IAE PW1133G-JM
Service difficulty reports · 191
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2024062506466Oil System · low pressureAIR TURNBACK TO BOS, DUE TO LT ENGINE LOW OIL PRESSURE MESSAGE & IAW QRH SHUTDOWN ENGINE. REPLACED THE LT ENGINE.SDR YENA2024060300809Valve · failedFLT#44, LGW-JFK. (ETOPS)' REF LOG PAGE 3970765, ITEM 1 POWER PLANT ENGINEERING AFTER BSI OF #2 ENG REVIEW ADVISED ENGINE REQUIRES REPLACEMENT; REF DEFECT 3970767, ITEM 1 (REM/INS ENG 2 PER TC A320-71-00-51-400-802-1. TESTS OK. A/C OK FOR SERVICE) FOR REPLACEMSDR HALA20240520138Fire Loop · faultedETOPS - BTB ENG 1 FIRE LOOP A FAULT ILLUMINATED RIGHT BEFORE T.O. LOW SPEED ABORT. PERFORMED ENG #1 LOOP A WIRE CHK, CONTINUITY CHK OK. NO SHORTS TO GND. BITE CHK OF FDU #1 LAST LEG REPORT FOUND 26-12-00 CHK FDU ENG 1 CHAN B SUPPLY, 26-12-00 CHK FDU ENG 1 LOOPSDR DALA2024051405214Engine · vibrationSHIP 5037 -ATB- PERFORMED AN AIR TURN BACK FOR HIGH ENGINE VIBES ON THE NUMBER 2 ENGINE. CORRECTIVE ACTION: INSPECTED INLET, NO DEFECTS NOTED ON FAN BLADES. PERFORMED EEC SOFTWARE UPGRADE, PERFORMED VIBE RUN ALL INDICATIONS NORMAL. (LP 5341912)SDR YENA2024050600703Wire Harness · failedFLT#1620, BOS-LHR. (ETOPS) 'ENG 2 MINOR FAULT, REF TSM 73-31-00-810-811-A, INSPECTED WC08 HARNESS AND FOUND HARNESS DAMAGED AND EXPOSED WIRES. REMOVED AND REPLACED WC08 HARNESS-CORE (4094 KS) IAW AMM 73-21-68. OPS CHECK OK. MX-4 UPDATED. PLACARD REMOVED. MCC NSDR HALA20240506122Wire Harness · missingETOPS - ENGINE 2 ESN P770479 MISSING A LOOP HARNESS 4165KS AND MISSING A LOOP ELECTRIC RAIL ASSEMBLY. INSTALLED ENGINE 2 A LOOP ELECTRIC RAMP ASSY PER AMM 26-12-61. OPS CK GOOD.SDR HALA20240417100Fire Loop · shortedETOPS - ENG 1 FIRE LOOP A FAULT. FOUND WIRE HARNESS (4165KS) SHORTING TO GND 1.8M OHMS. FOUND WIRE HARNESS (4181KS WHT) SHORTING TO GND 1.2M OHMS. REMOVED AND REPLACED WIRE HARNESS. WDM 71-51-75 PAGE 3. PENDING OPS CHECK. PER AMM 26-12-61 & 26-12-61 FOR 4181KSSDR HALA20240417101Wire · shortedETOPS - ENG 1 FIRE LOOP B FAULT. FOUND WIRE HARNESS (41WD1) SHORTING TO GND 3.9M OHMS. FOUND DETECTOR (4WD1) SHORTING TO GND 5.2M OHMS. REMOVED AND REPLACED HARDWIRE (41WD1) PER WDM 26-12-07. REMOVED AND REPLACED ENG 1 PLYON LOOP B (4WD1) PER AMM 26-12-16-000-SDR HALA20240417102Wire · corrodedETOPS - FOUND CORROSION AND NICK ON ENG 1 FIRE LOOP A HARDWIRE (4182KS). REMOVED & REPLACED ENG 1 LOOP A ASSY. PER AMM 26-12-61-400-807-A. OPERATIONAL CHECK OK PER AMM 26-12-00SDR HALA20240415096Fire Loop · faultedETOPS - AFTER HPR ENG 2 FIRE LOOP B FAULT. FOUND PYLON RAMP ASSY NO GOOD AND 4002WD2 ELEMENT SHORTING TO GROUND. NEED TO BE REPLACED. REMOVED & REPLACED AGB 4002WD2 DETECTOR PER AMM 26-12-17. REMOVED AND REPLACED #2 ENGINE PYLON FIRE-DETECTOR RAMP ASSEMBLY PERSDR YENA2024041500517Pump · failedFLT#1621, LHR-BOS. (ETOPS) 'ENG #2 HYDRAULIC PUMP LEAKING; REMOVED AND REPLACED #2 ENG EDP REF AMM 29-11-51. OPS CHECK REQUIRED REF LOG PAGE 3970574, ITEM 1 (#2 ENG EDP OPS AND LEAK CHECKS GOOD PER AMM 29-11-51).'SDR HALA20240415093Fire Loop · faultedETOPS - ENG 1 LOOP A FAULT. REMOVED AND REPLACED ENG #1 AGB LOOP A DETECTOR (4002WD1) OER AMM 26-12-17. OPS CHECK GOOD. OK FOR SVCSDR HALA20240415094Control Unit · faultedETOPS - FUEL OVERFLOW PROT FAULT. FUEL IDG 1 COOL FAULT. (POSSIBLE FUEL LEVEL SENSE CONTROL UNIT 1). REMOVED & REPLACED FLSCU1. CONDITION SAME. REINSTALLED ORIGINAL COMPUTER. NEED FURTHER TROUBLESHOOTING/WIRE CHECKS PER TSM 28-46-00-810-812-A. REPLACED OVSDR HALA20240415095Fire Loop · faultedETOPS - ENG2 FIRELOOP A FAULT. REMOVED AND REPLACED ENG2 LOOP A FIRE HARNESS (4165KS) PER AMM 26-12-61. BITE TEST GOOD.SDR DALA2024041304393Seal · leakingAIRCRAFT 5014, DIRTY SOCK SMELL ON TAXI IN. CORRECTIVE ACTION: REPLACED FAN SHAFT COVER SEAL. COMPLIED WITH ECS CLEAN AND BURN OUT, NOT SMELLS NOTED. (LP 4179769)SDR 2024F00114Rotor · crackedDURING THE INSPECTION PHASE, A CRACK IS DETECTED IN A BLADE WITHOUT REPAIR IAW SP1100G-B-72-35-30-00A-310A-B. DO A VISUAL INSPECTION OF THE HIGH PRESSURE COMPRESSOR (HPC) ROTOR ASSEMBLY FOR SERVICEABILITY TABLE 10. HPC 8TH STAGE (IBR) ROTOR - VISUAL INSPECTIOSDR HALA20240410089Duct · damagedETOPS - #2 ENG PYLON ECS INTERFACE DUCT PN 636D0005-527 DAMAGED. INSTALLED #2 ENG ECS INTERFACE DUCT PER AMM 36-11-49. 17934 OPS LEAK CHK PENDING. LEAK CK COVERED IN CARD 321-72-HWI-02.SDR YENA2024040800501Controller · illuminatedFLT#33, BOS-CDG. (ETOPS) 'AIR BLEED MAINT MSG ( 36-00-00-C CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY AIR BLEED );UNABLE TO ACCESS BMC 2 MENUS TO TEST. NO OTHER CORRELATED MESSAGES ANYWHERE. REMOVEDSDR DALA2024040604137Oil System · overservicedAIRCRAFT 5004, FA'S REPORTED DIRTY FEET/SOCK ODOR ON FINAL APPROACH. PILOTS DIDN'T SMELL ANYTHING UNTIL PARKING AT GATE W/APU ON FOR 3 MINUTES BEFORE TURNING APU BLEED ON. SMELL SEEMED TO HAVE DISSAPATED AFTER A FEW MINUTES AND COMPLETELY DISSAPATED AFTER APU SDR HALA20240405086Seal · leakingETOPS - DURING WALK AROUND, FOUND OIL SEEPING FROM EN1 S/N: P770687 INLET CONE. UPON INSPECTION, FOUND OIL INSIDE INLET CONE. REMOVED & REPLACED FAN SHAFT COVER SEAL PER AMM 72-15-00-960-801-A. NO LEAKS NOTED POST IDLE RUN. OK FOR SERVICE.SDR DALA2024040304048Oil System · overservicedAIRCRAFT 5022, AFTER SHUTTING DOWN ENGINES AT THE GATE AND TURNING ON APU BLEED SMELLED FUMES. CONFIRMED FUME SMELL FROM AFT FLIGHT ATTENDANDS SAYING IT SMELLED LIKE CHEMICALS. TURNED OFF APU BLEED. SMELL SEEMS TO HAVE DISPATED AFTER APU BLEED OFF. CORRECTIVE SDR HALA20240327077Packing · leakingETOPS - HYD LEAK COMING FROM LH AFT DRAIN MAST. REMOVED AND REPLACED PACKING ON # 1 ENG HYD PUMP PRESSURE SWITCH PER AMM 29-11-17, OPS AND LEAK CHECK OKAY.SDR YENA2024032600468Engine · odorFLT#169, JFK-PUJ. 'DURING DESCENT THROUGH CLOUDS INFLIGHT REPORTED "DIRTY SOCK" SMELL MID TO CABIN TO AFT; DUE TO REPORT OF ODOR EMANATING FROM ENG 2 BLEED AIR, INSPECTION OF #2 ENGINE AND BLEED AIR DUCTS WAS ACCOMPLISHED IAW INFO NOTICE 2017-T015J, SECTION B1SDR DALA2024032503755Engine · contaminatedAIRCRAFT 5030, DIRTY SOCK SMELL INTERMITTENT THROUGHOUT FLIGHT. ISOLATED SMELL TO NR 1 BLEED TYPE 2 ON WORK CARD. WORKING THROUGH WORKCARD 7100-2018, FOUND WELLING ON INSIDE OF SPINNER OF ENG 1. REPLACED FAN INLET CONE PER A321 AMM 72-11. REPLACED FAN SHAFT CSDR HALA20240319070Shuttle Valve · faultedETOPS - ENG1 OIL SYSTEM FAULT ON ECAM AFTER SHUTDOWN AT GATE. PERFROMED TSM 79-33-00810840A- NO DECTS NOTED REPLACED SHUTTLE VLV PER AMM 79-21-15-000-801A- REPLACED MAIN OIL PRESS OIL SENSOR PER AMM 79-33-21-400-801 SWAPPED #1 AND #2 PHMU TO ASSIT TROUBLESHOOTSDR HALA20240226052Sensor · faultedETOPS - ECAM ENG2 OIL SENSOR FAULT. REMOVED AND REPLACED PHMU PER AMM 77-31-01. AND TROUBLESHOT PER TSM 79-35-00-810-806-A. OPS CHECK GOOD. NO FAULTS NOTED OK FOR SERVICE.SDR DALA2024022602633Engine · stalledSHIP 5014 -RTO- REJECTED TAKEOFF DUE TO LEFT ENGINE STALL ECAM MESSAGE AND NO THROTTLE RESPONSE. CORRECTIVE ACTION: REPLACED LEFT ENGINE. (LP 5728358, 0217862)SDR HALA20240207039Plug · missingETOPS - SAW A FEW DROPS OF OIL UNDER #1 ENGINE FAN COWL. FOUND LP05 OIL MANIFOLD DRAIN PLUG MISSING SCREW REF PIPC 79-21-49-01 ITEM 320 & 140 & 150. INSTALLED MISSING BOLT P/N: ST2601-06. NO LEAKS NOTED OK FOR SERVICE.SDR HALA20240108006Unknown · unknownDURING THRUST LEVER ADVANCEMENT, ENG 1 STALL MESSAGE APPEARED. MESSAGE CLEARED ITSELF WITHIN 2 SECONDS WHILE BRINGING THRUST LEVERS TO IDLE. PER INDICATED ENG 1 STALL MESSAGE. PILOT NOTED ALL ENGINE INDICATIONS NORMAL. POWER LEVER NOT AT TAKEOFF POWER @ EVENTSDR DALA2023121510277Unknown · unknownSHIP 5011 DURING WATERWASH ON ENGINE 1 FOUND W4 HARNESS DAMAGED/ CHAFING. CORRECTIVE ACTION: REPLACED W4 HARNESS PER A321NEO AMM 73-21. OPS CHECKS GOOD. (5072307)SDR DALA2023111309280Unknown · unknownSHIP 5016 -ATB- AIR TURN BACK DUE TO RIGHT ENGINE VIBES PEAKED AT 5.3 IN CLIMB. THROTTLE WAS RETARDED TO 70% TO COME BELOW 5.0 ON VIBES. CORRECTIVE ACTION: PERFORMED GVI AND BORESCOPE INSPECTIONS WITH NO FINDINGS. REPLACED AODV PER A321NEO AMM 79-21. OK FOR SESDR F3LA2023111300210Eec · malfunctionedDISCREPANCY: REFERENCE LOG PAGE 391597 ITEM ONE THIS IS AN SDR REPORTABLE EVENT FLT 2755 ENGINE EXPERIENCED AN ENGINE 1 FADEC FAULT LEADING TO AN IN-FLIGHT ENGINE SHUT DOWN DUE TO ERRATIC FUEL FLOW AND ENGINE 1 FUEL LEAK MESSAGE ON ECAM.. FLIGHT 2755 DIVERTED SDR HALA2023083100184Unknown · unknownETOPS - ENG2 FADEC SYS FAULT ECAM ILLUMIANTED FOR 5 SECONDS AND CLEARED. PERFORMED TSM 77-11-00-818-811-A TO (3) (D), CHECKED CONTINUITY AT WIRE HARNESS WO4, P63 AND P3. PINS Y-4,1,5. CONTINUITY CHECKED GOOD. SWAPPED PHMU 1+2 CONDITION SAME. RETURNED PHU 1+2 TSDR HALA2023083100186Unknown · unknownETOPS - ENG 1 FIRE LOOP A FAULT ECAM CAME ON DURING DEPARTURE. REMOVED AND REPLACED # 1 ENG FIRE DETECTOR ELEMENT IAW AMM 26-12-17-000-802-A. OPS CHECK NORMAL IAW 26-11-00.SDR HALA2023071200143Unknown · unknownETOPS - WHILE PERFORMING BORESCOPE, FOUND #2 IGNITER PLUG WORN. REMOVED AND REPLACED #2 IGNITER PLUG PER AMM 74-21-01. OPS CHECK GOOD, OK FOR SERVICE.SDR HALA2023061200123Unknown · unknownETOPS - DURING #1 ENGINE CHANGE FOUND DAMAGED FIRE DETECTOR HARNESS. REMOVED AND REPLACED FIRE DETECTOR HARNESS PER AMM 26-12-16. CHECK IS GOOD NO DEFECTS NOTED OK TO CONTUNE SERVICE.SDR HALA2023061200124Unknown · unknownETOPS - ECAM: ENG 2 FIRE LOOP A FAULT. PER TSM 26-12-00-810-881-A. REMOVED AND REPLACED ENG 2 FIRE LOOP A CORE DETECTOR PER AMM 26-12-17. OPS CHECK GOOD.SDR HALA2023040500080Blade · damagedETOPS - DMI 206748 - #2 ENG FAN BLADE POLY COAT PEELING. 0.25"X0.25" AREA - A. DEFERED PER AMM 72-11-03-220-805-A. REPAIR OR REPLACE IN 2600FC. TRANSCRIBED TO E1128-321-72-065 CLEARED MIC SHEET. ORIGINAL SUBMISSION DATE: 4/5/2023.SDR YENA2023032000268Bleed Valve · failedFLT#1124, LAX-JFK. (ETOPS) AIR ENG 1 BLEED ABNORMAL PRESSURE AT 26,500 FEET; HPV AND PRV CHANGED ON LOG PAGES 3569615. REMOVED AND REPLACED ENG1 BLEED HPV PER AMM REF 36-11-51 REF LOGPAGE 3569615, ITEM 2 (RAN ENG 1 AND 2 PER 71-00-00-860-323A. AND OPS CHKECK SDR HALA2023011700005Seal · damagedETOPS - RH ENGINE #3 BEARING SEAL (AFT) APPEARS DAMAGED. PHOTOS SENT TO POWERPLANT ENGINEERING. REMOVED AND REPLACED #2 ENGINE PER TASK CARD J321-72-HWI-02. OK FOR SERVICE.SDR HALA2022120900306Blades · damagedNR 2 ENGINE N2 VIBRATION AT 6.2 NEED TO ACCOMPLISH TSM 71-00-00-810-873-A PARAGRAPH 4.D. DURING BORESCOPE, FOUND LPT 3RD STAGE BLADES DAMAGED. PER POWERPLANT ENGINEER, MANUFACTURER EVALUATION, REQUIRES ENGINE REMOVAL. REMOVED AND REPLACED RH ENGINE S/N: P7714SDR HALA2022120100304Blades · damagedNR 2 ENGINE N2 VIBRATION AT 6.2, DURING BORESCOPE, FOUND LPT 3RD STAGE BLADES DAMAGED. PER POWERPLANT ENGINEER, MANUFACTURER EVALUATION, REQUIRES ENGINE REMOVAL.SDR HALA2022112100297Hpc · usedETOPS-DURING PDC FOUND #2 ENG LEAKING FUEL AT HPC PRIMARY STATOR VANE ACTUATOR. REMOVED AND REPLACED #2 ENG HPC PRIMARY STATOR VANE PER AMM 75-31-02-400-801-A. MECH 16488 / 21800. PENDING IDLE RUN / LEAK CHECK. COMPLETED IDLE RUN & LEAK CHECK PER AMM 71-00-00-SDR HALA2022111700293Egt Indication · false activationETOPS-ENG 1 START FAULT, ENG 1 EGT OVERHEAT. ENG 1 TAILPIPE FIRE. PERFORMED VISUAL EXAMINATION AFTER EGT OVERTEMP PER TSM 72-00-00-210-809-A MX FOLLOWING TSM, TEMP WAS SHOWING 783 DEG, FALLS OK WITH IN AMM CHART, CONTINUING WITH EXHAUST INSPECTIONS AND INGITIOSDR HALA2022111000291Igniter · failedETOPS-TSI # 002223 REMOVED & REPLACED ENG 1 IGNITER PLUG A PER AMM 74-21-01. OK FOR SERVICE.SDR HALA2022110400284Engine · stalledETOPS - ENG 1 STALL / SURGE ON THROTTLE UP, RETURN TO BLOCK. TROUBLESHOOTING PER TSM AND BORESCOPE INSPECTION ARE IN-PROGRESS.SDR HALA2022110200282Fadec · faultedETOPS-DURING ENGINE START ECAM "ENG 2 FADEC SYS FAULT" RESET IN ACCORDANCE WITH HAL MX ENG 2 FADEC REMAINED. TWO ENGINE STARTS ATTEMPTED PER MOC DURING TAXI ENG 1 STALL FOLLOWED BY ENG 1 FAIL. ACTIONED ECAM AND TAXIED TO GATE. PER TSM 73-21-00-810-878-A REMOVSDR YENA2022090700877Engine · vibrationFLT1966, GEO-JFK. HIGH VIBS N2 AS HIGH AS 5.0 N2 IN CRUISE MULTIPLE TIMES AND AS LONG AS 30 MINS, AIRFRAME SHAKE LIKE LIGHT TURB ENCOUNTERED. ENGINE REMOVED REF WO 1214951. ORIG SUB DATE 9/7/2022.SDR YENA2022082300813Engine · vibrationFLT#1825, FLL-LIM. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' AFTER TAKE OFF HAD AN ENGINE VIBRATION FOLLOWED BY HI VIBRATION ON ECAM FOLLOWED BY ENG 2 OVER TEMP ECAM, MESSAGES DISAPPEARED WHEN THROTTLES PULLED BACK TO CLIMB; NO MAINTENANCE REQUIRED AT THISDR HALA2022011200012Oil System · overservicedINFO TO MX ON DESCENT PASSING 5000' FAINT WET SOCK SMELL THROUGH AIR GASPRES. WENT AWAY AFTER A FEW MIN. FOUND ENG 1 OVER SERVICED BY APPROX 3 QTS. REMOVED EXCESS OIL FROM TANK. OPERATED ENG @ IDLE FOR FOR APPROX 5 MIN. NO SMELL. OK FOR SVC.
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