boeing/aviation-ner-BIO huggingface dataset:
loss of cabin altitude , diverting to kmsy , masks were deployed . no injuries to pax or crew . flight landed safely , taxie d to gate without further issue . mx arriving on scene to troubleshoot .
aircraft was grounded : on descent flight attendant reported a burning waxy / oily odor in the aft cabin , no smoke was noticed and it lasted a while and went away . maintenance found oil residue on the apu inlet area and cleaned the inlet . a satisfactory leak / opeational check was accomplished .
aircraft was grounded : an emergency was declared 7 minutes prior to landing at clt due to the flight crew reporting a la nding gear door not closed ecam with left main landing gear door amber . the aircraft landed safely at clt and taxied to the gate under its own power . maintenance found forward target loose on left hand main landing gear door uplock and secu red it per amm 32-31-33 . a satisfactory operational check was accomplished .
while performing t / c 7273000 , found fault 73-11271 . " the alternator voltage to the eec is out of range " . short time faul t # 1 engine . grounded - yes . performed # 1 eec bite test . no recent faults or fault history . accomplished eec alternator resistance checks . wiring checks good . repair confirmation and ground verification required . ref fim 73-27 task 804 . per formed eec bite check engine run . ops check is good . no faults noted at this time . ref amm 71-00-00 .
aircraft was not grounded : an emergency was declared comming into the scheduled destination of pit due to a green hydrau lic system low level ecam message during decscent , flight crew reported that the reservoir appeared to have fluid . the a ircraft landed safely at pit without further incident . maintenance found the # engine hydraulic pump pressure switch 107 4gk leaking and replaced it per amm 29-11-17 . a satisfactory leak / operational check was accomplished .
aircraft was grounded : an emergency was declared and the aircraft diverted to abq due to the flight crew reporting at 33 , 000 ft a distinct smell of wood burning from row 21-27 . the aircraft landed safely at abq without further incident . sup plemental report will be submitted * * ( open )
during aircraft inspection prompted by similar defect on another fleet aircraft . crack found on lh ( longitudnal ) mr servo input flight control rod . ref ec135p2+ ipc ipc 22-18-10-01 , item 10
aircraft was grounded : an emergency was declared and the aircraft diverted to phx , whilie climbing out flight crew felt and heard wooshing and pressure in ears . then received cabin pressure system 2 fault . flight crew leveled off at fl 310 + / - 1000 vvi on cabin . cabin pressure alt got to 8000 '' . crew followed qrh advisory procedures by switching to man then t o auto . no help went back to man and cabin vvi pressure continued to swing + / - 1000 '' 'until decending thru 14000 '' ft . the aircraft landed safely at phx without further incident . maintenance replaced the # 2 cabin pressure controller per amm 2 1-31-34 and accomplished a satisfactory operational check .
lower outside engine cage bolt mount sheared in flight during a part 91 survey and mapping flight . camera system operator noticed engine cowling had black markings around the cooling inlet . pilot looked at the cowling and determined a landing would be required . did not declare emergency and landed without incident at mckinney , tx airport ( ktki ) . did not conduct an engine shutdown on the affected engine . post landing , crew determined the engine mount appeared broken and then removed the engine cowling and found sheared bolt in the engine cowling and the " loose " engine cage . pictures and video was taken and sent to tecnam italy and tecnam usa in florida for discussion . tecnam recommended a visual inspection of the engine cage and mounting points . local maintenance conducting the repair by replacing all hardware on all 4 mounting points on both engines .
crack angle trailing edge located ws253.0 lt wing . replaced angle loc ws 253.0 lt wing iaw b737700 ipc 57500025 and srm 514002 .
during climb , a bird struck the left windshield , cracking the outer ply of the windshield . the aircraft diverted its normal flight to el salvador station . after landing at sal station , technicians performed inspection due bird strike per amm 05-51-14 . the left windshield was found damaged . it was replaced per amm 56-11-11 . it was performed inspection of both engines per amm 72-00-00-200-010 . the inspection revealed no external or internal damage on both engines . no other damages were found on the fuselage . also an impact on the nose radome was found . the radome was inspected , per ntm 51-10-06 , no damage was found . the aircraft returned to normal operation . ( m )
defect 710819 : - - while climbing out of rsw using ctr tank fuel , rh tank qty began to decrease . by level off fuel had d ecreased from 8800 to 7800 . crew ran qrh 12.6 fuel leak eng and diverted to jax . mech reported fuel under # 2 after shutd own . - - resolution : ( in progress )
burning electrical smell after eng 2 start in cockpit and galley " transferred to nrwc 029-mia-03706 " -c / a-rar ricc iaw amm 24-51-03 . ops checks good , no smell present . a / c fit for service . ref item 2 this log p . for parts and sns on / off . burning electrical smell after eng 2 start in cockpit and galley " transferred to nrwc 029-mia-03706 " -c / a-rar ricc iaw amm 24-51-03 . ops checks good , no smell present . a / c fit for service . ref item 2 this log p . for parts and sns on / off .
at fl 190 noticed quantity dropping ( indicator in reverse ) we monitored closely but all other indications normal . in descent ; oil quantity went to zero ; then oil pressure fluctuated then dropped causing amber then red box to flash we did a precautionary shut down per the qrh . no egt or oil temp exceedance . also did not notice low oil pressure light or master caution light . ( # 2 engine ) [ 01 ] r and r # 2 engine ; see ttg8q008tszx for corrective action .
aircraft was grounded : an emergency was declared upon arrival into dfw . during cruise flight engine 1 oil quantity conti nued to drop . after approximately 2 hours oil quantities at 0.5 quarts . flight crew reduced thrust and engine operated a t idle for last 45 minutes of flight . engine continued to run . the aircraft landed safely at dfw without further inciden t . * * supplemental report will be submitted * * ( open )
on departure and climb out , the pilot noticed a vibration in the t / r pedals that would increase with power was increases . he returned to the airport and landed uneventfully . maintenance found the t / r teetering bearings were worn excessively .
accomplish permanet repair on left side of vertical pressure web at lbl 43 left of the wheel well ref aar n / r 9882293 ac complished permanent repair at left side of vertical pressure web at lbl 43 left of the wheel well per ref b737 srm 57-1 0-10 repair 3 add emp : v900454
while flying at 6000 heading to destination about 20 miles east of kmwl the com / nav # 2 started sparking and then there was smoke . the pilot shut the unit off but there was still smoke present . the pilot then requested atc to divert to kmwl . sparks stopped after a minute but you could still smell the burning in the cabin . landed safely and aircraft is safe at kmwl . subsequent inspection on site found the com / nav unit scorched with no damage noted to the surrounding wiring or electrical connectors .
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 . * * supplementa l report for aala202306015493 : maintenance found the # 1 engine grreen hydraulic pump pressure line chaffed / leaking and replaced it . also found the # 1 engine thrust reverser isolation control unit leaking and replaced it . ( aala202307282907 ) a satisfactory leak / operational check was accomplished . * * ( closed )
floor emerg exit light : during preflight , found emergency aisle path lighting under seat 10 to be inoperative .
on the take off roll we received a l gen drive light on statis message . per flight crew rejected takeoff speed was 85 kt . left gen . light stayed on . return to gate found left idg oil level low with eicas message displaying the same . servic ed with 1.5 qts per idg oil servicing amm reference : task 12-13-03-600-801 . ran left # 1 engine for 5 mins all freq amps volts parameters normal on left idg . no leaks noted . acp high energy stop / heat damage condition visual chk . no damage n oted . acft speed below 100 kts . reference amm 05-51-14 / 201 .
after takeoff , had r eng ovht eicas with associated r eng ovht caution light complied with qrh returned to memphis momentary status message r eng ovht lp2 we never had egt ovht on primary flt instrument panel . emergency declared . tested loop resistance found ok checked for shorts to ground checks good . found # 30 fuel nozzle missing 2 mount bolts . removed fuel nozzle for replacement . fim 26-11 ft 804 and amm 73-11-05-4 . performed borescope of combustion dome cold side of affected fuel nozzle position . no defects noted . amm 73-11-05-4 and amm 72-00-00-206-146-h00 . r and r rt eng fuel nozzle # 30 , safetied and pressure checked manifold . performed leak check , test 2 and 3 chkd good .
ship 9565 -atb / de- the crew performed an air turnback and declared an emergency with atc due to a slat disagree . the air craft required significant aileron correction for wings level attitude . the qrh was complied with , and the result was a normal slat extension for a normal approach and landing . corrective action : maintenance replaced the slat control valve and returned the aircraft to service . ( lp # 5603766 )
aircraft was grounded : an emergency was declared and the aircraft returned to clt , on takeoff flight crew got an ecam ecg engine 2 egt over limit below 1000 ft . at power reduction egt returned to normal , flight crew did not shut the engine dow n . the aircraft landed safely at clt . maintenance replaced the engine per task card 26l40071001 .
pit - flt 4041 - during approach , the flight crew heard several audible thumps from the left side of the aircraft . the aircraft landed with no further incident . pit mx conducted a bird strike inspection iaw mm 05-57-07 . also removed and replaced the lt engine cowl iaw mm 71-01-00 which was damaged as a result of the bird strike . aircraft was then returned to service .
ship 3277 -rto- rejected takeoff at 80kts due to right engine reported as slow to spool . crew did admit to not allowing engines to stabilize at 40 % prior to setting togo thrust . corrective action : flight crew got back in line for takeoff an d allowed engines to stabilize then departed .
ca advised on approach for flt 576 fll-cmh there was a slat failure . followed com procedures and were unable to get slat to extend . crew declared an emergency . landed uneventfully . at gate now . mx will troubleshoot issue .
r fmc went blank upon engine start . accompanied by squeal over the radios , noticeable electric smoke odor and circuit breaker fmcs cdu popped . ( e11 ) returned to gate . r / r 'd fo 's cdu per amm 34-61-02-4 . checks good . all radios check good iaw amm 23-12-00-5-2 .
aircraft was grounded : an emergency was declared and the aircraft retunred to clt . on takeoff both # 1 and # 2 engines egt was over limits . flight crew reported that engine # 1 egt was 966 for 5 second and engine # 2 was in the red but didn '' t get a reading . the aircraft landed safely at clt without further incident . maintenance evaluated the dfdr data and noted that # 2 engine max egt was 958 for 17 seconds which was in area ? ? ? a ? ? ? per amm 72-00-00-200-008a and was placed on a d eteration watchlist with no further action required . ( aala202307146158 ) . maintenance evaluated the dfdr data and noted t
aircraft was grounded : an emergency was declared and the aircraft returned to ord . flight crew reported that after take off the aircraft hit a flock of birds ( ducks ) along with recieving an ecam message for the green hydraulic system reserv oir low level and loosing the green hydraulic system . flight crew also reported having vibration from at least one engin e . the aircraft landed safely at ord without further incident and was towed to the gate . maintenance inspected the # 1 en gine and confirmed that the engine had ingested the birds and that the damage was beyond limits requiring the engine to
aircraft was grounded : an emergency was declared during descent into clt due the flight crew reporting that during cruis at fl 350 engine 1 stall ecam and n1 rollback . occurred , the engine self recovered and during descent engine 1 rolled back again without ecam message and self recovered again . the aircraft landed safely at clt and taxied to the gate under its own power . * * supplemental report will be submitted * * ( open )
on take off engine 2 did not exceed 91.5 n1 w / 98.5 required . t hrottles matched performed # 2 eng eec bite , no faulted noted as per 73-21-00 . will t / s as per fim 73-06-block 809 suspect low fuel flow during takeoff from pilot rejected take off report with comparison to e1 . idt requirements c / w for # 2 engine fuel pump package replacement iaw amm 73-11-01 . test [ 8 ] , 12 , 13 , and 3a need to be accomplished , and part power run for precautionary . ref fim 73-05 task 808 . on # 2 e ng inspected and performed test # 5 failed . # 2 engine did not meet required takeoff power . performed eec bite task 73-00
rejected t / o at 98 kias or turbine section / no leaks . information update : pilots reported throttles had 1 1 / 2 knob adde d pictures information only : pilots stated all other indications and completed eec bite , with right eec switch in test a nd right esc split . right engine power lag throughout throttle advancement . parameters were normal ( egt , etc . ) . switch e ngaged eec display remained blank , self test completed aborted at 98 knots . takeoff weight 237800 . right engine epr " cc " displayed during self test mm 73-21-00-902-002-r01 made only 157 . no obvious damage to right engine fan , compressor compcon and gt ; .
aircraft was grounded : flight diverted to lhr on account of integrated flight standby display inoperative . emergency was declared due overweight landing . maintenance performed inspection and removed and replaced the isfd indicator iaw dmc-b787-a-34-24-01 00a-720a-a . all ops and ind normal .
lg shock absorber fault cfds showing r lg shock absorber ( 2502gm ) ref tsm 32-31-00-810-870-a - post flight report breifed crew upon having the lg shock absorber fault landing gea r handle would no move up no matter what the crew tried landing gear handle stayed down , shortly after they recieved multiple fa ults a / p inop auto brakes inop , normal brakes inop , ran post flight report and report left on printer in flight deck t / s ref tsm 20ga inductance readings were in limits . some minor corrosion was found on the connector and sensor . replaced 20ga and cleaned connector . inductance readings still good . acp gap checks on 20ga ref amm 32-31-73-200-001-a . gaps are in limits . removed backshell of 20ga and examined wires for corrosion . wires and conduit looked good . accomplished continuity check of 20ga to lgciu1 . also check wires with megger , wire-wire , wire-ground , wire-connector . no discrepancies noted . per tsm 32-31-00-810-870-a step 4a rh mlg need to be inspected . verified gap checks on 20ga ref amm 32-31-73-200-001-a . gaps are in limits . ops checked mlg retraction system no faults or defects noted at this time . completed 3 mlg retract and extend cycles , no faults . returned aircraft to ground . reference lp 5868100 ,
aft lavatory water line broken under the sink . pilots declared an emergency and landed without incident . removed and replaced aft lav water heater pressure relief valve ref cmm 38-12-16 . ops and leak checks are good .
aircraft was not grounded : an emergency was declared inbound into dca due to the flight crew reporting that enroute into dca during imc conditions at fl040 near vaal i intersection , the weather radar became intermittent and then unusable . the aircraft landed safely at dca without further incident . maintenance reset the weather radar circuit breaker and accom plached a satisfactory operational check of the weather radar system per amm 34-41-00 with no issues noted .
area of corrosion found on top surface of floor structure strap in aft cargo just inside of door and just forward of sta . 954 and above longeron 28r- marked . nrc 001-0369:0593-2006 / 004 00127 : replaced strap per b717 srm 51-40-02 . ( lp # 18351 43 )
( can ) battery mounting shelf pn g249-1 found cracked at contact with battery fwd and aft outboard corners . ( tc # 20190403018 )
flt 490 - mid-mex - during takeoff after the rotation movement , left engine had a bird strike , the engine momentarily stalled but it recovered all parameters itself . at mex , performed borescope inspection to such engine iaw mm 71-05-00 fig 103 . engine was found without damaged in hpc inlet and outlet . engine chips and oil main filter were ok . just a first stage fan blade was bended and two fan blades were replaced iaw mm 72-31-02 . ( m )
discrepancy : reference log page 391597 item one this is an sdr reportable event flt 2755 engine experienced an engine 1 fadec fault leading to an in-flight engine shut down due to erratic fuel flow and engine 1 fuel leak message on ecam . flight 2755 diverted to phx sky harbor airport . the post flight report referenced # 1 engine eec internal failure . corrective action : eec was replaced and the phmu as a precaution per amm 73-21-01-420-050-a and 77-31-01-020-050-a . performed airbus tsm . aircraft returned to service . / end /
auto pressure fail on takeoff . removed inspected , cleaned and reinstalled auto pressure controller iaw amm ch 20-10-07 , performed pressurization check iaw amm ch 21-31-10 ops check good no defects noted at this time .
cabin floor panel 232bf is dented and delaminated . removed and replaced floor panel per amm 53-21-00 .
aircraft was grounded : an emergency was declared comming into clt due to the flight crew reporting that during cruise a green hydraulic sytem engine pump # 1 low pressure message displayed and the system quanity was reflecting little to zero . flight crew followed ecam procedures and shut off the pump . flight crew accomplshed a manual gear extension and landed safely without further incident . maintenance found the # 1 engine hydraulic pump delivery check valve 1050gm leaking and replaced it per amm 29-11-36 . a satisfactory leak / operational check was accomplished .
inspection type : na * atb * * a / c was oos * capt / crew experiance suspect smoke in cockpit shoryly after departure declared e mergency after level 3 lower aft cargo fire warning resulted and atb " upon landing emergecny egress via slide pulled all engines and apu fire handles disengagedb.o.w ts-md11-2100-t0611 to identify and remedy smoke source apu internal fail fnd to b e smk source k207022 issue and apu assy repl tc 9112 ipc 49 10 05 01 . fire handles rest on lp 488041 item 1-3 and 488042 i tem 1 l1 door slide r and r 25-61-01 eff 25-61-05-01 b.o.w ts-md11-2100-t0611 compl and per duct cln mm 21-51-00-160-802 op ck gd
aircraft was grounded : an emergency was declared on arrival at sea due to the flight crew reported that enroute in cruis e there was a yelllow hydraulic system low pressure and low quantity messages , and lost all hydraulic fluid . the aircraf t landed safely at sea and towed to the gate . maintenance found the # 2 engine driven hydraulic pump leaking and replaced it per amm 29-13-51 . a satisfactory leak / operational check was accomplished with no issues noted .
crew reported weight was 245k , speed 110kts at time of event . brake temps were at 2 at time of debrief . there where no e ngine exceedences and they didn '' '' t witness any engine flucuations . rejected take off noted . ref log page 5979268 . # 1 e ngine surged . failed boroscope inspection and esn 31537 is being replaced . this log no longer needs to be open . clearin g logpage.upon completing crew debrief it was reported that the # 1 engine was the cause of the suspected non typical noise se and subsequnet rto . opened outboard fan cowl to access gearbox drive pad to turn # 1 engine per management request .
upon reaching to epr loud bang with swerve right . rejected t / o . no fire . r rev isln val eicas eng2 sn . 724371 ( tsi= 16 306 ) surged at t / off power , chek inlet , lost n1 , oil pressure in red 60 to 70psi per flight crew exhaust , tail pipe for metal , check all chip detectors . ref fim 71-05 fault tree 803 for fault isolation and t / shooting . report findings to tom c engine controller.whqlm-emc arshad . 27aug23 . capt . u160941 , called to say that it was low speed 40-50 knots aborted t / off , thrust reverser and rto brakes were not used . whqlm-emc arshad . 28aug23 . ref egc log page 5587893 motor is sieze an
bird strike on eng 2 during takeoff . iaw amm 72-21-00-210-009 general condition of the fan rotor blade item 4-a-1-h was found rotor blade nr 5 deep 4.54 " and large 101 mm between limits . iaw amm 72-21-00-210-009 general condition of the fan rotor blade item 4-a-1-h was found rotor blade nr 6 deep 3.42 " and large 83 mm between limits .
aircraft was grounded : aircraft 7bc clt-dub diverted to jfk on account of loss of flaperon . the crew declared an emergen cy , and the aircraft landed overweight , without incident and taxied to the gate under its own power . * * supplemental repo rt will be submitted . * * ( open )
potential bird strike 30k ft shattered fo window declared emergency.-c / a-c / w bird strike inspection work card found fo windshield outer pain shattered . no further deffects noted see item 3 of this logpage for new discrepancy iaw wc 05-50-02-200-801 and srm 56-11-00
trailing edge flap disagree . eicas message te flaps disagree displayed with the flap control lever in any detent during normal operation reference : 27-51 fault tree 808 log page locked due to emergency declared for landing . discuss debriefe d flight crew . new crew member hovered between 20-25 too corrective action with tomc controller before signing off this long self generating te flap disagree . item . panel instl-capt and first officer and p3-1 ( trailing edge flap position in dicating system only ) reference : 27-58-00-0 p # 215-016-001 indicator in stock sfo due to crew error flaps locked up . used
r3 door does not seem to disarm . found debris under door arming bar . removed the debris . door operated normal iaw amm 52-11-80 .
crew reports evidence of bird strike on the fan exit guide vanes of the nr 1 engine at the 6 o'clock position .
aircraft was grounded : apu auto shutdown 23 minutes after takeoff . apu shutdown again after restart . returned to dfw , landing safely . replaced apu low oil pressure switch ( aala202205110105 ) per amm 49-94-14 . operational and leak checks good . replaced # 2 egt thermocouple probe ( aala202205127356 ) per amm 49-72-15 . operational check good .
aircraft was grounded : right pack caution msg out of 2000 on take off . crew declared an emergancy and returned to phl la nding overweight without incident . maintenance removed and replaced right hand cac inlet deflector door actuator iaw amm 21-51-16 .
believe to have impacted something in flight shortly after takeoff . impact sounded like it came from left side of a / c . emergency equipment rolled as a precaution . a / c returned to atl after t / o inspected a / c found bird remenents under lt . wing , cleaned and performed engine run . no defects noted . ( closed )
aft cargo bay sub threshold web corroded between bs . 787 to bs . 847 , rbl 23 . r and r web per srm and dwg .