IAE V2527-A5
Service difficulty reports · 8,006
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 = 'V2527A5' 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 = 'V2527A5' 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 YENA2021101100672Relay · failedFLT #603, EWR-SDQ(DIVERTED TO JFK). CLIMBING OUT OF FL200 ECAM ENG 1 N1 DEGRADED MODE, PERFORMED ECAM QRH, N1 MODE SEL. ENG 1 AND 2, AFTER SEL ENG 1 REQ TO REMAIN IN CLIMB DETENT, ENG 2 OUT OF DETENT, 1-N1 78.6, 2-N1 86.3 ; ACCOMPLISHED TSM 74-00-00-810-807-B SDR AALA202110121825Engine · overtempAIRCRAFT WAS GROUNDED: #1 ENGINE EXPERIENCED AN OVER TEMPERATURE EVENT AND A COMPRESSOR STALL AT THE TOP OF DESCENT ALONG WITH A COMPRESSOR VANE FAULT. THE ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TUS WHERE IT LANDED SAFELYSDR AALA202110181825Engine · overtempAIRCRAFT WAS GROUNDED: #1 ENGINE EXPERIENCED AN OVER TEMPERATURE EVENT AND A COMPRESSOR STALL AT THE TOP OF DESCENT ALONG WITH A COMPRESSOR VANE FAULT. THE ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TUS WHERE IT LANDED SAFELYSDR AALA202110081724Engine · overtempAIRCRAFT WAS GROUNDED: ENGINE # 1 ECAM MESSAGES FOR COMPRESSOR VANE FAULT, ENGINE 1 FAIL AND EGT EXCEEDED ENGINE SHUTDOWN IN FLIGHT. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT PHX SAFELY WITHOUT FURTHER INCIDENT. A REVIEW OF THE DFDR DATA NOTED THATSDR AALA202110131345Pump · defectiveAIRCRAFT WAS GROUNDED: ENGINE # 1 ECAM MESSAGES FOR COMPRESSOR VANE FAULT, ENGINE 1 FAIL AND EGT EXCEEDED ENGINE SHUTDOWN IN FLIGHT. NO EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED AT PHX SAFELY WITHOUT FURTHER INCIDENT. A REVIEW OF THE DFDR DATA NOTED THATSDR AALA202110131724Actuator · defectiveAIRCRAFT WAS GROUNDED: ENGINE # 1 ECAM MESSAGES FOR COMPRESSOR VANE FAULT, ENGINE 1 FAIL AND EGT EXCEEDED ENGINE SHUTDOWN IN FLIGHT. NO EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED AT PHX SAFELY WITHOUT FURTHER INCIDENT. A REVIEW OF THE DFDR DATA NOTED THATSDR GTIA2021100736032Seal · leakingDIRTY SOCK SMELL DURING DESCENT AND APP PROCEDUE APPLIED FOR PACK 1 ODER WENT AWAY ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED )-UPON INSP. FOUNSDR CALA2021091701598Eiu · failedEIU FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 1 OCCURED ON GNDRESET AND ECAM CLRDOCCURED AGAIN INFLT- FADEC 1B FAULT. BITE TEST OF FADEC HAD EIU/HC/EEC1. REPLACED #1 EIU. AND FADEC BITE TEST CK GOOD. RAN ENGINE,NO FAULTS NOTED. REF MM 73-25-00-810-887A. PASDR CALA2021090801534Rivet · missingPDA 3 #2 ENG AIR INTAKE COWL OUTER LIP SKIN HAS ONE RIVET HEAD BROKEN OFF/MISSING AT 7 O-CLOCK POS AFT LOOKING FORWARD-- SEE PHOTO PHOTO ADDED REPLACED DAMAGED FASTNER WITH NEW FASTNER WITH NEW FASTNER REF. EC/RA 7111-01387.SDR CALA2021090101474Seal · damagedON #1 ENG DO AN IDLE LEAK CHECK (TEST NO. 3) (REF. TASK 71-00-00-710-012-B). DUE TO DE-OILER GEARBOX SEAL REPLACEMENT. REF LP 6963611 AND 6961808. ACP IDLE LEAK CHECK( TEST #3) ON #1 ENG REF TASK 71-00-00-710-012-B. NO LEAKS NOTED FOR DE-OILER REPLACEMENT ADD SDR CALA2021080401256Valve · failedENG2 BEARING 4 OIL SYSHI PRESS ECAM ON CLIMBOUT OF ORD.ECAM WENT AWAYAFTER A FEW MINUTES. RELATED CLM ARE "CHECK HARNESS OR CHANGE VALVE 4006EN (ENG 2)" AND "CHECK N4 BRG SCAV PRESSXMTR2 CITCUIT 4005 EN. AS WELL AS A RELATED "ENG 2 EIU" FAULT. TROUBLESHOOT PERSDR CALA2021072801205Rivet · damagedPDA 3 TOTAL OF 6EA RIVET HEADS BROKEN/MISSING AT OUTER LIP SKIN OF #1 ENG AIR INLET COWL -- SEE PHOTO CORRECTION - #2 ENG AIR INTAKE COWL REPLACED 6 EA RIVETS REF ECRA 7111-01387SDR CALA2021070901052Actuator · failedPER CREW, NR 2 ENGINE EXCEEDS EGT. PLANE MADE A GATE RETURN UPDATED AIR RETURN CREW REPORTED EVENT HAPPENED IN FLIGHT BEFORE FLAP RETRACT BELOW POPPING FROM NR 2 ENG. 11,000'' ALT. DEAD HEAD PILOT CAPT SITTING ABOVE WING REPORTED (REPORT AIDS) SHOW TOVL1= 000SDR CALA2021070901049Engine · faultedDURING FLEX TAKEOFFRT ENG DID NOT DEVELOPFULL FLX EPR THRST SETT FOLLOWED BY CATION ECAM CREW REPRTED THAT ENG2 SN. V10497: LOW SPEED ABORTED T-OFF DURING FLEX TEMP OR DERATED T-OFF, AN ABORTED T-OFF CAN BE AVOIDED BY PUSHING THRST LVRS TO TOGA DETENT PER ECAMSDR AALA202107074281Engine · stalledAIRCRAFT WAS GROUNDED: AT APPROXIMATELY 1000' RIGHT ENGINE COMPRESSOR STALLING WITH HIGH EGT. AFTER RETURNING THRUST TO IDLE COMPRESSOR STALL STOPPED. PASSENGER REPORTED SEEING FLAMES. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT RETURNED TO MKE WHERE IT LANDEDSDR AALA202107134281Engine · stalledAIRCRAFT WAS GROUNDED: AT APPROXIMATELY 1000' RIGHT ENGINE COMPRESSOR STALLING WITH HIGH EGT. AFTER RETURNING THRUST TO IDLE COMPRESSOR STALL STOPPED. PASSENGER REPORTED SEEING FLAMES. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT RETURNED TO MKE WHERE IT LANDEDSDR AALA202106279001Engine · stalledAIRCRAFT WAS GROUNDED: ON TAKE OFF ROLL COMPRESSOR STALL AND EGT OVER TEMPERATURE IN AREA C ON THE RIGHT ENGINE. ACCOMPLISHED AN ABORTED TAKE OFF AND THE AIRCRAFT RETURNED TO THE GATE. REPLACED ENGINE PER TASK CARDS 26L40071004 AND 26L00071015.SDR AALA202105219016Engine · stalledAIRCRAFT WAS GROUNDED: #2 ENGINE STALL ECAM WARNING AND CREW SHUTDOWN THE ENGINE WITH SINGLE ENGINE TIME OF 7 TO 8 MINUTES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SJC WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED #2 ENGINE AND ACCOMSDR AALA202104019034Engine · smokeAIRCRAFT WAS GROUNDED DURING PUSHBACK TAXI OUT ANOTHER AIRCRAFT REPORTED THAT THE RIGHT HAND ENGINE HAD SMOKE COMING FROM THE TAIL PIPE. THERE WAS NO ECAM INDICATION OF A FIRE AND THE ENGINE PAGE SHOWED #2 ENG @ 8QTS AND DROPPING RAPIDLY. THE CREW SHUT DOWN ENSDR CALA2021011100037Engine · stalledSTALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN. ENGINE 2 APPROXIMATELY 3000 FT ON DEPT FELT MINOR THRUST REDUCTION FOLLOWED BY ENG 2 STALL ECAM, ECAM CLEARED AND TH REF TO TSM TASK:71-00-00-810-809-A SURGE OR STSDR 2021F00001Power Supply · failedF/A REPORTS EMERGENCY LIGHT CAME ON AT 10,000 ON DESCENT.SDR YENA2020120700564Eec · failedFLT 942, LAX-RNO. DURING CLIMB OUT OF LAX ENGINE 1 ROLLED BACK TO NEAR IDLE. THEN RETURNED TO CLIMB POWER. AFTER LANDING ECAM, ENGINE 1 OVERSPEED PROT FAULT, PER 77-11-00-860-010A SWAPPED ENGINE NR 1 N1 PROBE TO SPARE PROBE, PER MCC REQUEST. R & R NR 1 ENGSDR YENA2020120700566Fmu · failedFLT 1421, PHL-SJU. RETURNED TO FIELD. ON CLIMBOUT FUEL FLOW INDICATION INDICATED A FLUCTUATION OF BETWEEN 1800-8000 LB/HR ON ENGINE NR 2. PREVIOUSLY WRITTEN UP. R & R NR 2 ENGINE FMU, REF AMM 73-22-52. OPERATIONS CHECK OK. PERFORM HIGH POWER ASSURANCE RSDR YENA2020120800567Transmitter · failedFLT 1421, PHL-SJU. RETURNED TO FIELD. FUEL FLOW FLUCTUATION. R & R NR 2 ENGINE FUEL FLOW TRANSMITTER, REF AMM 73-31-17. OPERATIONS CHECK OK.SDR YENA2020120800568Pump · failedFLT 1421, PHL-SJU. RETURNED TO FIELD. FUEL FLOW FLUCTUATION. R & R NR 2 ENGINE FUEL PUMP, REF AMM 73-12-41. OPERATIONS AND LEAK CHECK GOOD.SDR CALA2020111801286Interface Unit · failedENGINE ONE THRUST REV FAULT AT CRUISE ALTITUDE UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003001535 AND PRTR LIVINGSTON, MATTHEW (V922838). NR 1 REVERSER DEACTIVATED, PER MEL 7830MSDR AALA202010259008Fault Message · false activationAIRCRAFT WAS NOT GROUNDED. ON TAKE OFF THURST LEVERS ADVANCED TO FLEX. ENGINE 2 ONE TLA FAULT DISPLAYED ON ECAM. TAKEOFF ABORTED AND ECAM MESSAGE SELF CLEARED. ACCOMPLISHED SATISFACTORY TSM 76-000-810-802. NO MESSAGE RECORDED.SDR YENA2020100900482Indication Sys · malfunctionedAFTER TAKEOFF FROM HMV ACFT RETURNED TO FIELD, DUE TO ENGINE NR 1 EPR INOPERATIVE. N1 LIMIT DISPLAY ON EWD NOT PRESENT & ENGINE NR 1 ANTI-ICE FAILED OPEN. DVDR DOWNLOAD HAS BEEN ACCOMPLISHED. SAL TECHS WILL TROUBLESHOOT NR 1 ENGINE FAULTS. PERFORMED CHECK SDR GTIA2020092435367Bleed Valve · faultedAIR ENG 1 BLEED FAULT BLEED OVERPRESSURE PSI 62+ RETURNED TO KIAH, PER SOC. PERFORMED TSM-36-11-00-810-809-A, FOUND PRESSURE REGULATOR BLEED VALVE FAULTY. REMOVED AND REPLACED BLEED PRESSURE REGULATOR VALVE, IAW AMM 36-11-52-000-010. OPS CHECK GOOD. NO FAUSDR AALA202009099018Engine · failedAIRCRAFT WAS GROUNDED: DURING TAKEOFF ROLL BELOW 80 KTS, ECAM MESSAGE FOR ENGINE #2 COMPRESSOR VANE, FOLLOWED BY REJECTED TAKEOFF AND ENGINE # 2 FAILURE. REPLACED #2 ENGINE IAW WORKCARDS 26L40071004 AND 26L00071015, OPS CHECK GOOD.SDR GTIA2020082435320Relay · failedENGINE # 1 PR MODE FAULT ( INFLIGHT) ( NO HARD LANDING )-REF TSM #73-22-00-810-817B. REMOVED AND REPLACED THE RELAY BOX ON # I ENG (P2/T2) AND ALSO RUN ENG # 1 AT IDLE FOR FIVE MM NO FAULT NOTED REF AMM 71-00-00.SDR GTIA2020080635301Wire Harness · failedENG 1 SENSOR FAULT ECAM AMBER X'S EGT APPEAR IN FLIGHT. AIR RETURN LANDING WHT WAS ABOUT 145.500LBS-REMOVED & REPLACED #1 ENG EGT HARNESS & JUNCTION BOX IAW AMM 77-21-43. REMOVED & REPLACED #1 ENG CORE HARNESS IAW AMM 77-21-43 OPS CK REQUIRED 64574 PERFORMED SDR AALA2020072219014Engine · slowAIRCRAFT WAS NOT GROUNDED, REJECTED TAKEOFF FOR SLOW LEFT ENGINE ACCELERATION BETWEEN 1.05 EPR AND FLEX POWER SETTING. IT WAS PROBABLY DUE TO HIGH AIRPORT ELEVATION. REJECTED WELL BELOW 80KTS. PERFORMED NR 1 ENG HIGH POWER ASSURANCE TEST IAW JOB CARD 26L0007SDR GTIA2020062935212Deoiler · leaking"SUSPECTED ODOR IN FWD GALLEY SUPPLEMENTARY PROCEDURE FOR ELIMINATION OF ODOR/FUMES IN THE COCKPIT/CABIN APPLIED IAW COM2. 3.226.1. APPLIED T.S.M. 05-50-00-810-8 FOUND SLIGHT EVIDENCE OF ENG. OIL # 2 LEAKAGE AT DROILER ASSY IAW AMM: 76-30-31 PERFORMED DECONTSDR YENA202003180251Engine · stalledFLT 1459. BDL-FLL. DIVERTED TO JFK NO EMERGENCY LANDING REQUESTED. “PASSING FL230 TO FL340 ENGINE 1 STALLED. ECAM DISAPPEARED SO WE COULDN’T RUN IT. ENGINE AT IDLE ECAM STAYED BLANKED”. A NORMAL LANDING. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE AND A DFDR DOSDR AALA202003179003Actuator · malfunctionedAIRCRAFT WAS GROUNDED: ENG 1 COMPRESSOR VANE ECAM MESSAGE OUT TAKEOFF ROLL AT FLEX POWER. REMOVED AND REPLACED #1 ENG VSV ACTUATOR PER J/C 26T40075005. PERFORM POWER ASSURANCE TEST IAW 26L0007104.SDR GTIA2020030935069Seal · leakingFA REPORTS STRONG " DIRTY SOCK" ODOR FROM EXIT ROWS TO FWD GALLEY STARTED ON DESCENT AROUND 10.000 TURNED PACK 2 OFF, APPEARED TO MAKE ODOR DISSIPATE-PERFORMED TSM 05-50-00-810-831-A AND FOUND # 1 ENG DEOILER SEAL TO BE LEAKING, R+R # 1 ENG DEOILER SEAL IAW ASDR GTIA2020030235055Oil System · lowON TAKEOFF. ENG #2 LOW OIL QTY ADVISORY FOR QTY OF .5 QT-UPON ARRIVAL ENG. #2 WAS SHOWING 14 QTS OF OIL. PER TSM 79-31-00-810-814-A , FILL ENG. #2 WITH 8 QTS OF OIL. OIL COMSUPTION WITHIN LIMITS PER GMM 12-.1.2. PERFORMED VISUAL INSPECTION OF INLET , COLS STEASDR GTIA2020030235056Engine · smokeAFTER LANDING . FIRE TRUCKS REPORTED A LIGHT SMOKE MIST FROM ENG #1. SO WE SHUT IT DOWN -PERFORMED PRECAUTIONARY ENG #1 IDLE RUN PER AMM 71-00-00 , NO SMOKE NOTED DURING THE DURATION OF ENGINE RUN. OF ANY OTHERS DEFECTS ENG#1 IS GOOD. PER SERVICE.SDR GTIA2020030235053Seal · damagedFUME EVENT DURING DESCENT. STRONGEST ON THE BACK OF A/C. PERFORMED ELIMINATION OF ODOR/FUMES PROC. SMELL STILL NOTICEABLE-R+R DEOLER CASING SEAL ASSY IAW AMM 72-60-31 & PERFORMED TSM 05-50-00 FOR IDENTIFICATION OF THE CAUSE OF CABIN ODOR, SMOKE FUME & NO SMELLSDR AALA202002189024Ring · defectiveAIRCRAFT WAS GROUNDED: CREW REPORTED THE NR 2 ENGINE EXPERIENCED 5-6 COMPRESSOR STALLS AND VIBRATION AT FL 250. THE ENGINE THRUST WAS REDUCED TO IDLE AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED AT BOS SAFELY WITH NO FURTHER INCIDENTS. REPLACED NR 2 ENSDR GTIA2020020644991Unknown · vibrationSIGNIFICANT ONFLIGHT ENGINE VIBRATION DURING CLIMB W/ CHANGES IN AIRSPEED AND RATE OF CLIMB.-REF TSM 05-50-00-810-801 SERVEY ACCOMPLISHED RESULT IS TYPE 1 ACCOMPLISHED CHECK OF THE ELEVATOR SERVO CONTROL AND HING BEARINGS ALL NUMBERS ARE WITHIN LIMITS NO DEFECSDR CALA2020020300325Unknown · vibrationHIGH VIBE NO 1 ENGINEHIGHEST READING 1.0CURRENTLY 0.7 AT CRUISEF L 200 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE DEBRIEF THE FLIGHT CREW FOR MORE INFORMATION. TAIL CLIMBING THROUGH FL220. IT WAS A MEDIUM FREQUENCY VIBRATION. ASKED THEM TO FILL OUT THSDR YENA2020040320266Engine · failedFT # 950, GND-JFK. RETURNED TO FIELD. THE A/C LANDED WITHOUT INCIDENT WITH THE #1 ENGINE SHUT DOWN. ENGINE #1 FAILED AT 400 FEET ON TAKEOFF, LOUD BANG. ENG ROLLED BACK NO FIRE ASSOCIATED; (REF WO 1039192 ON LP 2496877 ITEM 1) R & R #1 ENGINE LEAK AND OPS CHECSDR GTIA2020011134940Seal · damaged"VERY STRONG "" DIRTY SOCK "" ODOR DURING DESCENT.
FUME EVENT ON DESCENT. -R/R DEOILER SEALS BTH # 1 AND # 2 ENG. IAW AMM 72-60-31. PERFORMED PAC BURN BOTH # 1 AND #2 PACS IAW AMM 21-00-00. R/R BOTH # 1 AND # 2 PAC RECERC. FILTERS IAW AMM 21-21-41. NO ODOR NSDR YENA2020011510016Engine · failedFLT 2276, SJU-BDL. RETURNED TO FIELD. AFTER T/O LOUD BANG NR 1 ENGINE FOLLOWED BY HIGH EGT RAN ECAM POWER REDUCED TO IDLE RETURN TO LAND 30 MIN OF OPERATION AT HIGH EGT 600-700C; R & R NR 1 ENGINE PER AMM 71-00-20 ALL OPERATION ARE GOOD. NO LEAKS NOTED. A/C OKSDR SOKF20191208007Fitting · wornDURING CLIMB, THE AIRCRAFT RETURN TO LIM DUE TO HIGH VIBRATION DURING CLIMB BETWEEN FL 050 AND FL 270 . SPEED BETWEEN 200-300 KTS. VIBRATION MODERATE FELT IN ALL THE AIRCRAFT. AT LIM STATION PERFOMED T/S PROCEDURE IAW TSM 05-50-00-810-801-A AND TSM 27-10-00-8SDR AALA2019120429016Apu · leakingAIRCRAFT WAS GROUNDED: BOTH PILOTS SMELLED "OIL SMELL" DURING SEVERAL PHASES OF FLIGHT. MODERATE + LIGHT IN INTENSITY. MAINTENANCE ACCOMPLISHED SMOKE ODOR FUMES INITIAL TROUBLESHOOTING IAW JOB CARD 26L00021001. DETERMINED APU IS THE CAUSE OF ODOR. SUPPLEMENTALSDR AALA2019120429015Oil Cooler · leakingAIRCRAFT WAS GROUNDED: PILOT REPORTS DIRTY SOCK ODOR THROUGHOUT CABIN DURING DESCENT IN VISIBLE MOISTURE. NO PASSENGER OR CREW ISSUES. MAINTENANCE COMPLETED SOF EVENT IAW JOB CARD 26L00021001, APU FOUND TO BE THE SOURCE OF ODOR. FOUND EVIDENCE OF OIL LEAK FROMSDR AALA2019120319010Warning Message · false activationAIRCRAFT NOT GROUNDED: PILOT REPORTS AFTER TAKEOFF MCDU WENT INTO ENGINE OUT MODE EVEN THOUGH BOTH ENGINES WERE OPERATING NORMALY - EMERGENCY CANCELLED THE AUTO FLTA/THR LIMITED. MAINTENANCE REPORTS RAN # 1 AND 2 ENGINE POST FLIGHT WAS CLEAN. NO 30 DAY HISTORY
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