boeing/aviation-ner-BIO huggingface dataset:
aircraft was grounded : an emergency was declared and the aircraft diverted to orf due to the flight crew reporting airfr ame vibration at fl 280 . vibration stopped when we slowed to 270 knots . the aircraft landed safely at orf without furthe r incident . maintenance replaced the right-hand elevator outboard servo control actuator and the right-hand elevator in board servo control actuator ( aala202405252364 ) on the right-hand horizontal stabilizer due to excessive play . maintenan ce also replaced the elevator hinge fittings for positions 1 thru 6 on the left horizontal stabilizer and right horizont
khv - on takeoff , nr 1 engine compressor stalled at 140k with associated rise in egt to peak of 920 degrees and drop in n1 / epr . rejected takeoff . found evidence of bird ingestion . performed intake / exhaust inspection , nil damage noted . performed borescope inspection of nr 1 enigne / hpc stage 5 , 6 , 7 , 8 and 9 . found condition satisfactory . nil damage found . additional overtemp borescope to be performed within 80 flt hours . ( m )
suspected tail strike occurred on takeoff no indication in hud . grounded - yes . air turnback -- performed tail skid inspection ref b737-9 amm 05-51-32 and tail shoe inspection ref amm 32-71-00-211-801 . all inspection look good wear is below dimples .
after landing , nosewheel sterring tiller would not turn the nosewheel found bad connector pin at nose wheel steering electro hydraulic selector valve . removed and replaced pin " a " and connector assembly in ref to espm 20-44-00 ops normal in reference to amm 32-51-00
on takeoff roll crew reported bird strike and aborted takeoff at 130 knots . *s / d* found evidence of bird strike on nr 4 engine . inspected engine no damage found .
after takeoff during gear retraction master caution hyd and flt cont illuminated with both eng and elec hyd a sytem low pressure lights illuminating for 10-15 seconds . grounded - yes . air turnback - found a edp depressurization solenoid cannon plug backed off . r essary 82391 . replaced mw0312 harness ref mm71-51-03-400-801-f00 . op ck 's good . ( ref 60564037 and tsr715094 )
inspection type:3cl / h wing fixed l / e beaded doubler is cracked between sta . xos= 610.8-616.6.repaired cracked l / h wing f ixed l / e beaded doubler between sta xos-= 610.8-616.6 iaw srm 57-40-02 repair 15 fig . 205 . ( major )
aircraft was grounded : an emergency was declared comming into ord . in level cruise at fl 370 engine 1 and 2 stall . oat -64c , clean air . flight crew followed qrh and ecam procedure , descended to fl 270 and engine parameters returned t o normal . the aircraft landed safely at ord and taxied to the gate under its own power . note : see aala202401180715 for # 2 engine . * * supplemental report for aala202401184376 : engineering and ge reviewed the fdr data and concluded that both e ngines had experienced a beta stall . n1 dropped appoximately 30 % on both engines simultaneously which was likely the cau
while climbing out of rsw using ctr tank fuel , rh tank qty began to decrease . by level off fuel had decreased from 8800 to 7800 . crew ran qrh 12.6 fuel leak eng and diverted to jax . mech reported fuel under # 2 after shutdown . r and r fuel pro bes f7 , f9 , f10 for r / h fuel tank fuel indication ops checks good , iaw amm 28-41-21-000-801 .
en route the crew began to notice an alternator failure warning signals went off . crew notified atc to begin heading back or to land the aircraft at the nearest airport . shortly after the pic and copilot began to smell what they believed was a fire . pilot turned off switch to alternator and other electrical components . once on the ground they opened the engine cowling no evidence of smoke or fire however , they did discover a bolt that holds the wires connecting to the alternator was found broken .
'' supplemental infomation '' ship 180 -div / ifsd- diverted to lhr due to left engine compressor stall . flight crew shutdown engine on approach due to rising egt . corrective action : maintenance found metal in tail pipe , replaced left engine . ( 46 38134 )
on takeoff approx 500ft had bird strike in left engine . engine continued to run but had compressor stalls every few seconds ref l / p 8935556 for corrective action no caution lights in cockpit vibration was 2.6 below 65 percent n1 engine ran smooth did simulated single engine return . removed and replaced nr 1 engine .
aircraft was grounded : an emergency was declared during cruise enroute to sdq due to # 2 engine n1 dropped to 20 to 40 % . crew shutdown # 2 engine and landed safely at sdq without further incident . * * supplemental report for aala202308077234 : r eplaced # 2 engine electronic control ( eec ) per amm 73-21-60 . accomplished satisfactory operational test per amm 71-00-00 -700-818-f00 * * ( closed )
during climb at 1,000 feet , the aircraft encountered a flock of geese at which time the right engine ingested one bird . right engine epr dropped from 2 to 1.8 . crew reduced engine power and performed an air turnback to yqr where they landed without further incident . maintenance replaced the right engine .
aircraft was grounded : an emergency was declared and the aircraft diverted to dfw . during cruise ecam message gre reservoir low level flight crew followed ecam procedures and qrh follow up procedure . the aircraft landed safely at d fw without further incident . maintenance performed operational test of fluid low level warning per amm 29-31-00 , all tes t passed . no messages on ecam , fluid quantity on ecam and indicator is good . resevoir pressure is good per amm 12-14-29 . maintenance could not duplicate discrepancy .
aircraft in base maintenance : forward lavatory door difficult to open and close . door rubs on door jamb in flight . maintenance adjusted the lavatory door and accomplished a satisfactory operational check .
d ; radar altimeter 2 failed in flight . c / b out in mcdu.c ; mel 34-31-0acat : 'c " due 11 / 22landing gear €aural€ ? could not be cancelled at cruise . accomplished qrh procedure . radio altimeter 2 electronic cb is forced out in mcdu cb menu . ( flight 3746 filed closed ) nov 13 , 2023 station : san -- deferred radar altimeter # 2 per mel 34-31-0a . deactivated # 2 rad alt per amm procedure as required by mel . nov 14 , 2023 station : boi -- removed and replaced radar altimeter unit # 2 in reference to amm 34-31-01 . system ops check good at this time .
aircraft was grounded : tcas aural alert " tcas system test ok " continues in flight every 15-30 seconds , burning electrical odor from tcas box pulled cb k10 . maintenance replaced atc / tcas control panel ( aala202310025988 ) per amm 34-52-10 and tcas processor per amm 34-43-10 . ( aala202310027239 ) a satisfactory operational check was accomplished .
aircraft was grounded : an emergency was declared and the aircraft diverted to phx , after level off at fl270 ecam message fuel left wing tank overflood . crew accomplished qrh and ecam procedure . unable to reduce left wing tank fuel quantity . the aircraft landed safely at phx without further incident . maintenance replaced left hand center tank transfer valve actuator 11ql per amm 28-25-53 and accomplished a satisfactory operational check .
* atb * as advertised apu bleed valve closes above fl200 with apu bleed switch on . aircraft was at fl250 . crew caught thei r mistake in safety terminal area . air turn back per a300 aom 02.01.04.03 system operates normally . performed pack flow control and indicating test precautionary ref . amm 21-11-00 . checks good.ok for cont . service .
aircraft was grounded . l2 sliding window difficult to open and close . replaced l2 window with serviceable unit , iaw wo rkcard 56-94-01 . operations check good .
during the gear extension crew alerting system had left right inboard brake fail , following qrh procedures , messed up and still had a brake fault advisory . so we choose to divert to an airport 15 miles away with a longer runway so we could land safely in case of full brake failure .
lav waste showed full after level off in cruise . no toilets would flush . grounded - yes . diversion - performed waste tank continuous level sensor cleaning per amm 38-33-02 . inspected ball valve linkage assembly and proximity switch with no defects noted . verified waste tank empty . accomplished lav inop bite per amm 38-33-00 with no faults found . all lavatory toilets ops normalref amm 38-32-01 . aircraft okay for service . seamc steve notified.c # ap 4043953 .
aircraft was grounded : an emergency was declared due to : both autopilots inoperative in flight , aircraft return to and l anded safely at jfk . found auto stab trim cutout-trim cutout fault on dfcs bite channel " a " and " b " . returned the stab t rim cutout switch to the normal position . ran speed and stab trim library test 32 as per fim 22-13-00-810-813 . all test passed for channel " a " and " b " .
slide low pressure defered per mel 52-11-01-2-3 dmp c / w
aircraft was grounded : an emergency was declared due to a yellow hydraulic system reservoir overheat ecam message during climb out . flight crew accomplished ecam procedures and landed safely at clt without further incident.maintenance found the yellow hydraulic system engine driven hydraulic pump shaft had sheared on # 2 engine . maintenance replaced the hydra ulic pump and accomplished a satisfactory leak / operational check per amm 29-13-51 .
ship 3328 - ato - on application of takeoff power , engine parameters started surging with left engine fadec system ecam warning . takeoff was aborted . corrective action : t / s eng 1 fadec system warning per a330tsm , found hmu ( e1-4000kc ) fmv pos / j6 fault . replaced hmu per a330amm , operational check good . ( 4361334 )
aircraft was grounded : an emergency was declared and the aircraft returned to clt . flight crew reported that engine # 2 e gt over limit on take off climb was 400 degrees , approximately 920c . flight crew shutdown the # 2 engine and reported tha t later it cooled to 700c . the aircraft landed safely at clt and taxied to the gate . * * supplemental report will be submi tted . * * ( open )
aircraft was grounded : an emergency was declared due to system hydraulic number 2 low pressure light illuminated during flight . aircraft return to mia , and landed safely without further incident . **supplemental report for aala202309223972 : replaced hydraulic system a pressure transmitter t424 per amm 29-31-12 ( aala202309223972 ) and electric motor driven pump per amm 29-11-21 ( aala202309254469 ) .** ( closed )
stab out of trim lt illuminated during descent performed qrh main electrical ( p > found cb afcs ( b ) mach trim ac open . closed c / b accomplisjed fim 22-14 task 829 , 22-11 task 801 , 22-12 task 803 , 22-41 task 804 . found no issues . accomplished stab trim system test test pass c / w bite library 32 , 10 and amp ; 33 all tests pass a / c ok to release . / p > )
at100 kias crew reported audible rumbling from lt eng with yaw effect followed by eicas display of engine parameters spo oling down prior to lt eng shutting down . crew rejected take off and landing was without incident . post flt crew briefed f uel conditioning lever / switch was on . conditioning switch selected off to secure eng . ers reported fire / smoke from eng core cowl and foamed engine . aircraft grounded . emoved and replaced left inboard and outboard thrust reversers iaw b767 amm 78-31-01 . operational and leak checks good . inboard ( right ) core cowl replaced due to fire damage per b767 amm
pilot reported that after takeoff from kpbg , he noted an electrical smell in the cockpit and noticed traces of smoke from the lh landing light circuit breaker . pilot noted that the circuit breaker felt hot and had shut off on its own . pilot performed an air return to kpbg and landed without incident . pilot did not declare an emergency . maintenance troubleshot system to a bad lh landing light circuit breaker . maintenance removed and replaced the circuit breaker pn 7270-5-20 . all ops checks were good , and aircraft has flown with no further issues .
ship 9546 -div / ifsd / de- the flight crew noted that the # 1 engine stalled multiple times in flight which resulted in a " # 1 engine sys fail " message . flight crew shut down the engine per the qrh , they declared emergency with atc , and diverted th e aircraft to land at ord . corrective action : engine was found to have out-of-limits damage to the high-pressure compressor and was replaced . ( lp # 5937360 )
foul smelling liquid from lav leaking into fwd galley fwd galley sink drain clogged and the drain strainer is leaking form 46.6020 filled out by crew -- see all photo , s inside 109 with standing water -- see photo , s removed and replaced fwd galley drain basket and cleaned water as req all ops check normal ok to cont .
left eng anti-ice inop amber tai displayed with left eng anti-ic e switch on . updated parts information . replaced anti-ice valve per amm task 30-21-11-400-801 rotable parts change was indicated - tt # 1505412 sn off 2095 valve , anti-ice off 29-3021-9-0002 2095 on 29-3021-9-0002 7383 performed engine cowl anti-icing - operational test per amm task 30-21-00-710-801 ops ck good
ship 0189 -fcnt / de- crew declared emergency due to le slat disagree on approach . corrective action : found torque tube da maged . replaced screws reconnected torque tube and repaired damage section . ( 4557306 )
crew reported in flight that hydraulic quantity for left sys dropped to 0.49 , after continued loss , aircraft diverted t o mia from its original destination of sju . all fluid from lh hyd drained upon landing ( p and gt ; determined left stabilzer trim control module leaking . r / r lh stcm iaw amm 27-41-05 . ops check good and amp ; leak check good iaw amm 27-41-05 and amp ; 21-41 -00 . ref ipc 27-41-05-50a / p and gt ; )
enroute to kpdx crew reported , during climbout at 15000 '' and 290 knots with lnav , vnav and center cmd selected , eicas ms g autobrakes , auto speedbrake , and rudder ratio displayed . status msgs flap / slat elec and flt data acq displayed . no aut opilots , no autothrottles , left and center flight display inoperative . manual pitch trim required . air turn back to ki ln with an emergency declaration . landing was without incident and no additional precautionary actions . on arrival , airc raft was grounded for unscheduled maintenance . during inspection , line maintenance identified left dc bus sect 2 ? cb on
rt horizontal stab rib at station 92.70 is cracked at stiffener repair at nr 2 vertical transition radius ref n / r 998457 75 . accomplished rt horizontal stab rib sta 92.70 stiffener repair at nr 2 vertical transition radius ref srm 55-10-09 r epair 4 fig 202 detail b .
aft cargo bay floor to sidewall support corroded between bs . 887 to bs . 947 , rbl 23 . r and r support iaw srm and dwg .
during climb after departure , crew reported possible bird strike on right wing . during cruise flight , nr 3 engine had a low frequency vibration at lower power settings . nr 3 engine oil quantity began to decrease , nr 3 engine was shut down and later restarted prior to landing . maintenance found bird strike damage to nr 3 engine fan blades . the engine was removed and replaced .
pilot reported the right hand alternator out light on momentarily and electrical fumes on final . maintenance replaced the right hand alternator with no further defects noted .
css : 1 apu would not start ( with fault light ) at 340 . 2 apu would not start ( failed to start at 340 ) 2 total failed starts . grounded - yes . apu started normally on ground . placed on mel 49-99a . ref b737-900 amm 49-11-00-860-801 . per seamc ok to clear mel 49-99a . css passed as reported to seamc .
crew reports aggressive vibration through the main landing gear upon touchdown . upon performing visual inspection of the main landing gear , discovered the left hand side stay wing mounted attachment fitting cracked .
crew reported propeller heat inop-shows 8-9 amps in both auto and manual . modes . corrective action : removed propeller anti-ice leads . installed three new propeller de-ice leads . propeller anti-ice systems check good on engine ground run . subsequent flight was uneventful , with no issues
1 and 2 np and rotor rpm indicator ( triple tac ) was inop during the start sequence .
evidence of bird strike ingestion in nr 2 engine . performed visual inspection of engine 2 esn v10991 and inlet cowl per mt72-021 . no damage observed . bird debris observed on splitter fairing . acp borescope of nr 2 engine , no limiting defects noted . ref amm 72-00-00 , pg 601 .
aircraft was grounded : an emergency was declared , duirng descent into sfo flight crew reported a flight control slat fau lt message and no slats . the aircraft landed safely at sfo without further incident and was towed to the gate . maintenan ce found the left wing # 5 leading edge slat actuator 6037cm had failed and replaced it per amm 27-84-49 . a satisfactory operational check was accomplished .
aircraft was grounded : an emergency was declared comming into ord . in level cruise at fl 370 engine 1 and 2 stall . oat -64c , clean air . flight crew followed qrh and ecam procedure , descended to fl 270 and engine parameters returned t o normal . the aircraft landed safely at ord and taxied to the gate under its own power . note : see aala202401180715 for # 2 engine . * * supplemental report will be submitted * * ( open )
during takeoff , just after rotation , aircraft encountered a flock of birds , resulting in fod to both engines and subsequent shutdown of both engines . aircraft heavily damaged . investigation under way . ntsb and faa notified . ( k )
during cruise master warning illuminated at fl400 and cabin altitude warning eicas displayed with siren , ran qrh to co mpletion . cabin alt mode selector in auto 2 . crew declared emergency performed emergency decent to 10,000 and finished flight into cvg . after landing maintenance ground ac and troubleshot finding air driven pump shut off valve partially op en when off , auto , or on . replace valve iaw 29-11-30 ops check good , also performed ops checks on lh and rh packs both ope rating normally iaw b767 amm 21-51-00 . ac returned to service .
ship 0665 -div / ifsd / de- diversion to tpa due to left engine oil filter advisory message . crew followed qrh and shutdown engine . corrective action : checked mcd '' s and oil filter , found metal debris in oil filter . analyzed material and found m 50 bearing material . engine replaced . ( ata 7934 / ri 367 )
inflight had an oil cooler hose failure . rubber deteriorated . should have a life span of 10 years .
flt # 2715 , jfk-lax . ( aircraft performed an air turn back to jfk ) '' vibratio in rudder peddals in flight- when and gt ; 190 kts- c a and f / o side - no other anomales noted with flight controls . no change w / auto pilot on - off . vibration survey comple ted ; ref lg pg 3831272-2 ( performed check of rudder trailing edge play iaw amm 27-24-00-200-002-a . rudder deflection und er green at 9.45mm , yellow 9.29mm , and blue was at 9.98mm . well within limits on all three sys . ) backlash performed on rudder , performed following tests : iaw mm 22-61-00-710-001-a artificial and rudder trvl limt test , iaw mm 22-60-00710-00
rto at 10kts due to autothrot disc eicas tomc locks log for repeat writeup and second rto in 2 days unlock to clear performed mcdp tests 02 , 10 , 30 , 52 , and amp ; 60 . all tests passed except test 10 , showed tla l fail-fwd and tla r fail-fwd . needs further t / s . servo , autothro off 75-2232-9-0001 0351 on 64-2232-9-0001 1229 servo , autothro off 75-2232-9-0001 0351 on 0000 removed and replaced servomotor generator per amm 22-32-01 . performed mcdp test 10 servo a / t and mcdp test 30 per amm 22-00-02 . no faults . system checks ok . aircraft full cat capable .
aileron trim runaway . followed qrh no effect . returned a / c to normal config on grd . removed and replaced the aileron / rudder control panel iaw crj-700 amm 27-12-10-000 / 400-801-psa . ops check good .
momentary loss of adc 1 after rotation / removed and replaced adc # 1 iaw crj 900 amm 34-13-01-000 / 400-801-a01-psa . performed functional test of the # 1 atc alttitude reporting ( mode c ) iaw crj 900 amm 34-54-00-720-802 . fucntional test good . ifr 6000 used for test . "
event : on 28 february 2023 , garuda indonesia aircraft pk-gfg as ga-178 sector cgk-pku , during climb , aircraft experienced fuel imbalance on left main tank . pic decided to air turn back to sta . cgk . action : 1 . ref fim 28-21 task 802 performed tvf fuel form ct tank to mt no 1 result result normal ref amm 28-26-00-650-802 rev 80-15 feb 23 . 2 . ref msao 804674536 performed fault isolation unwanted duel transfer from tank no.1 to center ref fom 28-21 task 803 result no fuel transfer from maint tank 1 to center tank . 3 . ref fim task 23-22 task 817 reset button on left boost pump 6f1 r54 is normal condition ref fim task 28-22 task 801 cb ctr tank left fuel pump light ill momentary result satisfactory rev 80 / 15 feb 2023 . 4 . examine the left fuel boost pump and area shroud it no sign of fuel leak ref amm 28-22-41-000-801 rev 80 , 15 feb 2023 . insulation resistance rest continuity check pin 4 and bond jumper on fuel boost pump result 0.8 ohm ( limit 5 ) . 5 . replaced lh ctr tank boost pump performed ref amm 28-22-41-400-801 rev 80 / feb 15 , 2023 . continue action 6 . no found fuel leak from lh ctr tank booster pump and booster pump operate normally ref amm 28-22-41-710-801 after monitor for 25 minutes found lh ctr tank booster pump low press lt ill intermitten . 7 . for troubleshoot cross change between relay r54 and r55 result trouble moved part back to original position . replaced gfi relay r54 ref amm 28-22-18 / 401 gfi opc test ref amm 28-22-41-720-802 rev 80 , 15 feb 2023 result good . 8 . operational test lh ctr booster pump after replacement result good ref amm 28-22-41-710-810 rev 80 / 15 feb 2023 . monitor for one hours result low press lt not illuminate . preventive action safety meeting b737-800 has been conducted on 10 may 2023 related to events in 737-800 fleets to increase awareness for flight crew . issued safety briefing sheet ( sagtl-sbs-09-2023 ) related to the event for maintenance personnel to increase awareness for complete troubleshooting . detail of event will be included in 737-800 flight training syllabus to prevent re-occurrence of fuel imbalance cases .
ship 8301 - atb / ifsd -performed air turn back due to left engine fail message that resulted in an ifsd . corrective action : msp maintenance found metal in tailpipe . lt engine replaced . ( lp # 9717350 , 2831647 )
aircraft was grounded : an emergency was declared and the aircraft returned to phx . right after thrust red altitude after take off got air engine 2 bleed abnormal pressure . crew accomplished ecam procedures and landed safely at phx without f urther incidednt . * * supplemental report will be submitted . * * ( open )
takeoff aborted at 80 kts . due to possible bird strike . investigated possible bird strike iaw 05-51-25 . no damage noted at this time .
aircraft was grounded : an emergency was declared and the aircraft diverted to dfw , flight crew reported that they lost a ll water ( potable ) approximately 25 minutes into the flight , resulting in no faucets or toilets were operational . the ai rcraft landed at dfw without further incident . maintenance found potable water servicing nipple cracked and replaced it per amm 30-72-52 .
during cruise , crew reported loud pop audible from aft part of flight deck and odor of burnt insulation present . smell dissipated , then returned occasionally . crew suspected possible source of smell was acars printer . diversion to kafw . la nding was uneventful with no precautionary actions . on arrival , aircraft grounded for unscheduled maintenance . post flig ht line maintenance confirmed fault . acars printer circuit breaker pulled and collared . printer connector capped and sto wed . deferral maintenance item-42016 mel cat c initiated . removed and replaced acars printer iaw b767 amm 23-22-03 . acar
e912345 - vertical stab to fuselage lh drag angle is cracked at fwd end . . rar lh vertical stab to fuselage drag angle fwd section iaw emb 145 srm 51-40-02