boeing/aviation-ner-BIO huggingface dataset:
crew reported a bird strike to the right engine cowl . maintenance visually inspected for ingestion into the engine and found no defects on fan blades . no further defects noted in accordance with the aircraft maintenance manual . aircraft was released for service .
supplemental information ( this submission is for typo correction of hala2022101800274 - typo correction to block 2.j flight number , 3.a aircraft serial number , total time , and total cycle , 5.e parts condition ) - performed tsm 71-00-00-810-854-apar , 4.a ( 1 ) to ( 3 ) step , performed borescope insp of hpc and lpc per step 4.a ( 4 ) to ( 5 ) , performed step 4.a ( 6 ) to ( 10 ) , no problem found . replaced vsv actuator per amm 75-31-02 , hp bleed valve per amm 36-11-51 , prv per amm 36-11-52 , leak check good . borescope hpc outer seals and inner air from stage 4 to 8 per amm 72-35-00-290-801-a , sent video to powerplant engineering . removed and replaced buffer air valve per amm 75-26-02 ( pn / sn off 1020923-1 / lsgca56044 , pn / sn on 1020923-1 / lsgcam2454 ) . leak check good.accomplished power assurance test per amm 71-00-00 system checked normal , ok for service .
flt 4175 - crew aborted takeoff after encountering a bird strike during takeoff roll . aircraft returned to gate without further incident . maintenance inspected aircraft iaw mm 05-00-00 . no damage detected . aircraft returned to service .
the flight crew reported that the co-pilots interphone was inop , continuous static was emitted from speakers and co-pilots oxygen mask microphone was inop during flight . the maintenance provider troubleshot and determined that the nr 2 radio management unit ( rmu ) was defective . the rmu was removed , and a repaired unit was installed . ops checks were satisfactory , and the aircraft was returned to service .
lax - bird strike reported to right nose area . maintenance accomplished bird strike inspection of aircraft . no damaged detected . aircraft returned to service . ( m )
kin / fll - flt jm 087 - on arrival , crew reported suspect of bird strike to the nr 2 engine . engine inspected and confirmed the nr 2 engine had sustained foreign object damage ( fod ) due to a bird strike . inspection iaw mm 72-00-00-200-006 where the nr 1 fan blade of the first stage fan assy was found damaged beyond limits . nr 1 and nr 19 fan blades were replaced , and a borescope inspection found no further damage . an engine run was also carried out . aircraft returned to service afterwards . ( x )
pilot report28.feb.2023 wo 16 '' 893 '' 219= and gt ; idg 2 oil press came out at approx 80 ktsduring take off roll ecam idg 2 oil press came out at approx 80 kts , as a result the take off was rejectedactions taken : 28.feb.2023 wo 16 '' 893 '' 219= and gt ; th is item is transfered to dmi mel 24-20-01-prov 2 w / o 16893219 was performed mel procedure 230-tsr-2023-02-641.02.mar.2023 wo 16 '' 893 '' 219= and gt ; iaw amm 24-21-51-000 / 400-040-b rev 63 , 01 feb 2023 was replaced idg eng rh . pending operational te st of the idg.02.mar.2023 wo 16 '' 893 '' 219= and gt ; iaw amm 24-21-00-720-041-a rev 63 , 01-feb-2023 operational test of the idg .
aircraft ws not grounded : an emergency was declared and the aircraft diverted to mem due to the flight crew reporting re cieving an ecam alert for the forward cargo door at fl370 . after descending to 10000ft , the ecam went out . cabin pressur e was normal throughout flight . no other cockpit indications . the aircrft landed safely at mem without further incident . * * supplemental report will be submitted * * ( open )
received lt aoa heat after take-off then received lt pitot heat , lt static heat and pitot base heat . performed qrh and message remained . c / w fim reset . system operates normal . *******aircraft removed from service****** noted by maintenance
mel 34-15 - auth # 070867m-c . in flight landing gear warning . ra 2 fail . orig aml pg 4947449 , item 1.-c / a-rar ra2 iaw amm 34-31-01 . ops check good . mel restored .
aircraft was grounded : an emergency was declared and the aircraft returned to jfk . during cruise an ecam message for ecg excessive egt temperature on engine # 1 and the flight crew shut the engine down . the aircraft landed safely at jfk withou t 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 .
jfk - flt 4613 - aircraft experienced birdstrike on left corner of windshield . completed birdstrike inspection and ferried aircraft to saw for fuselage structural repair between frame 1 and frame 5 , forward of captains windshield . maintenance installed new fuselage skin p / n 12041320065 , upper left frame 2 p / n 12001897001 , and repaired stringer p / n 12041320043 4l iaw emb srm 51-40-02 , 53-00-00 fig 201 . aircraft was returned to service . ( m )
nr 2 pylon aft fairing , aft bulkhead , left and right attach angles aregouged . the airplane was grounded .
event : on 31 may 2023 , garuda indonesia aircraft pk-gmu as ga-607 sector mdc-cgk , during cruise , aircraft experienced engine # 1 severe damage at fl 220 . pic decided to air turn back to sta . mdc . action : 1 . do visual check engine 1 found some turbine blade was damage . a / c declare aog due to waiting spare engine for replacement . 2 . perform replacement of eng # 1 ref amm task 71-00-02-000-801 f00 and task 71-00-00-400-801-f00 . rev 80 , feb 15 / 2023 . engine spare taken from pk-gfx . pn cfm56-7 sn in 962784 sn out 960609 . 3 . perform engine depreservation not more than three months . ref amm task 71-00-03-600-816-f00 . rev 80 , feb 15 / 2023 . continue action 4 . eng # 1 ground run up to take off power for leak check and eng parameter check after eng replacement and eng depreservation result good . no leak found and all eng parameter normal . ref amm task 71-00-00-700-817 f00 . rev 80 , feb 15 / 2023 . fuel used 610kg , duration 32 minutes . 5 . eng # 2 ground run up to 64 % n1 for thrust balancing eng # 1 result good . no leak found and all eng parameter normal ref amm task 71-00-00-700-813-f00 . rev 80 , feb 15 / 2023 . fuel used 430kg duration 34 minutes . 6 . wac performed after eng # 1 severe damage at fl 220 result good ref amm task 05-51-42-210-802 rev # 80 , feb 15 / 2023 . 7 . a / c released after rtb b / d check performed ref mz 2-01 / b8-01 . 8 . a / c declared serviceable . preventive action continue the plan for hpt blades replacement for cfm56-7b engines . anticipate the hpt blades replacement planning for cfm56-7b engines when the replacement threshold ref sb 72-1082 is reached . cluster briefing to b737-800 pilots regarding hpt blade problem on cfm56-7b engines . notify b737-800 pilots to write down engine trend monitoring on aml .
( can ) vertical stabilizer to rudder middle hinge fitting ( # 3 ) corrosion at both lugs ( machine rib mounting ) ( tc # 20190627011 )
flt 730 - msy-phl - climbing through approximately 12,000 feet , cabin and cockpit started to fill with noxious fumes . packs were turned off , and fumes began to clear . returned to msy . found bird strike at intake right engine . inspected intake and exhaust and found no damage . performed inspection per md-80 mm 05-31-08 , pg 601 and 602 . ( m )
aircraft was grounded : an emergency was declared and the aircraft returned to dfw due to the flight crew reporting that on climb out the flight deck temperature climed as high as 102 degrees all controls were normal . no ecam indications . th e aircraft landed safely at dfw without further incident . maintenance replaced the pack zone controller 8hk per amm 21-6 3-34 and accomplished a satisfactory operational check .
unreliable nav information in flight between fo x ca mfd fms and gps-c / a-reset and performed opc check of fms / gps iaw amm 34-62-00 . opc check good . no faults noted at this time . found to be transitory condition . a / c ok for service .
aircraft was grounded : an emergency was declared and the aircraft returned to clt , on takeoff flight crew got an ecam e ngine 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 . * * supplemental report will be submitted * * ( open )
* * emergency declared * * on base vector at bwi level 2 slat disagree , accomplished lvl 2 check list ref aom , landed normal no unusual flight contorl positions . found # 4 slat position sensor loose . tightened sensor mount screws per amm 27-84- 03 . c / w test of slat position indication per amm 27-84-00-700-801 . ops check good . a / c ok for service .
te flap disagree message following selection of flaps 1 . flaps indicated up . completed qrh . declared emergency . landed flaps 20 . performed fim 27-51 ft 808 , no faults found . no overload inds were tripped on flap xmsns . flap control lev er moves freely when selecting each flap position . all flt deck inds normal and flaps move smoothly without binding or ab normal noise . no evidence of binding found on flap carriages , torque tubes , tracks / rollers , or ballscrews , gimbals . com pleted te flap sys lube iaw amm 12-21-09-3 . found water in inbd xmsn of lt inbd flap . found dirty oil in otbd xmsn of
aircraft was in the hangar for scheduled maintenance . aircraft was connected to gpu and powered up . during aircraft functions , the gpu auto shutdown several times and smoke was detected coming from the mec . aircraft electrical power was shutdown and the smoke was found emitting from a static inverter . the static inverter was removed and placed away from the aircraft in the open . a small flame was seen coming from the static inverter and a fire extinguisher was used to put out the flame .
crew acars message , during cruise left hydraulic quantity and pressure message displayed . diversion to kcof with emergen cy declaration . landing was uneventful with no additional precautionary actions . on arrival , aircraft grounded for unsch eduled maintenance . removed and replaced left engine , engine driven pump iaw b757 amm 29-11-05 . operational and leak ch ecks good . foreign object debris identified in hydraulic engine driven pump # 1 engine case drain filter system . all hyd raulic fluid from left engine driven pump system drained and replaced filter iaw b757 amm 29-11-17 . leak check go
aircraft was grounded : an emergency was declared and the aircraft diverted to tul . during cruise ecam message for fuel sed and fuel on board disagree . flight crew accomplished the qrh fuel leak procedures . during descent into tul , the firs t officer took a picture of ecam and it reflected fuel overland after clearing the initial ecam . the left main tank was about 1000lbs less then the right tank . the aircraft landed safely at tul without further incident . maintenance accompli shed tsm 28-11-00-810-805-a and the faults cleared with no additional faults or issues noted by maintenance . no specific
flt 407 phx-atl - diversion / burning smell - diverted into memphis due to strong burning plastic smell in cabin throughout climb and into cruise . maintenance found evidence of bird ingestion in nr 1 engine on stage 3 high pressure compressor . performed compressor wash iaw airbus maintenance manual 72-00-00-100-010 .
aircraft was grounded : an emergency was declared and the aircraft diverted to dfw due to the flight crew reporting that the weather radar system will not turn on nor display any data . flight crew reported that there hazardous weather on fli ght path . the aircraft landed safely at dfw and taxied to the gate under its own power . maintenance replaced the weather radar control unit and accomplished a satisfactory operational check per amm 34-41-12 .
aircraft was grounded : an emergency was declared , on approach to dfw the landing gear failed to extend and the crew perf ormed gravity extension per qrh . the aircraft landed safely at dfw and was towed off the runway . maintenance replaced le ft hand main landing gear door open proximity sensor 33ga per amm 32-31-71 ( aala202303214296 ) and replaced landing gear safety valve 49ga per amm 32-31-17 . ( aala202303215755 ) a satisfactory operational check was accomplished .
aircraft was grounded : an emergency was declared and the aircraft diverted to las . on takeoff from slc , flight crew hear d loud bang and brief shudder at 800 '' agl . # 2 engine had brief overtemp for 5-10 seconds , then returned normal . crew suspected bird strike and crew reported that all flight deck indications were normal for remainder of flight . the aircraft l anded safely at las without further incident . maintenance accomplished a birdstrike inspection and found no evidence of a birdstrike . a review of the dfdr data revealed the engine experienced an engine stall . * * supplemental report will be s
while extending the speedbrakes in flight with autopilot on , we experienced the left wing dip . the autopilot made corrections to the right with ailerons . also while using the speedbrake handle , it felt spongy . it felt smooth but as it got closer to the detent for fully extended position it felt like it want to move forward to the stowed position . performed spoiler power control unit pcu bungee rigging and found the rh # 7 speedbrake panel pcu bunjee out of rigging.adjusted the bungee rod as necessary until rigging pin was installed freely and the speedbrake travel was within limits . performed multiple satisfactory operational checks . all work performed in ref with amm 27-65-00 .
crew diverted to ord due to lose of " a " system hyd fluid debriefed pilot , stating that when hydraulic level reached 20 % , flight crew performed emergency checklist and shut of pump . reservoir is currently at 17 % . leak appears to be a burst l ine in lh mlg well . see attached photos . updated mh and gt . found pin hole leak in flex line to left main uplock acturat or . replaced hose ref amm task 20-10-52-400-801 . performed hydraulic power system activation amm task 29-00-00-800-802 f for system a . no leaks noted a / c ok to continue .
r 10 duct . warning in climb . ran qrh , msg extinguished within the 40 sec . returned to den . ( flight 5346 filed open )
sat comm lock up . grounded - yes . accomplished reset procedure per qrh . satcom restored normal .
pax door warning msg at fl370 . r / r aft baggage bay door harness iaw crj-amm-52-70-02 . ops checks good .
rh row 20 exit door , aft emegency threshold light is inop , relamped . op checks good . ref amm task 33-51-00-710-801 .
rto at 85 kts aircraft weight 249.000 . at time of rejected takeoff acp . high energy stop / heat damage condition inspectio n per amm 05-51-14 / 201 . no defect found . amber rev icon on lh epr gauge after takeoff thrust was set . left amber allumin ated after throttles were advanced for takeoff during take off roll amber light came on . per crewconversation . crew reje cts 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
aircraft was grounded : an emergency was declared and the aircraft returned to dfw due to the flight crew reported on cli mb out , they noticed hot air blowing into the flight deck . pack showed normal , but no pressure from engine one . the ecam alerts or indications other than 0 psi on bleed page for engine 1 . the aircraft landed safely at dfw without further inc ident . maintenance found a sense line severed on the # 1 engine and replaced the sense line per amm 36-11-49 . a satisfact ory leak / operational check was accomplished .
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 t back to and landed safely at tpa . accomplished tsi 0088379 , fim task 27-1-00-810-808 , fim task 27-21-00-810-811 , fi m task 27-31-00-810-801 evaluation and isolation procedures . no defects noted . dfcs operational test per amm 22-11-00-74 0-801 , no faults . dfdr download accomplished . high power assurance check per amm 71-00-00-700-813 , check good . condition
ship 3027 - div - to sdf due to lav smoke detect fault . crew declared emergency on landing . unable to reset message in f light . no indications of smoke / odor . corrective action : lav l and g both showing smoke detector faults . deferred each pe r mel and continued ; performed operational check of smoke detectors per 26-17 . operates normal at this time . ( lp # 426161 2 )
fuel imbalance caution occurred in cruise flight . flight crew executed appropriate checklist . fuel imbalancechecklist occurred again and appropriate checklist was executed again . the fuel began to show an imbalanceagain and at five hund red pound imbalance ac diverted to kabq . ( center tank fuel transfer system is suspectedcause ) corrective action performed bd500-a-j28-22-00-03aaa-320a-a center to wing xfer test . test passed , no defects noted at this time . ok for se rvice . this clears mel and all placards removed
aircraft was grounded : on takeoff lost n1 reference read out on displays , lost first officers flight director , and auto throttles failed . emergency declared ; flight returned to dfw landing safely . **supplemental report for aala202306153183 : maintenance found total air temperature ( tat ) probe signal fail . replaced tat probe per amm 34-21-06.** ( closed )
aircraft was grounded : an emergency was declared due to the flight crew reporting that yellow hydrailic system reservoir low level and yellow hydraulic system engine 2 pump low pressure messages displayed . flight crew accomplished ecam proc edures and landed safely at dca where the aircraft taxied to the gate under its own power . maintenance found the high pr essure line between the priority valve and the ptu leaking due to a damaged packing . maintenance replaced the packing an d accomplished a satisfactory leak / operational check with no defects noted .
aircraft was grounded : an emergency was declared due to : weather radar fail on pilot and copilot side ; aircraft air inte rrupted back to and landed safely at dfw . removed and replaced weather radar transceiver . ground checked ok . per amm 34- 43-31 .
atb - # 2 engine failure occurred at 100ft after takeoff / / per airbus recommendation dossier reference 81029165 , performed inspection after engine failure per amm 05-51-26 , nacelle gvi per amm 05-34-00 , and additional checks of fire extinguishing system per amm 26-21-49 and 26-21-00 . all inspections and checks ok . need to do additional inspections due to eng # 2 ifsd event per airbus dossier reference 81029165 . maintenance is now closed . please refer to sdr # hala2022030300065
ship 9547 -atb / gear / de- the flight crew returned the aircraft to atl following a " right gear door open " indication and a " right gear unsafe " light on climb out . an emergency was declared by the crew . the gear position showed good down and locked indications and the landing and taxi to the gate was uneventful . corrective action : maintenance replaced loose and missing hardware on the " right gear door up lock mechanism and performed a successful gear extension and retraction . ( lp # 9963368 )
aircraft was not grounded : left tire # 5 tire pressure low . pilot declared an emergency for landing due to low tire press ure . aircraft landed without incident and was towed to gate . maintenance replaced main landing gear tire assy at positi on # 5 in reference to job card 78l70032002 .
aft cargo compartment sta 1400 lbl 12 to rbl 6 frame has corrosion as marked . removed and installed new frame as per bac dwg 146n1011 rev e and srm 51-40-02 step 4b .
aircraft was grounded : an emergency was declared and teh 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 will be submitted * * ( o pen )
aircraft was grounded : an emergency was declared and the aircraft diverted to lax due to the flight control slats fault while requesting flaps at 225k . flaps and slats did not extend . flight crew performed qrh proced ure for landing . the aircraft landed safely at lax and taxied to the gate under its own power . * * supplemental report wil l be submitted * * ( open )
aircraft was grounded : an emergency was declared and the aircraft diverted to clt . flight attendants reported a fuel sme ll near rows 14-16 . also reported as a musky smell . flight crew went on oxygen and diverted to clt where the aircraft la nded safely without further incident . maintenance accomplished smoke odor fume trouble shooting task card 09l0002101 was complied with . inspection of apu compartment was also performed . no signs of leaks noted . engines were ran up to high p ower for 20 mins . no abnormal smell noted . although walking through rows 14-16 a personal can of pepper spray was found .
atb - air turn back due to unreliable airspeed - bug in pitot tube . found bug in f / o pitot probe ( 9da2 ) cleaned and flushed pitot probe per amm 34-10-00-170-004-a . ok for service .
crew reported rejected takeoff due to bird strike . inspected brakes no damage noted . brake temps did not exceed 410 degr ees f . performed bird strike inspection per amm 05-51-14 / 601 . no damage to aircraft noted , only bird strike evidence was to fo window . cleaned debris from fo window . ref task 05-51-14-200-803-a.ok for continued service , no further action re quired . ref 05-51-16-200-001-a .
aircraft was grounded : an emergency was declared comming into the scheduled destination of aua . at fl 330 green hydraul ic system quantity indicated zero . flight crew ran ecam and turned off green pump . turned back on for gear extension an d gear extended normally . indication is well below normal range . the aircraft landed safely at aua without further incid ent . maintenance found the engine driven hydraulic pump on # 1 engine leaking and replaced it per amm 29-11-51 . a satisfa ctory leak / operational check was accomplished .
ship 9538 -atb / gear / de- the aircraft was returned to the departure airport after the landing gear would not retract afte r takeoff . the flight crew declared an emergency with atc . the landing was uneventful . corrective action : maintenance di scovered the ground sensing mechanism was out of adjustment . after being re-adjusted the ground sensing system check goo d and all gear swings were normal . ( lp # 4294462 )
rows 16 and 12 h / k emergency lights out . performed troubleshooting iaw b767 amm 33-51-00 . found lamps to be burned out . corrective action - replaced lamps iaw amm 33-51-05 . performed ops test iaw b767 amm 33-51-00 . lamp test passed . not e : aircraft was in maintenance check at the time the issue was found . faa pmi has been notified .
during configuration for landing , landing flaps stopped at 5 degrees . attempted to select flaps 15 degrees , but only got 5 degrees flaps . trailing flaps disagree checklist completed . emergency declared . extended flaps to 15 degrees with alt ernate flaps switch . landed flaps 15 degrees . no flap assymetry observed . grounded - yes . performed fseu bite no existin g faults or history fault logged ref 27-51 task 801.kask 45851 per crew debrief : gross landing weight 132,000 lbs , brake s on speed 120kts , pressure altitude 415ft , oat 48 degrees f , autobrake 2 , thrust reversers deployed . pilots did not cat
during climb a hard bird strike down the lt side occurred . the lt engine experienced a vibration spike of 1.4 n-3 . retarded throttles and vibrations ceased . noted evidence of core ingestion in the nr 1 engine . performed inspection card 05-96-14 and found nr 1 eng missing annulus strip , missing at 11 o’clock position , scheduled for replacement . performed vibration survey test nr 6 and test nr 5 iaw amm task 71-00-00-715-327-ro3 . sys checked normal .