boeing/aviation-ner-BIO huggingface dataset:
large bird ingested , left engine at 1000 agl during takeoff from phl , gear extended performed air return to phl , landed at 43,700 lbs . c / w birdstrike insp ref amm 05-51-25 ref w / o 123145 for aw work found .
z chanel at st 460 to 480 ; lbl 23 have surface corrosion around 3 nutplate ( 228-036 ) _wl 154 / removed and installed new '' z '' channel ( side plate ) at fwd cargo lbl 23 '' from 396 to sta 480+11 '' iaw b737-700 srm 51-40-02-0g-0 ; 53-00-53-2r-5 and document number 143a7500 ( wl 154 )
ship 9570 -ato- the pilot aborted the takeoff at 100 kts due to the aircraft drifting left of center line . corrective ac tion : maintenance performed a high energy stop inspection and accomplished checks of all of the flight controls . no defe cts were found . ( lp # 4703424 )
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 . * * original report was aala202305192367 * * maintenance replaced the overpressure valve 5ha2 , the bleed p ressure regulator valve control solenoid / temperature limitation thermostat 10ha2 ( aala202307272150 ) and the bleed air precooler exchanger ( aala202307272325 ) on the # 2 engine . a satisfactory leak / operational check was accomplished .
aircraft was grounded : an emergency was declared on arrival to aus due to smoke in cabin , near seats 21a , 21b , 21c . smoke first appeared under the seats . note : video screens at 21a , 21b , 21c are now inoperative . the aircraft landed safely at aus and taxied to the gate without further incident . maintenance found a strong burnt smell fro the quad seat electronic box at 20abc and replaced it per amm 44-21-00 . a satisfactory operational check was accomplished .
ship 9569 gear / de- the crew noted the " gear door open " message after the landing gear was extended on approach into clt . they utilized the alternate gear extension method and declared an emergency with atc . the landing was uneventful excep t for the main landing gear doors remaining in the down position and touching upon landing . the aircraft was towed to th e gate . corrective action : maintenance found the left main landing gear door actuating cylinder was bypassing internally . the cylinder was replaced and rigged . also , the gear door bumpers were replaced . operational checks were good and the
ship 1801 - div - crew reported loss of oil from right engine at a rate of 1 quart / 30 minutes . out of an abundance of pr ecaution , crew decided to stop short . flight diverted to tpa . corrective action : replaced right engine starter and hydra ulic pump per b767 amm 72-64 . no further leaks from those seals . found oil leaking from b and c and 6 o '' clock recoup duc t . ran engine at 80 % n2 for 20 minutes , oil consumption within limits . ( lp 4535404 )
aircraft was grounded : an emergency was declared on approach into phl , after lowering gear # 1 brake tripple indicator sh owed 250 lb pressure remaining . the flight crew accomplished a go around to consult with moc and troubleshoot the issue . it was determined that the low level residual pressure would have minimal to no impact on landing and the aircraft land ed safely at phl . flight crew reported with direct right crosswind aircraft pulled left on taxi . maintenance found the # 1 brake very difficult to move with the brakes off and replaced the # 1 main landing gear brake per amm 32-42-27 . a satis
aborted t / o at 90 kiasfor eng 2 compressor vane ecam . no other p roblems noted ran pfr and cfds test , verified fault code per fault finder vsv replaced vsv actuator on engine two per amm 75-32-41 up to step verified eng 2 reverser and cowlings closed and latched . lock actuator fail . see attached photo . 5d ( 1 ) . need to perfor power assurance test per task release returned to flightdeck stowage compartment . 71-00-00-710-013-c . reversers and cowlings closed . parts used : 31-7532-9-0002 , qty :1 add emp:187550 rotable parts change was indicated - tt # 1721339 sn off 7064 actuator , varia off 31-7532-9-0002 7064 on 31-7532-9-0002 9722 accomplished high powerassurance test , test 11 . no ecam or cfds faults noted . add emp : u108809
flt # 788 , sxm-jfk . ( aircraft diverted to fll ) '' upon climbout of sxm we felt a medium vibration after flap retraction . the vibration continued on climbout to altitude fl 320 , the vibration seemed to diminish in cruise once we slowed the aircr aft down to 280 knots inflight crew also said they felt the vibration throughout the aircraft but mostly in the aft sect ion of the aircraft they stated that they did not have this vibration when they departed jfk . all flt controls and engin e gauges looked within normal parameters on the ecam pages . ''
fwd aft red cargo fire eicas illuminated for approx 5 seconds passing fl250 . with audible . on turnback , lights went out with no more warnings . no bottles expended due to short duration of light . r and r the fire detection printed circu it card m10427 iaw mm 26-10-01-4 , ops checked normal .
pilot report : upon departing ads ( gtx936 ads-lbb ) tower reported seeing a contrail streaming from the plane . pilot confirmed and said he would return . not long later reported the rt engine starting to run rough and requested priority to land . tower dispatched the fire trucks . landed without incident and returned to the ramp . on observation there is oil streaking down the side as well as under the cowling and dripping on the ground . maintenance has inspected the right engine and found the air / oil separator return line fitting had broken of the air / oil separator . maintenance replaced the air / oil separator cannister ( serviceable unit ) . nacelle and engine compartment cleaned . aircraft was taken to the maintenance run-up area , no leaks noted . mechanics performed a take-off power run to determine rough engine reported . engine fuel set-up checked and adjusted as needed . operational check was good .
flight crew reports via arinc pack 1 +2 fault on ecam , pack 1 already on mel ref log page 4192703 . pack 2 showing cfds ata 21-61-52 p2 ram air out actuator source temp ctl . declared and emergency , descended to to fl 100 . diverted to mci.va rgas tomc updated maa code fix using vendor maa screen updated maa code fix using vendor maa screen please contact tomc before commencing any work . due to pfr and temp ctl test on mcdu ref amm 21-61-00 , p2 ram air out actuator fin 29hh , rep lace p2 ram air out actuator fin 29hh iaw amm 21-61-52 , tsm ref 21-61-00-810-815-a . vargas tomc mac meter initiated for
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 . * * supplemental report for aala202304068570 : maintenance accomplished a borescope inspection of the # 2 engine and no defects were noted . during a test of the vbv system on the # 2 engine it was noted that the vbv position sensor was misaligned and maintenance was unable to move the vbv doors . the vbv master ballscrew actuator was replaced p
aircraft was grounded : an emergency was declared and the aircraft returned to lax . climbing through 10.000 to 29,000 air craft began moderate vibration in tail above 250 knots . flight crew reported there were no engine or flight control indi cations on the ecam but vibration was enough to create noise and make it difficult for the flight attendants to stand in the aft of the aircraft . the vibration could be felt in the flight deck as well . the aircraft landed safely at lax with out further incident . maintenance checked the flight controls and found no issues also checked for loose panels or seals
pilot reported smoke in the cockpit unknown location . upon investigation by our lead mechanic we found the heater flamed out . ops checked good no defects were found . and aircraft returned to service . the janitrol heater was close to tbo . and was replaced with a over hauled heater . the following month .
aircraft was grounded : an emergency was declared and the aircraft returned to ord due to the flight crew reporting that on takeoff low oil quantity indication . oil on number 1 engine went to 1.5 quarts and oil pressure remained solid at 4 0 psi . the flight crew reported that the engine was not shut down . the aircraft landed safely at ord and taxied to the g ate under its own power . maintenance noted oil in the hpc during the accomplishement of a borescope inspection of # 1 en gine . maintenance replaced the engine per task card 26l40071001 .
during climb number one engine adi light remained on after adi system was switched off , aircraft returned to base / kopf .
aircraft was not grounded : an emergency was declared on approach into dfw due to the flight crew reporting that when fla ps 2 were selected a flaps fault message for the slat flap control computer 2 flap channel . maintenance replaced the com mand sensor unit per amm 27-51-17 . a satisfactory operational check was accomplished .
ship 3272 during flight dirty sock smell in cockpit causing air turn back . corrective action : oil wetting in engine hpc . replaced number 1 engine . ( 2238276 )
aircraft was grounded : # 1 eng mode fault came on in climb around 23000 we did ecam procedure continued climb at level off 330 . we could not maintain speed.we told atc for lower altitude and returned to dfw . power was back descend thru mid 20s . throttle split was 3 / 4 with no help . levers were up to cub stop . an emergency was declared and the aircraft returned to dfw where it landed safely without further incident . **supplemental report : replaced engine electronic control and ignition supply harness ( aala202103099025 ) and pt2 / t2 cable assembly ( aala202103129012 ) . a satisfactory operational check was accomplished .
while in heavy check - crack at rh lower wing at rib 4a . installed doubler repair iaw etd2023-170-024595
uncommanded yaw control at reaching cruise altitude . declared an emergency . removed and replaced the nr 2 fcc card
aft cargo bay floor to sidewall support r / h bs927-bs947 rbl20 wl177 ; / [ 01 ] verified applicability of srm 53-70-53-0i-2 for identification and srm 53-00-53-1a-2 for allowable damage ; [ 02 ] removed corrosion from acb floor to sidewall suppor t r / h bs927- bs 947 rbl 20 wl 177 ; maximum blended area 3 '' x2 '' x0.018 '' deep ; found to be out of limit iaw srm 53-00-53-1a-2 par.4.a ( 2 ) fig . 103 detail . d . br > tool used : dial depth gauge ; id : ats401 ; s / n : unknown ; [ 03 ] corrosion out of limits pe r srm 53-00-53-1a-2 ; [ 04 ] removed acb floor to sidewall support r / h bs887- bs947 rbl 20 wl 177 iaw srm 51-40-02-og-0 ; [ 0 5 ] this discrepancy will accomplished on card ttg8q0055629 ; [ 06 ] this discrepancy will accomplished on card ttg8q005bq5y
in cruise at fl240 right vibration fluctuating between 3.5 and 4 .1 while capt varied r-h engine power . at cruise altittude and power , both engines were matched indicated vibration was negligeble . debriefed crew . vibration started during climb above 23,000 ft under power . vibration was not felt in the cockpit . vibe readings solely from eicas . flight attendants felt vibration mid cabin . flight officer verified flight attendants observations , r and amp ; r engine vib monitor ref amm 77-31-03 precautionary . checked lubricated engine # 2 mid-span fan blades as needed . ref amm removed and replaced avm accelerometer on # 2 as precaution . ran # 2 engine for avm system test . ops checked good .
inspection type : c1 , main cargo compartment floor panel 232xcf damaged . fabricated a new floor panel iaw sreo b757-5320 -9692-k .
nr 1 eng bird strike . nr 1 fec , stg 6 hpt 60 % airfoil missing . subsequent writeup for removal acct hpc stage 6 airfoil damage . nr 1 eng nose cowl 1 and 6 o'clock appears to have gone into engine and lt wing panel 521ab near fuselage . bird strike inspection completed . elevator delam within limits for 'c ' check . starting to remove engine . also have pit hyd leak . eng removed .
aircraft was grounded : an emergency was declared and the aircraft to sea . climbing through 17000 '' , 340 knots flight atte ndant called and indicated loud low mechanical rumbling . metal grinding , carts aircraft right vibrating and the left sid e stationary . they could feel vibration in touching floor when near door . flight crew leveled off at fl 210 and vibration dissipated.vibration returned upon pitch / power changes for climbs and descents . the aircraft landed safely at sea wit hout further incident . maintenance found the r4 door upper cover plate out of adjustment and adjusted it per amm 52-10-0
rh wing water drain valve 26qm between rib 1 and rib 2 outer drain valve missing m / e 99-2811-3-0021 part n.i.s at oma m / e 00-0596-3-2121 part n.i.s at oma added packing to parts needed outer water drain valve outer water drain valve
gear disagree tailskid and master caution illuninated on turn to final . ran qrh 14.17 which cleared gear disagree and ta ilskid gear doors illuminated . crew declared an emergency . aircraft landed with out further incident . aircraft was grpon ded by maintenance . maintenance deferrednthe landing gear retract system iaw mel 32-30-1 . maintenance procedures complie d with . placard installed . aircraft was relocated to cvg for further maintenance . mlg gear control lever module replace ment performed multiple gear swings per b767 amm 32-34-00 and 32-32-00 . completed rii forms 32-01-1 and 32-02-1 . this cl
yellow-green ptu leaking . replaced green-yellow ptu . bled system and checked for leaks . checked ok . ops check accomplished on smc 18 .
crew reported an aborted takeoff at 90 knots . due to avionics vent sys fault ( blower and extract ) max brake temp . at 5 90 on # 3 wheel cfds report faulting ( 22hq ) skin air outlet valve . req mel skin air outlet secured as required . performe d ddp , valve 24hq complied with with no additional faults . wheels and tires now 2126c . in open position , connector disc onnected and capped . aevc test inspected with no faults found . temps are normal ambient range ok to mel complied with requirements in mel 2126c in logpage 6201477 . reopen den u305451 04nov23 for : closed in error tech signed off in error .
rejected take off at 90 kts due to fwd entry door light crew verified to tomc that fwd entry door handle was never compl etely closed for departure , crew closed door handle completely with no defects . crew observed brake cooling period per t he fm .
aircraft was grounded : an emergency was declared and the aircraft returned to clt due to the flight crew reporting that after takeoff , they recieved an ecam for landing gear not uplocked , along with red nose gear indication . the ecam cleare d before we could address it . the aircraft landed safely at clt without further incident . maintenance accomplished tsm 3 2-31-00-810-865-a with no faults or defects noted . maintenance also accomplished a functional test of the normal extensi on and retraction of the nose landing gear with no faults or defects noted . maintenance reported that the gear indicatio
vvi - crew reported left engine ingested medium size bird . emergency declared , flight returned vvi landed without incident . aircraft removed from service . replaced left engine at mia on 05 / 26 / 2012 . system ground check normal operation .
fumes in cockpit . burning oder from fo overhead gasper vent . started near top of climb and was intermittent . then the sm ell became steady and crew made their decision to divert . corrective action : performed air conditioning system test ia w amp bd500-a-j21-51-00-01aaa-320a-a , air conditioning leak test iaw amp bd500-a-j21-51-00-01aaa-364b-a , visual inspect ion was also done to recirculating fan filters iaw bd500-a-j21-22-03-01aaa-520a-a , during all operation and test not fu mes or any distinct smells were present . ( apu ) drain lines -visual examination iaw bd500-a-j49-14-00-01aaa-311a-a ops c
magnetic mro as , performing maintenance under cayman islands approval received part 740-2040-503 with 8130-3 ( tracking a239896 ) from faa repair station 3s7r970b ( set aero ) . during inspection it was found that incorrect pn was used for mount assembling during workshop visit . used bolts pn nas6303u4 - are shorter , than correct bolts pn nas6303u5 . used washers pn *unknown* - are thinner , than correct washers pn vn936np3 .
fmc nav status irs l only . no fault lt . fo no mag comp or hdg b ug.fo tcas fail . on r adiru found fault 34-21009 " enter heading " fault on last good . performed land verify test per amm 22-11-00-700-801 . all leg . per fim 34-21 task 808 fault cleared after heading is test passed full cat capability retained . parts used : entered . no maint required per fim . no other faults found . 60-3421-9-0001 , qty :1 removed and replaced r adiru per amm 34-21-01 . all ops checks rotable parts change was indicated - tt # 1760096 sn off 3003 unit , adiru , ai off 60-3421-9-0001 3003 on 60-3421-9-0001 1449
fuel fltr bypass r amber cas : fl360 fuel filter bypass r amber cas illuminated . repeat write up .
found a crack on the window of aft entry door . replaced the window of aft entry door . amm 56-31-01-004-001 .
lo oil level on take off roll . rejected take off . pilots stated they apllied power to aircraft for t / o around 60 knots t hey got low oil light and stayed on for about 5 seconds . pulled back power and light went away . per crew information : le ft engine . performed tsm 79-33-00-810-822-a , suspect low oil sw , r and amp ; r eng # 1 oil press switch iaw amm 79-34-15.ops ch eck good no msg at idle run parts used : 1551669 , qty : 1 rotable parts change was indicated - tt # 1551669 sn off 9149 swi tch , eng oil off 31-7931-9-9003 9149 on 31-7931-9-9003 8718 switch , eng oil off 31-7931-9-9003 9149 on 0000 ran eng ref
aircraft was grounded : an emergency was declared due to : crew reports number 2 oven overheated ; aircraft diverted to and landed safely at tpa . performed operational test of oven per amm 25-32-03 , test passed . no fault found .
left mcdu failure at cruise . screen blanked and all keypad lights illuminated . after several seconds the lights extinguished and the screen momentarily displayed system data and then returned to the previously selected fmc page rather that the menu . all fmc functions remained operational the entire time . grounded - yes . performed bite of left fmc b737-800 fim 34-61 task 801 , performed fim 34-61 task 804 cdu blanks , performed cdu bite . no faults noted , ok for service .
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 will be submitted * * ( . pen )
left wing - wing side outboard flap inboard hinge barrel nut hole bore found corrosion corrosion at left wing - wing s ide outboard flap inboard hinge barrel nut hole bore reworked and found exceed limit as per md-11 cmm 57-44-08 . oversi zed bushing fabricated by machining and installed as per md-11 cmm 57-44-08 and e.a . # : 1- 5750- t0348296 part 1 step 1a . title : wings- flight surfaces- eo 1-5750-7-5002- lh wing- outbd flap inbd hinge assy ( wing side ) - corrosion rep air . repair classified as minor per gmm 6-2-100 . refer to e.a . # : 1-5750-t0348296 part 1 and snrm no . n00317 for wo rk details .
after takeoff eicas msg 1 ) chyd qty 2 ) c hyd 2 ovht center hyd system reaad 0.16 aircraft returned to field without further incident grounded by maintenance . trouble shot and found outboard slat pdu control valve module leaking .removed and replaced left outboard slat pdu control valve module iaw amm 27-81-12 serviced hydraulics and returned a / c to service .
aircraft was grounded : an emergency was declared and the aircraft returned to mco : flight crew reported a sudden loss of power experienced on number 2 engine during rotation . the aircraft experienced a violent yaw motion to the right . the f light crew reported that there were birds were observed during rotation and suspected it was a bird strike . the aircraft landed safely at mco and taxied to the gate under its own power . maintenance reviewed the fdr data for this event and c ould not find any anomalies with either engine . they did note there was a spot of approximatley 3 seconds when moving th
during to roll at 40 / 60 knots r reec fail illum with associated i cas . reec altn iluminated maint sts aborted t / o inspec ted tires and brakes . no damage found . ref amm 32-40-00 . reset r pimu ref amm 77-35-01 crew egr twice curently no msg co nt on lp 6251423 and lp 6251414 . lp 6251423 : ecs msg ecs msg0reng probe heat antiskid / autobrk r eng ecs mode reract r pi mu ref amm 77-35-01 . accompl eec bit test 7 ref amm 781-00-00-745-007-n00 . test passed . currently no pimu / eec msg . twice egr by crew . all indicator normal . lp 6251414 : multiple lights ovrhd annunciator illuminated and flickering . ra oa / tat fo p
return to field due to nr 1 engine compressor stall and subsequent shutdown . replaced engine . disassembly of removed engine revealed fractured 3rd stage blade as root cause . further analysis of blade fracture area revealed bird debris as most likely source of fracture initiation . bird remains will be sent to the smithsonian for species identification , and data entered into industry fod database .
pda 3 left wing # 2 slat has one fastener head broken off / missing and another loose at actuator attach point -- see photo photo added photo added photo added update -- one fastener missing and 3 fasteners loose -- see photo installed missing hi lock and tightened lse as required , ref srm 51-40-02 .
aircraft was grounded : an emergency was declared and the aircraft diverted to clt due to engine number 1 oil quantity dr ops from 14 qts at engine start to 2.0 qt in flight . crew reported they did not get ecam warning . the aircraft landed sa fely at clt without further incident . maintenance found b sump scavenge tube union 454k1 leaking on the left hand side . f # 1 engine . maintenance secured union per esm 72-00-00-h1a 710a-c and accomplished a satisfactory leak check .
aircraft was not grounded : an emergency was declared coming into pwm due to a flight control flaps fault on short final when selecting flaps 3 . after go around flight crew completed ecam procedures and message went away at flaps 1 position . the aircraft landed safely at pwm without further incident . accomplished operational test per amm 27-84-00 and 27-50-00 with no faults found . maintenance serviced yellow hydraulic system as a precaution per amm 12-12-29 .
aircraft was grounded : an emergency was declared and the aircraft diverted to phx : during climb lost all green hydraulic system . flight crew manually extended the landing gear and landed safely at phx without further incident . * * original re port was aala202306015493 * * maintenance found the # 1 engine grreen hydraulic pump pressure line chaffed / leaking and re placed it . also found the # 1 engine thrust reverser isolation control unit leaking and replaced it . ( aala202307282907 ) a satisfactory leak / operational check was accomplished .