IAE PW1133GA-JM

Service difficulty reports · 579

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 = 'PW1133GAJM'
  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 YENA2025120901183Fuel Heater · failedFLT#724, LAX-JFK. (ETOPS), ENG 1 HEAT SYS DEGRADED ON LANDING WENT AWAY ON ENG SHUTDOWN ( HEAT SYS DEGRAD CAUTIONS ON ECAM E/WD ); IFPC REPLACED REF LOG PAGE 4384073 ITEM 2. (REMOVED AND REPLACED THE INTEGRATED FUEL PUMP & CONTROL (IFPC) IAW AMM 73-11-01-400-8Dec 6, 2025 · N2169J · Airbus A321271NX · Engine Fuel Indicating SystemSDR DALA2025120508884Spinner · leakingFUMES EVENT IN AFT GALLEY WITH STINKY SOCK SMELL BEGINNING AT TOP OF DESCENT WHEN THROTTLES PULLED TO IDLE. FUMES LASTED FOR 10 MINS & WENT AWAY WHEN THROTTTLES WERE INCREASE FOR APPROACH NO FUMES IN FIRST CLASS OR FLIGHT DECK SMOKE & FUMES. FOUND OIL WETTINDec 4, 2025 · N519DT · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025120508922O-Ring · leakingF/AS NOTED WET/DIRTY/PAINT SMELL IN FRONT AND AFT OF CABIN DURING DESCENT & LANDING BOTH FLIGHTS. NOTHING NOTED IN COCKPIT. ENGINE RUN CONFIRMED SMELL EVIDENCE OF OIL BEHIND SPINNER. REPLACED NBR 1 ENGINE FAN SHAFT COVER O'RING. (LP 8118618)Dec 4, 2025 · N531DA · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025120408851Spinner · leakingAIRCRAFT 5049, ON DESCENT BELOW - 5000', MODERATE VINEGAR SMELL. CONTINUED ON TAXI IN. NR 2 ENG SPINNER HAD OIL AT FAN SHAFT SEAL, LEAKING OUT OF SPINNER WEEP HOLE. REPLACED NR 2 ENGINE FAN SHAFT SEAL PER AMM 72-15, C/W LEVEL B ECS CONTAMINATION PER AMM 21-0Dec 2, 2025 · N549DN · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025120108745Spinner · contaminatedDIRTY SOCK SMELL REPORTED IN CABIN ON DESCENT. FOUND RESIDUE IN NBR 2 ENG SPINNER. REPLACED NBR 2 ENG FAN SHAFT SEAL IAW A321 AMM 72-11-01. (LP 8139172)Nov 30, 2025 · N550DN · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025120108746Inlet · contaminatedON APPROACH CREW REPORTED A CHEMICAL/OIL/SWEET BAKED GOODS IN COCKPIT AND CABIN. FOUND OIL IN NR 1 ENGINE INLET CONE. REPLACED FAN SHAFT COVER PACKING IN IAW WITH A321 AMM 72-15-00 AND PERFORMED WATER WASH. (LP 8118610)Nov 30, 2025 · N531DA · Airbus A321271NX · Turbine Engine Oil SystemSDR F3LA202512020334Oil System · leakingACFT WAS GROUNDED. ODOR OF HOT ELECTRIC MOTOR NOTICED INTERMITTENTLY AFTER LARGE POWER CHANGES. ODOR WOULD CLEAR AFTER 2 OR 3 MINUTES BUT WOULD RETURN DURING DESCENT. ACFT FERRIED TO DENVER FOR ENGINE 1 CHANGE. INSTALLED ENGINE REF NR 137289, 137285, 13728Nov 28, 2025 · N622FR · Airbus A321271NX · Turbine Engine Oil SystemSDR YENA2025120201168Fuel Heater · failedFLT 1224, LAX-JFK. (ETOPS), NR 1 ENG HEAT SYS DEGRADED AFTER LANDING. HEAT SYS DEGRAD CAUTIONS ON ECAM EWD. REF L/P 4526714, ITEM 1. REMOVED AND REPLACED IFPC PER AMM 73-11-01. OPS CHK OK, PERFORMED TSM 73-11-00-810-880-A. OPS CHECK OK. NO FAULTS NOTENov 28, 2025 · N2151J · Airbus A321271NX · Engine Fuel DistributionSDR YENA2025112801128Idg · failedFLT 133, BOS-SFO. (ETOPS), ELEC GEN1 FAULT ILLUMINATED IN FLIGHT RESETS WERE NOT SUCCESSFUL ( ENGINE DRIVEN GENERATOR CHANNEL (IDG, GCU, LINE CONTACTOR) IDG NOT DISCONNECTED ); PERFORMED OPS CHECK OF ENG 1 IDG IAW AMM 24-21-51. OPS CHECK GOOD , MDDR CLEARED, Nov 27, 2025 · N2169J · Airbus A321271NX · AC Generator-AlternatorSDR DALA2025112708679Seal · leakingFLIGHT ATTENDANTS SMELLED DIRTY SOCK SMELL FORWARD SECTION OF PLANE AFTER GEAR DROPPED. DISSIPATED SOON AFTER. FOUND OIL WETTING ON NR 2 ENG SPINNER. REPLACED ORING ON FANSHAFT COVER & INSTALLED FANSHAFT COVER IAW AMM 72-15. (LP 8139258, 8139260)Nov 26, 2025 · N549DN · Airbus A321271NX · Turbine Engine Oil SystemSDR YENA2025112601123Igniter · damagedFLT#2116, SFO-JFK. (ETOPS) "DMG FOUND TO LOWER IGNITER; REMOVED AND REPLACED LOWER IGNITER IAW AMM 74-21-01. OPS TEST OK."Nov 25, 2025 · N2169J · Airbus A321271NX · Spark Plug/IgniterSDR DALA2025111808411Seal · bypassingCABIN REPORTED " DIRTY SOCKS" FWD CABIN AND BURNED RUBBER SMELL AFT CABIN BRIEFLY ON BASE / FINAL TURN BEFORE LANDINGS. SMELL CLEARED AFTER A MINUTE OR TWO. FOUND NBR 2 FAN SHAFT SEAL BYPASSING OIL. REPLACED FAN SHAFT SEAL NBR 2 ENGINE PER A321 AMM 72-11-01.Nov 17, 2025 · N549DN · Airbus A321271NX · Turbine Engine Air Inlet SectionSDR DALA2025111808413Seal · leakingFAS REPORTED SMOKE/FUMES "STRONG DIRTY SOCKS SMELL" ON APPROACH. FA'S REPORTED SMELL DISSIPATED SHORTLY AFTER LANDING. FOUND OIL WETTING FROM BACK OF SPINNER ON #1 ENG. REPLACED #1 ENGINE FAN SHAFT COVER SEAL PER A321 AMM 72-15. LEAK CHECK GOOD AFTER ENGINE Nov 17, 2025 · N550DN · Airbus A321271NX · Turbine Engine Oil SystemSDR F3LA202511190326Engine · leakingFUME EVENT INITIALLY WAS SMELLED IN GALLEY FUME REMOVAL APPLIED AND WENT AWAY RETURNED IN AFT GALLEY. NR 1 FOR APU DEFERAL REF TSM 05-50-810-831-A PERFORMED APU INSPECTION TYPE 1 EVENT ON LEVEL A IAW AMM 49-00-00-200-811 FOUND SIGNS OF LEAKAGE PERFORMED IDLE Nov 16, 2025 · N646FR · Airbus A321271NX · Engine (Turbine/Turboprop)SDR DALA2025111608366Seal · leakingAIRCRAFT 5050, INBOUND FA, REPORTED FUME EVENT ON DECENT AND STATED DIRTY SOCK AND ROTTEN EGG ODOR. CORRECTIVE ACTION: FOUND LEAKING OIL SEEPAGE AT #2 ENG FAN SHAFT SEAL BEHIND SPINNER CONE. REPLACED FAN SHAFT SEAL REF A321 AMM 72-11-01. (LP 8139106)Nov 15, 2025 · N550DN · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025110908155Seal · leakingAFTER LANDING WHILE ON ENGINE BLEED. DIRTY SOCK ODOR IN COCKPIT. TURNED ON APU BLEED, ODOR WENT AWAY. REPLACED NR 1 AND 2 ENGINE SPINNERS AND FAN SHAFT COVER SEALS. (LP 8065770)Nov 7, 2025 · N549DN · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025110408054Packing · leakingAIRCRAFT 5049, AFTER LANDING ON LT + RT ENG BLEED AIR, DIRTY SOCK SMELL IN FLIGHT DECK. CORRECTIVE ACTION: FOUND OIL WETTING IN BACK OF SPINNER OF #2 ENG. #1 ENG AND APU INSPECTIONS NORMAL. REPLACED PACKING AND FAN SHAFT COVER. PERFORMED LEVEL B DECONTAMINATIONov 3, 2025 · N549DN · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025103007938Oil System · overservicedAIRCRAFT 5091, WHILE CLIMBING THROUGH FL 280- FL 300, FLIGHT ATTENDAT REPORTED "ROTTON EGG" SMELL DURING CLIMBOUT. CYCLING FROM PRESENT TO NOT PERSENT EVERY FEW MINUTES. EQRH STEPS TAKEN TO ISOLATE ODOR COMING FROM PACK 1. PACK 1 TURNED OFF FOR REMAINDER OF FLOct 30, 2025 · N591DT · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025102807906Seal · leakingAIRCRAFT 5035, FA'S REPORTED DIRTY SOCK SMELL LAST 15 MINUTES OF FLIGHT DURING DESCENT & LANDING. TRANSITIONED TO AN EXHAUST/BURNING FUEL SMELL. FOUND OIL ON ENG NR 2 SPINNER REMOVED ENG NR 2 INLET CONE PER A321 AMM 72-11 AND REPLACED SHAFT COVER SEAL PER A3Oct 27, 2025 · N535DN · Airbus A321271NX · Turbine Engine Oil SystemSDR YENA2025103001073Bleed Valve · failedFLT#1407, JFK-CDG. (ETOPS) "CLASS II ENG 1 FADEC FAULT; FOLLOWED TSM PROC 75-32-00-810-840-A REV 107 AFTER BITE TEST AS PER AMM 73-21-00-710-806-A REV 107 HAVE MESSAGE ENG 1A -0403-2.5 BLEED VLV TM ELEC FAIL CLASS1 NO DISPATCHABLE; 2.5 BLEED VALVE REPLACED IAWOct 27, 2025 · N4064J · Airbus A321271NX · Compressor Bleed ValveSDR DALA2025102707891Seal · leakingAIRCRAFT 5038, DIRTY SOCK SMELL ON DESCENT THRU 5,000'. PERFORMED SMOKE AND FUMES QRH. ISOLATED SMELL WITH PACK 1 OFF. SMELL ONLY IN FLIGHT DECK. CORRECTIVE ACTION: REPLACED NBR 1 ENGINE SPINNER SEAL IAW A321 AMM 72-15. PERFORMED LEVEL B TYPE 2 DECONTAMINATIONOct 26, 2025 · N538DN · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025102707895Seal · leakingAIRCRAFT 5039, SHORTY AFTER TAKEOFF FA SMELLED TO REPORT CHEMICAL/ELECTRICAL SMELL ALL PAX AND FS SMELLED IT. RAN SMOKE AND FUMES CHECKLIST SMELL DISAPATED AFTER PILOTS SMELLED ACRID SMELL FOR A MOMENT AS WELL. CORRECTIVE ACTION: T/S PER AMDS W/C 0550-2002 FOUOct 25, 2025 · N539DN · Airbus A321271NX · Turbine Engine Oil SystemSDR YENA2025102801062Wire Harness · failedFLT#31, BOS-AMS. (ETOPS) "REF LP # 4482219 ITEM #1 (REMOVED AND REPLACED ENG#2 EEC WIRING HARNESS W03 REF AMM 73-21-63. OPS CHK AND IDLE RUNS NORMAL NO FAULTS NOTED A/C OK TO RETURN TO SVC) ENG #2 FADEC FAULT; PFR SHOWS N2 SPEED SENSOR AS PRECAUTIONARY REMOVEOct 25, 2025 · N4073J · Airbus A321271NX · Engine Indicating System WiringSDR DALA2025102407780Oil System · leakingDIRTY SOCK ODOR AT 8000 FT ON ARRIVAL. LASTED TO GATE. APU OFF DURING FUME EVENT. FOUND OIL LEAK IN #1 ENG SPINNER, #2 ENG IS GOOD. REPLACED #1 ENG SHAFT COVER SEAL PER A321 AMM 72-15. (LP 7203500)Oct 23, 2025 · N534DT · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025102407781Oil System · leakingDURING DESCENT AROUND 11,000 FT AFTER SELECTING ENGINE A/ICE SWITCH ON A VERY LIGHT DIRTY SOCK SMELL CAME THROUGH THE COCKPIT AND CABIN. IT LASTED FOR APPOX 1 MINUTE THEN CLEARED. ACCOMPLISHED W/C 0550-2002 FOUND WETTING BEHIND NR 1 ENGINE SPINNER. REPLACED NOct 23, 2025 · N548DN · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025102207730Spinner · leakingDURING ARRIVAL, DESCENDING THROUGH 8000'. BOTH PILOTS NOTICED A DIRTY SOCK SMELL. FLIGHT ATTENDANTS CONFIRMED THE ODOR. BOTH PILOTS DONNED 02 MASKS. AFTER ARRIVAL, APU WAS STARTED AND NO ODOR NOTICED. FOUND NBR 1 ENG SPINNER WET WITH OIL. REPLACED NBR 1 INLEOct 22, 2025 · N531DA · Airbus A321271NX · Turbine Engine Oil SystemSDR YENA2025101601041Valve · faultedFLT#1178, LAS-BOS. (ETOPS) CR 2 ALERT (APPROVAL REQUIRED FOR RESOLUTION) ENG 2 TURB COOL FAULT AFTER LANDING ( TCC/TACC VALVE ); REMOVED AND REPLACED ENG 2 TURBINE CASE COOLING AIR VALVE IAW AMM 75-24-01. OPS CK GOOD. PLACARD REMOVED, MX-4 UPDATED, MCC NOTIFIOct 16, 2025 · N2193J · Airbus A321271NX · Engine Cooling SystemSDR HALA20251017321Pump · failedETOPS - Y ENG 2 PUMP INOP. REMOVED AND REPLACED NR 2 ENG. DRIVEN HYD. PUMP CONDITION SAME. ACCOMP. TEST OF PTU W/ENG. PUMPS PER AMM 29-23-00-710-004-A. ALL ENG.DRIVEN HYD PUMPS,ELECT HYD. PUMPS & PTU OPS NORMAL OK FOR SERVICE. SECURED NR 2 ENG.COWLINGS. P/N OFOct 16, 2025 · N216HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR F3LA202510180316Oil Cooler · leakingENGINE 2 FIRE ON TAKE OFF. SHUT ENGINE DOWN AND FIRE ALERT WENT AWAY. SPARKS AND SMOKE REPORTED SEEN BY FAS AND PASSENGERS. PERFORMED INSPECTION AFTER ENGINE WINDMILLING ON ENG#2 AFTER ENGINE IN-FLIGHT SHUTDOWN AND FOUND HARNESS CONNECTOR DAMAGE ON CONNECTOROct 16, 2025 · N671FR · Airbus A321271NX · Turbine Engine Oil SystemSDR HALA20251015319Rod · damagedETOPS - RETURN TO GATE AFTER ENG. START DUE TO ENG.1 BLEED FAULT. FOUND FAN AIR VALVE ACTUATOR ROD DAMAGED. REMOVED AND REPLACED ACTUATOR ROD PER AMM 36-11-54-400-803-A. OPS CHECK OF FAN AIR VALVE ACTUATION GOOD W/IDLE RUN. NO FAULTS NOTED. OK FOR SVC.Oct 14, 2025 · N226HA · Airbus A321271N · Pneumatic Distribution SystemSDR YENA2025101601038Warning Message · illuminatedFLT 1080, EDI-BOS. (ETOPS) CLASS 2 AIR AIR BLEED, CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1, FAULT INDICATED BY AIR BLEED; NO FAULTS OR ECAM MESSAGES UPON ARRIVAL TO A/C NO FAULTS IN PFR PERFORMED TSM 36-00-00-810-8Oct 14, 2025 · N2142J · Airbus A321271NX · Compressor Bleed ControlSDR DALA2025101207444Oil System · overservicedVERY MILD DIRTY SOCK SMELL ON ARRIVAL DESCENDING THROUGH HEAVY CLOUDS / MOISTURE. FOUND BOTH ENGINES OVERSERVICED. REMOVED EXCESS OIL. FOUND LIGHT OIL WETTING ON NBR 1 ENGINE. REPLACED FAN SHAFT COVER O-RING REF A321AMM 72-15. RAN BOTH ENGS. NO SMELL NOTED. Oct 11, 2025 · N548DN · Airbus A321271NX · Turbine Engine Oil SystemSDR HALA20251013313Fire Loop · faultedETOPS - ENG 2 FIRE LOOP A FAULT. REMOVED & REPLACED LOOP A FIRE HARNESS PER AMM 26-12-61. OPERATIONAL CHECK OK.Oct 10, 2025 · N220HA · Airbus A321271N · Fire DetectionSDR YENA2025100801012Wire Harness · failedFLT#72, EDI-JFK. (ETOPS) "ENG 1 FADEC SYS FAULT HAPPENED AT CRUISE FL 350; PERFORMED TSM 77-11-00-810-812A FOUND W04 HARNESS CHAFFED AT N2 SENSOR. REMOVED AND REPLACED W04 HARNESS REF AMM 73-21-64 FADEC SYSTEM TEST OK PERFORMED IDLE RUN REF AMM 71-00-00 ALL PAOct 7, 2025 · N2165J · Airbus A321271NX · Engine Fuel System WiringSDR HALA20251008308Fire Loop · faultedETOPS - IN FLIGHT, ENG 1 FIRE LOOP B FAULT. REMOVED AND REPLACED #1 ENG PYLON FIRE DETECTOR RAMP ASSY PER AMM 26-12-16. OPS CHECK GOOD. OK FOR SERVICE.Oct 7, 2025 · N216HA · Airbus A321271N · Fire DetectionSDR YENA2025100300997Seal · damagedFLT#1926, LGW-BOS. (ETOPS) "FOUND FUEL PUMP DRIVE OIL SEAL TO BE DAMAGED; REMOVED AND REPLACED FUEL PUMP OIL SEAL IAW ENGINE MAINTENANCE MANUAL 72-61-01-02A-920A-D."Oct 6, 2025 · N2169J · Airbus A321271NX · Engine Fuel PumpSDR DALA2025100707284Seal · leakingAIRCRAFT 5047, AFT FA'S REPORT "DIRTY SOCK" ODOR STARTED APPROX 5 MIN BEFORE LANDING AND STAYED CONSTANT UNTI LEFT ENGINE SHUT DOWN AT GATE WHEN IT STARTED TO DISSIPATE. SMELL WAS CONCENTRATED IN AFT GALLEY. NO SMELL NOTED BY PILOT. REPLACED ENG 2 FRONT SEALOct 6, 2025 · N547DE · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025100707283Sensor · faultedATB- AIR TURN BACK DUE TO LEFT ENGINE VIBRATION SHOWING 10.0-12.0 COCKPIT UNITS. CORRECTIVE ACTION: INDICATION ERRATIC AND FAULTED FWD VIBE SENSOR. PLACED N1 VIBE INDICATION ON MEL 77-00-02C. LATER, REPLACED FORWARD VIBRATION SENSOR ON NBR 1 ENGINE. (LP 737621Oct 6, 2025 · N532DN · Airbus A321271NX · Engine Vibration AnalyzerSDR YENA2025100300996Controller · failedFLT#1926, LGW-BOS. (ETOPS) "AFTER LANDING GOT ENG 2 HEAT SYSTEM DEGRADED CAUTION MSG; REMOVED AND REPLACED IFPC IAW AMM 73-11-01. LEAK AND OPS CHECK REQUIRED.(PERFORMED LEAK OPS TEST TL IFPC IAW AMM 73-11-01 LEAK K OPS NORMAL AT THIS TIME A/C IS OK FOR SVC.Oct 5, 2025 · N2169J · Airbus A321271NX · Engine Fuel DistributionSDR YENA2025100301009Wire Harness · failedFLT#287, BOS-LAX. (ETOPS) "( TCC/TACC VALVE ) ECAM MESSAGE ON TAXI IN. ENG 2 TURB COOL FAULT; UPON INSPECTION FOUND CHAFING/WIRE SHOWING ON "WC08" HARNESS. R/R "WC08" WIRE HARNESS IAW AMM 73-21-68-400-802-A. ALL OPS OK. VSV IFPC REQ OPS CHK DUE TO SYSTEMS DISTOct 4, 2025 · N2193J · Airbus A321271NX · Engine Bleed Air System WiringSDR YENA2025100300993Eec · failedFLT#224, LAX-LAX. (ETOPS) "ENG 1 FADEC SYS FAULT; PER TSM 73-21-00-810-870-A AND FAULT CONFIRMATION REMOVED AND REPLACED ENG #1 EEC. PERFORMED OPS CHECK WITH SATISFACTORY RESULTS, NO FAULTS NOTED. A/C OK TO CONT SVC."Oct 3, 2025 · N2165J · Airbus A321271NX · Fuel Controlling SystemSDR DALA2025100307194Seal · leakingFA'S REPORTED DIRTY SOCK SMELL ON APPROACH. DURING INSP FOUND OIL ON #1 ENG SPINNER. REPLACED SHAFT COVER SEAL REF A321 AMM 72-15. PERFORMED LEVEL B DECONTAMINATION AS PER A321 AMM 21-00-00-615-803-A, NO SMELLS NOTED. (LP 7574004)Oct 2, 2025 · N536DN · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025100307195Seal · leakingDECLARED EMERGENCY AFTER GETTING DIRTY SOCK SMELL ON DESCENT FOR PLANNED FUEL STOP IN SLC. DONNED MASKS. PERFORMED VISUAL INSPECTION OF BOTH ENGINES AND FOUND OIL LEAKING FROM BOTH SPINNERS. REPLACED FAN SHAFT COVER SEAL ON NBR 1 AND 2 ENGINES PER A321 AMM 7Oct 2, 2025 · N548DN · Airbus A321271NX · Turbine Engine Oil SystemSDR F3LA202510040308Seal · leakingFUME EVENT FROM FL 230 TO LANDING. ELIMINATION OF ODOR PROCEDURES UNSUCCESSFUL. MAINTENCE ACTION AS REFERENCED ON LOGPAGE LP674239, ITEM 1: PERFORMED TSM TASK 05-00-810-831-A TO IDENTIFY CAUSE OF ODOR. IDENTIFIED CAUSE TYPE 3 ENGINE 2. FOUND ENG 2 FAN SHAFT Oct 2, 2025 · N631FR · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025100107137Packing · leakingCREW REPORTED ODOR IN FLIGHT DECK ON DECENT AND EMERGENCY DECLARED. O2 MASK DONNED. 1 FLIGHT ATTENDANT REPORTED FEELING LIGHTHEADED. FOUND OIL BEHIND BOTH SPINNERS, REPLACED BOTH ENGINE FAN SHAFT COVER PACKING AND FOAM WASHED BOTH ENGINES PER AMDS WORK CARD Oct 1, 2025 · N538DN · Airbus A321271NX · Turbine Engine Oil SystemSDR YENA2025100200990Igniter · wornFLT#687, BOS-LAX. (ETOPS) ENGINE IGN 1 B FAULT ( IGNITION SYSTEMS B) SYSTEM B ); FOUND L ENG IGN-B IGNITER PLUG FULLY WORN OUT. REMOVED AND REPLACED L ENG IGNITER PLUG-B PER EMM 74-21-01. OPS CK'D SATIS & ITEM OK FOR SVC AT THIS TIMEOct 1, 2025 · N2169J · Airbus A321271NX · Magneto/DistributorSDR HALA20251002297Fire Loop · faultedETOPS - FIRE LOOP A CORE ECAM MESSAGE. REPLACED FIRELOOP A CORE PER AMM 26-12-17. OPS CHECK NOT GOOD. REPLACED LOOP A FIRE LOOP HARNESS PER AMM 26-12-61. OPS CHECK NOT GOOD. REMOVED AND REPLACED FIRE LOOP CORE LOOP B PER AMM 26-12-17. OPS CHECK IS GOOD. OKAY TOct 1, 2025 · N213HA · Airbus A321271N · Fire DetectionSDR HALA20251002298Igniter · damagedETOPS - DURING T/C 321-724000-W2-1 FOUND ENG 2 LOWER IGNITER DAMAGED. REMOVED AND REPLACED IGNITER PER AMM 74-21-00. OPS TEST GOOD, OK TO CONTINUE.Oct 1, 2025 · N227HA · Airbus A321271N · Spark Plug/IgniterSDR DALA2025100307192Seal · leakingFUMES EVENT AT CRUISE, DESCENT AND AFTER LANDING. NOTICABLE IN GALLEY DURING APPROACH. STRONGEST WITH POWER AT IDLE. FOUND #1 ENG SPINNER WITH EVIDENCE OF OIL. REPLACED #1 ENG FAN SHAFT COVER SEAL PER A321 AMM 72-15. C/W LEVEL B DECOMTIMINATION PER A321 AMM Sep 30, 2025 · N534DT · Airbus A321271NX · Turbine Engine Oil SystemSDR DALA2025100307193Seal · leakingDIRTY SOCK SMELL MOMENTARILY AT FL 340 BEFORE DESCENT, ALSO AT FL 190 + 13000FT STILL GIVE PUFFS OF SMELL THAT LINGER. FOUND OIL IN #1 SPINNER. REPLACED #1 ENGINE FAN SHAFT COVER SEAL AND LEAK CHK NML. (LP 7317990)Sep 30, 2025 · N531DA · Airbus A321271NX · Turbine Engine Oil System
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