boeing/aviation-ner-BIO huggingface dataset:
glideslope left and right side did not match on ils approach . for the entire approach . r and r rt nav unit , iaw emb amm 34-32-01 . operations check good ok for service . performed ils check , iaw tic box , nav sensitivity check good . clear mel 34-10 and sil 34-51 .
ship 3850 -div / fumes- diverted to abq due to electrical fumes in flight deck . no visible smoke . corrective action : found fo 's control column memory device shorted . replaced same . ops checks good .
aircraft was grounded : an emergency was declared and the aircraft diverted to mia due to the flight crew reporting that approximately at 10000 '' air bleed 2 message annunciation . flight crew ran ecam procedures and after engine bleed was tu rned off per ecam actions we got spurious messages for engine 2 bleed leak . the spurious messages would trigger then disappear before any actions could be taken . this occurred approximately 6 times . the aircraft landed safely at mia witho ut further incident . maintenance replaced the # 2 engine thermostat - fan air valve control and accomplished a satisfacto
engine oil pressure light illuminated shortly after take off . light flickered a couple of times , than stayed illuminated as aircraft turned back towards base , than extinguished on decent into base . oil pressure light was not illuminated upon shutdown . aircraft was inspected , ground and flight checks performed and unable to duplicate caution light . oil pressure gauge shows normal indications
pre-departure crew reported main cargo fire indication with smoke smell . positions 8 a and b green lights annunciated . 8 a turned amber , 8b extinguished . emergency declared and aircraft grounded . to facilitate maintenance , cargo freight unl oaded . fault isolated to apu battery and battery charger . removed and replaced apu battery and charger iaw b767 amm 24-3 1-04 / 05 . operational checks good . general visual inspection of apu battery and charger wiring satisfactory iaw swpm 20-1 0-06 . aircraft released to service .
after t / o out of ord , heard loud noise from nose of aircraft . rh side . ******aircraft removed from service********* found crew o2 servicing door open on arrival . visually inspected door and latches , no defects at this time . door secures closed .
ship 5643 -misc / de- crew declared emergency due to te flap asym on approach . corrective action : secured loose connector on flap power drive unit .
acft experienced a bird strike . *s / d* inspected area of bird strike and performed walk-around inspection per 05-51-37 , no defects noted .
oil quantity indication ( engine ) shows lo fim task ref : 31-90-f8-03a-421b-a cmc msg # 7931791 flight status : a intermittence code : m ph : cruise narrative : 31 dca ops ( right 3 ) . note talking to dispatch engine was never shutdown . crew diverted due to falling oil pressure before they got to a point of having to shutdown the engine . updated maa code fix using vendor maa screen local mx from air canada found oil cap off , resecured cap and please meet acft and evaluate engine one for signs of oil loss cleaned are under fan cowls , cowls resecured . oil tank requires servicing . tomc-meredith serviced the left engine with 28 quarts of oil and secured cap in reference to amm 12-22-01 . performed idel leak check and no other defects noted .
aircraft was grounded : an emergency was declared and the aircraft returned to dfw due the flight crew reporting a yellow hydraulic reservoir low level message . the aircraft landed safely at dfw and taxied to the gate under its own power . ma intenance found the yellow hydraulic system reservoir was actually overserviced and drained the system to the correct le vel . a satisfactory leak / operational check was accomplished with no defects noted .
# 2 eng o / b fan cowl is delaminated ( p > accomplished and nbsp ; hot and nbsp ; bonded and nbsp ; permanent and nbsp ; repair and nbsp ; on and nbsp ; # 2 and nbsp ; eng and nbsp ; o / b and nbsp ; fan and nbsp ; cowl and nbsp ; per and nbsp ; 54-22-00-0g-0 / p > / p > 54-21-01-0i-1 , and nbsp ; and nbsp ; 54-21-01-01a-1 ; and nbsp ; 54-21-01-2r-1 and nbsp ; and nbsp ; and nbsp ; repair 1 / p > / p > 51-70-04-0g-0 , and nbsp ; and nbsp ; and nbsp ; work and nbsp ; accomplished and nbsp ; per and nbsp ; avenir and nbsp ; aviation and nbsp ; faa # and nbsp ; 8avr479b and nbsp ; and nbsp ; feam and nbsp ; ro # and nbsp ; 5002790 / p > / p > and and nbsp ; and nbsp ; avenir and nbsp ; and nbsp ; wo and nbsp ; # w16039 and nbsp ; and nbsp ; and nbsp ; and nbsp ; 8130 and nbsp ; attached / p > )
ship 9579 -fcnt / de- the crew noted a " pseu " message displayed on the ead during cruise . the qrh was complied with , an em ergency was declared with atc , and the crew safely landed in ewr with zero degree flaps and slats . corrective action : ma intenance determined that the pseu was faulty and replaced it . all rts tests performed passed and the aircraft has retur ned to service . ( lp # 4289890 )
battery temp light : on climbout the master warning and steady batt o'temp annunciator lights illuminated . carried out qrc but no amp decrease noted . carried out qrh procedures . the battery temperature gauge remained in amber range . battery was disconnected using batt disc switch . eventually the batt o'heat light went out but came back on again as we descended through 5000 feet and remained illuminated through remainder of flight . on postflight the battery was hot to the touch . manually disconnected the battery . by an hour later battery was cool to the touch . / / signoff / / removed and replaced main ship battery with an overhauled battery iaw ce560xls amm 24-32-00 . battery is charging normally . the battery temperature indication in the cockpit is reading correctly and the battery is the ambient temperature outside . pn off / on 9914058-ll sn off 000698de . sn on 0021f793 .
aircraft was grounded : an emergency was declared and the aircraft diverted to iad due to the flight crew reporting that on climb out they heard a loud bang at fl160 and the right engine fail message displayed followed by the n2 dropping to 2.5 % . the flight crew followed checklist and shut down the right engine . the aircraft landed safely at iad without further her incident . maintenance noted several damaged blades and excessive fluid in the rear of the engine . ( open )
pilot observed smoke in cockpit caused by faulty transponder installed under stc # sa01512wi-d 07 / 09 / 2010 . found burnt chip on circuit board .
aircraft was grounded : emergency declared on approach to sti due to hydraulic system b low pressure light . aircraft landed safely at sti without further incident . maintenance replaced o-ring righthand number 8 spolier actuator filter cap per cmm 27-60-42 .
the landing gear circuit breaker tripped while en route to kgeg . the pilot performed emergency gear down procedures and landed without incident . maintenance found two wires damaged , g19h22 and d41a22 . wire repairs were made and functional checks of the landing gear were performed on aircraft jacks . all checks were successful after the repair and the aircraft has been returned to service .
ship 0654 - atb - due to loss of nav systems enroute . corrective action : iru 's realigned after arrival with ntf . completed mcc workscope and replaced iru control panel precautionary . rts .
after takeoff , large bird or birds hit near left nose wheel well . aircraft returned to dal and made an uneventful landing . inspected and found slight evidence of strike to nose left side , within boeing srm and number 1 engine . borescoped and performed engine run-up , with no damage noted .
aircraft was grounded : an emergency was declared and the aircraft returned to jfk . during cruise an ecam message for excessive egt temperature on engine # 1 and the flight crew shut the engine down . the aircraft landed safely at jfk without further incident . maintenance found the # 1 engine egt cj13 harness chaffed by the engine cowl and replaced it per amm 73-29-00 . a satisactory operational check was accomplished .
spd 190 selected f20 and got te flap disagree eicas . ran chklst . did not clear . log locked for positive fix , iah notifie d . flight crew declared emergency landing unlocked : fseu and m838 card replaced , numerous ops test with no faults locked t / s per fim 27-51 task 809 , all faults , info . , and parts replaced per fim stated in the logpage . debriefed capt : at 190 kias moved flap lever from fl5 to fl20 , te flap disagree appeared after both needles reached fl20 . ran disagree checklis t , did not clear . disagree checklist drives to te asymmetry checklist , msg still did not clear . per fim 27-51 task 809 f
ship 9500 -atb- the aircraft was returned to atl following compressor surges in the # 1 engine . the pilot declared an emergency with atc and the landing and taxi to the gate was uneventful . corrective action : maintenance replaced the # 1 engine ( esn 13197 ) and the aircraft was returned to service . ( lp # 9635642 )
aircraft was grounded : an emergency was declared and the aircraft diverted to clt due to the flight crew reporting on ta keoff climb ecsm electrical dc essential bus shed . flight crew performed ecam procedure no help . dc essential shed inope rative . the aircraft landed safely at clt without further incident . maintenance accomplished tsm 24-60-00-810-801-a and found high resistance across contactor 8ph . contactor 8ph replaced per amm 24-62-55 and a satisfactory operational check was accomplished .
main deck cargo floor panel # 261gf l / h sta 1940 found with 4 scratches with largest with having 3 " max diameter and amp ; no delamination ( p > main deck floor panel # 261gf lh sta 1940 floor panel repaired iaw and nbsp ; en # 1051-19 rev- / p > )
mdis 938 24-22 9631 30oct23 ind fact u upon powering up aircraft , noticed an acrid smell in cockpit with associated stby inverter eicas msg . part 30oct23 16:24 mc1 u identified parts static inverter mpn : 1-002-0102-2090 cpn : 2413802 qty : 1 r / i 30oct23 16:33 ind u reason code : premature removal / installation off mpn : 707760-4 pos : onl on mpn : 1-002-0102-2090 srl : cj002100 tag nbr : 8g9069 fact 30oct23 16:33 ind u amm : 24-33-03-4 r and r static inverter ref amm , volts and freqs normal , checks ok . fact 30oct23 16:33 ind amm : 24-33-03-4 r and r static inverter ref amm , volts and freqs normal , checks ok .
approx 2 min after gear retraction , level 2 hyd 3 fail caution . turned back towards memphis and proceeded with qrh for hyd 3 fail . nose gear showed unsafe , after discussion with moc , fleet captain , and tech pilot a low approach was cond ucted to verify nose gear down . after tower confirmation , proceeded with the rest of the qrh and landed without furth er incident . * * * emergency declared * * *
crew reported ecam for aft cargo door at fl 1200 . declared emergency and descended down to fl 10000 . ecam went away . pe rformed post flight report and found aft cargo dr prox snsr ( 32wv ) tgt pos . fault . inspected aft cargo door upon arriva l and found aft cargo door locked and latched closed requesting mel for aft cargo door indication placed on mel ok to ap ply mel 5270cd for aft cargo door indications inop * dm * recommend tsm 32-31-00-810-886-a for initial t / s . possible cause prox sw ( 32wv ) attached on m / l .
thrust management system a / t disc light illuminated with autothr ottle engaged in ( state mode ) mode . thrust reference mode displa y on eicas and amp ; amp ; f / s pointer display on eadi normal in vnav path mode arrival crew information : a / t disconnected in cruise , reset accomplished mcdp tmc test 2 , tested passed . mcdp flight faults accomplished . a / t disconnected again no reset , also eec 2 c1 for -1 flight leg shows a / t disc eec r prim / tmc message . pimu message . showing eec a chan tmc i / f fault . ref fim 71-01-task 820 , 350-29 eec a / b-chan tmc i / f . fim 71-01-task 820 , para b ( 5 ) for pimu msg 350-29 eec a / b-chan 01 fault tree 804 . if fault msg persists , replace eec . pls c / o m tmc i / f on 1 ch ( ch a ) for right eng only accomplished . no wirin cdp test 30 in raised cat lp to retain cat status . idt raised fo g fault found between eec connector d11114 and wing / strut discon r eec / fadec harness connectors nect d6382p . no msg present in pimu recall procedure ref fim 71- add emp : u405155 all eec connectors checked for fitment and security post wiring checks ref gmm 09-10-05 i . ( 21 ) ( a ) 4 .
lower vertical stab leading edge panel has suspected erosion damage on bottom two thirds of panel as viewed from ground level . removed and replaced lower vertical stab leading edge panel 322al iaw a300 amm 55-32-11-401
pilot reported in cruise flight the rotor tach was moving erratically . mechanic inspected the connector and cleaned cannon plug and applied heat shrink per the amm
* emergency declared * on short final got ? ? ? flaps drive ? ? ? , did goaround , ran checklist and made normal landing left flap s down . for precautional , performed lubricate outboard trailing edge flap ball screw assembly iaw amm 12-21-20-301 , ops normal for trailing edge flaps system iaw amm 27-51-00-201 .
ship 9504 gear / de- on approach for landing the flight crew received an " nlg unsafe " indication after selecting the gear to extend . the qrh was complied with , an emergency was declared , and the alternate gear extension procedures were perfo rmed . the nose landing gear did extend at that time and the landing was uneventful . corrective action : maintenance repla ced the nlg bungee actuator , a missing upper pin right inboard bolt , a damaged left inboard bolt , and the corroded upper lock link pin ( both bolts ) . investigation showed the bolts to be sheared and that no sealant was present . ( lp # 5625362 )
irs 2 fo side in flight lead to diversion . speed trim fail on re call . maint light on touchdown on omf existing flight d eck effects r adir faulted . as well as stab / trim test no . 60.32 , test passed . fault corrected . maint fault light on mo de select unit for r adir per crew . replaced r light no longer illuminated . parts used : 42-3421-9-0001 , qty adir ref am m 34-21-01-400-801 . tests good . troubleshot speed : 1 trim light ref fim 22-11 task d71 . accomplished surface test rotab le parts change was indicated - tt # 1527975 sn off 5748 unit , adiru , ai off 42-3421-9-0001 5748 on 42-3421-9-0001 160
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 a ft 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 will be s
aft cargo compartment r / h " z " angle had multiple cracks at the frames between bs . 727 to bs . 767 , rbl 21 . / r and r z-angle iaw srm and dwg .
( aus ) rt wing root fairing suffered a fruit bat strike during landing . the bat caused a hole in the kevlar fairing but did not penetrate . the hole size was approximately 180mm ( 7.08in ) . ( other cause : birdstrike ) ( casa nr 510001924 )
high speed rejected t / o for directional contol.reqest mx inspecttomc update : per flt crew verbal , high speed rto was app rox at 100 kts . locked lp tp ensure high energy stop amm 05-51-07 is complied with before departure . mm changed all 6 la nding gear tires . checked stall management / yaw damp computer # 1 for existing fault . no existing faults . i did not cha nge any parts , but i acp '' d installation test of rudder solenoid and electrohydraulic servo valves per amm 22-23-21-740-8 01 , to check rudder . no faults . flt performed gvi and dvi of main brakes ref amm 05-51-07-210-801 . ops checks good , no
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 . ( note : no emergency was declared . ) * * supplemental report for aala202301135322 : maintenance found nose landing gear proximity sensor 24ga to be out of adjustment and adjusted it per amm 32-31-73 . a ssatisfactory operational che ck was accomplished . * * ( closed )
triple tach / rotor rpm failure during flight . during rotor speed failure troubleshooting , found nr sensor bad during function test of the rotor speed monitoring sys amm 62-41-00 , 5-1 . removed and replaced speed pick-up ; limited test flight successfully completed .
during cruise flight , washers and retention ring were seen on the copilot floor . discovered the right tail rotor pedal was slipping off . returned to base with no further incident .
ship 9500 -atb- the crew declared an emergency and returned the aircraft myr due the # 2 brake over temperature warning i lluminating . qrh procedures failed to lower the temperature indication . the landing was uneventful and the aircraft brak ing was normal . corrective action : maintenance found the # 2 brake temperature sensor broken in half and replaced it . ( lp # 4076698 )
number 1 engine failed at fl370 pilot said all the left engine display indications started flashing and about a minute later the engine rolled back to idle then they shut it down . they said oil pressure seemed to be normal . and they noticed the # 1 engine fuel flow was 3.8 and # 2 was 2.4 . also mentioned the left tank quanity was significantly lower than the right . added pictures of faults found 2 bolts on output line of fuel flow transmitter loose . tightened bolts to specs in amm 73-31-01-400-801 . two bolts were loose on fuel flow transmitter all bolts , threads and heli coils on fuel flow transmitter are intact and bolts were tightened back to specs transmitter , fu off 42-7331-9-0001 1730 on 0000 transmitter , fu off 42-7331-9-0001 1730 on 42-7331-9-0001 0972 removed and replaced # 1 engine fuel flow xmitter i.a.w . amm 73-31-01-400-801-g00 performed engine idle test . test passed . leak check good . parts used : 42-7331-9-0001 , qty :1 rotable parts change was indicated - tt # 1039422 sn off 1730 .
aircraft was grounded : an emergency was declared and the aircraft diverted to stl . flight crew reported that during cruise at fl 350 they lost # 2 engine epr and n1 degraded message occured . crew accomplished qrh procedures and the aircrft landed safely at stl without further incident . maintenance replaced the p2 / t2 probe per task card 26l40073005 .
rtfl under amber alert due to bird injestion in the nr 2 engine . engine shut down after landing .
left fuel bypass illuminated in climb [ 01 ] r+r # 1 main eng fuel filter no contaminates noted iaw amm 73-34-01 ev # e027503
aircraft was grounded : an emergency was declared and the aircraft returned to dfw : during climb air engine 1 bleed abnor mal prressure ecam message . flight crew accompished qrh but reset was unsucessful . the aircraft landed safely at dfw wit hout further incident . maintenance found the # 1 engine pressure regulating valve top sense line loose and tightened it p er amm 36-11-52 .
aircraft was grounded : an emergency was declared inbound to dfw due to a yellow hydraulic system reservoir low level eca m message . flight crew accomplished ecam actions and yellow hydraulic system quanity indicated zero . the aircraft lande d safely at dfw without further incident . maintenance found hydraulic fluid leaking from the right pylon drain due to a ruptured hydraulic line in the ponyl and replaced the hydraulic line per eo 2922e003-004 .
flight 827 multiple bird strikes during takeoff at approx v1 . smell filled acft and felt several thumps from bird strikes . returned and found evidence of bird strike to nr 1 eng . performed borescope iaw card 26l40072006 , with no defects noted .
lt stow bins emergency light inop between row 3 to row 4 . r and r light iaw amm .
on climb out crew reported , main cargo door light illuminated at fl280 . pressurization ok . crew elected air turn back to klal with an emergency declaration . landing was without incident and no additional precautionary actions noted . post f light line maintenance verified operational check of main cargo door good . fault transferred to deferral maintenance ite m 52639 per ati minimum equipment list 52-71-01-02 . main deck cargo door forward instrument panel certified inoperative . aircraft resumed service . main cargo door operational check per iai supplemental maintenance manual 52-32-00 satisfa
during flight the actuator master caution illuminated . aircraft started to experience heading / trim anomalies . flight controls also became increasingly sluggish . during test flight eval , 35 minutes into flight , actuator illuminated on cad . pfd displayed a yaw amber indication . after landing , ap test was conducted and ap1 and ap2 failed test with yaw actuator along with yaw sas failing . removed and replaced t / r actuator iaw amm 67-34-00 , 4-1 . test flight successfully completed .
bumps or bubbles were found in the upper sheave grooves . these seem to be corrosion pockets between the metalized plating and the cast aluminum base . if this continued in service , accelerated drive belt wear will occur .
aircraft was grounded : an emergency was declared . flight crew reported fume event descending through 12k feet . crew acco mplified qrh . procedures but smell perrsisted through entire aircraft until after landing when packs were off . the airc raft landed safely at the scheduled destination of dfw without further incident . maintenance accomplished the smoke odor fume troubleshooting task card and found source for the odor and no defective components were identified .
aircraft was grounded : an emergency was declared and the aircraft diverted to pwm due to the flight crew reporting that during cruise the engine page popped up and both oil quantities were fluctuating between 2 and 4 quarts and both oil pressures were in the red at 2 psi . the aircraft landed safely at pwm . ( note : this report is for # 1 engine , see aala2024061 45548 for # 2 engine ) * * supplemental report for aala202406145803 : maintenance found # 1 system data acquisition concentrat or ( sdac ) inoperative and replaced it per amm 31-55-34 . a satisfactory operational check was accomplished * * ( closed )
aircraft was grounded : an emergency was declared and the aircraft returned to clt . flight crew reported that engine # 2 e gt over limit on take off climb was 400 degrees , approximately 920c . flight crew shutdown the # 2 engine and reported tha t later it cooled to 700c . the aircraft landed safely at clt and taxied to the gate . maintenance replaced the # 2 engine and accomplished a satisfactory leak / operational check per task card 26l40071001 . * * ( closed )
aircraft was grounded : an emergency was declared due to : flaps would not extend past 15 on approachaircraft landed safely at phx without further incident . removed and replaced fseu ( flap slat electronics unit ) . performed successful bite test of fseu . per amm 27-51-00 . no defects noted at this time .
sap - during landing , engine nr 2 experienced a bird strike . after landing maintenance personnel performed inspection of the engine nr 2 . at the moment , aircraft remains on ground at sap station for inspection and maintenance . ( m )
aircraft was grounded : excessive oil consumption on # 1 engine was monitered by the pilots suspecting a leak . when it was calcutaed that they would not have enough oil the flight was diverted to yul and an emergency declared . aircraft landed without incident . maintenance found a broken bolt on the lpt scavenge oil tube . maintence replace the lpt scavenge oil tube iaw afmm 20-51-5 and ea 349322 .