boeing/aviation-ner-BIO huggingface dataset:
aircraft was grounded : fuel imbalance message amber displayed on right fuel tank indicator on climb out . leveled off at 7,000 , ran fuel imbalance procedure , took us to fuel leak procedure . fuel greater than 1000 lbs low . diverted to iad , and emergency was declared on landing fuel imbalance light went out showed 900 lbs off after single point pressure fueling and right main tanks were 8.50 fueler and crew noticed 250 pounds from right main tank transferred uncommanded to center tank . troubleshot per fim 28-21-00-810-813 . inspected and cleaned the check valves in the manifold . performed general visual inspection of the the manifold , checked ok . found number 2 tank and center tank fueling shutoff valves bad . removed and replaced number 2 tank ( aala202207119866 ) and center tank fueling shutoff valves per amm 28-21-51 .
during cruise flight , the pilot noticed the right engine oil pressure suddenly indicated 0 psi . the nearest airport was the destination airport approximately 30 miles away . the pilot did not observe any abnormal oil temperature , cylinder head temperature , egt , and manifold pressure , fuel flow and fuel pressure remained nominal . after approximately 10 minutes and approximately 7 miles from the destination airport , the right engine rpm began to decrease uncommanded and fuel flow decreased . the pilot feathered the right propeller , and shutdown the right engine and landed without incident . post flight inspection revealed a substantial amount of oil on the lower nacelle section of the right hand engine . further visual inspection isolated the source of the oil leake to be on the oil cooler outlet hose integrated metal fitting / angle . the hose and associated fitting had accumulated a total of 544 hours since new and 15 months since installation .
aircraft was grounded : an emergency was declared into hnl due to the loss of the green hydraulic system in flight . the f light crew accomplished a manual gear extension and landed safey at hnl without further incident . maintenance replaced p ylon hydraulic system pressure ssav line per amm 29-11-49 and accomoplished a satisfactory leak / operational check .
aborted take-off due to low fuel pressure master caution and fuel boost pump illuminated after setting take-off thrust
on removal of the apu fire bottle for scheduled weight check on gulfstream giv aircraft n936am work order sc23257 task 14.108 , it was noted to be empty . the engineer involved in the apu fire bottle removal informs the bottle was not discharged while undergoing maintenance .
*sdr filed open* fault - found main deck cargo zone temp sensor cover crack at sta 654+33 right side ( replace ) ok to work
on takeoff , heard a loud noise , upon landing , discovered nose of acft encountered bird strike . lt engine ingested bird causing damage to n1 compressor blades .
rejected takeoff due to uncommanded nosewheel deflection . reques t inspection . per flt crew , rto at approx 10 kts , ac ved ered right on takeoff ground time and labor hour information update only . spoke to pilots , said aircraft veered right im mediately after this item is marked for sdr reporting . roll . starting takeoff roll around 10 knots . taxi to and from run way was normal . inspected nose tires reference amm 32-45-00 , no defects noted . locked lp to confirm fim task 32-51 task 810 is fully complied confirmed that the fim task for this issue was accomplished . with and taxi checked . unlocking for
pilot made a pl for tail rotor chip light indication . performed inspection iaw msm 05-51-00 , 6-13 and amm 65-40-00 , 6-1 and figure 601 . found one small fine hair on the chip detector , defined as cat a . cleaned and reinstalled chip detector and performed a 20 minute ground run with no discrepancies noted .
aircraft was grounded : an emergency was declared and the aircraft returned to lax . at fl250 green hydraulic system reser voir overheat ecam message followed by a green hydraulic engine # 1 pump low pressure ecam message . flight crew followed ecam procedure for gear extension and recovered the green hydraulic system for landing . the aircraft landed safely at la x . maintenance accomplished tsm 29-11-00 and found the power transfer unt ( ptu ) was overheating and knocking . maintenanc e replaced the power transfer unit ( ptu ) per amm 29-23-41 and accomplished a satisfactory leak / operational check .
cabin door open amber cas : amber cabin door open cas message will not extinguish with door closed . amber door open light will mot extinguish with door handle down . no audible click when cabin door closed .
approximately 2 : 00 hours out of kont , past our etp , received lvl 1 crg flow fwd disag and single amber triangle in the lower fwd air synoptic page . while reviewing the qrh , 2-5 min after initial alert , crew received red cargo fire lower . complied with qrh and fire warning extinguished within 60 seconds . declared an emergency and diverted to land at t he nearest airport . discharged 2nd bottle . installed 5 serviceable cargo smoke detectors in fwd cargo compartment r ef amm 26-14-01-4 , all ops check good . as a precaution , also removed and replaced msc ref amm 31-42-01-4 , ops check good .
aircraft was grounded : an emergency was declared during descent into clt due the flight crew reporting that during cruis e 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 for aala202406262668 : maintenance accomplished tsm 73-00-00-810-866a and replaced the # 1 engine bleed pressure regulator valve control thermostat solenoid per amm 36-11-55 . a satisfactory leak / operati
crew reported after takeoff , during flap retraction we had a flap fail indication . no overspeed of the flaps . the indication of the flaps was stuck at 11 . crew returned to bjc with no further issues . corr action- mx found rh otbd flap roller and guide discrepancy . r and r 'd roller and guide all flaps ops tests checked good .
ingested large bird on approach to aku , shut-down engine and completed missed approach . diverted to scc and made uneventful landing . removed and replaced nr 1 engine .
aircraft was grounded : an emergency was declared and the aircraft returned to pei . flight reported a birdstrike to the # 1 engine that resulted in an inflight shutdown and indication of an engine fire . the flight crew discharged one fire bot tle and the engine fire was extinguished . the aircraft landed a pei safely without further incident and the aircraft tax ied to the gate under its own power . due to the extent of the damage the engine will be replaced . * * supplemental report for aala202305168654 : maintenance replaced # 1 engine per task card 26l4007100 * * ( closed )
# 2 eng would not start- n2 would not get above 15 % . crossbleed start also unsuccessful- n2 less than 15 % . grounded - yes . replaced # 2 eng starter ref amm 80-11-01 lk and ops ck good .
strong order of paint thinner at level off . complied with fumes checklist in qrh . used 100 % oxygen for remainder of fl ight . emergency declared . confirmed spill in d.g . container . ( entered for flight crew member 5148579 over phone . gmm : 03-4-200 met crew on arrival reviewed item , received emd spill form report . spill was contained in haz contain er , no spillage in aircraft . inspected main cargo deck floor no spillage . a / c ok to continue
ship 9567 -hyd / de- the flight crew noticed a loss of hydraulic fluid indication with the left system . the qrh was compli ed with and the left engine driven hydraulic pump was shutdown . an emergency was declared due to the loss of the left sy system hydraulics while on approach . the landing was uneventful . corrective action : maintenance replaced the left engine driven hydraulic pump , the left case drain , pressure , and return filters . also replaced the left inboard spoiler actuator strainer packing . the aircraft was returned to service . ( lp # 9415054 )
ship 6801 main cabin @ bs1280 existing repair has a gouge bewteen s9l and s14l . corrective action : accomplished repair o n frame sta 1280 str 10l to str 15l iaw er / a # 513680-14ad rev b section ii permanent repair . ( 1048926 )
on climb out , dcu a , dcu b , ap pitch control fail , ifis miscompare and ap fail . upon arrival of mx no fault was found . gained access to the fault history and verified there was a dcu channel b fault in the air with a fdr-1 modules bus inop message present during fault which triggered an a / p pitch trim fail message and pressurization 2 fail message . removed card from ares box and downloaded file for 8 / 03 / 23 to forward to team cj for evaluation . powered aircraft again to verify no faults are present at this time .
r / h lower horizontal fillet panel light surface corrosion at approx . station 2123 , longeron 33r . installed fabricated doubler iaw e.a.1-5330-t0373990 . blended out corrosion ref md11 srm 53-00-00-2r figure 202 sheet 03 . *major repair*
on initial takeoff when n1 / epr button pushed auto throttle disconnect eicas and lights low speed abort ( flight crew defe rred per mel 22-30-1a ) aircraft departed without further incident .
ship 650 smoke and fumes cockpit e11 cb popped . corrective action : found dme 1 interrogator bad-r / r no 1 dme per b757 amm 34-55-op test ok ref log 2605656 . ( 9405262 )
after t-off , gear slow to retract and recieved l / g doors not closed message left main gear door did not close.-verified mx procedures were followed , no damage or misalignment found on l / h mlg door . however found slack in lock wire ( fin 2517gm ) . r / r lockwire ( fin 2517gm ) iaw amm 32-12-00-040-006-a . ops chk good . no ecam faults , all indications gree , no defects at this time . item remains on dmi # 68636
flt # 8384 , mco-jfk . ( aircraft did an air turn back to mco ) '' dirty sock smell , very strong after t.o . upto fl330 would not go away , both pilot on oxy till door open ; found source of odor when # 1 pack is in operation . normal - no smell from p ack 2 . performed eng 1 -2 boro insp ref logpages 3867870 ( borescope insp . accomplished on rh eng . hpc 1 thru 8 iaw pw ma nual ch 72-35-00-00a-312a no oil stains or oil puddling found during borescope insp . ) and 3867872 ( ch eng lpc1 , lpc2 and lpc 3 boroscope insp . accomplished iaw pw manual 72-31-00-00a * 312a foundoil stain on lpc 2 weep hs ) . eng wash of # 1 eng
return to field , bird strike after takeoff . nr 1 engine inlet shows evidence of ingestion . inspected aircraft and nr 1 engine iaw garrett maintenance manual . no parts replaced , operational check good .
aircraft was grounded : an emergency was declared and the aircraft returned yellow hydraulic engine 2 system low pressure ecam in flight . flight crew observed hydraulic quantity as empty . maintenance found the hydraulic pressure line in the # 2 pylon leaking and replaced it . a satisfactory leak / operational check was accomplished . * * ( closed )