boeing/aviation-ner-BIO huggingface dataset:
climbing through fl250 main cargo door light and master warning alarmed . subsequent to message cabin altitude started cl imbing . crew elected to turn back to kjfk with an emergency declaration . landing was uneventful with no additional precautionary actions . on arrival , aircraft grounded for unscheduled maintenance . on arrival line maintenance inspected main deck cargo door and verified door closed and locked . aft sill lock down noted . deferral maintenance item 41090 initiated , mel cat c . iaw b767 amm 52-71-00 depressor and surrounding area checks good . with system interlinked to breakout box
aircraft was grounded : an emergency was declared due to : on climb out , aircraft had high vibrations at high power settin gs . flight controls felt mushy and autopilot kicked off twice after gear and flaps were retracted ; aircraft air interrup ted back to and landed safely at tpa . * * supplemental report will be submitted * * ( open ) .
ship 8137 - misc - crew declared emergency due to " dmc 1a fail " and associated messages . corrective action : reset aircra ft power , message cleared . downloaded non-volatile memory and replaced data concentrator module ( dcm ) 1a downline . ( lp # 5 302870 )
crack - found shear tie have crack at sta 1000 rbl 33.99 remove damage shear tie iaw srm 51-40-02 rev 94 . 2 ) install new shear tie iaw ei t2022a53m-1601 rev 2 and srm 51-40-02 rev 94 . 3 ) condition check normal and job completed / p > )
aircraft was grounded : an emergency was declared into phx . during cruis at fl 320 , the # 2 engine vibes reached 6.6 alon g with a # 2 engine oil filter clog message . the crew then recieved # 2 engine stall and # 2 engine fail messages which wa s followed by # 2 engine inflight shut down . the flight attendant reported sparks comming from the # 2 engine tail pipe r esulting in the crew discharging the # 2 engine fire bottles . the aircraft landed safely at phx and taxied to the gate un der its own power . * * supplemental report will be submitted * * ( open )
aircraft was grounded : during final approach into las while selecting flaps 2 the flight crew reported a flaps locked al ignment fault ecam message and aborted the approach . the flight crew accomplished the ecam procedures and landed at las without further incident . maintenance found flap interconnecting struts on the left wing ( aala202406240192 ) and the righ t wing ( aala202406245048 ) out of rig . maintenance rigged both flap interconnecting struts per amm 27-51-44 and accomplis hed a satisfactory operational check with no faults noted .
aircraft was not grounded : vmo gear down status message . pilots retruned to phl , declared an emeregency and landed overw eight without incident . maintenance performed fim 31-50-f1-14a-421 . overspeed warning in gear down-switched to norm .
rh engine zone 1 fire indication and lh engine zone 2 fire indication . found rh tailpipe disconnected causing rh zone 1 fire indication . lh zone 2 fire indication was false warning cause by bad diode .
left engine elc limiter at start of take off roll . left engine limiter inop , crew complied with mel procedures . rejected take off was less than 50 knots , low energy with no hot brakes . deferred directly by tomc performing engine run eng eec msg was observed on eng / apu further troubleshooting required . ref . 73-21-07 . parts used : performance page , unit had no power while engine was running . 19-7321-9-0013 , qty : 1 rotable parts change was indicated - tt # 1764207 sn off 8864 rem oved and replaced lh engine , engine supervisory control unit . bite checked box before engine run with no faults . while c
rh main landing gear , aft trunnion bearing , outer race with corrosion ( p > rh main landing gear , aft trunnion bearing , outer race , the bushing was replaced iaw engineering order a-32-045-01-2 / 001 and amp ; cmm 57-54-13 . pn : 113t1108-17 and amp ; 113t1108-23 / p > )
flt # 523 , jfk-lax . ( etops ) ' condition trim air sys fault - cockpit trim valve ( cockpit / cabin trim air valves ) . performed bite test of temp ctl sys . found no previous or pfr of faults . ok ref tsm 21-63-00-710-057-b . mddr cleared . mx-4 updated . placard removed .
between 1000-1500€™ the packs blew out a cloud of dark grey smoke smelling of exhaust fumes . the smoke lasted only 2 seconds before clean air began coming out again . following this , the packs would not cool below 30 degrees for the remainder of the flight even at full cold . after returning to the field , we received a €l pack autofail€ ? caution message as we pulled up to our gate . ( flight 3270 filed closed ) performed ops check of both packs . pressurized both packs in reference to amm 21-50-00 . rh pack ops check good . no defects with rh pack . performed gvi of rh pack area . no defects noted . " l pack autofail " continued to show . found b1 code # 211941 . upon further inspection , found hole in lh plenum . troubleshot abnormal smell in cockpit and cabin in reference to fim 21-21-00 and fim 21-22-00 . found smell to be coming from lh pack plenum hole . the smell coming from the plenum hole was similar to smell in cockpit area and cabin area . removed and replaced lh plenum in reference to amm 21-51-02 . b1 code was flagging the lh temperature control valve . removed and replaced lh temperature control valve in reference to amm 21-51-20 . removed and replaced lh pack-discharge temperature sensor in reference to amm 21-51-22 . performed ops check of lh and rh temperature control valves in reference to amm 21-51-20 . rh pack valve ops check good . " l pack autofail " message remained . performed ops check of air-conditioning distributio
left engine ingested bird on takeoff . takeoff aborted , aircraft returned to ramp . engine was cleaned , inspected , and ground run satisfactory . aircraft test flown and returned to service . ( x )
aircraft was not grounded : an emergency was declared into mia due to stabilizer trim failure with both autpilots on and off . flight crew also reported periodic speed trim failure light illuminated . the aircraft landed safely at mia without further incident . maintenance detected message 22-11125 and accomplished amm fim task 22-12-00 with no hard faults noted . also accomplished stabilizer trim and elevator position system tests per amm 22-11-00 and 22-12-00 with no faults note d .
ato - on takeoff roll at approx 50 kts fo saw air spd tape red . stopped a / c on rwy . returned to normal . cms showed adiru 1 fault . performed task and 3411-7002-ha2 airspeed discrepancy incidents . removed and replaced adiru # 1 per 34-12-34 . removed and replaced # 1 pitot probe per 34-11-15 . performed task 34-11-00 . low range leak check of principle pneumatic circuits and functional test of the altitude and airspeed data . task 34-13-00 . all tests passed . no faults noted . ok for service .
main cargo - over wing - floor board - has damaged and missing inserts - panel # 262gf sta 1159 , rbl 48 . fabricated new main cargo deck floor panel 262gf at sta 1159 per fedex drawing srz-25-005 and md11 srm 53-00-50-2r paragraph 4 . steps e-g .
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 will be submitted . * * ( open )
# 1 engine failure during to . rejected to at 135 knots . severe damage in turbine section found on post flight . both fire bottles were discharged after fire crew reported flames in turbine section [ 01 ] removed and replaced # 1 engine per mt 77 1-00-01 ; ref : ttg8q008qady br and gt ; br and gt ; removed and replaced both engine fire bottles per amm 26-21-01 ; ref : ttg8q00skarh ; [ 02 ] c / w rii requirements for this task
right center fuel pump inop , center rt pump did no operate after start of right a / c returned to block and maintenance grounded a / c.deferred system iaw mel 28-22-2a . for dispatch . ac flown to lim . performed ground fault interruptor ops test . found relay k10696 popped . upon reset of relay pump still inop . ( low press light ) per amm 28-22-00 . di # 46402 remains open performed reactivation of right center fuel pump iaw mel 28-22-2a . ops check good iaw amm 28-22-00 . this clears di 46402 . acft remains etops 180 . placards removed . ac returned to service
ship 180 -div / ifsd- diverted to lhr due to left engine compressor stall . flight crew shutdown engine on approach due to rising egt . corrective action : maintenance found metal in tail pipe , will require engine change . maintenance in progress . ( a008054 )
aircraft was grounded : an emergency was declared and an aborted take off was accomplished due to during take off roll at approximatley 20 knots , flight crew could hear and feel a compressor stall in the right-hand engine . flight deck ecam h ad messages for compressor vane fault , right hand engine stall and right-hand engine fail along with a fire indication . large flames could be seen by the passengers along the right wing . the flight crew followed ecam procrocedures and disch arged both fire bottles for the right engine to extinguish the fire . the aircraft taxied to the gate under its own power
aircraft was grounded : an emergency was declared and the aircrat returned to mia due to the flight crew reporting a gree n hyd sys reservoir low level ecam message in cruise along with a secondary ecam mesasges for green hyd sys engine 1 pu mp low pressure and green hyd sys low pressure . the flt crew accomplished qrh procedures to include gravity extension of landing gear . the acft landed safely at mia without further incident . on post flt insp , first officer noted hyd flui d draining from nr 1 eng pylon and green hyd sys resevoir empty . maintenance found the hydraulic pressure line elbow in th
pushed toga for takeoff and the no.1 engine would not make t.o . power . removed # 1 engine hmu , removed and replaced # 1 engine fuel pump package . r and r unit , hydromech ( 29-7321-9-0012 0485 ) . performed test 5 - power assurance check per amm 71-00-00-700-813-f00 . test pass , no faults noted .
elongated hole plate located bs 540 between rbl 45 to rbl 57 at center wing box . replaced plate located bs 54o between rbl 45 to rbl 57 at center wing box i.a.w . b737-700 srm 51-10-02 item 9 and dwg # 143a5246 sheet 16 ; rev - .
at100 kias crew reported audible rumbling from left engine with yaw effect followed by eicas display of engine paramete rs spooling down prior to left engine shutting down . crew rejected take off and landing was without incident . post fligh t crew briefed fuel conditioning lever / switch was on . conditioning switch selected off to secure the engine . kcvg air tr affic control dispatched emergency response services ( ers ) to taxiway . ers reported fire / smoke from engine core cowl a nd foamed engine . aircraft grounded for unscheduled maintenance and inspections .
acft had uncommanded yaw , continued after pressing stabilization cut off push button . landed at nearby airport without further incident . inspected all t / r linkage from nose to tail , without removing medical floor with no defects found . inspected drive shafting from aft of mgb to t / r gb , t / r and intermediate gearbox for security and oil , fuselage at tail boom area for corrosion , metal fatigue , cracks or any other irregularities , no defects found . inspected tail boom attach point all bolts and nuts secure . performed visual inspection of yaw csas components , found connector at yaw computer dirty . cleaned connection , re-installed connector , performed gnd runs with pilot acft performed normally .
rejected takeoff at 10 knots due to failure of left eng to accel erate 22-31-00 , both test pssed and no autothrottle fau lts . flt crew report : with autothrottle engaged both thrust levers note : autothottle reponded normally when toga switch was advanced normally but left engine was about two seconds slow to actived . accelerate causeing an assemetery problem . as precautionary performed both autothrottle servo loop system test ref amm acp test no . 4 on eng # 1 power acceleration / decelation ref task amm 71-00-00-720-801-n00 . no discrepancies noted . also , contacted jesy , at tomc a gave him a status
ship 3244 - atb - due to a ra 1 and gpws fault . systems are required for fca approach . corrective action : replaced gpws and ra1 transceiver . replaced all 4 ra antennas and gaskets and inspected all coax cables . ops check good . ( 4367006 )
during start / run-up , transponder would not display oat or da . removed and replaced # 2 adu iaw amm 34-11-00 , 4-1 . moc successfully completed .
aft l lav not flushing no motor sound lav switch was cycled several times to operate . ordered lav switch and will pass it to day shift supervisor . removed and replaced flushing switch ref amm 24-25- ops check good plackard removed ok for service .
aircraft was grounded : an emergency was declared on descent into clt due to a strong electrical smell , flight crew donne d oxygen masks and landed safely at clt without further incident . flight crew reported that the smell disappeared after engine shutdown . maintenance determined the source of the smell was due to the failure of the # 2 flight management and g uidance computer ( fmgc ) which was replaced per amm 22-83-34 . a satisfactory operational check was accomplished .
ground crew reports that the air conditioning panel access door wil not close / [ 01 ] removed and replaced air conditioning access door iaw b737 amm 52-49-01 .
aircraft was grounded : an emergency was declared on approach into dfw due to the flight crew reported recieiveing an lgc iu # 2 fault ecam message . the flight crew performed a go around and accomplished the checklist procedures and noted ther e was no computer reset available in the air . the flight crew reported that upon landing gear extension they had 3 green light and the aircraft landed safely at dfw where it taxied to the gate under its own power . maintenance found fault co de 32-31-71 for landing gear control interface unit ( lgciu ) # 2 and replaced it per amm 33-31-71 . a satisfactory operatio
replaced current limiter . removed and replaced left starter generator for precautionary per amm 24-30-20 sec 2a-b . operational check good . "
rh pack hi flow inhibit . ( p > t / s fim 21-51- task 875 and amp ; w / d 21-51 -- 21 / p > / p > rh flow control card m864 fault and nbsp ; / p > / p > and nbsp ; / p > / p > removed cleaned up and amp ; installed flow ctl card m864 and amp ; ops check rh a / c pack . sys ok per amm 21-51-00 / 808 / p > )
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 e ngine . the aircraft landed safely at pdx and taxied to the gate . maintenance replaced # 1 eng inbd thrust reverser upper blocker door latch iaw amm 78-31-19 , also replaced nr 1 eng inbd thrust reverser upper blocker door actuator iaw amm 7 8-31-41 . maintenance also found the # 1 engine thrust reverser hyd control unit dpi extended / tripped and replaced hyd co
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 unlo aded . fault isolated to apu battery and apu battery charger . removed and replaced apu battery and charger iaw b767 amm 2 4-31-04 / 05 . operational check good . general visual inspection of apu battery and charger wiring satisfactory iaw swpm 20 -10-06 .
pilot reported left engine lost fuel pressure when climbing through 7000 feet . crew noticed it was when the left fuel pump would cycle on automatically and the fuel pressure went into red arc accompanied by a 'low fuel pressure cas message' . maintenance inspected and determined the manifold air temp sensors to be at fault . both mat sensors were replaced with no further defects noted .
after amber and red gov light illuminated , myself and the crew could smell an electrical smoke odor . after landing and shutdown . arrived at aircraft , cleaned electrical connectors on fadec and nf sensor . gov light went out .