boeing/aviation-ner-BIO huggingface dataset:
flt nr 3169 - dca-phl - on departure from dca , a noticeable amount of smoke filled the cockpit . aircraft continued on to phl and landed without incident . inspected engines nr 1 nr 4 bleed valves and ducting , flow control valves and ducting . inspected nr 2 acm for condition and security . found bird lodged on intake screen nr 2 engine . removed bird debris and cleaned intake screen . no other discrepancies noted . ( m )
# 2 engine chip light after start . burnt chip and it came back . shutdown and called mx
ship 3152 - atb - due to elec dc ess bus shed ecam message with numerous ecam warning messages . corrective action : found 1ph c / b popped . r / r 21xe relay , contactor 8ph and c / b 1ph . also found # 2 idg over serviced . drained and serviced . all ops check normal . ok for service . ( 4677422 )
crew reports all lavs not flushing . grounded - yes . airturnback -- found circuit breaker c11 p91 panel open . ( vacuum waste cont ) . reset circuit breaker iaw b737-900amm 20-60-05 . ops cks normal .
aircraft was grounded : an emergency was declared and the aircraft diverted to phx , after level off at fl270 ecam message fuel left wing tank overflood . crew accomplished qrh and ecam procedure . unable to reduce left wing tank fuel quantity . the aircraft landed safely at phx without further incident . maintenance replaced left hand center tank transfer valve a ctuator 11ql per amm 28-25-53 and accomplished a satisfactory operational check .
ship 6716 - atb / ifsd / de - air turn back to cun for left oil filter clog message on climb out , crew pulled throttle back and engine shut itself down . corrective action : checked mcd '' s and oil filter , found metal debris on mcd '' s and in oil fil ter . removed and replaced engine .
ship 3264 - div - to mco due pax o2 masks dropped at row 3c / d . passengers could not be moved . corrective action : inspected and restowed passenger o2 masks . aircraft rts . ( 9900614 )
aircraft was grounded : an emergency was declared and the aircraft diverted to iad due to the flight crew reporting an ep r load fault ecam message simultaneous with generator 1 fault and tr1 fault.with both thrust levers at cruise power was receiving about 25 % less thrust in the number one engine during this event and then 1 '' s were evenly matched at idle thru st . flight crew accomplished ecam procedures for generator 1 fault and reset . the generator came back online and appoxim atley 5 minutes later the same generator fault message came back and would not reset . the aircraft landed safely at iad
( can ) lower flange of upper rudder upper hinge bracket cracked ( airframe bracket ) . discovered during removal of bracket due to worn actuator attach holes .
aircraft was grounded : during climbout below 10,000 ft . a mild / transient dirty sock odor was present in both front and aft sections of the aircraft . odor dissipated by 10,000 feet but was detectable again below 1000 ' on landing but very faint . maintenance isolated the source of the odor to the apu . **supplemental report will be submitted** ( open )
aircraft was grounded : an emergency was declared and the aircraft diverted to lax due to a forward cargo duct overheat fault ecam message . flight crew reported that the ecam indicated 194 degrees . the aircraft landed safely at lax without further incident . ( open )
l pack over temp . crew rejected take off around 80knots . crew report not sure left or right pack temp msg req tomc aprvl deferred lt and right pack auto function per mel to def auto mode lt and rt pack no faults noticed . on controllers . precautionary put both packs on manual temp . approved . tomc mo preformed pack temp controller bite test ref amm tas k 21-51-14-705-035 . no faults noted . reversed mel , returned aircraft to normal configuration . performed high energy insp per amm task 05-51-14-212-089 no problems or dmg found ok for svc
aircraft was grounded : an emergency was declared comming into sea due to the slats not deploying for landing due to a flight control slat fault . the flight crew accomplished ecam procedures and landed safely at sea with flaps 25 . maintenanc e found the right wing slat track # 11 actuator 6091cm torque limiter tripped and replaced it per amm 27-84-49 . a satisfa ctory operational check was accomplished .
discrepancy : air return due to multiple failures . # 4 engine overheat on take-off . corrective action : performed inspection for overheat indications iaw amm 72-00-00-286-064-00 . referenced auto snap shot , all parameters within limits . transferred engine 4 to watch carry over 25405 , 20 cycles due .
multiple fan blades damaged on nr 3 eng due to bird strike . during borescope of nr 3 eng for bird strike , found large tear on le 10th stage through port b1-10 . replaced nr 3 eng .
aircraft was grounded : an emergency was declared and the aircraft diverted to iad . descending through fl230 , the flight crew reported autopilot 1 fault message and a alternate law message along with the flaps being stuck between zero and on e . the decision was made to divert to iad in order to have a longer runway , the aircraft landed safely at iad without f urther incident . maintenance replaced the # 1 slat and flap control computer per amm 27-51-34 . ( aala202305012838 ) and replaced the # 2 air data and inertia reference unit ( adiru ) per amm 34-12-34 . ( aala202305015776 ) a satisfactory operatio
during inspection , found emergency lights from row 23-aft , was inoperative after being on for 10 seconds . found the bat tery pack m1672 was inoperative . r and r the battery pack iaw mm 33-51-06 . ops checked normal .
aircraft was grounded : during boarding external power caught fire , aircraft had a hard change over to apu power , subtle smell of electrical smoke in cockpit , unsure of external power damage . maintenance replaced ground aux panel control unit and accomplished a satisfactory operational check per amm 24-41-34 .
aircraft was grounded : an emergency was declared during descent into dfw : flight crew reorted while decending thru 2600 in clouds anti ice on got a capt pitot fail ecam following procedure then had a cascade of pitot failure lost all alt- airspeed indicatons , ran procedure got some indications back , alt law approach . the aircraft landed safely at dfw without further incident . maintenance replaced probe heat computer # 3 ( 6da3 ) per amm 30-31-34 and accomplished a satisfactory operational check .
ship 9548 -misc / de- the flight crew declared an emergency with atc due to a " stick shaker pusher fail , followed by the " slat disagree " message , and an amber x on the right wing config page . corrective action : maintenance found that the fla p / slat handle transmitters went bad . the transmitters were replaced per b717 amm 27-51-01 on log page 0013015 . return to service tests all passed . the aircraft is ok for service . ( lp # 4825414 )
upon gear retraction on takeoff in ind we got a brake temp light on climb out . the # 6 brake continued to climb and peaked at 7 . we ran qrh procedures and extended the gear to cool the brake . upon landing in phx the # 6 brake indicator was the first one to show any ride in temp . it was at a 3 almost immediately after turning off the runway . by the time we were in the chocks after a short taxi the indicator showed 7 . all other indicators appeared normal . removed # 6 main wheel assy.ref m / m b767 32-45-01-4 . found # 6 brake assy . locked up . upon freeing # 6 brake it is still extremely difficult to rotate installed new brake assy . per 767 m.m . 32-41-08-4-4 . ops and leak check normal . due to # 6 brake dragging also removed and replaced # 6 tire and wheel assy . per 767 m.m . 32-45-01-4 . a / c ok for service
a crack was observed in the lower part of the bracket hinge point horizontal , it was discovered during a routine inspection , the crack seems to be product of the material loss caused by rubbing tools against the fillet , tools are used to torque the adjacent bolt .
right engine oil filter eicas message displayed during climb out from departure station kriv . per ati-quick reference ha ndbook , crew elected to shut down right engine . air turn back with emergency declaration . landing was without incident a nd no additional precautionary actions . on arrival , aircraft grounded for inspections and fault isolation . powerplant e ngineering has requested qar data download . crew reported rh engine windmilled for approx 10 minutes . no loss of oil pre ssure , oil quantity or vibration indications presented . post flight , dfdr removed for analysis iaw b767 amm 31-31-01 and teledyne cmm 0g2243800-300 . per b767 fim 79-21 fault tree 802 , removed and replaced scavenge oil filter per b767 amm 79
ship 1801 -smke / fume- passenger entertainment screen at 40a smoking . corrective action : itu replaced . ( 4511560 )
ship 3948 -ufc / de- declared emergency due to flap lockout at 15 degrees on approach atl . corrective action : maintenance found number 1 and 8 flap trans dpi popped . serviced trans fluid and lubed flap jackscrew per b737 amm 12-22 .
aircraft was griounded : an emergency was declared and the aircraft returned to dfw . while in cruise flight at fl270 and 1 hr after takeoff hydraulic green engine # 1 pump low pressure ecam . flight crew accomplished the ecam procedures and po wer transfer unit successfully powered the grreen hydraulic system . the aircraft landed safely at dfw and taxied to the gate under its own power . maintenance replaced left engine hydraulic pump pressure switch and accomplished a satisfacto ry leak / operational check .
l / h elevator upper surface is gouged approx 9.5 ' o / b of the i / b hinge . repaired l / h elevator upper surface noted damage by performing permanent wet lay up repair iaw b767 srm 55-20-01-1a , srm 55- 20-01-2r , srm 51-70-17-06 , fedex ea # h-5520-t0376037 new rework moment found to be 2492.2
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 for aala202402145589 : maintenance noted that the oil scavenge filter housing inserts are pulling out an d the seal was showing . a review of the dfdr data revealed that the engine operated below 13 psi for more than 2 minute s requiering the engine to be changed . maintenance replaced engine per task card 26l40071001 . * * ( closed )
aircraft was grounded : an emergency was declared and the aircraft returned to lax due to the flight crew reporting that during cruise several ecam messages '' fwc # 2 '' sdac # 2 dmc # 2 appeared along with other associated faults . later on , during follow ups found a tripped c / b on 123 vu panel . the aircraft landed safely at lax without further incident . maintenance removed and replaced circuit breaker 3xn2 ( aala202405208322 ) , contactor 9xu2 ( aala202405204769 ) and contactor 11xu2 ( aa la202405206953 . ) a satisfactory operational check was accomplished with no faul messages noted .
the pulleys used in the vent ( red ) line assembly one at the parachute and one at the side to the envelope near the bottom are under designed and not raised for the forces needed to set / open the parachute . both balloons have had total failures of both pulleys . this has occurred during normal flying over 300 hours on each balloon . it is noted that these balloons are part of a flight school and as such see more flights and more vent line operations during training than a privately owned balloon . it is made more apparent by the excessive force needed to reset and to open the parachute on the adams / apr designs . this excessive force has been noted on larger ( 125,000ft3 ) versions as well , and has been reported to the manufacturer on numerous occasions , with no solutions . the pulleys appear to be standard off the shelf parts available from normal hardware stores . the recommendation to solve the issue is an immediate emergency ad grounding all adams / apr balloons from further flight until an adequate pulley is provided and retro fitted into all existing balloons manufactured by the adams / apr company by the company .
pilot reported the garmin 430 stopped working , screen went blank and noted electrical burning smell . maintenance replaced the gps 430w unit in accordance with garmin 430w installation manual with no further defects noted .
aircraft was grounded : an emergency was declared and the aircraft returned to lax . climbing thru fl200 engine 2 bleed fa ult on ecam displayed . while flight crew was performing the ecam procedure they lost cabin pressurization . since the # 1 engine bleed was placarded as inoperative the aircraft returned to lax where it landed safley without further incident . maintenance replaced the # 2 bleed management computer ( aala202307141203 ) and the # 2 pylon bleed air overheat sensing ele ment 1hf2 . ( aala202307149385 ) . a satisfactory operational check was accomplished with no bleed messages or cabin pressurization
aircraft was grounded : an emergency was declared and the aircraft diverted to phx due to the flight crew reporting that after departure none of the toilets would flush . the aircraft landed safely at phx without further incident . maintenance found circuit breakers for the lavatory vacuum generators out and reset the breakers . maintenance found connector 7211vc and terminal block 7492vt with no damage noted per tsm 38-31-00-810-834a . a satisfactory operational c heck of the lavatories was accomplished with no faults noted . maintenance was unable to duplicate the issue .
on takeoff roll at 75 kts received ecam yellow hydraulic system low pressure , aborted takeoff . fact 14mar23 03 : 51 a tl u amm 29-00-00-06 amm 29-10-00-05 per crew debrief , yellow hydraulic pressure was normal on taxi back to ramp . in spected yellow system hydraulic module and # 2 engine hydraulic hydraulic pump for obvious discrepancies , none found . ref m.m . 29-10-00-05 . no leaks noted per m.m . 29-00-00-06 . a / c ok to continue . r and r '' d yellow hyd system low pressure s switch 31ww per above ref . operational check and leak check good . a / c ok for service .
low speed reject 90kts due to fwd entry door light..fa cycled do or handle . door showed clsd crew advised once pulled . f active rnwy door 1l entry door handle was cycled from inside , visually checked no obstructions and indication now norm al . no previous history and capt okay for further flight . iterm open for event - lw spd abort 90knts no further action r equired .
while working water intrusion deferral barcode t3f18e002sm1q found floor panel 231kj damaged . marked with green tape.***sm eval req*** temporary repair iaw eo-88400-req1 deferral requested . open
# 2 start switch wo n't stay in grd position during start attempt . grounded - yes . ( resolved on w / o : 1961049 taskcard : n / r-00002 ) removed and replaced # 2 engine start switch per amm 80-11-00 . test good per same . clear mel 80-2b c / n 11034532 . placard removed . seamc ashraf notified .
at takeoff compressor stall on nr 1 engine . bird strike confirmed . compressor borescoped per mm . no damage . engine continued in service .
ref nr l / p 9470008 bulk cgo compartment bs1958-1979 stringer surface corrosion found on str47r . bulk cgo compartment bs1 958-1979 str47r stringer repaired as per srm 53-70-03 repair1 rev 78 and ecra 5341-01146 rev - . add emp : v906646 rii by t a328
aircraft was grounded : after takeoff the stabilizer trim totally failed with speed trim failed annunciation . emergency declared , flight returned to lga landing safely . maintenance replaced horizontal stabilizer trim motor per amm 27-41-71 .
aircraft was grounded : an emergency was declared and the aircraft diverted to bna . after takeoff the aft flight attendan ts reported a sweet maple syrup odor in the last third of the aircraft . the flight attendants reported that the odor dec reased midway through the flight but came back and was getting stronger . the odor was most prominent from row 21 to the aft of the cabin . the crew deployed the passenger cabin oxygen masks and dooned their oxygen masks . the aircraft landed s afely at bna and the passengers were deplanned on the taxiway and bused to the terminal . * * supplemental report for aala2
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 . * * supplemental report will b e submitted * * ( open )
aircraft was grounded : an emergency was declared and the aircraft diverted to phl . after take off during climb the engin e cowl anti-ice valve failure lights illuminated on both engines . the flight crew accomplished the qrh procedures and la nded safely at phl without further incident . maintenance accomplished a satisfactory operational check of the # 1 engine anti-ice system per amm 30-21-00-71-801 with no faults noted . ( aala202311020922 ) maintenance replaced the # 2 engine anti -ice valve per amm 30-21-11 . ( aala202311027992 )
aircraft was grounded : an emergency was declared and the aircraft returned to dfw . on climb out got ecam fuel right wing tank overflow . crew complied with ecam but continued venting . follow ecam down to gravity feed . got ecam at fl 240 and leveled at fl 260 to work issue . the aircraft landed safely at dfw without further incident taxied to the gate . maintena nce replaced the right hand surge overflow sensor per amm 28-46-16 . a satisfactory leak and operational check was accomp lished .
ship 3354 - div - into bos due to loss of the blue hydraulic fluid . corrective action : replaced # 1 eng blue hydraulic pump , blue case drain filter , replaced low- and high-pressure filters . motored engine , no debris found . ( lp 5497610 )
air diversion - r eng sys fail . / / inspected # 2 eng tgt harness and found terminal t1040-2 leg broken . removed and replaced per 71-52-01 . ops ck pending . ran engines for 4 minutes -- no faults noted ( amm 71-00-11 ) . ok for service .
rh i / b elevator i / b aft upper surface found dent mark ( p > performed composite wet layup repair as per srm 51-70-04 repair 1 . no further defects noted / p > )
after take off , lgciu 2 fault indication was shown . atb procuedure to bogota station due to by mel manual , both reversibles should be operative to aproach in santa marta station / / as per tsm 32-31-00-810-819-a fault insolation lgciu 2 was removed and replaced test satisfactory . software configuration the lgciu1 was replaced test satisfacgtory .
engine fire and multiple systems warnings and cautions after rotation in light rain . engine temperature indications we re normal autopilot automation was not available . emergency declared . indicator were all replaced and all ops checks being satisfactory . a gvi was performed of engines and found no evidence of a fire or pneumatic leak damage . ops checks good . ok for service .
*supplemental rvsm* f / o and capt . altimeters differed by 270ft @ fl 330 . standby matched cpt altimeter . f / o selected air data to alt . t / s sys . ; no leaks noted . ref item [ t3f18e0037wat ] ( aoa sensor rr ) per tech service .
forward rh emergency light battery pack inoperative . / r and r battery pack per amm .
left thr rev illum on takeoff roll 70 kts after achvng takeoff thrust item placed back on mel due to history . ref logpa ges 6098424 and log 6104186 for mels . amber rev icon on lh epr gauge after takeoff thrust was set . left amber alluminate d after throttles were advanced for takeoff during take off roll amber light came on . per crew conversation . crew reject s takeoff all system and indications normal . rev opened and closed normal . control of aircraft normal . after reverser stowed and aircraft turned off runway amber light extinguished and has not returned . complied with mel requirements . add e
ship 669 -atb / ifsd- performed air turn back for left engine stall on climb out . n1 rolled back and engine was shut down by crew . metal found in tail pipe . corrective action : r / r number 1 engine
aircraft was grounded : an emergency was declared and the aircraft diverted to mci dur to fuel auto transfer fault messag e . fuel transfer uncontrollable which resulted in uncontrolled imbalance . right wing tank overflow . crew reported the aircraft landed with 7k imbalance . the aircraft landed safely at mci . * * supplemental report will be submittted * * ( open )
electrical smell with smoke seen coming from under seat 3f locking to confirm completion of amm 05-51-56 unlocking for mx performed ifim task 21-00-00-810-830 . no maintenance messages found . ran lru for 10 minutes and no smoke detected . removed and replaced high power seatbox p / nrd-fa3871-01 s / n off / on j416274 / j535249 . before installing new seatbox inspected all harnesses and surrounding seatboxes for damage . no damage noted . found source of smoke to be coming directly from seatbox at 3f after installing new seat box and applying power , waited and observed for 45 min to see if smell or smoke would return . there wa s no further smoke or smell .
high speed rejected to due to aft cargo door open indication . per crew rto at 100 knots . ts found aft cargo door flap li nkage out of adjustment . adjusted per amm 52-32-11-820-002 . reinstalled and operated aft cargo door handle . ops ck ok . i ndication is normal . preformed inspection afterbrake emergency application per amm 05-51-16-200-001 . no faults . ac ok fo r service .
aircraft was grounded : an emergency was declared and the aircraft diverted to orf due to the flight crew reporting airfr ame vibration at fl 280 . vibration stopped when we slowed to 270 knots . the aircraft landed safely at orf without furthe r incident . maintenance replaced the right-hand elevator outboard servo control actuator and the right-hand elevator i nboard servo control actuator ( aala202405252364 ) on the right-hand horizontal stabilizer due to excessive play . maintena nce also replaced the elevator hinge fittings for positions 1 thru 6 on the left horizontal stabilizer and right horizon
emergency power assist system status on the r2 door was inoperative , green light inoperative . maintenance replaced the emergency power assist system battery pack iaw amm 52-11-20 , and performed a satisfactory operational check .
at cruise l pfd blanked . pfd transfer switch did work to regain captains display , but with f / o€™s now blank as a result . removed and replaced left ggu per mm31-65-02 cw software check . system ops check
low oil pressure indication on right engine . performed " engine failure precautionary shutdown " abnormal procedure .
corrosion in shear clip fr 87 between str 27-28r . removed and replaced shear clip fr-87 between str 27-28r srm 51-40-08 .
on takeoff roll , right prop was struck by a bird . aborted takeoff and returned to the gate without further incident . maintenance inspected aircraft and no damage was found . aircraft was approved for return to service .
right engine oil filter eicas message displayed during climb out from departure station kriv . per ati-quick reference ha ndbook , crew elected to shut down rt engine . air turn back with emergency declaration . landing was without incident and no additional precautionary actions . on arrival , aircraft grounded for inspections and fault isolation . powerplant engi neering has requested qar data download . open