IAE PW1133G-JM

Service difficulty reports · 191

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'PW1133GJM'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR YENA2022011900020Ignition Switch · failedFLT #20, LHR-JFK. ENG 1 HUNG START; REMOVED & REPLACED IGNITER PLUG FOR IGNITION A ON #1 ENG. ENGINE RAN 3 TIMES ALL SUCCESSFULLY PER AMM 74-21-01. OK FOR CONT SERV REF AMM 71-00-00 FOR RUNJan 10, 2022 · N4058J · Airbus A321271N · Spark Plug/IgniterSDR YENA2022011800015Engine · false indicationFLT # 20, LHR-JFK. HUNG START ENG 1 ; PERFORMED TSM 71-00-00-810-865-A. NO FAULTS FOUND. NO MESSAGES GENERATED AFTER ENGINE STARTS. OK FOR CONT SVCJan 8, 2022 · N4058J · Airbus A321271N · Engine (Turbine/Turboprop)SDR YENA2022011800016Engine · hot startFLT# 20, LHR-JFK. HOT START NO INDICATION EGT OVERTEMP NO INDICATION AVIED BY AC TO THE LEFT THAT ENG 1 ON FIRE TAIL FOLLOWED BY INITIAL. ON FIRE INDICATION, FIRED BOTTLE ; REF LOGPAGE 3277496 ITEM #1 INSPECTION OF THE ENG #1 AFTER FIRE, CONT. TASK 72-00-00-21Jan 8, 2022 · N4058J · Airbus A321271N · Engine (Turbine/Turboprop)SDR YENA2022011800017Engine · hot startFLT# 20, LHR-JFK. HOT START NO INDICATION EGT OVERTEMP NO INDICATION AVIED BY AC TO THE LEFT THAT ENG 1 ON FIRE TAIL FOLLOWED BY INITIAL. ON FIRE INDICATION, FIRED BOTTLE ; REF LOGPAGE 3277496 ITEM #1 INSPECTION OF THE ENG #1 AFTER FIRE, CONT. TASK 72-00-00-21Jan 8, 2022 · N4058J · Airbus A321271N · Engine (Turbine/Turboprop)SDR YENA2021120600828Sensor · failed(ETOPS) FLT # 44, LGW-JFK. ENG 2B-0448-N1 SPEED SNSR FAIL ; RAR ENG#2 N1 SPEED SNSR IAW EMM TASK 77-11-21-520-000. PERFORMED OPS CHK BY ENG#2 IDLE RUN IAW AMM 71-00-00. OPS CHK GOOD. NO FAULTS PRESENT. RAR SNSR PER MCC JAIME #17939 REQUESTDec 5, 2021 · N4058J · Airbus A321271N · Engine Pressure Ratio (EPR)SDR YENA2021111000750Sensor · failedFLT 2824, LAX-JFK. ENG FADEC 1 CAME ON INFLIGHT FOR ABOUT 3 MINUTES. NO OTHER UNUSUAL PARAMETERS; PERFORMED TROUBLESHOOTING PER TSM 77-11-00-710-057-A NO FAULTS FOUND. NO MAINTENANCE MESSAGE ON MCDU EXAMINED HARNESS. NO FAULTS FOUND. OK FOR CONT SVC. TROUBLESHOct 26, 2021 · N4058J · Airbus A321271N · Engine RPM Indicating SystemSDR HALA2021051100061Igniter · faultedETOPS - ENG START 2 FAULT. ENG 2 IGN A FAULT. SUCCESSFUL AUTOSTART AFTER SECOND ATTEMPT. BTB// REMOVED AND REPLACED IGN PER AMM 74-21-01-00-801-A ON #2 ENG. OPS CHECK GOOD. OK TO CONTINUEMay 7, 2021 · N202HA · Airbus A321271N · Engine Oil CoolerSDR HALA2021042600050Sensor · defectiveETOPS - ENG 2 OIL SYS FAULT ON ENGINE SHUTDOWN. PERFORM TSM JOSV 79-21-00-810-822-A. REMOVE AND REPLACED MAIN OIL PRESSURE SENSOR PER AMM 79-33-21-000/400-801-A, OPS CHECK OK. OK FOR SERVICEApr 25, 2021 · N223HA · Airbus A321271N · Engine Oil PressureSDR HALA2021042600051Oil System · contaminatedETOPS - ENG #1 OIL CHIP DETECT. PERFORMED TSM 79-35-00-810-808-A, FOUND NO CONTAMINATION ON CHIP DETECTORS. PER POWERPLANT ENGINEERING REPLACED OIL FILTER ELEMENT PER AMM 79-21-06-960-801-A AND REPLACED ENGINE NR1 OIL PER AMM 79-00-00-610-802-A. PERFORMED ENApr 25, 2021 · N220HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2021040500041Screw · failedETOPS - SCREW SNAPPED IN LH ENG OIL CONTROL MODULE // REMOVED STRIPPED FASTENER AND HELICOIL, REPLACED PER AIRBUS 321 AMM 70-24-00-910-803-AApr 4, 2021 · N220HA · Airbus A321271N · Engine Oil System (Airframe Furnished)SDR HALA2021020800013Balance Weight · out of balanceETOPS - #2 N1, HIGH VIBRATION DURING FUNCTION TEST. AMM 71-00-00-710-807-A // REMOVED AND INSTALLED FAN TRIM BALANCE (CA) WEIGHTS AT LOCATIONS 11,13,15 AND 19 AND C2 WEIGHT AT LOCATION 17 (5897) FUNCTION TEST (FAN TRIM BALANCE) PENDING. PERFORMED #2 ENG FUNCTFeb 5, 2021 · N226HA · Airbus A321271N · Turbine Engine Air Inlet SectionSDR YENA2021012900079Engine · fireFLT 1710, PAP-FLL. RETUNRED TO FIELD. EMERGENCY DECLARED. ENGINE 2 FIRE, HI EGT TEMP, BOTH FIRE BOTTLES USED. ENGINE 2 WAS SHUTDOWN AND QRH S-4 WAS ACCOMPLISHED. SUPPLEMENTAL INFORMATION TO FOLLOW.Jan 25, 2021 · N2029J · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2021011900006Flow Divider · looseETOPS, NR 2 ENGINE HAS FUEL LEAK. FOUND FUEL LINE FROM FLOW DIVIDER LOOSE, TIGHTENED LINE. GROUND RUN AND LEAK CHECK OK. OK FOR SERVICE.Jan 18, 2021 · N226HA · Airbus A321271N · Engine Fuel DistributionSDR YENA2020121700605Engine · warning messageFLT 262, SJU- BOS. RETURNED TO FIELD. EMERGENCY DECLARED. JUST AFTER LEAVING OFF AIR CRUISE ALTITUDE RECEIVING ECAM ENGINE 2 HEAT SYSTEM FAULT. THIS WAS IMMEDIATELY FOLLOWED BY MASTER WARNING LIGHTS AND ENGINE 2 OIL LO PR ECAM WARNING. THE NR 2 ENGINE WASDec 13, 2020 · N2029J · Airbus A321271N · Engine Indicating SystemSDR HALA2020112000210Exciter · defectiveETOPS DMI NR 202688 BTB. ENGINE 2 IGNITION A FAULT (IGNITION SYSTEMS PW ENGINES SYSTEM A (EXCEPT FOR ER OPERATIONS, MAY BE INOPERATIVE ON ONE ENGINE ONLY)). PERF TSM 74-00-00-810-931-A. REMOVED AND REPLACED IGNITION EXCITER, PER AMM 74-11-01. OPERATIONSS CNov 18, 2020 · N212HA · Airbus A321271N · ExciterSDR HALA2020091430181Blade · damagedNR 4 FAN BLADE ON NR 2 ENGINE S/N JB1AEA4305 MISSING POLYURETHANE COAT. REMOVED AND REPLACED NR 4 FAN BLADE, PER AMM 72-11-03-400-801-A. FUNCTIONAL TEST FAN TRIM BALANCE AMM TASK 71-00-00-710-807-A PENDING. PERFORMED FUNCTION TEST (FAN TRIM BALANCE), PER AMSep 13, 2020 · N213HA · Airbus A321271N · Turbine Engine Air Inlet SectionSDR HALA2020080400167Panel · leakingETOPS SIGNIFICANT SYSTEM - DURING CRUISE ECAM AIR ENG 2 BLEED LEAK. THIRD WRITE UP TODAY. FOUND GAP CLEARANCE OF OVER PRESSURE FLAP DOOR ON PANEL 423DT. REWORKED PRECOOLER PANEL 423DT #2 PYLON PER TASK CARD E105-213003-INI. REPLACED PANEL AND CLEARANCE CHEAug 3, 2020 · N213HA · Airbus A321271N · Compressor Bleed ValveSDR HALA2020060500121Valve · malfunctionedETOPS SIGNIFICANT SYSTEM. ENG 1 TURB COOL FAULT. PERFORMED DRY MOTOR OF ENG NR 1 PER AMM 73-21-00-710-809-A. PER MOC NEED TO CHANGE ACC VALVE. REMOVED AND REPLACED NR 1 ENG ACC VALVE PER AMM 75-24-01-400-801-A. PENDING OPS CHECK. OPS AND LEAK CHECK GOOD Jun 4, 2020 · N215HA · Airbus A321271N · Engine Cooling SystemSDR HALA2020031100059Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB - ECAM: ENG 2 FADEC SYS FAULT FOLLOWED BY ENG 2 MINOR FAULT OIL CHIP DETECTED. // INSTALLED NEW PHMU ON #2 ENG, CONDITION SAME. RE-INSTALLED ORIGINAL PHMU PER AMM 77-31-01. REMOVED AND REPLACED #2 EEC PER AMM 73-21-01. LAND TEST Mar 10, 2020 · N227HA · Airbus A321271N · Fuel Control/Turbine EnginesSDR HALA2020030600052Engine · overservicedFLIGHT CREW REPORTED THAT DURING DESENT THERE WAS DIRTY SOCKS SMELL IN THE CABIN//PERFORMED TSM71-00-00-810-847-A FOUND #1 ENGINE OIL OVER SERVICED DRAIND OIL TO CORRECT AMOUNT REF AMM 79-00-00-610-801 PERFOMED IDLE RUN REF AMM 71-00-00 BOTH PACKS OPERATED NO Mar 5, 2020 · N228HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2020022700044Chip Detector · false indicationETOPS SIGNIFICANT SYSTEM- AFTER LANDING: ECAM ENG 1 OIL CHIP DETECTED. // PERFORMED TSM 79-35-00-810-808-A "CHIP DETECTED ALERT BY ODM" NO METAL DEBRI FOUND. OK TO CONTINUE. REMOVED AND REPLACED OIL FILTER PER AMM 79-21-06-960-801-A. PERFORMED IDLE RUN LEAK CHFeb 26, 2020 · N208HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2020011700016Engine · vibrationATB, NR 2 ENGINE. HIGH VIBRATION. IFSD. REMOVED AND REPLACED THE NR 2 ENGINE.Jan 17, 2020 · N217HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2020011500015Engine · vibrationETOPS SIGNIFICANT SYSTEMS - ECAM ENG 1 - ENG VIB. BTB. NR 1 ENGINE REPLACEMENT. REMOVED NR 1 ENGINE S/N P770609 AND INSTALLED NR 1 ENGINE S/N P770677, PER W/O 172866 TASK CARD J321-72-HWI-02.Jan 11, 2020 · N209HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR GTIA2019121644865Oil System · low pressureCRUISE FLIGHT WE RECEIVED MASTER WARNING OIL LEVEL LOW AND PROCEEDED TO SHUT DOWN #2 ENGINE AS DIRECTED BY ECAM. OIL PRESSURE WAS READING 2 PSI. AIRCRAFT DIVERTED TO RNO--Dec 14, 2019 · N917NK · Airbus A320271N · Engine Oil PressureSDR HALA20191106470Engine · damagedATB- ENG 1 COMPRESSOR STALL (LOUD BANG), POWER LOSS, FOLLOWED BY HIGH ENG 1 VIBS. IN MIDDLE OF HIGH VIS QRH, ENG 1 FAILED FOLLOWED BY ECAM ENG 1 FAIL. // REF W/O 167588 REMOVED AND REPLACED #1 ENG PER T/C J321-72-HWI-02. OPS AND LEAK CHECK GOOD. OK FOR SERVICENov 3, 2019 · N214HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2019110600466Engine · stalledSUP - ATB- ENG 1 COMPRESSOR STALL (LOUD BANG), POWER LOSS, FOLLOWED BY HIGH ENG 1 VIBS. IN MIDDLE OF HIGH VIS QRH, ENG 1 FAILED FOLLOWED BY ECAM ENG 1 FAIL. // REF W/O 167588 REMOVED AND REPLACED #1 ENG PER T/C J321-72-HWI-02. OPS AND LEAK CHECK GOOD. OK FOR SNov 3, 2019 · N214HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2019091700377Engine · leakingECAM ENG. 1 CHIP DETECTED AFTER LANDING, STRANGE ODOR. DURING BOROSCOPE FOUND OIL LEAKING AT HPC STAGE 2. // ACCOMPLISHED #1 ENGINE CHANGE PER J321-72-HWI 02. OPS AND LEAK CHECK GOOD. VERIFICATION FLIGHT FOR #1 ENGINE CHANGES COMPLETED SATISFACTORY.Sep 15, 2019 · N215HA · Airbus A321271N · Turbine Engine Compressor SectionSDR HALA2019090300361Engine · malfunctionedSUP - ETOPS SIGNIFICANT SYSTEM - AT 4000 FT ON BASE LEG FOR 8L, DIRTY SOCK SMELL FILLED IN COCKPIT AND FIRST CLASS GALLEY, SMELL DISSIPATED ONCE ENGINES WERE SHUT DOWN. LT PACK FLOW CONTROL VALVE INOP FOR ODOR SMELL, (PACK FLOW CONTROL VALVES (AIRCRAFT WITH MOSep 3, 2019 · N218HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2019081900343Eec · malfunctionedETOS SIGNIFICANT SYSTEM - NR 2 ENG MINOR FAULT EEC INTERNAL FAILURE FROM SYSTEM TEST. REMOVED AND REPLACED EEC PER AMM 73-21-01 SECURITY AND OPS CHECK GOOD.Aug 18, 2019 · N212HA · Airbus A321271N · Fuel Controlling SystemSDR HALA2019081900344Metering Unit · malfunctionedETOS SIGNIFICANT SYSTEM - #2 ENG MINOR FAULT SYS TEST FAULTED PHMU. // REMOVED AND REPLACED PHMU PER AMM 77-31-01 OPS CHECK GOOD OK FOR SERVICE.Aug 18, 2019 · N212HA · Airbus A321271N · Fuel Controlling SystemSDR HALA2019081100388Engine · malfunctionedAFTER LANDING ECAM: ENG 2 OIL CHIP DETECTED. INSPECTED. INSTALLED NR 2 ENG IAW WO 162228 TASK CARD NO J321-72-HWI-02. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.Aug 11, 2019 · N212HA · Airbus A321271N · Engine Oil Distribution (Airframe Furnished)SDR HALA2019073000373Engine · making metalETOPS SIGNIFICANT SYSTEM - AFTER TOUCHDOWN ON LANDING ECAM: ENG 2 OIL CHIP DETECTED. PERFORMED INSPECTION OF MAGNETIC CHIP COLLECTORS PER AMM 79-00-00-281-802-A. FOUND FILINGS ON FBC CHIP DETECTOR AND MAIN OIL FILTER. CONTAMINATION OUT OF LIMITS. PW REP & ENGRJul 29, 2019 · N217HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2019031100111Rotor · damagedATB - NR 2 ENGINE SHUTDOWN DUE TO HIGH ENGINE OIL TEMPERATURE. IAW ENGINEERING, INSPECTED NR 2 ENGINE MAGNETIC CHIP DETECTORS AND MAIN OIL FILTER. FOUND SHAVINGS ON THE (1,1.5,2) BEARING CHIP DETECTOR. IAW AMM 79-00-00-281-802A. INSPECTED NR 2 ENGINE PMA ROTOMar 10, 2019 · N212HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2019022500062Compressor · leakingSOCKS SMELL ON DESCENT OUT OF 8000' ODOR STRONGEST OVER WING INTENSIFYING AT LANDING.// CONFIRMED ODOR COMING FROM #2 ENG WITH BOTH PACKS RUNNING REF. TSM 71-00-00-810-847 ACP'D TO STEP 5. NO CONTAMINATION FOUND. NEXT STEP BORESCOPE. ACCOMPLISHED TSM 71-00-00-Feb 22, 2019 · N202HA · Airbus A321271N · Turbine Engine Compressor SectionSDR HALA2018122400677Warning Light · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED WHILE ATTEMPTING TO START ENGINE #2.// PERFORMED CHIP DETECTOR INSP PER TSM 79-00-00-281-802A. NO FAULTS FOUND. CLOSED COWLS. RAN ENGINE, NO ECAM MESSAGE NOTED.Dec 22, 2018 · N213HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2018121000639Warning Message · false activationETOPS SIGNIFICANT SYSTEM - AIR ENG 1 BLEED FAULT DURING CLIMB OUT. ECAM ACTIONS ACCOMPLISHED. MX ADVISED TO RESET SYSTEM, OPS OK TO CONT.// NO ECAM MSG DISPLAYED ON ARRIVAL, OK TO CONTINUE.Dec 8, 2018 · N212HA · Airbus A321271N · Engine Bleed Air SystemSDR HALA2018120300624Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 IGN A FAULT ON LANDING. // PERFORMED OPS TEST ENG 2 IGN SYS A AND B PER AMM 74-00-00-710-802-A. OPS NORMAL. PERFORMED ENG RUN SWITCHING TO IGN B. NO CURRENT FAULTS DISPLAYED. OK FOR SVC.Dec 2, 2018 · N204HA · Airbus A321271N · Ignition Harness (Distribution)SDR HALA2018112000600Oil System · pressure lossOPEN - ETOPS SIGNIFICANT SYSTEM - AIRCRAFT DIVERTED TO NEAREST AIRPORT, DUE TO #2 ENG OIL PRESS LOSS IN FLIGHT. ENGINE WAS SHUTDOWN IN FLIGHT. // REMOVED AND REPLACED #2 ENGINE. OPS AND LEAK CHECK OK. OK FOR SERVICE. VERIFICATION FLIGHT COMPLETED SATISFACTORY.Nov 19, 2018 · N215HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018110500561Ignition Sys · faultedETOPS SIGNIFICANT SYSTEM - ENG 2 IGNITION A SYS FAULT DURING START.// PERFORMED IGNITER AUDIBLE TEST PER AMM 74-00-00-710-802-A. OPS CHK OK. PERFORMED TASK CARD E1128-321-74-004. OPS NORMAL. OK FOR SVC.Nov 4, 2018 · N209HA · Airbus A321271N · Ignition SystemSDR HALA2018102300538Bearing · failedETOPS SIGNIFICANT SYSTEM - IN CRUISE, ECAM MASTER WARNING AIR-BLEED LEAK. FOLLOWED ECAM PROCEDURE AND ECAM CLEARED. REMAINING ECAM: AIR ENG 1 AND 2 BLEED FAULT RIGHT COND HOT AIR FAULT, ENG 1 OIL CHP DETECTED. SMOKE SMELL DETECTED AFTER ENGINE NR 1 START// BOROct 21, 2018 · N213HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2018091500422Carbon Seal · damagedSUP - ETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE CHIP DETECTOR. FOUND AFT CARBON SEAL BAD. REMOVED AND REPLACED NR 2 ENGINE. OP'S AND LEAK CHECK OK.Sep 15, 2018 · N214HA · Airbus A321271N · Turbine Engine Oil System
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