATROL AT NIGHT THE GENERATOR FAILED AND WOULD NOT RESET.  ALL NON ESSENTIAL EQUIPMENT WAS SHUTOFF AND THE PILOT RETURNED TO BASE UTILIZING BATTERY BUSS POWER WITHOUT FURTHER INCIDENT.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                             1G71 3U3  U  H9EU    E19EU                
20070612001492007061200149NE  2007       6          12         Y4MR200700521    220070521G7200PT6A135         ENGINE                                  BEECH 90    F90         1152909CE  PWA   PT6   PT6A135     52043NE                              RIGHT           MAKING METAL    B  W1MAE   ENGINE SHUTDOWN                                                                                 J  WARNING INDICATION                                                            CRCRUISE         1                      SO0989CA 6546 3399              LA152       PCE92418                    DURING CRUISE, RT ENGINE CHIP DETECTOR ILLUMINATED.  OTHER RT ENGINE INDICATIONS WERE MONITORED CLOSELY FOR ANY SIGN OF MECHANICAL PROBLEM.  NO OTHER INDICATIONS THAT WOULD SUGGEST MECHANICAL PROBLEMS WERE NOTED AT THAT TIME.  THE CHIP LIGHT WENT OUT WITHIN A FEW MINUTES AND PILOT CONTINUED TO CLOSELY MONITOR RT ENGINE INDICATIONS.  PRIOR TO START OF DESCENT (FROM 15000) FOR DESTINATION AIRPORT (BHM) PILOT NOTED SMALL FLUCTUATION IN RT ENGINE OIL PRESSURE FOLLOWED BY TORQUE FLUCTUATION (APPROXIMATELY 200 LBS); ITT INDICATION WAS STABLE.  DECLARED AN EMERGENCY, SECURED ENGINE AS PRECAUTIONARY MEASURE, AND LANDED AT THE NEAREST AIRPORT WITHOUT INCIDENT.  MAINTENANCE WAS DISPATCHED TO INVESTIGATE AND UPON INSPECTI1L72 4T4  T  A31CE   E4EA                 
20071016000752007101600075NM  2007       10         16         Y5CR200700001    120071005G6320369D2512311     BEVEL GEAR                              DOUG  MD500 MD500E      3027372NM                                                               M/R GEARBOX     BROKEN          B  Y5CRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP05          687                                                       PART OF TOOTH ON INPUT BEVEL GEAR BROKEN OFF.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                   1G72 3U    NC                             
20071205000582007120500058NM  2007       12         5          Y5CR200700002    120071120G6510                JOURNAL                                 DOUG  MD500 MD500E      3027372NM                                                               TAIL ROTOR      BROKEN          B  Y5CRK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      WP05     3149                                                           BEARING JOURNAL BROKEN OFF ON OUTPUT PINION.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                    1G72 3U    NC                             
20070614002212007061400221EU  2007       6          14         YNTA20070001     120070516G2750                FLAP SYSTEM                             HAWKERBAE125BAE125700B  7450007EU                                                               TE FLAPS        INOPERATIVE     E      L   ABORTED APPROACH                                                                                O  OTHER                                                                         APAPPROACH       1                      SW05281B                        281                                     ON APPROACH, THE FLAPS BECAME STUCK AT 15 DEGREES. AFTER TRYING THE FLAPS 25 DEGREE SETTING NOTICED THE FLAPS DID NOT MOVE FROM THE 15 DEGREE POSITION. RESET THE FLAPS TO THE 15 DEGREE POSITION AND UP TO 0 DEGREE, NO MOVEMENT WAS NOTED. RESELECTED THE FLAPS TO 15 DEGREE EXECUTED A GO-AROUND WITH TOWER. REFERRED TO THE CHECK LIST FOR NO FLAP LANDINGS, NOTED THAT THERE IS NO LANDING DISTANCE DATA. DECLARED AN EMERGENCY DUE TO ABNORMAL LANDING CONFIGURATION. THE SIC BRIEFED THE PASSENGERS ON THE SITUATION.  AFTER LANDING, TAXIED OFF THE RUNWAY INTO A RUN-UP AREA SHUT THE AIRCRAFT DOWN. MET WITH FIRE DEPARTMENT LOOKED AT THE TIRES AND BRAKES , NOTICED NO SMOKE OR FIRE. AIRPORT OFFICIAL SAID THEY SAW NO SMOKE ON LAN2L72 4F    RTA3EU                         
20070205000452007020500045    2007       2          5          ZB0R20070001     420070131G3197                WIRE                                    CESSNA172   172S        2072439CE                                                               INSTRUMENT PANELCHAFED          B  ZB0RC   ABORTED TAKEOFF                                                                                 B  SMOKE/FUMES/ODORS/SPARKS                                                      TOTAKEOFF        1                      SO056026S                       172S10206                               PILOT REPORTED SMOKE ODOR AND STANDBY INSTRUMENT LIGHTS FLICKERED ON RUN-UP PRIOR TO TAKEOFF. INVESTIGATION REVEALED WIRE BUNDLE WHICH CONTAINS THE POWER WIRE FOR THE STANDBY INSTRUMENT LIGHTS WAS CHAFING ON THE LOWER LEFT CORNER OF THE AUDIO PANEL RACK. MAINT REPLACED A SECTION OF THE AFFECTED WIRE. OPS CK GOOD.                                                                                                                                                                                                                                                                                                                                                                                                                      1H71 3O    NT3A12                         
20071023001682007102300168EA  2007       10         23         ZB0R20070002     220071015G7322105220          CARBURETOR                              CESSNA150   152         2071835CE  LYC   O235  O235*       41505EA                              ENGINE          LEAKING         B  ZB0RK   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA3995300     1413              15285871    L2379515                    DURING PROGRESSIVE INSP, FOUND CARBURETOR BOWL LEAKING AT GASKET. BOLTS WOULD NOT TIGHTEN - STRIPED THREADS.  REPLACED CARBURETOR TO CORRECT DISCREPANCY.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                       1H71 3O3  ONT3A19    E223                 
20071023000222007102300022SO  2007       10         23         ZB0R20070003     120071015G32339686002         ACTUATOR                                PIPER PA34  PA34200     7103405SO  LYC   O360  IO360A1A    41514EA                              NLG             LEAKING         B  ZB0RK   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA3915412                       347350060                               DURING GEAR MAINTENANCE, FOUND NLG ACTUATOR LEAKING. INSPECTION REVEALED WORN SEALS. REPLACED SEALS BUT STILL LEAKED. FURTHER INSPECTION WITH BORESCOPE IN BODY OF ACTUATOR REVEALED LONGITUDINAL SCORING ON INSIDE WALL OF ACTUATOR BODY. REPLACED ACTUATOR TO CORRECT DISCREPANCY.                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L72 3O3  O  A7SO    1E10                 
20071023001742007102300174EA  2007       10         23         ZB0R20070004     220070915G8520LW18840         CAM                                     PIPER PA28  PA28R200    7102811SO  LYC   O360  IO360A1A    41514EA                              ENGINE          WORN            B  ZB0RA   UNSCHED LANDING                                                                                 R  PARTIAL RPM/PWR LOSS                                                          CLCLIMB          1                      EA3941331     1216              28R7435169  L1561051A                   ON CLIMB-OUT, PILOT NOTICED LOW POWER. RETURNED TO AIRPORT. MAINTENANCE INSPECTION REVEALED BELOW MINIMUM VALVE TRAVELS FOR ALL INTAKE VALVES. REMOVED NR 1 CYLINDER.  FOUND CAM LOBES SEVERELY WORN AND TAPPETS CORRODED AND WORN IN A CONCAVE MANNER.  ENGINE REPAIRED BY SERVICE CENTER.  REINSTALLED ON ACFT.  ALL SYSTEMS OPS CK NORMAL.                                                                                                                                                                                                                                                                                                                                                                                                   1L71 3O3  O  2A13    1E10                 
20071023001772007102300177EA  2007       10         23         ZB0R20070005     220071001G8530                CYLINDER                                CESSNA150   152         2071835CE  LYC   O235  O235*       41505EA                              NR 2            LEAKING         B  ZB0RK   NONE                                                                                            K  FLUID LOSS                                                                    ININSP/MAINT     1                      EA3995300                       15285871    L2379515                    DURING PROGRESSIVE INSP, FOUND NR 2 CYLINDER UPPER TOP THROUGH BOLT LEAKING SEVERELY.  REMOVED ENGINE FOR REPAIR.  REINSTALLED AFTER REPAIR BY SERVICE CENTER. (CASE WAS FOUND FRETTING AND BEARING WEAR WAS EVIDENT AT BOLT LOCATION).                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         1H71 3O3  ONT3A19    E223                 
20071204000722007120400072SO  2007       12         4          ZB0R20070006     120071102G573062061002        SKIN                                    PIPER PA28  PA28R200    7102811SO  LYC   O360  IO360A1A    41514EA                              RT WING         CRACKED         B  ZB0RK   NONE                                                                                            O  OTHER                                                                         ININSP/MAINT     1                      SO05151434617                   28R7335027                              DURING PROGRESSIVE INSPECTION, DISCOVERED WING WALK ON RT WING SPONGY. INSPECTION REVEALED SUBSTRATE REINFORCEMENT CRACKED IN SEVERAL LOCATIONS. REPLACED WING WALK.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            1L71 3O3  O  2A13    1E10                 
20071204000812007120400081CE  2007       12         4          ZB0R20070008     120071102G2560                DETECTOR                                CESSNA172   172S        2072439CE  LYC   IO360 IO360L2A         EA                              CARBON MONOXIDE INOPERATIVE     B  ZB0RO   OTHER                                                                                           J  WARNING INDICATION                                                            CRCRUISE         1                      SO056045785   85                172S10212                               CARBON MONOXIDE DETECTOR FAILED. SECOND FAILURE WITHIN 6 MONTHS                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                 1H71 3O3  ONT3A12    1E10                 
20080108003752008010800375SO  2008       1          8          ZB0R20070009     120071214G760389307000        ROD END                                 PIPER PA34  PA34200     7103405SO  LYC   O360  IO360C1E6   41514EA                              FUEL CONTROL    SEPARATED       B  ZB0RE   ENGINE SHUTDOWN                                                                                 O  OTHER                                                                         CRCRUISE         1                      EA3915412376  39                347350060                               IN CRUISE, PILOT ATTEMPTED TO REDUCE POWER FOR MANEUVERS PRACTICE. LT ENGINE WAS UNRESPONSIVE. INSTRUCTOR IDENTIFIED LT ENGINE THROTTLE PROBLEM, ENGINE RPM WAS STABLE AT NEAR FULL POWER. RETURNED TO HOME BASE. PILOT FEATHERED AND SHUTDOWN LT ENGINE ON APPROACH. MAINTENANCE DISCOVERED LT ENGINE THROTTLE CONTROL ROD END AT FUEL CONTROL HAD SEPARATED.                                                                                                                                                                                                                                                                                                                                                                                  1L72 3O3  O  A7SO    1E10