boeing/aviation-ner-BIO huggingface dataset:
rejected takeoff via tower request . autobrakes actuated , right brake temp reached 375 degrees temp . crew reports low sp eed rej , approximately 75knots with no brake locking . temps cooled .
ship 3569 -de / fume- crew declared emergency due to fuel odor between l3 and l4 doors . corrective action : performed apu a nd engine runs per tsm with no odors found . ( lp 0032908 )
aircraft was grounded : an emergency was declared into phx due to the flight crew reporting an engine 1 green hydraulic s ystem resevoir low level and green hydraulic system engine 1 pump low pressure ecam messages . the flight crew accomplish ed a gravity gear extension and landed safely at phx . upon landing the nose gear steering system did not function and th e aircraft was towed off the runway and to the gate . maintenance found the green hydraulic system pressure switch leakin g and replaced it per amm 29-32-12 . a satisfactory leak / operational check was accomplished with no defects noted .
at fl360 crew reported left engine n1 fan high vibe with engine anti-ice on . in light rime icing noted . after descendin g to fl240 vibe still present . after 15 minutes engine returned to normal . highest tracked n1 4.7 . crew elected divers ion to rpll with an emergency declaration . landing was without incident and no additional precautionary actions . on arri val , aircraft was grounded for unscheduled maintenance . supplemental information for previous submittal ixxa20230916063 on 15 september 2023 at kiln . iaw b757 fim 71-05-fault tree 808 engine may be returned to service . left engine n1 vibe
pilot was in cruise flight and experienced a partial power loss and then oil pressure loss of the right engine . pilot shut down engine and landed without further incident . upon inspection of engine it was found that the shaft was broken and bother turbine and compressor blades were damaged . turbo was a recent install after overhaul by atc and had 87.9 hours tso . mechanics verified that the turbo was pre-oiled prior to return to service and no issues were reported post-install .
aircraft was grounded : an emergency was declared and the aircraft returned to sfo . yellow hydraulic reservoir low level / indicates empty ecam message . flight crew accomplished ecam procedures and landed safely at sfo without further incide nt . maintenance replaced # 2 engine hydraulic pressure / suction line per amm 29-13-49 . a satisfactory leak / operationa l check was accomplished .
rt pack illuminated passing 17000 ft , ran checklist would not reset . grounded - yes . fim 21-62 task 831 p2tc-2 show s this pack tvc on verify . circuit breakers reset , no help . verifies power and ground at rt tcv d3872 pins 11-3 . removed and replaced temp control valve iaw amm 21-51-10 . bite was good iaw amm 21-61-00-700-806-002 . leak checked good .
aircraft was not grounded : an emergency was declared on aproach to aus due to a slats fault / slat jammed . flight crew recycled the flap lever but it did not clear fault . aircraft landed configuration 3 safely at aus without further inciden t . maintenance reset the wing tip brake of the flap system per amm 27-50-00 and accomplished a satisfactory operational check .
aircraft was grounded : the aircraft diverted to phx , at fl 320 the # 2 engine began stalling , flight crew reduced power p er qrh procedures and engine was able to accept some power at reduced setting . the aircraft landed at phx without incide nt . maintenance found metal in the bleed valves and damage starting at the 7th stage compressor blades during the bore scope inpection . the engine was replaced per task card 26l40071004 .
aircraft was grounded : an emergency was declared into dfw . during climb 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 will be submitted * * ( open )
inspection type:1clh horizontal stab elevator # 3 actuator hinge support fitting is chafe at sta xe=122.repaired chafed hinge support fitting iaw vt-saa ea 011-5510-01-a9501 rev i / r and ups eo md11-5550-83032-a ( minor ) .
the crew reported that they received a right-engine fire warning message in flight . the crew declared an emergency . the aircraft landed at its intended destination without further incident . maintenance reported no evidence of fire from the engine at this time . the aircraft is still out of service for further troubleshooting at this time . a final corrective action will be submitted as a supplement to this report .
aircraft was grounded : aircraft returned to clt due to a landing gear shock absorber fault after take off and crew repor ted having difficulty raising the landing gear handle to the up position . the aircraft landed safely at clt without furt her incident . no emergency was declared . ( open )
seat track corroded between bs 727+10 to bs 727a , rbl 25 . repaired seat track per srm .
aircraft was grounded : an emergency was declared into scheduled destination of dfw due to a complete loss of the green h ydraulic system . flight crew manually extended the landing gear and the aircraft landed safely at dfw and was towed to the gate . * * supplemental report for aala202306060705 : maintenance noted hydraulic fluid leaking from the # 1 engine cowli ng and found the green hydraulic pipe in the pylon chaffed / leaking . replaced hydraulic pipe per amm 29-11-49 . a satisf actory leak / operational check was accomplished . * * ( closed )
several dents were found between 5:00 to 8:00 hrs of rh inlet cowl acoustic panel ( p > dents were repaired in accordance with b767 srm 54-15-01-2r-3 repair 3 and eo 1971a291 / p > )
fa 's reported a pungent odor on recent through approach . odor went away when we landed fa 's say it was level 1 severity level . fwd cabin , a flight attendant mid cabin and aft . no smell in cockpit . grounded - yes . removed and replaced air re-circulation hepa filter ref . amm 21-25-01 and the water coalescer bag ref . amm 21-51-05 . ops check and leak good . no unusual odor present .
aircraft was grounded : an emergency was declared on final approach into mco due to a brakes normal system ecam fault mes sage . flight crew aborted the approach and went around to accomplish the ecam procedures . the aircraft landed safely at mco and the brakes worked fine so the aircraft taxied to the gate under its own power . maintenance replaced normal braki ng system pressure transducer 14gg per amm 32-42-21-000-001-a and accomplished a satisfactory operational check .
ship 5645 crew received call from fll tower after t / o that carcas of 757 nose tire was found . flt crew declared emergenc y . corrective action : no vibrations noted when wheels were retracted . no unusual vibes when wheels extended . landing was smooth , no dragging . no issues with taxi . nose tires were inspected per b757 amm 32-45 , no trouble found . nose tire pre ssures checked good . ( 5591372 )
ship 5807 - atb / fume - due to reports of air noise , vibration and smell in aft cabin . corrective action : t / s found rt recirc air check valve oriented sideways , reinstalled . removed and replaced left and right recirc air filters . found apu duct support brackets broken in aft cargo bin , replaced brackets .
doors light on at 85 kts rejected takeoff . 1l handle was 1-3 in ches ajar . cleaned and inspected door latches and perfo rmed ops ck of door , verified door latches normal per amm 52-11-00 , ops checks good . crew reported normal braking no i nsp required per amm 05-51-07-210-801 . ac ok to continue
nose wheel extreme vibration high speed takeoff roll and climb out-c / a-rar nose wheel tire assy iaw envoy w / c 32-49-01-000-801 .
rt sys press eicas on departure . unable to restore system pressure via qrh . declared emergency and rtb to can . emerge ncy declared . consulted with flight crew just r hyd sys light illuminated and r sys press eicas , elec pump low press light and edp low press light not illuminated , r and r rt hyd sys pressure switch s32 iaw amm 29-11-17-4 , eng run check all parameters normal iaw jrh . precautionary r and r rt press sense eng hyd pump relay k127 iaw swpm 20-81-22 , wdm 29- 31-11 , and ipc 29-31-01-01a-060 , precautionary r and r rt hyd pressure transmitter m343 iaw amm 29-31-01-4 . performed hyd sy s ops test iaw amm 29-11-00-5 , all 3 hyd sys pressure were stable at 2800-3200 psi , no leaks found .
pitting corrosion on slat tracks 1-3 ( several location at upper surface ) , slat # 1 , lh wing .
ship 3008 -ifsd / div- diversion to mco due to left engine egt indicating max of 1203 deg . crew shut down engine per qrh a nd diverted to mco . corrective action : parameters at shutdown showed an egt indication issue . performed bsi with no find ings . replaced ecu , all wiring harnesses in the egt indication system and egt probes . performed engine run , all indicati ons normal . ( lp # 4161604 )
flt # 771 . bos-cun . ( aircraft performed an air turn back to bos ) . '' after first engine start , inflight crew alerted us that the cabin cms screen went blank . we utilized the cabin com reset guide , waited 8 mins and the system reset and fault cl eared . once airborn the cms failed and we lost all comm from flt deck to cabin to pax ; oms fault code 4411f0033 , perform ed on the ground reset of cms cabin ctlr pri / sec iaw amp j24-00-00-10aaa-398d-a with no cabin interuptions . no further f aults noted . ops test ok of cabin handset functions iaw amp j44-11-09-01aaa-320a-a . ''
aft cargo bay floor to sidewall support corroded between bs 727 to bs 767 , rbl 22 . r and r support assembly iaw srm and dwg .
aircraft was grounded : an emergency was declared on arrival to the scheduled destination of dfw due to loss of flight co ntrol system backup systems . flight crew reported a flight control alternate law ecam message whiile at fl 350 approxima teley 2 hours after take off . the aircraft landed safely at dfw without further incident . maintenance toubleshot flight control alternate law message per amm 27-93-00 and a satisfactory operational check of the elevator / aileron computers ( elac ) was accomplished with no active messages on the ecam .
aircraft was grounded : an emergency was declared and the aircraft diverted to tul . after takeoff amber speed limit flag on upper left capartains pfd intermittent with associated loss of flight director in pfd and hud intermittent . red lower airspeed bar intermittently . the aircraft landed safely at tul without further incident . the crew also reported that af ter landing , the # 1 stick shaker test failed . maintenance replaced the left-hand angle of attack sensor ( aoa ) per amm 34 -21-05-400-801 and accomplished a satisfactory operational check .
ship 0685 -misc / de- crew declared emergency due to le slat disagree on approach . corrective action : t / s per fim . l / e ope rates and indicates normal .
pdis 936 27-50 1303 22feb23 msp fact u te flap disagree between 5-15 . ran qrh and landed msp . * * * emerge ncy declared * * * fact 22feb23 13 : 11 msp u fim : 21-51-00-815-808 fim : 21-51-00-815-815 upon entering flight deck no ted t / e and l / e flap slat systems in alternate . crew stated altn sys worked normally . reconfigured both to normal c onfig . pressurized hyd systems and lowered flaps / slats . inspected all flap transmissions for servicing and overtorqu e conditions . all serviced normal , no overtorque indicators popped . interrogated fseu '' s 1,2 , and 3 . fseu 1 showed a flap disagree for prior flight leg . no other information given with it . operated flap / slats three complete cycles .
rejected takeoff appx 95 kts aircraft pulled hard left . debriefed crew . crew states brakes were not dragging . wind at ti me of takeoff was 9 kts . all indications were normal and no fault messages displayed . crew stated it felt like engine fa ilure . upon mx arrival of ac cycled brakes to verify all main gears jacked and tires rotared . no brake dragging noted on either gear . no discrepences noted from vusual inspection of brake units . performed high speed taxi , confirmed aircraft pulling to the left after 40kts . performed tsm steering deviation during taxi ref tsm 32-51-00-810-823-a , found n / ws se
cabin rate alert on climb out . cycled contollers with no change . leveled off at 11,000 then descended down to 9,000 wi th cabin alt alert . air turn back to kind . found mian cargo door vent door open . flight crew said they never had a d oor open indication . opened and closed door several times . light was out initially but indication did return to normal . suspect switch is intermittent . door latch is serviceable and latches securely . cargo door upr a alert - inop . ve rify door is closed and locked prior to block-out.removed and replaced vent door warning switch ( s1-1346 ) , ref ssm 52-3
aircraft was not grounded : an emergency was declared during descent into abq due to the flight crew reporting that aroun d 20,000 ft the cabin pressure exceeded 10,000ft . the flight crew accomplished qrh / abnormal procedures and landed saf ely at abq without further incident . maintenance accomplished tsm 21-31-00-810-808a and 21-31-00-810-810a . no faults co uld be confirmed . accomplished operational test of cabin pressure controller system per amm 21-31-00 , and pressurized ai rcraft per amm 05-53-00 . no faults found . maintenance noted that the post flight report messages were warnings , not faul
aircraft was grounded : an emergency was declared and the aircraft returned to gnd due to the flight crew recieving an ec am message for forward cargo smoke at 9000 feet . the flight crew accomplished ecam procedures and returned to gnd where the aircraft landed safely without further incident . maintenance inspected the forward cargo compartment and found no ev eidence of smoke . original report was aala202407223195 * * maintenance replaced forward cargo caompartment smoke detectors 1wh and 2wh ( aala202407264475 ) per amm 26-16-25 . a satisfactoy operational check was accomplished .
ias disagree message shows on airpseed display first officer '' '' s at gate bot capt and f / os read 45 kts . capt said a t no time did airspeed go to 0kts . debrief from crew indicated no airspeed split on climbout from den . ias disagree msg 10 min after level off at fl350 . airspeed split was 10 kts compared to captains and standby airspeed . divert to housto n -- -split became larger on descent . replaced # 2 pitot adm ref . to amm 34-21-04 , tested good . parts used : 29-3413-9-0001 , qty : 1 verified # 2 pitot adm quick disconnect installed ref . to amm 34-21-04 . parts change info only . rotable parts cha
during allegiant task 534143-01-3-001 on pass cabin from fr66+40mm to fr66+150mm and y+1420 mm sill web with corrosion was found . coopesa performed repair on lh aft pass crewdoor sill beam in accordance a320 srm task 53-41-14-300-001 parag 2a fig 001 sheets7 repair principle # 11 . this repair is cover with coopesa job a1n117 item 2-40
rejected takeoff at 65knots for avionics vent fault on ecam removed and replaced skin air outlet valve iaw amm 21-26-53 . performed avec test on cfds mcdu . ops ck good , no faults noted at this time .
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 2 , 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 . ( open )
ship 3030 - atb - due to a failure of the nlg to retract with ecam message , shock absorber fault . corrective action : found nlg shock strut centering cam not indexed correctly . re-indexed and returned to service . ( lp # 4838836 )
lt horiz stab lower skin cracked a sta 184.70 approx 8 " from l / e front spar . repair performed on n / r 9633760 .
fuel leak # 1 eng [ 01 ] accomplished test 12 actuators test per m / m 71-00-00 . no leaks noted . accomplished test 3a idle power leak check per m / m 71-00-00 . no leaks noted . bagged all # 1 engine fuel drain tubes and accomplished test 3b part power leak check per m / m 71-00-00 . no leaks noted . reference log page 1728315 for troubleshooting corrective action . [ 01 ] replaced hptacc valve per m / m 75-21-01 . ops checks ok ; [ 02 ] replaced # 1 engine hptacc valve per m / m 75-21-01 . ops checks ok .
aircraft was grounded : an emergency was declared and the aircraft diverted to gso due the flight crew reporting that at fl320 , engine 1 stalled several times . ecam indication engine 1 stall flashed twice and went away . the aircraft landed s afely at gso and taxied to the gate under its own power . * * supplemental report will be submitted * * ( open )
aircraft was not grounded . 9c exit fixture fell off . resecured 9c exit light fixture , per amm 33-51-01 .
cont cabin light zone temp on recall , resets with master caution reset . grounded - yes . verified fault , accomp pack / zone temp cont . bite cont # 2 shows trim valve flt deck fault . cont # 1 no faults . accomp reset on # 2 . accomp bite verify test on both cont . both pass test ref . b737-900 amm 21-61-00-700-806-002 .
nr 2 engine had bird strike followed by vibs - diverted to mad performed bird strike inspection per 05-51-18 amm aircraft fuselage no defects noted rt engine shows damage on fan blades and acoustic liner ( dl75e101749 ) .
aircraft was not grounded : an emergency was declared on final approach into atl after recieving a ecam slat fault messag e . flight crew accomplished ecam procedures and the message cleared . the aircraft landed safely at atl and taxied to the gate under its own power . maintenance accomplished gvi of flap and slats . also accomplished bite test of the sfcc-1 / 2 s ytem faulting ( lever out of detent for more than 10 sec ) . cycled flap / slat several times no fault .
ship 0695 -div- to mco due to gear disagree eicas message . corrective action : replaced nose landing gear door operated gear sequence valve . jacked aircraft and swung gear . all operations and indication normal . a / c rts .
aircraft was grounded : an emergency was declared and the aircraft returned to phl . after takeoff flight crew received ri ght gear hot brakes indications . once gear temperature was below 200 c , the flight crew raised gear and noted that it wa s slow to retract . eventually they got an unsafe gear ecam message . the wheel page showed the gear up and all doors open ed . triple indicator showed 3 reds above gear handle . they followed ecam / qrh procedures , cycled the gear and received landing gear not uplocked ecam message , however the gear showed 3 green on triple indicator and wheel page showed doors gr
engine 2 high lp vib climbing through 11 , ooo ; high vibrations did not go away climbing through fl ; 200 . qrh procedure acomplished / emergency declared / overweight landing . -c / a-a full workscope was performed to troubleshoot vibrations on rh engine 902446 , fan blade retaining pins were replace .
ship 5017 - atb / fumes - crew reported oily smell in flight deck and cabin shortly after takeoff . ran qrh and returned to sfo with emergency declared . corrective action : inspected engine spinners , prv , ip and a / i valves with no findings . ins pected apu with no findings . can not duplicate odor when running engines or apu . replaced recirculation filters and perfo rmed ecs decontamination per amds 2100-2003 and 2100-2004 . ok for service . ( 4143812 )
ship 5652 -diversion / ifsd- diversion to mco with declared emergency due to right engine oil temp in the red band . flight crew performed ifsd per qrh . corrective action : inspected '' s and oil filters , all clean . drained 2.5 gallons from ma in gearbox . replaced gearbox scavenge pump and lsop . performed high power run with no issues .
total electrical system failure in flight . inspection revealed that the main power wire’s ring terminal to the alternator had failed causing arcing which shorted the alternator out and caused the main and essential buss circuit breakers to pop . possible cause is too short of a wire harness which does not allow for engine vibration . remedied with new alternator and new alternator cable assy provided by mfg . the new cable assy is a couple of inches longer to prevent this from occurring . ( k )
lt main landing gear forward trunnion fitting upper lug outboard face had corrosion . repaired lug face ea .
cabin altitude warn in flight . 02 , 04 see f.i.m below on pic . crew reports flight alt of 28000ft and cabin alt of 10500f t , no cabin pressure contrl faults . ops check on ofv has no faults . inspected pack bay area , no leakage noted . cabin pre spressure ctrl bite check has lo infl / hi leakg in fault history on flt leg 00 , ref.logpage 5820708 for action taken . due to report of excessive cabin pressure loss noted in flight with subsequent diversion to ewr : accomplish cabin pressure lea k test amm 05-51-91-790-801 and report all all findings to tomc . performed cabin pressure leak test as per amm 05-51-91-790-801 and report all all findings to tomc .
apu fault on ground , bite check of the apu ecu iaw amm 49-61-05 and self test . no fault found . ops checked good iaw am m 49-11-00 .
rejcted takeoff for pws at 105 knots verified ac weight w / flt crew was 161.7 lbs , speed at rto was cooling time of 50 mins . flt crew advised . 105 kts . under tomc guidance , verified within cooling range and no mx insp req '' d ref amm 05-51-07-210-801 . 50 min cooling time and no other special procedures req '' d . ok to continue after also ref flt manual 7.170.6 .
cabin floor panel 221ff has damage to lower surface . repaired damage to lower surface on cabin floor panel 221ff iaw sr m 53-00-50-2r-1 . damage was beyond allowable limits iaw srm 53-00-50-1a-1 para 4b . ( 1 ) damage was greater than one ply i n depth . 80733u 18feb2020
aircraft was grounded : an emergency was declared and the aircraft diverted to phx due to the flight crew reporting a yel low hydraulic system reservoir low level message . flight crew accomplished ecam actions successfully and landed at phx w where the aircraft was towed to the gate . maintenance found the yellow hydraulic line cracked and replaced it . a satisfac tory leak / operational check was accomplished .
eicas message rt engine speed card displayed . c / w fim 73-21 ft 815 . removed and replaced n2 speed card iaw amm 73-21-54s g cleared performed ground engine run no messages and ops check good .
aircraft ws grounded : an emergency was declared and the aircraft returned to dfw due to e-12 circuit breaker which power s the ecam pages popped preventing the flight crew from being able to monitor the ecam system . the aircrft landed safely at dfw without further incident . maintenance inspected the e-12 cicuit breaker and ecam control panle connectors per wd m 31-54-87 with no defects noted . maintenance replaced ecam control panel per amm 31-61-12 and accomplished a satisfacto ry operational check .
wxr fail on l / r nd performed bite check of weather radar no patern show amm : 34-43 fault tree 805 panel , control , off 64-3443-9-0001 0972 on 64-3443-9-0001 7979 panel , control , off 64-3443-9-0001 0972 on 0000 replaced weather radar control panel , ops ck normal . ref amm 34-43-02 parts used : 64-3443-9-0001 , qty :1 rotable parts change was indicated - tt # 1585731 sn off 0972 .
right wing - wing side outboard flap inboard hinge lower mount inboard hole bore found corrosion corrosion at right wi ng - wing side outboard flap inboard hinge lower mount inboard hole bore ( # 7 hole ) reworked and found exceed limit as per md-11 cmm 57-44-08 . shoulder bushing fabricated by machining and installed as per md-11 cmm 57-44-08 and e.a . # : 1-5750-t0348277 p1 step 3c and step 3 . title : wings- flight surfaces- eo 1-5750-7- 5002- rh wing- outbd flap inbd fw d hinge ( wing side ) - corrosion repair . repair classified as minor per gmm 6-2-100 . refer to e.a . # : 1-5750- t03482 77 p1 and snrm n00323 for work details .