boeing/aviation-ner-BIO huggingface dataset:
aircraft was grounded : an emergency was declared and the aircraft returned to pty , left engine vibration climbing past f l 260 . vibration was 9.8 on the left engine . flight crew followed ecam directions and shut down the left engine . the air craft landed safely at pty without further incident . maintenance found the n1 fan seized and the gas path report recorde d a 980-994 degree area c exceedance for 60 seconds . the engine requires replacement . * * supplemental report will be subm itted * * ( open )
aircraft was not grounded : mid cabin lavatory smoke detector ecam and aural alert during cliimb . maintenance accomplished a satisfactory operational test of the lavatory smoke detection system with no defects noted .
at fl340 cabin alt eicas message and discrete light illuminated and stayed on until descent to 13,000 . crew declared an emergency and oxygen masks were used . aircraft returned to departure airport without further incident . maintenance grounded aircraft . maintenance found left bleed output very low . removed and replaced the left , prv iaw amm 36-11-10 prv con t . iaw amm 36-11-19 and the left prsov iaw amm 36-10-09 all 3 components ops normal aircraft remains etops 180 . aircraft returned to service
aircraft was grounded : an emergency was declared and the aircraft returned to pei . flight reported a birdstrike to the # 1 engine that resulted in an inflight shutdown and indication of an engine fire . the flight crew discharged one fire bot tle and the engine fire was extinguished . the aircraft landed a pei safely without further incident and the aircraft tax ied to the gate under its own power . due to the extent of the damage the engine will be replaced . * * supplemental report will be submitted * * ( open )
aircraft was grounded : an emergency was declared and the aircraft diverted to lax due to the flight crew reporting a lou d bang on rotation at sna with a right yaw . the aircraft landed safely at lax and taxied to the gate under its own power . maintenance reviewed the post flight report which indicated the # 2 engine had stalled . * * supplemental report for aala2 02401234063 : maintenance replaced the # 2 engine and accomplished a satisfactory leak / operational check per task card 2 6l40071020 . * * ( closed )
air turnback due to bird strike nr 1 engine . aircraft made an uneventful landing . performed borescope of eng , no damage noted . removed and replaced all fan blades as per boeing mm . no vibration noted on eng run , ok to continue .
brake failure on both pilot and co-pilots side . both brake calipers had been replaced 2 days prior . the corrective action for this incident was removing trapped air by back bleeding brake system . there was no part or component failure
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 ecam . the aircraft landed safely at pdx and taxied to the gate . ( open )
aircraft was grounded : crew declared an emergency into iah on account of hydraulic issue . eng 1 hyd low pressure light illuminated . maintenance found broken connection line on the lt mlg shimmy damper . removed and replaced lt mlg shimmy damper and also performed torsion link assembly inspection . found all dimensions in limits , iaw amm 32-11-81-000-801 , amm 32-11-81-400-801 , amm 32-11-81-200-801 .
de-ice press light illuminated de-ice boots ceased operation removed and replaced de-ice press caution lt . pressure switch . ran engines ops checked good
aircraft was grounded : an emergency was declared inbound into xna the flight crew reported that during climb out of dfw a cabin pressure system 1 ecam fault message displayed . then at the top of descent at fl270 cabin pressure system 1 an d 2 failed in auto mode . the flight crew manually controlled the outflow valve and landed at xna without further inciden t . maintenance found insulation / debris interfering with the outflow valve and removed the obstruction . an inspection o f zone 170 behind the aft cargo was accomplished with no defects found . a satisfactory operational check of the cabin pr
during offloading , dg containers has been pulled out with fire extinguisher hoses connected , resulting to broke fire extinguisher rigid line . both main deck dg fire extinguishers - removed / inop . ea f-2622-t0374370 . application ea # f-2622-t0374370 part 1 . performed . a / c ok for service ea f-2622-t0374370 rev no . pos . p2 . complied with ea f-2622-t0374370 rev no . pos . p2 , a / c ok for service , mel cleared . main deck fire extinguisher aft and fwd installed per mm : 26-26-99-4-0 . a / c ready for service .
hyd b sys lo pr removed and replaced the blue system pressure switch . performed operational check and leak check of blue hyd system pressure switch.ops check good .
during cruise at fl 340 , an altitude disagree eicas illuminated intermittently . captain '' s altimeter reading 34,000 ft , first officer '' s altimeter reading 34,220 ft . atc msp notified unable to rsvm . performed low level and high level leak c hecks on pitot and static . replaced left adc .
aircraft was grounded : an emeregency was declared and the aircraft returned to dfw . after takeoff thrust 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 will b e submitted * * ( open )
aircraft was grounded : rh hyd low msg . fluid at 38 % dropping.01 every 10 min . turned pumps off to retain fluid . pumps on for app landing . pumps off for taxi . pilots decided to divert to lhr and landed without incident . maintenance found r eng lower t / r actuator flexhose found leaking at torque box bracket face . lower t / r actuator r and amp ; r iaw amm 78-34-12-4 00-801-h01 .
at 12,000 ft , climbing , we hear a whistle coming from emerg . exit . when we climbed to 14,000 ft our cabin alt was 11,000 and delta p was at recline . we stopped climbing and started down to 10,000 . after flying at 10,000 for a short time the medics hears a woosh of air from the main door and the pressure pegged at -7000 and ours popped hard . we declared an emergency and descended to 6000 and was unable to maintain pressure ( -200 -700 ) . found emergency exit door seat de-tatched . secured door seal with 1300l iaw king air 90 series mm 52-20-03 . found door seal inflation connection leaked . secured connection as required iaw king air 90 series mm 52-10-13 . performed aircraft run up . noted no audible air leaks from cabin and aircraft pressurization ops check .
at 1000 feet found evidence of sparks coming out of # 1 engine exhaust .
during adverse weather lost multiple nav guidance instruments , auto throtle and auto pilot , declared emergency diverted to kiah . upon landing everthing retorned to normal .
pda 2 rt retract landing lightbretention and bulb departed acft see log item 6039852 rpl ring and bulb see log page 6039852 . lens on rt landing lightmissing rh landing light . right landing light assy clamp is missing as well as bulb requesting cdl 33g , high speed tape is applied over opening created by missing landing light lamp . cdl 33g landing light wires damaged , unable to use cdl re-terminated wire for right landing light and installed new bulb , seal and retainer . ops check of right landing light good at this time ref am 33-42-11 .
aircraft was grounded : rejected takeoff due to main crew door lite came on at approximately 84 knots . maintenance adjust ed horizontal control rod on left hand entry door .
rud trvl limiter cautniflight . ran ecam . didnot resolve . rudder a cted normal on lnding flt crew reported '' rud trv lim sys '' fault . cycled fac1 and amp ; 2 twice , no help . locked for positive fix . pilot declared and emergency coming . into sfo . can not just test and sign off , suggest replacing 4cc again acpd idt inspection for interface of limiter and structure . removed and replaced rudder limiter unit ref amm verified proper pn and effectivity of part per ipc and task 27-23-51-000-001 and amp ; 27-23-51-400-001 . 27-23-51-400-001-a . add emp:340838 rotable parts change was indicated - tt # 1130714 sn off 0731 unit , artificia off 31-2720-9-9001 0731 on 31-2720-9-9001 1616 performed ops check of the rudder-travel limiting function ref amm 22-61-00-710-001-a ops check ok . inspected installation of rudder limiter and safety / security and 3 each rig pins were removed .
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 . * * original report was aala20 2305196816 * * maintenance replaced the # 2 engine lpc master bleed actuator , all three 7th stage bleed valves ( aala2023072 88194 , aala202307284855 , aala202307283970 ) and all 3 7th stage bleed valve solenoids ( aala202307287487 , aala202307283610 )
aircraft was grounded : flight jfk-mad diverted to bos on account of l1 window cracked . crew declared pan pan status with atc . aircraft was not overweight . flight landed without issue and taxied to the gate under its own power . * * supplementa l report for sdr aala202402291717 * * ( closed ) maintenance replaced capts fwd window iaw j / c 72l21056001 and amm 30-41-01 .
ship 8139 - fume / misc - crew declared emergency and donned oxygen masks due to dirty sock smell . corrective action : r / r # 01 engine . ( lp # 5506498 , 0298942 )
per flight crew during gear extension on approach left hydraulic system went to zero . declared emergency . upon arrival a t gate found lt hyd sys eng driven pump case drain filter assy broken off of housing . started removal of lt edp ( p / n # 75 88587-103 ) , ref removed mounting bolts per amm ref 29-11-17-004-001 , bushing removed hyd module per amm 29-11-17-004-001 . needs bushing 29-11-17-004-001 , up to step f ( 3 ) with one hyd line remaining to still attached . ipc 29-11-17-02 item # 5 7 . p / n bacb28ak04-140 . nis ewr be disconnected . parts used : 75-2917-9-9001 , qty : 1 installed , module ready for installa
aircraft was grounded : an emergency was declared and the aircraft returned to den due to on take off after rotation the # 1 engine and the # 2 engine had overtemp ecam warnings . the flight crew reported that after thrust reduction the # 2 engi ne overtemp cleared but the engine # 1 overtemp ecam warning remained with the rest of the engine 1 instruments in the gr een , the aircraft landed safely at den without further incident . during a review of the dfdr dat it was noted that # 1 en gine was in area c exceedance with a max temp of 977 c for 46 seconds and # 2 engine was in area a exceedance with a max temp of 999 c for 45 seconds and dfdr was in area a exceedance with a max temp of 1100 c for 45 seconds and ah was in area c exceedance with a max temp of 999 c for 45 seconds
ship 1815 -atb- to jfk due to bumping noises reported from aft cargo area . corrective action : empty and unsecured cargo container found in aft cargo upon arrival . c / w overweight landing inspection . a / c rts . ( lp 4914030 )
autothrottle repeatidly disengages in decent . placed on mel mel cleared by replacedment of thrust control quadrant , op test good per e175 amm 22-11-00-710-801-a . returned to service .
aircraft was grounded : an emergency was declared and the aircraft returned to las due the the flight crew reporting that on departure recieving an ecam message for engine # 2 egt over limit . flight crew followed the ecam procedures and shut down the # 2 engine . the aircraft landed safely at las and taxied to the gate under its own power . a review of the dfdr d ata showed maximum egt was 975 c at take off for a total time over the limit of 42 seconds . maintenance found the # 2 en gine hptacc 9th stage outlet seal damaged and replaced it per amm 75-21-10 . a satisfactory operational check was accompl
aircraft was not grounded : an emergency was declared and the aircraft returned mco : flight crew reported fuel used and f uel on board disagree . the aircraft landed safely at mco without further incident and taxied to the gate under its own p ower . maintenance accomplished tsm 28-11-00-810-805 for fuel used and fuel on board disagree and no issues were noted . n ote : no discrepant part was identified .
both fmc '' s went off-line after landing fmc prompt came back up during taxi in . grounded - yes . l and r fmc logged " pgm f ault " . performed fim 34-61 task 807 , cycled 2 cb '' s . ops nml per same . no history last 30 days . etops ground verification test nml , ref fim 34-61 task 801 .
return to field due to multipule bird strikes fo windshield emergency declared landed safely . -c / a-peformed bibrdstrike inspection iaw task card 05-50-02-200-801 no damage noted ac ok for service
aircraft was grounded : an emergency was declared and the aircraft returned to dfw . after take off during climbout the f irst officer reported acrid smell . we were unable to identify source smell of the smell . the aircraft landed safely at d fw flight crew reported that upon gate arrival smell was still detectable . maintenance read thru form 8533-a for sof eve nt , accomplished black light inspection on apu with no oil in door or intake of apu , performed high power runs of both engines to simulate event no odor noted at this time . maintenance was unable determine a specific part that would have ca
rt stowbins emergency lights inop between row 1 and row 2 . r and r battery iaw amm .
eicas blanked out with burning smell swapped eicas and fo mfd iaw amm 34-22-01 per mel 34-1 . ops check good . inspected electrical connectors with no defects noted . see this lp seq 2 for mel . swapped eicas and fo mfd due to eicas blanking out with burning smell . main panel displays
during cruise flight at 13000 , we had prop oil pressure low on # 1 engine . proceeded according to qrh pg e3-6
ship 9505 -hyd / de- the flight crew declared an emergency with atc due to the right hydraulic quantity reading low . the c rew was able to pressurize the r hyd system between 5,000-10,000 psi per the qrh . during this time when the r hyd light went out and press was normal , the crew lowered the landing gear normally . then the r hyd light illuminated again , press ure remained at 3000 psi . the landing was uneventful . corrective action : maintenance found an aft hydraulic line on inbo ard filter housing leaking and replaced an o-ring . leak and operational checks were good . ( lp # 4642322 )
aircraft was grounded : cabin left hand aisle , ceiling , emergency lights from seat 26 to seat 31 were inoperable . mainten ance replaced power supply per amm 33-51-06 and performed satisfactory operational check .
aircraft was grounded : speed trim fail light illuminated during climb out . both autopilot channels inoperative . emergency declared ; flight diverted to dfw landing safely . speed trim fail corrected by replacing left hand aoa vane ( aala202211180728 ) per amm 34-21-05-400-801 . autopilot corrected by replacing first officers control column switching module m1201 ( aala202211191280 ) per amm 27-41-51 . accomplished satisfactory tests .
vibration felt on climb and gradually got worse as altitude increased . vibration same with or without autopilot on . decision made to divert . vibration increased when making turns and really increased on approach configuration . vibration went away below 200knts on final approach . found right elevator middle trim tab with pushrod separated from rod end . found bolt missing and fitting damaged to attach point inboard of middle trim tab . replaced rt elevator and all 3 trim tabs . required inspection completed for all associated installations .
in accordance with amm 29-24-00-863-001-a was pressurized yellow hydraulic system with electric pump and its working in normal condition "
aircraft experienced 2 bird strikes . flaps stuck in the nr 1 position . returned to field 5 kt above vfe , amber alert . overweight landing , no further incident . *s / d* bird strike caused flaps remain in nr 1 position . overspeed of 5 kts is addressed in mm 05-51-13 and temp revision 5-002 . flaps were checked per the mm with no visible damage found . no further action is required .
possible bird strike left eng n1 vib 4.5 to 5.0 eng1 sn . 724634 ( tsi= 17363 ) **t / 0012-23jul22 zrh-ord rtfl** due to birdstrike eng1 with 4ea fan blades damage ( also ref l / p 9135078 and 9135120 for other damage ) . ref fim 71-05 faut tree 802 . for birdstrike / fod inspection . whqlm-emc arshad . 23jul22 . this is a supplemental report for the same control number submitted on 7 / 25 / 22 . bird strike left eng n1 vib 4.5 to 5.0 . performed bsi . removed and replaced # 1 eng . ops cks good .
aircraft was grounded : an emergency was declared and the aircraft returned to mem . at cruise flight crew reported a engi ne # 2 compressor vane ecam message . while the flight crew was accomplishing the ecam / qrh procedures the # 2 engine stal led and went to idle power and egt climbed to max temperature . flight crew followed the ecam / qrh procedures and shut d down the engine . the aircraft landed safley at mem without further incident . * * supplemental report for aala202308184456 : maintenance replaced the # 2 engine per task card 26l40071004 * * * ( closed )
ship 9580 -atb / de- functional check flight . the crew returned to the departure field after the landing gear failed to re tract properly . gear retraction shortly after takeoff produced a red " right gear unsafe " indication . qrh 14.18 was compl ied with . lowering the gear , crew received three green safe indications . raising the gear again , crew received both left and right red gear unsafe indication . crew declared an emergency with atc and returned to qro . gear handle placed back in the down position , three green gear received . normal landing and taxi to the hanger . ( lp # 5049610 )
on t / o at approximately 120 knots , heard a loud bang on left of a / c followed by slight yaw . airspeed pause and bad smell . found evidence of bird ingestion of nr 1 eng . c / w bird strike inspection per awm 382 . a / c determined to be ok for service .
the angles at bl 27 lh and rh and intercostal at rbl 36 at fs 484 were found cracked.remvoed discrepant parts , fabricated and installed and replacement parts i / a / w wvac eo 601r-53-3380 dated 07 / 22 / 02 .
upon climbing through fl 230 , pressurization climb rate was indicating in red . noticed rate was fluctuating between 400 and 800 fpm in climb . after level off at fl380 , cabin continued to climb . crew initiated decent to 13000 ft . cabin continued to climb during descent until reaching lower altitude where cabin descent rate normalized . after 13000 ft , cabin pressurization behaved normally remainder of flight back to our departure airport . interrogated for current or stored fault id . no faults found . accomplished amm task 21- 31-00-860-803-a aircraft pressurization . pressurized aircraft to duplicate crew squawk . unable to duplicate crew squawk . pressurized aircraft iaw amm 21-31-00-860-803-a multiple times could not dupucate crew write up . cleaned outflow valve and gvi iaw amm 21-31-02-000-801-a . no defects noted . inspected fuselage drain valves iaw amm 53-05-00-200-801-a . no defects noted .
flt # 2283 , bos-rdu . ( aircraft performed an air turn back to bos ) ' stby airspeed unreliable ; removed and replaced stby airspeed indicator iaw amm 34-21-26 . '
aircraft was grounded : an emergency was declared and the aircraft diverted to pit . with pack 2 inoperative and on mel , # 1 pack temperature displayed amber xx and crew was unable to monitor pack . the aircraft landed safely at pit without fur ther incident . maintenance replaced the # 1 pack controller per amm 21-61-34 .
during approach , # 1 master caution light came on ( other one stayed off ) and vemd lane 2 display failed with red : beware soft error code 1049 message . no event preceded this . elected to land and shut down aircraft and was unable to get vemd lane 2 to come on after that . tried a process of turning off both vemd displays then turning then both back on one at a time . during run-up , had an issue with gen1 amps fluctuating between 5-45 . removed and replaced vemd ; moc ok iaw ec 145 wp 31-60-00 , 4-2 .
aft galley left hand nr 3 oven smoking when in use . circuit breaker pulled . oven placed on non-essential furnishing de ferred maintenance item , in accordance with nef manual 25-20-01 .
fwd cargo pit door cutout threshold web is corroded in numerous places . grounded - yes . removed damaged web drilled and installed new web p / n 654a0003-58 tag a77600 iaw srm 51 40 02 0g 0 step 5.b w 10 " o .045 r .035 l 4ft . d .010 .
aircraft was grounded : an emergency was declared and the aircraft returned returned to clt . while climbing thru 5000 fee t , the flight crew heard a bang followed by the sound of air rushing above . the flight crew thought thye had hit somethi ng and subsequently believed there was a hole in the fuselage . the aircraft landed safely at clt without further inciden t and taxied to the gate under its own power . upon arrival the fligth crew saw that some speed tape over the flight deck had peeled away . maintenance re-applied speed tape above the left and right flight deck windows per afmm 20-11-33 .
etops- a / c pack nr 2 regulator fault during climb through 14,000 ft . cabin crew stated temp too warm . removed and replaced the a / c pack flow control valve iaw amm 21-51-51-400-001-a and 21-51-51-000-001-a . ops and leak checked good . ok to continue .
aircraft was not grounded : an emergency was declared and the aircraft returned to rdu . flight crew reported a door aft c argo ecam message after takeoff passing through 2000 ft . message extinguished after landing with ac un-pressurized . the aircraft landed safely at rdu without further incident . maintenance adjusted the aft cargo door and accomplished a sat isfactory operational check . * * ( closed )
adf became very hot to the touch during flight , it was turned off . a few minutes later flames appeared between the hf radio and adf .
aircraft was grounded : an emergency was declared and the aircraft returned to phl due to the flight crew reporting the l oss of the green hydrauilic system quantity shortly after departure . the aircraft landed safely at phl without further i ncident . ( open )
on climb at 7,000 ft crew reported flight control malfunction . in both autopilot and manual mode flight controls unrespo nsive . crew diverted to kriv with an emergency declaration . landing was uneventful and no additional precautionary acti ons . on arrival the aircraft was grounded for unscheduled maintenance . work in progress
rto due to multiple bird strikes , return to blocks for inspection . performed bird strike inspection per mm 05-51-41 . no damage or strike in engines . some strikes on leading edge . no damage a / c . okay for service .
rejected takeoff at 120 knots for windshear warning . as per information from crew - rejected take off gross weight 153.3 k lbs at 120kias performed phase 1a inspection per amm 05-51-01 no damage found a / c ok to cont .
l aft fuel pump eicas with l aft fuel boost pump cb popped . recent history shows gfi k10703 was replaced but that could be i debriefed crew and stated that cb popped . boost pump out of stock m and e 76-2821-9-9001 . lt aft pump ops on gfi k1070 5 circuit . due flt diversion at cruise . location p6-3 grid g15 . , replaced left aft tank fuel boost pump ref . amm 28-22-03-004-051 and 28-22-03-404-074 . sold inspection buy-off to inspector . operational check good . no leaks noted .
fume event : fa 's reported dirty sock fumes at rear of a / c from back galley thru row 35 . in cruise when smell started . descent to 10,000 and fume procedure actioned . packs off ram air on . fumes dissipated partially but still present.-perf # 1 and # 2 eng run with packs iaw amm 71-00-00 . no odors within cabin . applied tsm 05-50-810831.ac okay for continued service .