boeing/aviation-ner-BIO huggingface dataset:
fuel leak lh wing root aft of spar 2 approx 1 1 / 2in ob of wing end . removed from service and ferried for repairs . / w e175 amm task 28-11-00-790-801-a the leak has been classified as 'stain' . aircraft down for repairs .
inflight shutdown of nmbr 1 engine for 0 oil pressure at fl300 . divert to katl . s / n 804292 ( tsi 40117 ) . crew debrief : to tal oil qty loss , oil press 27-40 psi for about 2min then eng shut down when oil press caution light illuminated . windmi ll time approx . 20 min . mx found rear chip detector ( rear sump ) laying in the bottom of the fan cowl . eng . performed '' '' 'insp after eng ops above limits '' '' amm inspected and seals replaced , with no defects found . amm amm 71-00-00 . 71-00-00-80 0-804-f00 sect 4h '' '' low or zero oil press '' '' . per fig 71-00-00-210-802-f00 inspection after windmill acp '' '' d with 605 oil
aircraft was not grounded : an emergency was declared and the aircraft diverted to tul due to center tank left transfer f ault in flight . flight crew followed ecam procedures . leading to engine 1 fuel pumps off allowing fuel burn from right t ank only . the aircraft landed safely at tul . maintenance accomplished tsm 28-26-00-810-828-a and fault could not be dupl icated . a satisfactory operational check was accomplished per amm 28-26-00-710-001 .
flt # 897 , bos-lir . ( aircraft diverted to fll ) '' eng1 high oil consumption . note : according to flt crew they departed bos w eng1 oil qty indicating 12 qts ; upon arrival to gate performed eng1 gvi no leaks noted . serviced eng1 oil with 7 qts . iaw 12-13-79 . opened eng1 fan cowls performed engine idle run and no leaks noted . performed oil consumption report / ana lysis from trax and 100 f / h consumption is 0.15 well within amm limits . complied with tsm 79-00-00-810-838a no defects n oted . ''
jfk - log page f03795 - at rotation , loud bang , nr 2 engine stalled , egt 1,000 , suspected bird strike . dumped 37,000 pounds fuel . returned to jfk . performed bird strike and overtemp inspections on compressor stage 1,2,3,4,5,7,9,15 , and turbine stage 1,2,3 per mm 72-00-00 . nil defects , item transferred to coi 003 for 80-hour flt limit per mm 71-00-00 , page 220 , fig 205 . ( x )
aircraft was grounded : an emergency was declared and the aircraft returned to dfw due to the flight crew reported reciev eing yellow hydraulic system reservoir low level and and yellow hydraulic system low pressure ecam messages . the flight c rew followed the ecam procedures and landed at dfw safely without further incident . the aircraft taxied to the gate unde r its own power . ( open )
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 will be submitted * * ( open )
attach bracket for the 326cr panel is cracked . rt fwd side of v stab . r and r with new serviceable part iaw crj 200 srm 51-24-21 , 51-40-11 and 51-42-21 .
after takeoff when gear retracted right main remained red on primary and secondary . emergency declared . flt crew ver bal reported a / c little viblation after gear up . r / h main gear gvi checked no defect found . rt main gear proximity se nsor work normal . need to gear wing check but wing and fuselage jack adapter nis in icn , requested tool to nrt . remo ved and replaced rt main landing gear retract cylinder and performed leakage check and operation test normal iaw amm32-3 3-20-4 .
aircraft was grounded : " elec gen off r2 " displayed on synoptic would not reset . maintenance found electrical arc flash with heavy soot contamination discovered on over voltage transient protection unit . **supplemental report for aala202308024413 : maintenance replaced p2 power distribution panel per dmc-b787-a-24-09-70-05a-720a-a ( aala202308024413 ) . replaced r1 and r2 overvoltage transient protection units per amm 24-09-08-00a-720a ( aala202308047690 , aala202308046894 ) . replaced r1 and r2 generator control unit per amm 24-22-02-01a-720a ( aala202308042930 , aala202308044626 ) . replaced r2 variable frequency starter generator per amm 24-21-08 ( aala202308041359 ) .** ( closed )
during takeoff roll at 110 knots , atc comananded crew abort takeoff due to confilicting traffic . t / s iaw amm chp 05-51- 07-210-801 . no defects on all tire assy and brakes assy . inspected t / r for defects no defects noted . c / w tire pressures checks , all within limits . ok for service .
aircraft was grounded : an emergency was declared and the aircraft returned to dfw due to the flight crew reporting an ri ght wing air leak indication that exitinguished when bleed 2 was shut off . the aircraft landed safely at dfw and taxied to the gate under its own power . * * supplemental report will be submitted * * ( open )
ship 667-atb / ifsd / de- performed air turn back with declared emergency due to left engine oil temp in the amber band for 20 minutes . flight crew performed ifsd per qrh . corrective action : inspected mcd '' s , all clean . drained 4 quarts from mai n gearbox . replaced gearbox scavenge pump and lsop . performed high power run with no issues .
ship 9524 gear / de- after takeoff and landing gear selected to retract , the crew received a " left gear unsafe " indicatio n after retraction . the qrh was complied with and the gear was extended without any problems , until the " pseu fail " mess age . the qrh was complied with for that and an emergency was declared with atc . the landing was uneventful . maintenanc e ran bite which did confirm gear fault code 326084 . the left main landing gear up and latched sensor was replaced . all operational checks were good ; including gear swings . the pseu was replaced as a precautionary . ( lp # 5459016 ) .
aircraft was grounded : an emeregency was declared and the aircraft returned to dfw . after takeoff thurst in climb detent ecam message engine 2 egt over limit . crew followed ecam procedures retarded # 2 thrust lever until egt within limits ap prox 3 % n2 less than engine # 1 . the aircraft landed safely at dfw without further incident . * * supplemental report for aa la202305196816 : maintenance replaced the # 2 engine lpc master bleed actuator , all three 7th stage bleed valves ( aala2023 07288194 , aala202307284855 , aala202307283970 ) and all 3 7th stage bleed valve solenoids ( aala202307287487 , aala202307283970 )
floor panel support intercoastal cracked sta . 312-328 rbl 32 . grounded - yes . removed and replaced instercostal iaw 737- 900 srm 51-40-02-0g-0 .
ship 9576 -misc / de- the flight crew declared an emergency with atc due to the " anti-skid fail '' message illuminating duri ng approach . the landing was uneventful , and the aircraft taxied to the gate . corrective action : maintenance found the a nti-skid connector # r5-6020 to be loose . once the connector was re-secured properly , the anti-skid system functioned nor mally . the aircraft has returned to service . ( lp # 4950228 )
ship 9518 -de- the crew declared an emergency due to intermittent right hydraulic pump fail message . corrective action : maintenance replaced the right engine driven hydraulic pump low pressure switch . ( lp # 4594298 )
ldg gear would not retract after t / off . removed debris from ldg manual extension system access door and switch ops check iaw amm 32-34-00 .
aircraft was grounded : an emergency was declared and the aircraft returned to gdl . engine 1 advisory for vibration in n1 after takeoff . aircraft vibrations felt in flight and aircrew opted to emergency return to gdl runway 29 for an overwei ght landing at 140,000 lbs . the aircraft landed safely at gdl . maintenance found 6 pairs of fan blades mid span shrouds shingled and un-shingled them . maintenance accomplished an inspection of the blades with no defects noted . a satisfactor y engine run and vibration check was accomplished .
bird strike engine 2 . accomplished bird strike conditional inspection on a / c . no damage other than nr 2 engine found . removed and replaced nr 2 engine . leak and ops checks normal .
eng 3 fire loop a and b failed ( p > r / r upper and amp ; lwr aft detector assy iaw amm 26-11-02 . r / r harness 61b45322 iaw amm 26-11-02 . r / r harness wire and eng idle test run normal iaw amm 71-00-00 . performed ops check , no faults found for eng 3 fire loop . / p > )
declared an emergnecy due to an standby attitude indication problem-c / a-rar ies iaw erj-175 amm 34-11-01.ops check good.t / s per fim 34-11-00 , found to be transitory condition of eiss . ac okay for service .
aircraft was grounded : an emergency was declared and the aircraft diverted to aus . climbing out of fl240 airspeed about 310k . felt heavy vibration nose to tail . leveled off , reduced airspeed and vibration went away . autopilot on , flaps sla ts retracted . no engine vibration noted on ecam . the aircraft landed safely at aus without further incident . * * suppleme ntal report will be submitted . * * ( open )
aircraft was grounded : an emergency was declared and the aircraft returned to dfw due to a # 2 engine stall ecam message during climbout . flight crew reduced # 2 engine power to flight idle and power was slowly restored . the aircraft landed s afely at dfw and taxied to the gate under its own power . * * supplemental report will be submitted * * ( open )
ship 3225 - atb- performed air turn back to dtw due to number 1 eng over-temp . crew pulled the throttle back but egt did not subside . corrective action : replaced engine per work card 7100-9901-lt . ops and leak check good . ( 4690742 )
aircraft was grounded : an emergency was declared and the aircraft returned to sju . during climb an ecam alert for egt ex ceedance displayed for the # 2 engine followed by a bang and a compressor stall . the aircraft landed safely at sju withou t further incident . * * original report was aala202304068570 * * maintenance accomplished a borescope inspection of the # 2 e ngine and no defects were noted . during a test of the vbv system on the # 2 engine it was noted that the vbv position sen sor was misaligned and maintenance was unable to move the vbv doors . the vbv master ballscrew actuator was replaced per
r eng vibra 3.3 climbing to 380 mod turb and ice.kept eng at reduce setting divertden attached pic of what crew reported . also flagged for sdr auto and man event pictures added . see attached photo for vib ref additional log pages 5788441 an d 5787996 . acp vibration run survey ref mm.71.0.00.715.327.r03 . test num 6 . # 2 eng nose cone fairing cracked , ref ipc 72 -35-01-01 item 37 . needing fairing in stock removed # 2 eng spinner fairing per amm 2 f . ( 1 ) ( a ) . rpl fairing ref mm72-35- 01-404-010-r04 . # 2 eng spinner fairing seal disbonded . see photo . spinner , rotor off 53-7235-9-0003 4706 on 0000 spinner
*diversion* enroute at fl350 isfd failed.screen went blank / dark . diverted to ksdf r / r isfd iaw mm-34-24-03-410-010 . ground ops ck normal . ok for service .
after departure from cvg , the aircraft encountered a bird strike on nose section . aircraft returned to the field . complied with bird strike inspection , no defects noted .
rejected takeoff due speedbrake do not arm light on at 95kts no takeoff warning horn performed fim 32-42 task 801 , 27-62 task 801 and fim 27-62 task illuminate . this is a 2nd write up . ref log 7615172 . requires scheduling . requesting mel 27 07f . 802 , no faults found on aacu and ds1 / ds2 on speed brake module further troublshooting . no time to further work due to flight mel 2707f due to previous history and possible crew refusal due to reverser also on mel . please fix . locked fo r positive fix . performed fim 27-62-task802 step e ( initial evaluation ) ( 3 ) troubleshot per ssm 27-62-11-102 and fim 27-
on t / o at 1000 ft , heard loud bang and aircraft yawed momentarlly lt and rt . passenger reported blue flame from fwd of lt engine . fowl smell in cabin . engine parameters normal . returned to cvg . found evidence of bird ingestion in nr 1 engine . inspected same . ok for service .
aircraft was grounded : at cruise arching on l1 window with cracking of outer window pane . pressurization normal during cruise and descent . **supplemental report required** ( open )
ship 199- atb -right engine fuel filter eicas message . flight crew choice to return to jfk due to qrh stating engine may flame out or operate erratically with this message . corrective action : replaced fuel filter per b767-300 amm 73-34 . replaced fuel press switch per b767-3 amm 73-34 . ops chk nml . ( 8941142 )
config gear steering eicas warning either main gear aft axle is not centered and locked and takeoff thrust selected on e ngine l or r . conf disp 60 and flt deck crew - determined maybe sharp turn ont low 60 knts , continued 1000 '' '' , throttles retarded and message cle . runway and advanced throttles which set warning messge . no pre ared and okay to continue . thr ottle adviance not no repeat of of me vious history and ahm reflect messages intermittant and crew con ssage firmed eicas c lear . ref fim 31-78130 - this was low spd abort be add fault : 32-63010
during cruise atfl230 the nr 2 engine rolled back to idle . turned off auto pilot and autothrottle . nr 2 engine parameters were low but normal for idle . nr 2 throttle had no response at all ran qrh and landed flaps 15 . emergency declared . taxi t o gate was normal . during troubleshooting found the entire a channel of nr 2 eec failed . also found ch b tra signal in op causing a complete loss of thrust resolver angle on nr 2 engine . found connector dp0460 loose causing a loss of ch b sine signal . resecured connector dp0460 and removed and replaced the nr 2 eec iaw amm 73-21-06 and 73-21-60 . performed high p
the flight crew reported they experienced a cabin overpressureization of 9.0 psi at cruising altitude of fl400 . they indicated they were able to control and arrest it with manual press - mode . the maintenance team removed and cleaned and replaced the the cabin pressure controller . ops checks were satisfactory . the aircraft was returned to service .
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 , 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 . maintenance replaced the right-wing interconnecting strut proximity sensor 40cv per amm 27-51-44 and the # 2 slat flap control computer per amm 27-51-34 ( aala202407018999 ) . a satisfactory operational chec
during the cruise phase of aircraft n689ta on flight av665 on june 13 , 2024 , route from jfk to sap , the pilot reports th that the aircraft displays " system green 3050psi / system blue 3050psi / system yellow 3250psi " on the screen . the pilot , in agreement with the maintenance control center , made the decision to divert the aircraft to the sal maintenance base . in accordance with the troubleshooting performed the yellow engine pump was removed and replaced using the amm 29-13-51 -000-004-a / 400-004-a rev 68 . additionally a bleeding of the systems was performed iaw amm subtask 29-13-51-870-054a rev
aircraft in base maintenance : cracked forward cargo compartment baffle clip at bs 500g and s25l . replaced clip per srm 5 3-00-01-6 .
aircraft was not grounded : an emergency was declared during descent into phl . the flight crew reported that after takeof f with gear up a hot brakes ecam for # 2 brake displayed , the flight crew levelled off the aircraft at 4000 '' , 210 knots a nd put the gear down . temperature continued to climb up to 900-1000 deg . the flight crew brought gear up and climbed to 31000 '' . after a discussion with moc , the aircraft continued to phl . the flight crew reported that at cruise alt , tempera ture on # 2 decreased to 490 . when the flight crew descended into phl the temperature rose back up to 550 degrees and the
ship 6715 -misc / de- crew declared emergency due to le disagree indication during approach . c / w qrh and landed . correctiv e action : contract maintenance checked for faults and were unable to duplicate . le / te ops normal . rts cleared by mcc .
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 . * * supplemental report will be submitted * * ( open )
cic - bird strike on left wing leading edge reported . maintenance c / w bird strike inspection . replaced left inboard stub wing leading edge . de-ice system operational check satisfactory . aircraft returned to service . ( x )
gnd splr 5 ecam on takeoff . crew reset sec switches per qrh and fault cleared . abort was aprox 30 knots .
floor panel 231yf insert is damaged at fwd l / h upper corner ( marked ) / identified floor panel 231yf iaw srm 53-00-50-0i- 1 figure 4 ; sheet 1 ; table 4 . upon inspection of panel found multiple areas of damage to upper and lower surfaces . damag ed insert at fwd l / h upper corner ; as marked ; and damage found on floor panel 231yf are out of allowable damage limits i aw srm 53-00-50-1a-1 par 4e ( 2b ) . due to the extent of damage opted to fabricate new floor panel iaw srm 53-00-50-2r-0 pa r 1a ( note ) ; 4a ( 2 ) . fabricated new floor panel out of bms 4-17 tyvi lot # 420733-1 ; located ; drilled ; upsized ; and instal led all inserts using bms 5-107 lot # ak0hp5746k ; cured ; and part marked panel iaw dwg 144a5810-124 ; bac5085 par 8.4.2.2
( can ) mutiple bird strikes on radome . maintenance inspection of radome confirmed bird strikes , no damage to radome , engines / vanes or pitot static system .
r hpsov valve message appeared in cruise crew diverted from sjo to mia . destination was cvg . maintenance grounded ac an d deferred rh hpsov and lock out iaw mel 36-11-2.and returned ac to service to continue to fly to cvg . where they repl aced the prsov and cleared the deferral .
aircraft was grounded : right engine failed on climb out . emergency declared ; flight returned to fco landing safely . **supplemental report for aala202208100311 : replaced right engine fuel metering unit per job card 72l40028001 ( aala202208100311 ) ; fuel pump per amm 73-12-11 ( aala202208110212 ) ; variable stator vane actuator control valve per amm 75-33-12 ( aala202208115261 ) ; fuel flow transmitter per amm 73-31-11 ( aala202208114052 ) ; high pressure fuel filter per amm 73-11-14 ( aala202208113583 ) ; low pressure fuel filter per amm 73-11-13 ( aala202208119446 ) . accomplished satisfactory engine tests.** ( closed )
ship 3143 - div - to mia due to flight crew report of airframe vibration felt in aft fuselage . vibrations lessened at lower speeds and stopped at 250kts . corrective action : found aft drain mast heater c / b popped and heavy ice buildup on mast . placed system on mel and continued flight . removed and replaced drain mast control unit iaw a319 amm 30-71 . ( 8715448 )
aft cargo compartment sta . 727f+5.3 / 4 wl 155 rbl 21 z angle has corrosion . accomplish r / h z angle repair on work card y175976 verified material loss org t .040 " loss of .008 " found to be out of limits iaw srm 53-00-53-1a-2 p / n 146a75 02-34
right engine starter / generator failed in flight with no indication of failure . results of the indication failure resulted in main batteries and emergency battery discharge , coupled with failure to properly load shed . these several instances resulted in loss of indications in the cockpit . crew took emergency measures to safely land the aircraft .
received alternator failure annunciation accompanied by no alternator amps and smell of burning electrical while enroute cruise . alternator was deactivated . cause of failure was the ring terminal connector to alternator had broken . arcing burned insulation and caused internal damage to the alternator which required replacement . grounding jumper ring terminal from alternator to starter on starter lug was also sheared . it appears the wire loom containing field , ground , starter and power cables were secured with little to no slack to allow for vibration .
loss of altimeter 1 during take off run by fault msg " loss of the fcu data input bus on the adiru1 " in accordance with tsm : 34-13-00-810-921-a the system test of the adr ( sys 1 ) was performed , test ok . by tsm task : 34-13-00-810-921-a - asm fig : 34-13-02 sch 02 - awm fig : 34-11-15 p0001 the wiring check by continuity of the digital baro correction a bus from adiru1 ( 1fp1 ) pins 15g and 15f connector a to the first terminal block 1851vt module 41 pin-p and module 42 pin-u , was performed ; the wiring check was found in normal conditions . in accordance with ammtask 34-13-00-790-002-a the leak measure test of the principal static and total air data system were performed satisfactory no leaks found in accordance with amm 34-12-34-000-001a / 400-001a adiru # 1 was replaced test operational satisfactory .
aircraft was not grounded : closet door hard to open by 1l door . adjusted latch mechanism on closet door by l1 entry doo r as required
aircraft was grounded : an emergency was declared due to : in all phase of flight a persistent light air frame vibration a nd buffeting was felt with and without autopilot engaged ; aircraft diverted to and landed safely at dfw . inspected aircr aft per amm 05-51-67-280-801 , found apu door open . no other defect noted at this time .
inspection type : na * * diversion * * during climb out of phx crew recieved level 1 air sys off message . red manf fail light . n overhead panel illumited for approx . 10 sec . and went out . bleed air valve # 1 closed . system is depressurized.accompl ished fim 36-23-02 fig 104 , pnue 1-27c displayed in cfds . removed and replaced manifold failure sensing element d1-156 p er m / m 36-23-07 and mfc per m / m 36-23-01 . ops check good .
aircraft was grounded : right elevator tab control mechanism , aft outbd spring is broken . removed and replaced rt elevator tab control mechanism aft outbd spring iaw amm 27-31-34 .
aircraft was grounded : an emergency was declared upon arrival to the scheduled destination of dfw . cabin crew reports ch emical / electrical odor # 2 flight attendant jumpseat center aisle aft galley . odor was getting faint in cruise but was reported strong just before top of decent . odor began during boarding and continued during takeoff and climb . reported to flightdeck in cruise flight . the aircraft landed at dfw safely without further incident . maintenance accomplished smo ke / odor / fume troubleshooting task card 26l00021001 and was unable to duplicate the odor .
during climb thru 27,000 left engine surge . egt hit 937 . crew complied with qrh procedures leveled at 28,000 and surging abated . audible pops during climb and descent . around 17,000 ft airframe vibrations were noted . both climb and descent in the 60 % n2 band . air turn back to departure station ( ksbd ) . air traffic control declared emergency for crew . landin g was without incident and no additional precautionary actions . on arrival , aircraft was grounded for unscheduled mainte nance . work in progress .
bird strike on copilots windshield , during takeoff . bird strike inspection and no damage found .
aircraft was grounded : an emergency was declared on approach into rdu : landing gear did not extend on first attempt . eca m advised to recycle and wait 120 seconds , but gear still did not extend . crew followed ecam instructions and accomplish ed a gravity extention of the landing gear . the aircraft landed safeley without further incident . maintenance replaced s afety valve 49ga per amm 32-31-17 and accomplished a satisfactory leak / operational check .
ship 3722 -div- diverted to pbi due to loss of crew oxygen . indication down to 690 psi . corrective action : found observe r '' s o2 mask box leaking . tightened b-nut . replaced crew o2 bottle . also found o2 bottle regulator hose leaking . replaced hose . leak checks good . ok for service .