boeing/aviation-ner-BIO huggingface dataset:
l rev caution on takeoff .rev caution out after throttle retarded mel to be applied with tomc approvel rev isol valve pin installed , mech deact pins installed , left eng sync lock p11 pulled and safetied . placard installed fwd of throttle thrust rev inop performed proximity sensor electronics unit bite procedure ref fim 32-09 fault tree 812 , found five faults in fault history on the same leg . l t / r in transit , t / r not locked l , t / r auto restow l , l t / r deployed , t / r not stowed l . further trouble shooting required ref fim 78-30-00 / 301 material update material update performed pseu system test ref amm 32-09-812 . faulted t / r not locked l msg # 78-360063 . ref fim 78-30-00 / 301 left engine , right side actuator lock proximity sensor s10436 indicates far for t / r locked . this sensor needs to be checked for proper rigging ref amm 78-30-00-835-024-r04 . performed adjustment of the lock proximity sensor per amm 78-30-00-835-024-r04 , added .010 shim washer to bring sensor while accomplishing # 1 eng lower reverser actuator locking indicator found would not fair while cleaning mechanism found amm 78-30-00-835-016-r04 ref . suspect lower inboard synchronized actuator mfg . p / n 1616000-1 , m and amp ; e p / n 19-7831-9-0004 within limits . reactivated t / r system per 78-31-00-912-023-r04 . cycled t / r no help . found rh locking indicator not fully engaged . when indicator is pushed in manually yellow rev light c
btb- during start of engine 2 eng 1 fadec sys fault illuminated followed ecam . shut engine down and returned to gate / / removed and replaced eng 1 eec per amm 73-21-34-400-804-a performed engine idle run and fadec sys fault illuminated on eec chan b ( fmu ) ( e1-4071ks ) sov pos . 28 / jan / 2022 761261 . need to accomplish land test and continue troubleshooting . accomplished tsm 73-21-72-810-921-a . no faults noted . wiring checks continuity check ok . no shorts to ground . resistance check ok all within limits 502110 6 / 28 / 22 . removed and replaced # 1 eng fmu per amm 73-21-52 . ops and leak test ok . nofaults noted on eng run . control , engine off 33-7321-9-0004 s / n 90767 on 33-7321-9-0004 s / n 91774 meter , fuel ; po off 43-7321-9-0012 s / n 11251 on 43-7321-9-0012 s / n 15114
rejected takeoff at 110 knots for takeoff config light illuminated pilot reports weight 156,000 lbs . thrust reversers we re engaged . light manual braking . couldnt duplicate . no rto brakes . performed troubleshooting per fim 31-51 task 803 . f ound all good . ref amm 32-09-10-400-801 and 32-09-10-710-801 . performed inputs to be correct for corresponding position s . found no ops check of takeoff warning per amm 31-51-04-000-801 . checks discrepancies from d10982 pin 53 to aural wa rning module d940 good . parts used : 29-3260-9-0003 , qty : 1 pin 3 . removed and replaced pseu precautionarily . ops checks rotable parts change was indicated - tt # 1773188 sn off 0464 switch , proximi off 29-3260-9-0003 0464 on 29-3260-9-00
aircraft was grounded : on approach into fsd when the crew lowered the gear the landing gear did not come down . the fligh t crew aborted the final approach and after 30-45 seconds the crew cycled the gear handle and the landing gear extended . * * supplemental report for aala202304282005 : maintenance accomplished tsm 32-31-00-810-808-a and replaced hydraulic contr ol relay 62ga and the green hydraulic system priority valve ( aala202305020108 ) . a satisfactory operational check was acc omplished . * * ( closed )
upon removal of horizontal stabilizers and vertical fin on the aircraft it was noted that their are several cast fittings located inside the empennage that were showing singes of surface corrosion as well as possible inner granular corrosion on a couple of the parts , in general this was a problem that we suspected would be evident with all the terminal attachment points . so all fittings were removed for a closer inspection , this consisted of 8 horizontal attachment fittings and 2 of the vertical fin attachment fittings . all of the attachment fittings were sent to ( aircraft inspection services in michigan ) ndt report shows that there are a number of problems in various areas with all of these fittings , as mentioned above , the report shows indications of surface corrosion possible inner granular corrosion and stress crack corrosion . for one reason or another the parts are no longer within serviceable limits . we are going to replace al f these fittings with new manufactured or old stock parts . ( note : none of these parts were showing any sings of catastrophic failure . ll taper pin attachment points were fittings would attach to other components were free of defects .
aircraft was grounded : an emergency was declared into dfw . during climb out , leading edge flaps transit light illuminate d intermittently with associated # 3 leading edge slat light on the overhead panel . flight crew ran the appropriate chec klist and proceeded as if the panel was deployed . flight crew reported normal flaps 15 landing at dfw and indications we re normal in the landing configuration . the aircraft landed safely at dfw and taxied to the gate under its own power . * * supplemental report for aala202402028115 : maintenance replaced the left wing leading edge outboard slat 4 sensor and acc
flt # 211 , fll-aus . ( aircraft declared an emergency and performed an air turn back to fll ) '' upon rotation and climbout a / c required fwd press on stick . once stable in fd '' s once lvl off a / c would not maintain lvl flight and pitched up . both fd '' s were center and aligned . same was true on capt and fo side . on descent i turned ap off and a / c would lvl off then cli mb . manual flight required fwd press in all phases of flight . including approach and landing ; accomplished tsm 27-30-00- 810-853-a a / c pitch up more than 2.5 deg . flt crew confirmed / observed fault by selecting a / p on / off several times . dfdr
on approach no nose landing gear indication . crew elected to abort the approach and go around . emergency declared and la nding was without incident . master dim and test system replamped per boeing aircraft maintenance manual 33-16-02 . opera tional check good . no additional faults noted . previously noted in body of text omitted to select in drop down option . f precautionary procedures .
engine roll down just after take-off . after landing , engine would only start on lt mag . determined that the ignition vibrator was shorting rt mag due to an internal failure . also found lt and rt mags p-leads ground faulting together through an ignition filter mounted in firewall . speculated that capacitors ( sprauge 10283-64 and 1032364b ) in the filter suffered corrosion and moisture contamination to provide additional ground to bring both mags down .
aircraft was grounded : an emergency was declared on approach into lax due to the flight crew reporting a flight control flaps locked message with the flaps jammed at position 1 . aircraft landed afely at lax without further incident . ( open )
smoke rest upr door 3 at fl380 acrid smoke diverted smell went away . smell did dissipated quickly . no smoke or smel l inside the flight dissipated on decent and no longer noticeable . deck . operating flight crew did confirm the upper f a crew reaching flt lvl 380 , smoke in fa rest alert , contacted aft rest switch panel ( inside entrance enclosure ) there w as an amber cabin fa and they reported an acrid smell with eye irritation . flashing smoke light and smoke alarm sounded in upper f / a . crew fa verified amber flashing smoke in fa rest light near fa rest area . on approach at 5k agl f / a noti
ship 9500 -atb- the aircraft was returned to atl following compressor surges in the # 1 engine . the pilot declared an eme rgency with atc and the landing and taxi to the gate was uneventful . corrective action : maintenance replaced the # 1 engine ( esn 13197 ) and the aircraft was returned to service . ( lp # 9635642 )
ship 3406 - div / de - aircraft diverted to mci and crew declared emergency due to right engine oil quantity loss with oil pressure degrading . corrective action : installed new breather assembly and carbon seal . ( 4513181 )
aircraft was grounded : an emergency was declared and teh aircraft returned to phx due to the flight crew reported an ove rheat at 1061 degrees on engine 2 on max power takeoff . event occurred at approx 200 ft and stayed until engine out alt itude of 2160 . ft meal . ecam went out on power reduction to climb power . engine 2 get is 50 degrees higher than engine 1 in cruise.the aircraft landed safely at phx and taxied to the gate under its own power . engineering reported that the engine has a low remaining egt margin of -4130 . maintenanance accomplished a download of the dfdr data and no exceedanc
aircraft was grounded : an mergency was declared and the aircraft returned to phx . during take off from phx flight crew reported at rotation an ecam engine 2 egt hi . then egt overtemp . flight crew pulled thrust to idle but did not shut dow n engine as egt went back to normal temps . the aircraft landed safely at phx and was towed to the gate . ( open )
aircraft was grounded : an mergency was declared and the aircraft returned to phx . during take off from phx flight crew reported at rotation an ecam engine 2 egt hi . then egt overtemp . flight crew pulled thrust to idle but did not shut dow n engine as egt went back to normal temps . the aircraft landed safely at phx and was towed to the gate . maintenance acc omplished tsm 77-00-00-810-849-a and accomplished an engine compressor wash per task card 26l40072023 .
aircraft was grounded : an emergency was declared and the aircraft returned to mia . after takeoff the flap selector was b roken in the flaps 1 position and flight crew was unable to move the flaps . the aircraft landed safely at mia without fu rther incident . replaced flap and slat control lever per amm 27-51-43 .
air turn back -- pilot reports pressurization failed . grounded - yes . air turn back -- found aft e and e door open . perform ed e and e door indication test iaw amm 52-71-42-710-801 . ops cks normal .
during cruise flight the fuel quantity gauge failed en-route to mc773 . the crew elected to divert to their offshore alternate to be evaluated by mechanic .
aircraft was grounded : an emergency was declared and the aircraft returned to jkf . during climb at approximately 17,000 the aft cargo compartment fire light illuminated and the bell activated . flight crew ran the qrh procedures and discharged the aft cargo compartment fire bottles . during the return to jfk the fire light and bell activated several more times . the aircraft landed safely at jfk without further incident . maintenance inspected the aft cargo compartment and found no evidence of smoke or fire . maintenance found the aft cargo compartment smoke detectors at positions a1 ( aala202309013
enroute , center hyd qty eicas and light illum in cruise . status page showed 0 qty and magenta rf with 3000 psi . diverted , e mer declared . landed without incident . acft grounded . center hyd ind deferred iaw mel 29-33-02-01 . hyd ind inop . ac ft released to service . iaw fim 29-11 fault tree 820 accomp gvi of hyd qty xmitter . removed connector and verified no pin s backed out iaw amm 29-33-02 . reracked qty montior iaw amm 29-33-01 . crew debriefed , no defects during all phases of f lt . wire shakedown and ind monitor unable to recreate fault iaw amm 29-33-11 . pulled c / b 11l20 . reset c / b , disconnect co
aircraft was grounded : an emergency was declared and the aircraft returned to pty , left engine vibration climbing past f l 260 . vibration was 9.8 on the left engine . flight crew followed ecam directions and shut down the left engine . the air craft landed safely at pty without further incident . maintenance found the n1 fan siezed and the gas path report recorde d a 980-994 degree area c exceedance for 60 seconds . the engine requires replacement . * * supplemental report for aala2023 03289495 : maintenance replaced # 1 engine per task card 26l40071001 and accomplished a satisfactory operational check * *
avnx mau 1b fail during arrival into airport . degraded navigation performance . loss of ca and fo pfd . loss of nav / com 1 . loss of gps 1 . declared ife . the following cautions , advisory , and messages were displayed on eicas : ice detector 1 fail , vhf 3 fail , emerg lt on , ads 1 fail , avnx mau 1b fail , ap fail , spoiler fault , hyd 2 elec pump fail , rep ar not avail , appr 2 not avail , slat lo rate , gps 1 fail , ralt 1 fail , ccd 2 fault , spdbrk fail , eng 1 rev fail , rat fail , eng 2 rev prot fault , eng 1 rev tla fail , flt ctrl no dispatch , display ctrl fault , cmc fail , ads probe 2 fail , load shed , ads probe 1 fail , flt ctrl ads fail , flt ctrl fault , hyd elec pump 2 fail , slat lo rate , gps 1 fail rad alt 1 fail , ccd 2 fail , spdbrk fail , bleed apu valve open , steer off , a-i eng 1 valve open , printer fault . ( flight 3919 ) please reference aml 728330 / troubleshot in reference to fim 32-41-00-810-809-a for avnx mau 1b fail caution message . found mau 1 nic proc 2 and mau 1 ps3 at fault . removed and replaced mau 1 nic proc 2 in reference to amm 31-41-01 . software uploaded completed . removed and replaced mau 1 power supply 3 in reference to amm 31-41-02 . all messages cleared . no defects noted at this time . a / c okay for service .
*emergency declared* r eng low oil pressure around 10 - 15 caution ligth came on upon arrival , found oil cap to be not secured after adding oil , replacing missing oil cap , ran engine . no further , oil low pressure message . aircraft good for service
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 ) maintenance found # 1 system data acquisition concentrator ( sdac ) inoperative and replaced it per amm 31-55-34 . a satisfactory operational check was accomplished . * * ( closed )
flt # 62 , pbi-lga . ( aircraft declared an emergency and performed an air turn back to pbi ) 'bird strike # 1 engine ; ref l.p . 3567287 , item 1 ( accomplished bird strike insp . iaw 05-51-14 . found # 1 eng ingestion . airframe free of bird strke . ref lp 3567288 , item 1 for # 1 eng fod insp . ) for airframe bird strike inspection and l.p . 3567288 , item 1 ( performed gvi and borescope insp # 1 eng . per amm 72-00-00-200-010-a . reference l / p 3567288 , item # 2 ( ref l / p 3567293-1 for # 1 engine replacement under w / o 1229522 corrective action . ) for findings . ) for the engine inspection . also l.p . 3567293 , item 1 ( wo 1229522 accomplished . # 1 eng replacement . ) for # 1 engine replacement . '
found safety release cap attched to engine fire bottles removed safety release cap from both fire bottles ref amm26-21-01 . verified both fire bottles saftey release caps have been removed . inspected both fire bottles for installation , servicability and hydostatic expiration dates . ref amm 26-21-01 / 401 . ok to continue in service .
on flight 99 from icn to anc , ten minutes into the flight , the flight crew reported a high engine vibration on # 2 engine , followed by related fire warning . the crew proceeded to discharge both fire bottles and performed emergency procedure s , returning to icn and landing with single engine . emergency was declared . aircraft landed without further incident . after landing , engine damaged was discovered . manufacturers were contacted for evaluation and cause of failure . # 2 en gine gearbox failure is suspected at this time .
actuator light came on and would not reset . t / f evaluation revealed autopilot test failed with yaw sas and backup sas cautions on cad . when ap1 and ap2 are turned on actuator caution on cad and y caution on pfd appear . removed and replaced yaw sema iaw amm 22-10-00 , 4-7 .
flt no : mge301 . event - lp62288 item 1 - stab trim stuck wouldn '' t move nose up . flt crew declared emergency into hnl . fo und alternate stab trim switch faulty . removed and replaced alternate stab trim switch per amm 27-41-03 . ops check norma l .
aborted takeoff , at approx 90 knots nr 1 eng suffered bird strike . visually inspected nr 1 eng , performed eng run up and high energy stop check . no defect noted .
aircraft was grounded : an emergency was declared on final approach crew selected flaps 2 and a flight control flap fault message displayed . aircraft landed safely at bos without further incident . maintenance replaced right flap actuator per amm 27-54-49 and accomplished a satisfactory operational check .
birdstrike to nr 2 engine . rtfl . crew suspected a birdstrike , and shut the engine down as a precaution . borescope inspection revealed no core damage ; birdstrike damage confined to fan bypass area . five fan blades were bent forward , with minor nicks to other blades . removed and replaced the fan blade set .
during climb to 8,000 feet power decreased , un-commanded , from 92 % to 70 % . troubleshooting revealed the electric change over valve , p / n-e4a-41-300-801 was defective . that part was replaced and all operational checks showed proper operation .
aircraft was grounded : an emergency was declared due to : flaps one selected , leading flaps transit light remained illuminated . green leading flaps extended light did not illuminate . aircraft landed safely at mia without further incident.**supplemental report will be submitted** ( open ) .
crew reports rejected takeoff at 80 knts , brake temps 385 updated maa code fix using vendor maa screen updated maa code fix using vendor maa screen mac meter initiated for with vendor id v936162 please contact tomc before commencing any work . inspect per amm please contact tomc before commencing any work . inspect per amm mac related work order 0000000030 78173 and prtr 05-51-16 , inspect wheels for flat spots 05-51-16 , inspect wheels for flat spots schoenfelder , hayden ( v93 6162 ) inspeceted wheels per amm 05-51-16 , no defects noted schoenfelder , hayden ( v936162 ) inspeceted wheels per amm 05-51-16 ,
ship 9554 -ato- the flight crew aborted the takeoff at 130 kts due to the # 1 primary flight display and multi-functional display blanking out . corrective action : maintenance found 2 each coax cables loose on via # 1 splitters and replaced bo th display units . ( lp # 6196222 )
pdis 593 32-60 6599 08mar23 icn open u after takeoff when gear retracted right main remained red on prima ry and secondary . * * * emergency declared * * * shgn 08mar23 09 : 07 icn u nrr : no reference required nrr : no reference r equired flt crew verbal reported a / c little viblation after gear up . r / h main gear gvi checked no defect found . r / h main gear proximity sensor work normal . need to gear wing check but wing and fuselage jack adapter nis in icn , request ed tool to nrt . 1 .
aircraft was grounded : an emergency was declared and the aircraft returned to phl due to the flight crew reported an eng ine 1 epr mode fault in flight , with degrade n1 mode active . at fl 240 with left thrust lever in climb detent only 79.1 % n1 was attainable . the aircraft landed safely at phl and taxied to the gate under its own power . maintenance replaced t he # 1 engine relay box 4100ks per amm 71-51-49 and accomplished a satisfactory operational check with no faults noted .
flt 6083 - received a r rev warning message along with other indications on climb-out . replaced nr 1 dcu iaw mm 31-31-01 . ops checks good , p / n 822-1310-104 , s / n 1mb3n .
while conducting clearance below path run , a pair of pigeons dived and struck left engine area . heard a thump and all crew members started noticing a burning smell . no abnormal engine indications were observed . crew requested immediate landing and was given a landing clearance . aircraft landed without incident , taxied clear of runway and shutdown . fire department checked ac and released it to be towed . pigeon remains were found on the left engine intake , inside the engine in the screen , on the left wing leading edge , and on the rt side of the rudder .
while in climb out of miami eicas fwd cargo illuminated . crew elected to turn back to miami , flight landed without further incident . aircraft grounded by maintenance . maintenance verified door was closed and deferred fwd cargo ind ication per abx mel 52-71-1-1 aircraft returned to service
on approach to den , bird strike occurred on left wing . the bird impacted the nr 2 slat and the fixed leading edge at wing station xfs equals 250 . slat was damaged and the wing leading edge was dented just forward of the round access panel . ( m )
ship 9579 -misc / de- the flight crew declared an emergency with atc into atlanta due to a suspected left side brakes grab bing condition . corrective action : maintenance determined the problem was an internal bearing failure of the # 1 mlg whee l assembly . ( lp # 4746476 )
# 2 engine would not start on apu . , accomplished apu ops and leak check iaw b767 amm 49-11-00 . apu pneumatics work good in all modes . 30-35 psi . in mes . found rh isolation slip joint with pneumatic leak , see lp 38740-91 / 1 for duct repair further t / s required . during # 2 engine inspection found bad # 1 igniter plug . removed and replaced rh engine # 1 igniter plug iaw b767 amm 74-21-01 . ops check good . see log page 38740-91 item 1 . performed ops check iaw b767 amm 71-00-00 . ops check good . no defects noted apu ops check good iaw b767 amm 49-41-00 . di cleared . placard removed . no mx action required at this time .
inflight shutdown air turn back , during to roll , at least one large bird was ingested by nr 1 engine . tower advised smoke and flames erratic engine indication but no overheat or fire indication . engine was shut down and fire switch pulled . r and r nr 1 engine idg ail / oil cooler panels , fan blade set iaw mm .
ship 9550 -misc / de- the flight crew noticed the fuel to be trending low and a 1000lb imbalance . the tanks were re-balanc ed , but the imbalance returned . fuel quantity was also lower than planned . the qrh was complied with and the fuel leak c hecklist was followed , but the leak continued . the crew declared an emergency with atc and requested arff to meet them . on arrival . the landing was uneventful but they exited the runway at highspeed for arff inspection . a fuel leak was noted and it decreased after the # 2 engine was shutdown . normal taxi to gate where the aircraft was met by maintenance who co
in the accomplishment of eo 53-767-767-7487 , structural findings were noted . aircraft grounded for paint work in progres s .
l1 door emergency exit light damaged . replaced emergency exit area light in aisle iaw 33-50-00 . ops checked good .
upon selecting flaps 1 , the right flap stayed at up while left flaps were between up and 1 . le devices remained up . used alternate flaps which drove c / o le devices per qrh . grounded - yes . emergency landing declared . fseu bite test shows fa ult msg 27-52260 " te flap snsr r " . accomplished b737-900 fim 27-51 task 820 " right flap position transmitter disagree pr oblem " fault isolation . removed and replaced rt flap position transmitter ( t428 ) iaw amm 27-58-01 . accomplished flap posit ion transmitter adjustment and test iaw amm 27-58-01-820-801 , ops ck normal .
while enroute back to base from san antonio , about five miles east of hondo , texas ; medical crew reported the smell of " burning plastic " in the aft cabin . the smell went away and then came back . i never smelled anything in the cockpit . i elected to make a precautionary landing at the hondo , texas airport and called maintenance . rear a / c blower was found to be the problem .
multiple bird strike at 1300 ft , flaps 5 degrees . nr 1 engine was shut down for vibration and subsequent failure . removed and replaced nr 1 engine assembly per work card 70t0001 and operational checks good . no leaks noted on run check . reference work card 70t0001 , 70t0002 , 70t0303-1 .