boeing/aviation-ner-BIO huggingface dataset:
center right fuel pump low pressure light come on in flight center tank fuel quantity at that time was approximately 1,500 lbs qra procedure completed . grounded - yes . on deferral .
mdw - flt 815 - aborted takeoff , no emergency declared , returned to blocks . at approximately 100 knots during takeoff roll , ingested bird in nr 1 engine . ( x )
left bleed trip off / trip reset / light illuminated again debriefed crew on arrival . left bleed annunciated at 40000 ft with corresponding bleed to " 0 " . reset per qrh . reset lasted several minutes before left bleed tripped again with " 0 " pressure on left side . they contacted tomc and decided to divert into den . note : # 1 engine just replaced 2 / 4 / 24 par ts information update rotable parts change was indicated - tt # 1522515 sn off 5579 note : installed valve pn : 63292146 s n : 5579 should not be failing as it is allegedly new . coincidentally , alternative pn 3289562 should read 8.5 +or- 2.5 tro
crew reported ecam for aft cargo door at fl 1200 . declared emergency and descended down to fl 10000 . ecam went away . perf ormed post flight report and found aft cargo dr prox snsr ( 32wv ) tgt pos . fault.pics attached . inspected aft cargo door upon arrival and found aft cargo door locked and latched closed requesting mel for aft cargo door indication placed on m el ok to apply mel 5270cd for aft cargo door indications inop * dm * recommend tsm 32-31-00-810-886-a for initial t / s . pos sible cause prox sw ( 32wv ) attached on m / l . replaced aft cargo compt door prox s / w 32wv.ops test normal.ecam door page i
# 2 eng front spinner cone worn to limits . grounded - yes . removed and replaced front spinner cone on # 2 eng ref . b737-80 0 amm 72-21-01-401 .
ship 3126 - div - to abq due to loss of the yellow hydraulic system fluid . crew also reported ths jam message appeared d uring diversion . corrective action : r / r yellow case drain filter , yellow edp filter , and yellow hydraulic system ptu man ifold 3015gm per a319 amm 29-13 . ops and leak checks good . ( 5077764 )
about 15 minutes prior to arrival to klan from kpln , the electrical instruments started surging and occasionally the comms , gps , and navs on the pilot side would flash off and on . prior to getting the airport in sight , the electrical power shut off and it took a couple seconds of chattering in the instruments before it came back on . the pilot was able to get the power back and informed approach that the airport was in sight . upon switching to atc , the power went out again and when pilot was finally able to reach the atc called airport in sight and received landing clearance . when flaps selected to 1 / 2 and gear down , the power went out almost completely . # 2 nav and comm was still powered , but unable to transmit . pilot leveled off at pattern altitude and flew down the runway while running the qrh . pilot was able to restore power to the airplane by turning just the generators on and leaving the batteries off and reestablished contact with atc and informed them , the aircraft was having electrical issues and declaring an emergency . pilot requested tower flyby for visual gear down verification and the pilot was able to complete the rest of the pattern and landing with no additional issues .
( can ) during climb , acft experienced strong vibration on rt engine , crew return to ground safe and discover rt engine had a bird strike .
aircraft was not grounded : left oven smoking when turned on . **supplemental report will be submitted** ( open )
ship 5807 initial inspection : corrosion on stringers 2.90 , 7.55 , 10.45,16.10 lh sta 1328 . corrective action : summary of nrc 00395 : corrosion level 2 on stringers 2.90 , 7.55,10.45 , 16.10 lh sta 1328 were repaired per b-757-300 srm . ( 1763236 )
ship 9522 -misc / de- during approach for landing , the " bus dc r off " indication illuminated . which was followed by 15 oth er discrepancy indications . the qrh was complied with and the crew declared emergency due to the impending no flap and n slat landing . a hot brake condition existed after the landing . corrective action : maintenance found that the right pcd u circuit breaker had tripped . the pdcu was replaced and the contactors were cleaned , the dc bus feed c / b was replaced , and the messages were all cleared . a high-energy stop inspection resulted in no findings and the aircraft was returned t
corrosion fcb floor to sidewall support lbl24.75 ; bs500+10.5 '' ; wl157 ; / [ 01 ] verified applicability on srm 53-30-53-oi- 2 for identification and srm 53-00-53-1a-2 for allowable damage ; [ 02 ] removed corrosion from fcb floor to sidewall suppo rt bs 500+10.5 '' '' lbl24.75 wl157 p / n 143a7501-183 in area of 3 '' x1 '' x0.020 '' deep ; original material thickness 0.040 '' '' found to be out of limit iaw srm 53-00-53-1a-2 par . 4.a . ( 2 ) fig . 103 detail a . br > tool used : depth gage ; id : ats 2473 ; s / n : un known . ; [ 03 ] verified removal of corrosion from fcb floor to sidewall support bs 500+10.5 '' '' lbl24.75 wl157 p / n 143a7501- 183 in area of 3 '' x1 '' x0.020 '' deep ; original material thickness 0.040 '' '' found to be out of limit iaw srm 53-00-53-1a-2 par .
on takoff , took numerous bird strikes , nr 1 engine was shut down , returned msp . replaced engine and nose cowl for return to service .
rh vert aft spar is heavily corroded . located above rudder upper hinge . repaired 2 blended areas of vertical stabilizer r / h aft spar cap at approximately vfs 172 and vfs 237 due to corrosion per aqrd ero-108612 rev . ir , titled , " rfts-108612 - n370qs - vertical stabilizer aft spar repair " dated nov 3 , 2023 . supported by faa form 8110-3 dated 11 / 03 / 2023 . the fatigue and damage tolerance ( f and dt ) evaluation required per 14 cfr part 25 , section 25.571 is not included as part of this engineering document . per netjets aviation , inc . general maintenance manual 11.2.5 - the f and dt evaluation must be completed within 12 months from the date of issue of the associated 8110-3 . ( alternate terminating actions to the f and dt evaluation requirement must be separately approved and are not included in this ero . ) repair recorded on form 337 dated 13 nov 2023 .
flt # 779 , jfk-mlb . ( aircraft declared an emergency and perfromed an air turn back to jfk ) '' fume event immediately after t take off very strong smell of sock odor did not go away until after landing . indflight crewmember became very sick apu wa s off . emergency returned to jfk . '' ( supplemental information to follow )
submitted to reveal the systemic and premature failure rate of the tail rotor shaft bushings due to excessive play and worn beyond limits .
ship 6711 -div / ifsd / de- diversion to msy due to right engine oil filter advisory message . crew followed qrh and shutdown engine . corrective action : inspected mcd '' s and oil filter , found metal debris on main and gearbox mcds . analyzed materi al and found 52100 bearing material . engine change required .
ship 5016 -atb- air turn back due to right engine vibes peaked at 5.3 in climb . throttle was retarded to 70 % to come below 5.0 on vibes . corrective action : performed gvi and borescope inspections with no findings . replaced aodv per a321neo amm 79-21 . ok for service . ( 4271285 )
main cabin bs 377-345 seat track crown has corrosion removed and replaced seat track at rbl 14 sta 377-345 iaw dwg 3504-nc-2 , swg 3470 rev g and accomplished ea f-5310-t0372129 .
inspection type : etop fod - bird strike nr 1 engine . emergency declared . on short final crew reported bird ingestion in nr 1 engine . engine vibration reached 3.8 and was reduced to idle . a / c is oos . found damage blades 24,25,26,27 beyond repair . installed bld ingt pos 7-178310 and int in pos 26 , inst new 177208in pos 6 , inst new 178246 in pos 7 , inst new 177486 in pos 27 , all as per amm 72-31-02-4 .
eai prsov l advisory . left engine anti-ice ( eai ) prsov failure . fim task ref : 31-90-f8-01a-421b-a . cmc msg # 3010011 flight status : l intermittence code : m ph : cruise narrative : 30 wwfds eai cips ops ( left ) . left engine anti ice valve prsov photo added locked in mid position rof reference left engine anti ice valve checked full and free movement.requesting mel 3021be . left engine anti ice prsov locked in mid postion ref ddg 30-21-01-04 . mm 75-32831 confirmed on existing faults . mel 3021be complied with dispatch desk : 3361 name : bp date : 21-aug-23-noc desk : 787 name : mm date : 21-aug-23- item deferred per mel and dispatch and opb advised.picture added for ground test pass all valves reactivated iaw with amm 30-21-01 . for trouble shooting all valves checked for full and free movement . ground test anti ice with engine run completed and passed . to verify operation . iaw amm 30-21-00-200e-330b . no correllated msg showing.reopen mel u331165 23aug23 for : insufficient info provided tomc approved reopened for sdr indication selection item updated sdr corrected mel clear all valves reactivated iaw with amm 30-21-01 . for trouble shooting all valves checked for full and free movement . ground test anti ice with engine run completed and passed . to verify operation . iaw amm 30-21-00-200e-330b . no correllated msg showing .
aircraft was not grounded : an emergecny was declared and the aircraft diverted to phl due to potable water shows empty on flight attendants panel . the aircraft landed safely at phl without further incident . maintenance inspected airframe no water leak detected and serviced potable water system .
aircraft was grounded : an emergency was declared into lax due to the flight crew reporting yellow hydraulic reservoir lo w level ecam caution displayed . flight crew accomplished ecam procedures and they reported that after running the proced ures the yellow hydraulic system engine 2 pump low pressure and yellow hydraulic system low pressure ecam messages displ ayed the aircraft landed safely at lax without further incident . maintenance replaced the right hand pylon yellow hydraulic line / hose per task card 2922e003-004 .
ctr tk pumps lo pr displayed on upper ecam screen . - fuel upper ecam fuel ctr tkpumps also both ovrhdctr pump switches ha vefault lights yyc mechanic gupta , ritesh ( v937228 ) found 420 lbs in center tank automatic fuel feed system requires further troubleshooting . deferred directly by tomc updated maa code fix using vendor maa screen mac meter initiated for found 420 lbs in center tank automatic fuel feed system requires further troubleshooting . see l / p for replacement of ctr tank gfi . performed operational c heck to ensure both ctr tank pump feed for 2 mins after engine s tart as per mm-28-21-00-710-005 and functional test as per mm-28 -21-00-720-001 . all checks good .
acrid smell in cockpit and cabin shortly after takeoff in dca . smell worsened according to flt attendants . diverted to iad . flt crew discovered bird remains on stator blades of left engine intake about 6 above bullet nose . no apparent damage to fn blades . smell had begun to dissipate during descent . performed bird strike insp . 05-51-08 no defects noted . clean stator vane and inspected eng , ran engine and a / c packs , no odors or smells present , engine run normal .
aircraft was grounded : approximately 30 minutes prior to landing auto flight , # 1 flight control unit ( fcu ) ecam fault . qrh system reset ok but only 5 minutes then fault re-occurred . an emergency was declared and the aircraft landed at dfw safely without further incident . maintenance replaced flight control unit ( fcu ) per amm 22-18-00 . and accomplished a satisfactory operational check with no faults noted . tt 6460411
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 will be submitted * * ( op en )
during t / o had birdstrike on left side of aircraft . returned mco . mtc found dent in fuselage fwd of left pitot probes . aoa vane sheared off . pitot probes impacted . left engine has 2 fan blades bent out of limits and some minor acoustical liner damaged . visual and hpc boro insp ref mm 72-00-00-206-24 . no discrepancies noted . replaced lt aoa sensor per amm . insp area per srm 51-10-03 area is within limits . replaced blade 7 8 26 and 27 per mm . eng run vibe chks nml .
aircraft was grounded : an emergency was declared into scheduled destination of dfw . flight crew reported a fume event du ring climb and cruise that was a heavy chemical smell -burnt sock odor near 4l door . the aircraft landed safely at dfw a nd taxied to the gate under its own power . maintenance accomplished the smoke / odor / fume troubleshooting task card 26l0 0021001 and determined the odor to be excessive residual cleaning fluid in the right aft lavatory and cleaned the lavato ry walls , floor and toilet to remove the residual cleaning fluid as required .
wo 17 '' 250 '' 631 - rejected t / o at 80kts due to adr 1 fault , wo 17 '' 250 '' 632 - after reject t / 0 cond trim air sys fault fwd cab trim valve , wo 17 '' 250 '' 633 - inforandmation the pilots brake # 2 with 550 ? c and brake 1 with 350 ? c . rejected t / o a t 80 kts , in accordance with tsm 34-14-00-810-996-a step 4.a.2 , and amm 34-12-34-000-001-a , adiru 1 was removed . in a ccordance with amm 21-63-00-710-004a operational test of the operational test of the cockpit and cabin temperature contr ol was performed satisfactory , and i.a.w amm 21-63-00-710-005a operational test the trin air was performed . in accord
after t / o in clo passing 6000ft , bird strikes right engine immediate return , eng vibration went up to 9.2 n1 , moderate vibration other parameters were normal . in accordance with amm 05-51-19 pb 601 task 72-00-00-200-006-a item 4-a ( 8 ) and b ( 2 ) ( a ) ( b ) boroscope inspection was accomplished no damages were found . in accordance with amm 05-51-14 pb 601 check of the airframe after a bird strike in flight were accomplished no damage found and inspection of the airframe after a bird strike were performed and no were found damage .
aircraft was grounded : an emergency was declared and the aircraft returned to fll after the flight crew reported loosing engine # 2 epr indication . the aircraft landed safely at fll without further incident . maintenance accomplished tsm 73-2 2-00-810-818-b . epr indication operational checks normal with no faults noted .
when selecting gear up on take-off , got gear disagree warning . ran qrh and gear extended normally . nose gear red symbol and nose door open red warning . gear disagree message appeared within 5 secs . *******aircraft removed from service*********** visually inspected nlg . no obvious damage , leaks or defects noted to gear assy , retraction components or proxi sensors . c / w " m " action for mel 32-30-01 . gear pins installed and flags removed .
lt wing aft panel support channel for panel 561ab cracked on inboard aft edge . r and r channel iaw srm .
smoke in the cabin during climb . crew declared emergency and returned to departing airport ktmb . mechanic noticed oil accumulating on rh engine inlet . pratt and whitney in partnership with west star troubleshot to engine oil over-service . mechanical difficulty report submitted to chdo .
left start valve open light illuminated after start . grounded - yes . ( resolved on w / o : 1877189 taskcard : n / r-00002 ) removed and installed new mw0312 nacelle wiring harness on # 1 engine per b737-900 mm 71-51-03 / 401 , ops check normal . no faults found . ground verification successful . opened , collard , reset 4 c / b's . placard removed . this clears mel 80-3b . seamc todd notified .
dfw crew reported strong oil odor in the cabin followed by a strong vibration in the tail during climb out . emergency declared flight returned dfw landed without incident . found evidence of bird strike to lt engine with two blades bent and nr 1 bearing leaking . replaced lt engine at dfw on 08 / 11 / 2013 . system ground checked normal operation open .
high speed reject for several large flocks of birds crossing the runway . speed at rej ect was 120 of 79min . crew debrief gross weight 144,000lbs and with thrust reverse crew also noted minimum manual braking used to stop , mostly stop relied on autobrake function . accomplished high energy stop - in caution range ref amm 05-51-07-210-801 no damage noted at thi s time , ok to continue . will observe max quickturn time on ground completed bird strike inspection amm 05-51-18-210-801 no damage noted add emp : u386235
rejected takeoff uneven spool rates number 2 slow to spool per flt crew engines spooled evenly to mid 40s , eng 1 spooled up performed eec bite check of # 2 engine and no faults for recent to 85 % n1 with toga , eng 2 only went to mid 40s % n1 f for 2-3 secs or fault history . before crew rejected . performed fim 73-05 task 814 and accel test 8 amm for further crew e valuation . 71-00-00-700-824-f00 . time to target n1 from starting n2 target was 3.83 seconds ( limit is less than 6.3 sec onds ) . visual inspected hmu connections and ps3 connection found no faults . ok also monitored control loops for # 2 engin
aircraft was grounded : an emergency was declared and the aircraft returned to dfw , approximatley 22,700 excessive engine vibration on # 2 engine . flight crew brought # 2 thrust lever to idle engine ran smooth , tried to advance back to climb d etent and vibration resumed . flight crew kept # 2 engine at idle for remainder of flight . the aircraft landed a dfw safel y without further incident . maintenance accomplished engine vibration survey and determined vibration was within accepta ble limits .
speed trim fail illuminated on master caution recall prior to top of descent . grounded - yes . ref fim 22-11-00-810-d73 performed surface test 60.32 all tests passed.tech services sam notified . seamc andy notified .
# 2 eng egt exceeded 913 degrees c on take off for about 3 seconds . ( ref tsr714984 ) grounded - yes . ( resolved on w / o : 1970040 taskcard : n / r-00001 ) interrogated cdu for engine exceedance page check per amm 71-00-00-740-801-f00 , found # 2 eng egt exceedance was 960 degrees c for 9 seconds , no exceedances for # 1 eng . c / w inspection after engine operations above the limits per amm task 71-00-00-800-804-f00 , found # 2 eng egt exceedance during take off to be within area a of figure 603 . performed visual inspection of # 2 engine inlet and exhaust , no defects found . no current engine faults logged on # 2 eng . further trouble shooting required to be placed on plt deferral for 150 hours per amm 71-00-00-800-804-f00 step 6 ( b ) . seamc arnie notified . c / n # 17068459 applied .
during push back maintenance noted toilet door service snapped . reallighnment hinge springs and secured door closed iaw amm 52-49-07
inspection type : na during wai found # 2 eng inlet dented at 2 o'clock position . mapped out damage sent measurements to eng need hfec for cracks 2020250 09 / 04 / 23 accomplished hfec per ndtspm cw interior repair iaw eo md11-7110-88105-a sect 6a item requries repair or repalcement within le pns assigned control # d 812090.removed inlet cowl in ref to 54-22-01 [ ao 0968045 09 / 10 / 23 ] installed upto step ( e ) ( 4 ) in ref to amm 54-22-01 [ ao 9168045 09 / 11 / 23 ] accomplished installation remaining steps per amm 54-22-01-400-801 . this clears d812090 . esr : ipc ref 54-62-45-01 .
aircraft was grounded : an emergency was declared and the aircraft returned to pdx due to receiving engine 1 thrust reverser ser unlock just after takeoff . the flight crew accomplished the ecam procedures which instructed them to shut down the e ngine . the aircraft landed safely at pdx and taxied to the gate . maintenance replaced # 1 engine inboard thrust reverser upper blocker door latch per amm 78-31-19 , also replaced the # 1 engine inboard thrust reverser upper blocker door actuat or per amm 78-31-41 . maintenance also found the # 1 engine thrust reverser hydraulic control unit dpi extended / tripped
aircraft was grounded : an emergency was declared due to crew o2 dropped from 1410 departing lhr to 1250 psi . aircraft di verted to kef landing safely . accomplished satisfactory leak check per amm 35-00-00 . replaced crew oxygen bottle per amm 12-15-08 .
bird strike during t / o out of dkr , lt eng vibs went to 5.0 . all other parameter normal . returned to dkr . mtc found 5 fan blades damage out limits and 1 ogv within limits . sending parts on flt 34 / 02 . will need update when mtc complete ma key 5-0145 . removed and replaced nr 1 eng fan blade assy per m / m . perform vibe survey , all chks good per m / m . p / n installed c1-1 fan s 6101 .
ship 3420 - atb / de aircraft performed air turn back to hnd and crew declared emergency due to lightning strike with righ t engine stall message . corrective action : per tsm cleared faults ran engine for five minutes and no faults returned . no further action required . no findings on lightning strike inspection . ( 5766447 )
aircraft was grounded : an emergency was declared and the aircraft diverted to las . on takeoff from slc , flight crew hear d loud bang and brief shudder at 800 '' agl . # 2 engine had brief overtemp for 5-10 seconds , then returned normal . crew suspected bird strike and crew reported that all flight deck indications were normal for remainder of flight . the aircraft l anded safely at las without further incident . maintenance accomplished a birdstrike inspection and found no evidence of a birdstrike . a review of the dfdr data revealed the engine experienced an engine stall . * * supplemental report for aala2
ship 3883 at departure l1 door would not arm . corrective action : adjusted girt bar latch . cks ok . ( 5487070 ) .
pdis 679 27-80 1336 16feb23 lax open u slats sys 1 and 2 fault on configuring approx 4000 ft , 220 knots , with no associated sfpi light . per ecam cycled slat lever , they remained in the up position . followed the qrh perfor med uneventful no slat flap 40 landing . info 16feb23 15 : 55 mc1 r emergency declared fact 18feb23 06 : 22 lax amm : 27-84-22-04-0 ref wri 27-80 / 1341 and 27-80 / 1342 and parts changed both # 1 and # 2 j ackscrew actuator for number # 1 left slat replaced and ops check good per amm
aircraft was grounded : an emergency was declared due to : crew reports smoke odor fume event witht three ( caution lights ) in the cabin , lavatories , and cockput . aircraft air interrupted back and landed safely at bcn without further incident . accomplished job card 72l00021001 . no odor or fumes noted .
auto throttles disconnected on take off roll . low speed abort . aircraft exited runway and contacted maintenance control . auto throttle system was deferred by the crew per mel 22-30-1a . aircraft returned to service .
during the cruise phase of aircraft n689ta on flight av665 on june 13 , 2024 , route from jfk to sap , the pilot reports th at 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.a ctionsin 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
aircraft was grounded : an emergency was declared and the aircraft returned to clt , flight crew shut down engine # 2 due t o loss of engine oil and pressure . the aircraft landed safely at clt and taxied to the gate under its own power . * * supp lemental report will be submitted * * ( open )
aircraft was grounded : during climb out mach electric stab trim failed . autopilot trim ok . emergency declared ; flight re turned to mia landing safely . removed and replaced main trim flaps relay r1192 per swpm 20-81-16 . accomplished satisfact ory stabilizer trim motor test at flap units 1 and 5 per amm 27-41-71-700-801 .
ship 5801 -div- to dfw due to row 34 abc oxygen masks dropped during takeoff from lax . corrective action : applied mel and blocked seat row . ( 8986264 )