boeing/aviation-ner-BIO huggingface dataset:
the flight crew reported the pitch trim did not work with auto-pilot electric pitch trim on both the left and right side below 200kts on descent . operations were continued under mel 27-31-01 . the base maintenance team determined the elevator electric trim motor servo drum drive shaft required adjustment per amm . ops checks were satisfactory and the aircraft was returned to service .
ship 3715 -div / press- diverted to aus due to cabin altitude climbing to 10,000ft . crew donned o2 masks , declared emergen cy and descended to fl100 . unable to make atl with fuel on board . corrective action : performed cpc 1-2 bite test iaw b73 7 amm . performed cabin zone temp controller bite . no trouble found . ops checks good .
efis comp mon caution inflight . roll pitch hdg yellow flags . hdg red flags displayed as well . fos hsi unreliable , cas hsi unreliable as well . qrh did not fix the issue , flight diverted . gps was also unreliable . ( flight 3112 filed closed ) this discrepancy was transferred to camp item 27206304 with the following corrective action : " troubleshot efis comp mon in flight in reference to fim 34-25-00-810-804 . performed opeerational check of ahrs # 1 and ahrs # 2 in reference to amm 34-21-01 . performed operational check of gps # 1 and gps # 2 in reference to amm 34-58-00 . all operational checks are good at this time . interrogated mdc for faults associated with efis comp mon in flight in reference to amm 45-45-00 . found faults for ahrs # 1 , ahrs # 2 , tcas all at the same time . no current faults . removed and replaced hirf # 1 and hirf # 2 in reference to amm 22-12-08 . ops check good at this time . complied with crj7 / 900 cat ii return to service test task card : 34-220-1008-sky . ! ! ! ! aircraft remains qualified for cat ii status ! ! ! ! "
aircraft was grounded : an emergency was declared and the aircraft returned to phx . flight crew reported blue hydraulic loss of pressure after generator 1 kicked off line then recovered . the aircraft landed safely at phx and taxied to the ga te under its own power . * * supplemental report will be submitted * * ( open )
ship 9523 -hyd / de- the crew received a " hyd r qty low " message at top of climb . they were unable to repressurize the sys tem . the qrh was complied with and performed the alternate gear extension ( due to a right hydraulic system low quantity ) . an emergency was declared with atc and the landing was uneventful . corrective action : maintenance replaced the electri c auxiliary hydraulic pump and the right main landing gear door ( due to runway contact on landing ) . the ship has returne d to service . ( lp # 4580142 )
cabin floor panel 232gf is dented on upper surface . / removed and replaced floorboard per amm 53-21-00 .
( can ) ac has threaded type fuse holders . in cruise , lost oil pressure indication on nr 2 engine . low pressure light did not come on , ( it 's on a separate press switch ) . pilot reduced nr 2 eng to idle . temp remained normal with no other changes in systems . an uneventful landing was completed . investigation revealed fuse holder had vibrated loose and caused fuse for oil pressure indication to lose contact causing a power loss for the indicator . about 10 other fuse holder caps were also found loose . fuse holder has no positive locking feature and as a result , now will be checking periodically . though not a terribly serious issue it is one that deserved mention as other mfg products may use same fuse holder .
during takeoff , the right hand engine sustained a bird strike . the aircraft aborted takeoff and returned to the field without further incident . maintenance inspected and replaced the propeller spinner in accordance with dornier maintenance manual 61-13-00 and the intake assembly in accordance dornier maintenance manual 71-63-00 . operational checks were performed and the aircraft was ferried to dayton where maintenance performed a borescope inspection in accordance with dornier maintenance manual 72-00-00 . the inspection showed no injestation and the aircraft was released for service .
rib corroded in the left elevator es 256.811 . removed , fabricated , and repaired iaw srm 51-40-02 , rev 41 , ei t2018p55m-6105 , and t2018a55m-6099 . installed iaw srm 51-40-02 , rev 41 , and dwg 65b03663 sh 2 and 3 .
on approach , on flair aircraft hit a bird . once on the ground the crew reported to maintenance personal who after inspecting the aircraft found a dent on the rt flap bottom skin . due to the location of the dent which was not covered under srm . support engineering was contacted and a engineering disposition was issued to return the aircraft into service . an inspection of the area is required approximately every 50 hour until repair is completed or another flap is installed .
damage found at rh no . 4 slat trailing edge , outboard , upper surface . completed # 4 slat installation per mm 27-80-30-400-802 item is closed .
ship 9521 -atb / gear- the crew declared an emergency and returned the aircraft to dtw following the failure of the nose landing gear-retract . corrective action : maintenance adjusted nose landing gear retract actuator . ( lp # 4110406 )
ship 3512 -de / misc- due to number 3 tire pressure low . corrective action : replaced number 3 and 4 tires . ( 8984382 )
# 2 fire light intermittent in flight . removed and replaced # 2 engine upper inboard fire detector iaw amm 26-10-00 , 4-1 .
main deck seat track : sta . 1731-1741 lbl = 75.25 - worn . removed and replaced seat track at sta 1731 -1741 lbl 75.25 per srm 53-70-00 fig 1 vol1 and fedex drwg sr10-53-002 and srm51-31-01 vol2 and srm 51-41-01 vol 2
aborted takeoff greater than 100 knots due to an e / e door indication . corrective action : checked e / e door + tracks + sensor , no damage noted . pseu fault 215 thru 202 , 196 thru 194 . target test ok . replaced prox sensor per b767 amm 52-71 .
aircraft was grounded : an emergency was declared and the aircraft returned to ord due to the flight crew reporting that on takeoff before flap retraction , they received an ecam message for engine 1 high risk egt . engine showed overtemp . egt was considerably higher than the other engine for the entire flight and taxi in . the aircraft landed safely at ord and taxied to the gate under its own power . maintenance found both lower egt thermocouples 4012ks2 ( aala202407053143 ) and 40 12ks3 ( aala202407052331 ) damaged on the # 1 engine . maintenance replaced the thermocouples and accomplished a satisfactory .
atb - air / gnd disagree status message appeared . communicated this to flt control and amc . we were directed by artr to re turn to sdf ref alert t 181888.accomplished mlg tilt sensor adj / test iaw amm 32-09-07 and amm 32-09-03 . found pseu to fa il r / h tilt sensor st68 near on ground , replaced sensor 5268r gear tilt sensor per amm 32-09-13 , sensor now shows fan on ground . ops chks and test good .
returned to field due to bird strike . *s / d* bird strike caused right engine damage . replaced fan blade set and nose cowl . borescoped 6th stage blades , checked ok . accomplished vibration survey , checked ok .
while performing a preflight inspection the pilot found the aft spinner bulkhead cracked at the edge where the prop exits the spinner . removed prop and installed new spinner bulkhead p / n 0550321-12 .
ship 8127 - misc / de - declared emergency due to gear fail msg . crew did receive all 3 gears down and locked indicating g reen . flight landed safely . corrective action : r / r lgcl per a220 amp 32-31-07 . performed alternate lgscu 1a and 2a per a220 amp 32-30-00 . both tests passed . ( lp # 5668780 )
evidence of corrosion on bottom of main deck seat track sta 960 to 980 rbl 34
on climb at 7,000 ft crew reported flight control malfunction . in both autopilot and manual mode flight controls unrespo nsive . crew diverted to kriv with an emergency declaration . landing was uneventful and no additional precautionary acti ons . on arrival the aircraft was grounded for unscheduled maintenance . supplemental information to previous submittal i xxa202309011056 on 11 september 2023 at kiln . iaw b767 fault isolation manual ( fim ) 22-02-815 and 22-04-811 the followin g flags were noted : no infc fcc l auto trim vld ? and left sam fault ball sam . removed and replaced left stab trim and a
aircraft was grounded : an emergency was declared and the aircraft returned to phx . on climb flight crew noticed oil quan tity 2.5 quarts , crew started to move the throttle for engine one to idle then low oil pressure and crew shut engine do wn as per ecam . the aircraft landed safely at phx without further incident . * * supplemental report for aala202303148086 : replaced left engine per task card 26l40071001 * * ( closed )
inspection type : segmain cargo compartment floor panel 231xcf damagedfabbed panel 231xcf from 5024n400001ss-g batch # 348 9461 per sreo b757-5320-9692-k
aircraft was grounded : an emergency was declared and the aircraft diverted to msp due to the # 1 engine stalling messafge during cruise at fl320 . flight crew also reported there was an # 1 engine n2 advisory engine vibes at 4.7 . flight crew d escended to fl 240 and noted a reduction in oil quantity to 1.0 with vibes at 9.0 flight crew shut down the # 1 engine . the aircraft landed safely at msp and taxied to the gate under its own power . maintenance replaced the engine per task card 26l40071001 . * * ( closed )
lt pack inop due burning odor above pack area . removed and replaced hot air line hose as per amm 21-51-10-434-043 and lt pack leak and ops checks ok .
flaps / slats stuck 15 / 15 on departure . emergency declared . qrh followed . flaps overspeed at 15 / 15 to approx 225 kts . * * * emergency declared * * * ref tsi 27-80 / 6666 for rh wing # 1 slat screwjack torque indicator found tripped . all servicing and other work performed on tsi . rh # 1 slat screwjack mpn : cha 1237-002a / / msn : 2413 . serviced # 1 r / h s lat jack screw per mm ops check good . ref amm 12-13-27 , 12-22-27 , 27-84-00 , and tsm 27-80-02
on final approach aural warning " to low gear " with gear handle down and three green lights . kiln air traffic control tow er confirmed the gear was extended . crew conferenced maintenance operations control , cpo and made the decision to shoot the approach and land into kiln . an emergency descent was declared and air rescue and fire fighting support ( arff ) reque sted . landing was without incident and no precautionary arff nterventions . on arrival , aircraft was grounded for mainten ance . upon inspection , line maintenance isolated fault to s4 microswitch in the landing gear lever module intermittentl
aircraft was grounded : an emergency was declared and the aircraft returned to phl due to the flight crew reporting the l oss of the green hydrauilic system quantity shortly after departure . the aircraft landed safely at phl without further i ncident . * * supplemental report for aala202407151665 : maintenance found a ruptured hydraulic line in the left pylon and r eplaced it . a satisfactory leak / operational check was accomplished . * * ( closed )
aircraft was grounded : an emergency was declared and the aircraft returned to dfw . on departure climb received ecam mes sage for air engine 1 bleed abnormal pressure . flight crew accomplished the ecam actions and landed safely at dfw withou t further incident . maintenance replaced # 1 engine high pressure bleed valve and accomplished a satisfactory operational check .
exit sign lens at the r2 door was found damaged . replaced the lens iaw amm 33-51-01 .
aircraft was grounded : on takeoff the number 1 engine did not develop full takeoff thrust at 26 k max . number 1 showed 98.7 should have been 100.7 n1 low speed reject at 75 knots . **supplemental report for aala202305047739 : replaced engine 1 fuel pump per amm 73-11-11 ( aala202305047739 ) , hydromechanical unit per job card 08l40073001 ( aala202305119633 ) , and servo fuel heater per amm 73-11-07 ( aala202305115493 ) . accomplished satisfactory power assurance run per job card 08l40072006 and leak check per amm 71-00-00.** ( closed )
flt # 2549 , fll-sdq . ( aircraft performed an air turn back to fll ) 'loud bang at 6k ft . followed by eng2 fail ecam . ' ( supplemental information to follow )
aircraft was grounded : aircraft diverted to dfw due to the flight crew reporting that while climbing through fl230 ecam message for engine 2 fuel filter clog came on at 13452 and went out at 14052 during cruise at fl280 . the aircraft landed safely at dfw without further incident . maintenance replaced # 2 engine fuel filter per task card 26c40073002 and the # 2 engine differential pressure switch per amm 73-34-15 .
aft cargo tie down rail corroded between bs 947 to bs 927 , lbl 3 . r and r tie down iaw srm and dwg .
aircraft was grounded : an emergency was declared and the aircraft diverted to clt . flight crew reported an engine 2 fade c a fault on climb out that went away followed by engine 2 fadec b fault and then engine 2 fuel control fault at cruise . flight crew decreased engine power setting to idle . the aircraft landed safely at clt and taxied to the gate . maintenan ce replaced engine 2 electronic control unit per task card 26l40073008 and accomplished a satisfactory operational check .
ship 9543 -div / de- the crew diverted the aircraft to mem and declared an emergency on approach due to the right generato r failing and the apu already on mel deferral . corrective action : maintenance replaced the apu ecu , the right pcdu , the left and right bus tie relays , and the right generator relay . operational check was good and the aircraft returned to serv ice . ( lp # 4680524 )
aircraft was grounded : an emergency was declared and the aircraft returned to dfw due to eicas message anti ice wing . aircraft landed safely at dfw without further incident . maintenance replaced wing anti-ice zone control card # 3 per amm 30-11-03 .
ship 9501 -misc / de- the " tailcone unlock " master caution illuminated three times during flight . the qrh was complied wit h and an emergency was declared by atc for the crew . ewr maintenance cleaned the connector plugs of both the internal an d external tailcone unlock switches . the dcu was also replaced per amm 31-43 . the operational test was good . the " tailco ne unlocked " master caution message has not returned . the aircraft is ok for service . no thirty day history . ( lp # 528762 4 )
aircraft was grounded : the aircraft diverted to dfw . hot brakes after take off , crew cycled the gear per the qrh and not ed that the gear would not retract and had multiple ecam messages for hot brakes , landing gear doors not closed , landing gear not uplocked and landing gear shock absorber fault . the aircraft diverted to dfw with the gear down and landed saf ely without further incident . * * original report was aala202306195151 * * maintenance replaced the # 2 brake assembly per am m 32-42-27 . maintenance also found the nose landing gear support mounting bracket for proximity sensors bolt was loose /
aircraft was grounded : engine 1 reverser unlock in flight , engine 1 shut down by flt crew as precaution . flight continue d to phl and declared and emergency and landed without incident . maintenacne found tr sync lock actuator to be at fault . replaced sync lock actuator iaw amm 78-31-19 .
inspection type : n / a * * sdr filed open * * diversion * * on approach , ap1 disconnected and w / not re-engage in cmd . deferred # 1 auto pilot per mel 22-18-01-2-0-1 control # m802916 . pitch trim # 1 disconnected and w / n re-engage . c / w a300 tsm 22-20-00 . ops c k normal .
after takeoff crew observed pitch trim fault cas message and experienced increased back pressure on the yoke during climb out . crew performed qrh procedures , switching to stby trim and executed divert to nearby airport . aircraft landed without incident .
aircraft was grounded : an emergency was declared and the aircraft diverted to tpa due to at cruise , left engine oil temp erature rose to yellow arc eventually rising to red line . oil quantity dropped to a low of 3 quarts . oil temp indication failed . crew shutdown left engine . aircraft landed safely at tpa . * * supplemental report for aala202307201104 : maintenan ce replaced left engine per job card 08l40072003 . accomplished satisfactory operational checks . * * ( closed )
( aus ) nr 2 engine bird strike . investigation could find no airframe damage or evidence of engine core ingestion . bird debris exited via bypass duct . nr 12 fan blade damaged beyond limits .
aircraft was grounded : an emergency was declared into den due to the flight crew reporting that while configuring for ap proach from flap 1 to flaps 2 , receiving a flight control system 2 fault and flight control flaps locked ecam messages . the flight crew accomplished ecam procedures which did not resolve the issue . the aircraft landed safely at den and taxi ed to the gate under its own power . * * original report was aala202406280797 * * maintenance replaced the right-wing interco nnecting strut proximity sensor 40cv per amm 27-51-44 and the # 2 slat flap control computer per amm 27-51-34 ( aala202407
flt # 1592 , fll-nas . ( aircraft declared an emergency ) '' fo side windscreen cracked 15000 / 315 kts . no birdstrike or fod no ted by crew ; ref lp 3524325 , item 1 ( installed f / o '' s window iaw 56-11-11 . ) for removal and replacement of f / o '' s windshie ld . this clears mddr 521831 . placard removed . mx-4 updated . mcc notified . ''
on climb out from hma , the mgb bypass light illuminated . performed ep and returned for landing .
ship 9586 -atb / hyd / de- the crew returned the aircraft back to msp and declared an emergency with atc during the approach due to the loss of the right hydraulic system fluid quantity . the landing gear was extended using the alternate gear ex tension procedures . the landing was uneventful except for the main gear doors contacting the runway . corrective action : maintenance found a b-nut on the transfer line to be loose and tightened it . all of the hydraulic pumps used without eno ugh fluid were replaced . the main gear doors were repaired . ( lp # 5939976 )
aircraft was grounded : an emergency was declared and the aircraft diverted to stl . flight crew reported that during crui se at fl 350 they lost # 2 engine epr and n1 degraded message occured . crew accomplished qrh procedures and the aircrft l anded safely at stl without further incident . maintenance replaced the p2 / t2 probe per task card 26l40073005 .
during ap test , yaw trim and ap2 failed . troubleshooting revealed yaw breakout does not display on logics page in maintenance mode . removed and replaced yaw trim motor iaw amm 67-14-00 , 4-1 .
ship 9584 -atb / gear / de- following takeoff and landing gear retraction , the crew received a " left main gear unsafe " messa ge . an emergency was declared , and the crew returned the aircraft to atl and landed without further incident . corrective action : maintenance replaced the left main landing gear door latch cylinder in ref b717 amm 32-34 . operational and leak checks were good . gear functional check was good . ( lp # 5296266 )
on takeoff roll ingested a bird in left engine , aborted takeoff and returned to block . preliminary inspection found evidence of ingestion noted on engine inlet and exhaust . inspected lt engine as required , cleaned remains of bird from intake . borescoped engine as required , bird went through bypass duct only , no defects noted . all work performed iaw cessna 560xl mm chapter 5-50-00 section e and nja aaip .
during takeoff , a / c suffered bird strike , fodding out nr 1 engine . replaced engine .
flt no : mge301 . esi - rh eng egt at 520 idle power during taxi . r / r lcc per amm 75-24-01 performed eng run test 6 and test 13 . no defects noted per amm 71-00-00 .
aircraft was grounded : an emergency was declared and the aircraft returned to dfw due to the flight crew reporting brake system fault ( aala202311309870 ) and flight control spoiler 3 fault ( aala202311304225 ) messages occured during climbout . the aircraft landed safely at dfw and taxied to the gate . maintenance accomplished a satisfactory ground scan of both b rake steering control units along with a test of the brake pedal transmitter unit with no faults noted . maintenance was unable to duplicate the brake system 2 fault . maintenance found the flight control spoiler 3 fault was due to # 1 spoiler
aircraft was grounded : an emergency was declared and the aircraft diverted to ord due to the flight crew reporting a blu e hydraulic pump low pressure ecam along with circuit breaker 11 and 12 on the overhead panel popped in flight . the airc raft landed safely at ord and taxied to the gate . maintenance accomplished tsm 31-54-00-810-925-a , inspected blue hydrau lic system wires with no faults noted and reset the circuit breakers . while examining the wiring of the blue hydraulic s ystem maintenance found the blue electric pump phase -unbalanced detector / sensor inoperative and replaced it per amm 2
accessory gear [ pn : 3103590-2 ] bearing galled [ pn : 3103585-1 , sn : 13-151725-07567 , tsn : 4,525.7 , csn : 5,527 ] . resulted in failed soap report due to m50 platelet detection .
ship 3812 lt wing tank plate opening has fretting corrosion 532ab . corrective action : summary see nr for additional info rmation 003-0007:5700-2543 / 017 00397 cleaned area checked limits / repair ref : b737 srm 57-20- 01 repair 1 . ( 1318649 ) .
aircraft was grounded : an emergency was declared and the aircraft diverted to pwm due to the flight crew reporting that during cruise the engine page popped up and both oil quantities were fluctuating between 2 and 4 quarts and both oil pre ssures were in the red at 2 psi . the aircraft landed safely at pwm . ( note : this report is for # 2 engine , see aala2024061 45803 for # 1 engine ) * * supplemental report will be submitted * * ( open )
aircraft was grounded : aircraft diverted to pit due to the flight crew reporting a dirty sock smell just after takeoff t hrough cruise . maintenance isolated the source of the odor to the apu . * * supplemental report will be submitted * * ( open )
cracked beam nr 1 bs 206 . the beam was replaced iaw srm 51-41-02-0g , 51-41-04-0g , 51-41-05-0g , dwg 9911582 rev t , and 9 911579 rev l .
l valve ( wing anti ice ) caution light remained illuminated after selecting switch on . grounded - yes . accomplished left wing anti ice valve health check . ref amm 30-11-11-200-801 . anti ice valve ops normal . ok for service .
aircraft was grounded : an emergency was declared , and the aircraft diverted to akl and landed safely . 5 each lavatory went inoperative with screen saying fault red . **supplemental report will be submitted** ( open ) .
triple tach went to zero during flight . all other indications had rtr and n2s within the normal operating range . removed and replaced triple indicator rpm iaw 77-14-00 , 4-1 ; testflight successfully completed .
entrance stair extension : the entry door slams open with zero tension to support it / / corrective action / / checked all hardware and cables and verified no broken components . gained access to the main door balance drum . performed main door opening speed adjustment as required . performed ops-check and ops-check good . returned aircraft back to its original condition . work performed irw phenom 300 amm 52-10-00 .
aircraft was grounded : an emergency was declared during descent into sea due to the flight crew reporting a nose wheel s teering ecam fault message that occurred during cruise flight . flight crew accomplished ecam procedures and the aircraft landed safely at sea where the nose wheel steering system regained functionality resulting in the aircraft to taxi to t he gate under its own power . maintenance replaced the nose wheel steering servo control per amm 32-51-51 .
aircraft was grounded : an emergency was declared and the aircraft returned yellow hydraulic engine 2 system low pressure ecam in flight . flight crew observed hydraulic quantity as empty . ( open )
aircraft was grounded : emergency lights inoperable . maintenance replaced battery pack per amm 33-51-07 .