IAE V2527-A5
Service difficulty reports · 8,011
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 2004UALA01150Fan · damagedLAND ASAP ECAM DISPLAYED. FOUND FOD IN AVIONICS EXTRACT FAN (18HQ). REPLACED SAME.SDR 2004UALA01125Warning Light · illuminatedGEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM. AFTER GEAR RETRACTION, RECEIVED A LANDING GEAR SHOCK ABSORBER FAULT ON UPPER ECAM.ACCOMPLISHED A COMPLETE NOSE GEAR STRUT SERVICE. CLEANED GREASE FROM NOSE PROX SENSORS. JACKED NOSE GEAR CLEAR OF GROUND AND GEAR CESDR 2004UALA01042Skin · dentedTHREE DENTS ALONG RIGHT SIDE OF NOSE WHEEL OPENING FROM CONTACT WITH GROUND EQUIPMENT. DOUBLER AND TRIPLER INSTALLED.SDR 2004UALA01047Windshield · crackedFIRST OFFICER'S WINDSHIELD CRACKED. CRACK APPEARS TO HAVE INITIATED FROM A BUBBLE AT THE TOP CENTER OF THE WINDOW WHICH DID NOT IMPAIR VISIBILITY.SDR 2004UALA01019Line · obstructedNR 1 ENGINE OIL QUANTITY DECREASED FROM 15 TO 7 QUARTS. AFTER LANDING THERE WAS SMOKE AND A SMALL FIRE FROM THE EXHAUST AREA. EXCESSIVE COKING OF THE NR 5 BEARING COMPARTMENT OIL SCAVENGE LINE CAUSED OVER PRESSURIZATION OF THE COMPARMENT. OIL WAS FORCED PASSDR 2004UALA01015Pump · malfunctionedRIGHT TANK FUEL BOOST PUMPS FAULTED AND UNABLE TO CORRECT FUEL IMBALANCE. DUE TO FUEL IMBALANCE WITH BOTH RIGHT WING NR 1 AND 2 BOOST PUMPS INOPERATIVE. THE AIRCRAFT DIVERTED, RT WING NR 2 BOOST PUMP CONTACTS WERE CLEANED AND THE NR 1 RIGHT WING BOOST PUMP WASDR 2004UALA01000Cable · brokenDOOR 2R WILL NOT ARM. THE CABLE AT BOTTOM OF SLIDE/RAFT ASSY WAS FOUND BROKEN WHICH DISRUPTED THE NORMAL FUNCTION OF EMERGENCY SELECTOR MECHANISM. THE SLIDE RAFT CABLE SYSTEM IN THE SLIDE LOWER LACING COVER IS A SENSITIVE DESIGN. RELEASING THE CABLE SYSTEM SDR 2004UALA01025Tape · separatedHINGE TAPE IN SLIDE RAMP SEPARATED DURING OVER PRESSURE. THE TAPE SEPARATION COULD BE ATTRIBUTED TO ADHESIVE FAILURE. THE UNIT WAS SENT TO OEM (AIRCRUISERS) FOR REPAIR.SDR 2004UALA01032Hose · out of positionSLIDE HOSE WAS PACKED INTO ONE FOLD ON THE RIGHT FRONT CORNER. SLIDE ASSEMBLY PREVIOUSLY PACKED INCORRECTLY. REPACKED SLIDE TO SPECIFICATIONS.SDR 2004UALA00995Bracket · brokenSLIDE ASSEMBLY STEP BRACKET BROKEN. STEP BRACKETS OF SLIDE/RAFTS (LT & RT) ARE THE TWO BOTTOM ATTACHMENT POINTS THAT HOLD THE SLIDE/RAFT ONTO THE AIRCRAFT DOOR. THESE PARTS ARE STICKING OUT OF THE WHOLE ASSEMBLY AND ARE LIABLE TO DAMAGE ESPECIALLY DURING TRASDR 2004UALA00994Valve · separatedVALVE ASSEMBLY PASSED LOW VOLUME LEAK CHECK AT 3000 PSI FOR 24 HOURS. DURING FILL PROCESS AT 1500 PSI THE VALVE SEPARATED FROM CYLINDER AT BOTTLE ADAPTER. THE CRACKED FITTING WAS MADE OF ALUM 7075-T6 OR 2024-T4. NEW FITTINGS MADE OF SUPERIOR MATERIAL 7075-TSDR AWXA200401161Battery · dischargedEMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE AFT GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR YENA200450Fan · seizedDURING CRUISE, LOUD VIBRATION AND A SLIGHT BURNING ODOR APPEARED. TURNED THE BLOWER SWITCH TO OVERRIDE AND ALL PROBLEMS IMMEDIATELY DISAPPEARED. PERFORMED TSM TASK 24-00-00-810-823 AND NO DEFECTS NOTED. AIRCRAFT RELEASED IAW MEL 21-26-01. LATER DISCOVERED SDR AWXA200401135Actuator · faultyORD - ABORTED TAKEOFF - FLT 0738 - ON TAKEOFF AT ORD EN ROUTE FOR LAS, RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 65 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, ENGINE RUN OPERATISDR AWXA200401129Computer · inoperativeAFTER TAKEOFF EN ROUTE LOST ALL FUEL QUANTITY INDICATIONS, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE R/R FUEL QTY INDICATION COMPUTER (FQIC) IAW AMM 28-42-34, OS CHK GOOD. FUNCTIONAL TESTING OF FQIC S/N 1772 PRODUCED NO FAILURES OR FAULTS. UNISDR 2004UALA00940Light · failedEMERGENCY LIGHTS TEST FAIL, FAULTS EXT LOADS FWD LT. AMPERAGE READING ON RECEIPT 0.00. CHANGED LIGHTS. AMPERAGE READING WAS .870 (NORMAL) AFTER REPACK.SDR 2004UALA00935Outflow Valve · faultyUNABLE TO PRESSURIZE THE CABIN. REPLACED FAULTY SKIN AIR OUTLET VALVE.SDR 2004UALA00927Windshield · crackedFIRST OFFICERS WINDSHIELD ARCING AND CRACKING. MOISTURE INGRESSION THROUGH A SEAL. WINDSHIELD REPLACED.SDR AWXA200401152Connector · damagedDURING BC-2 CHECK FOUND A DAMAGED CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD.SDR 2004UALA00892Transmitter · leakingFLIGHT EXPERIENCED GREEN HYDRAULIC SYSTEM LOSS OF QUANTITY. GREEN SYSTEM TRANSMITTER ON NR 1 ENGINE BROKEN AND LEAKED GREEN SYSTEM HYDRAULIC FLUID. REPLACED GREEN SYSTEM TRANSMITTER.SDR YENA200448Electrical Box · odorAT CRUISE REPORT FROM FA THAT THEY THOUGHT THEY SMELLED SMOKE, TURNED OFF GALLEY SHED CONFM ELECTRICAL, HAD THEM TURN OFF MASTER TV, WENT AWAY, WITH 10 MINS OFF NO FURTHER SMELL. PERFORMED VISUAL INSP OF ALL TV IN CABIN. ALL WORKING OK, ACCOMPLISHED INFO NOTSDR AWXA200401094Floor Panel · corrodedDURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 222FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 222FF IAW T/C C1D25306.SDR BB04087Wire · brokenCDG FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE, ROWS 13-18 LT. MAINTENANCE4 FOUND AND REPAIRED A BREAK IN THE WIRING.SDR AWXA200401083Dummy Rail · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF DUMMY RAIL Y503, AT FR 16. MAINTENANCE REMOVED DUMMY RAIL Y503, AT FR 16; INSTALLED A NEW REPLACEMENT RAIL IAW A320 SRM 51-42-1, FIG. 9-12.SDR AWXA200401084Floorbeam · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.SDR AWXA200401085Beam · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 LT, AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D53472092; INSTALLED REPAIR PART IAW A320 SRM 51-72-11SDR AWXA200401086Beam · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, FORWARD AND AFT OF FR 67. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 66 TO FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D534-72172; INSTALLED REPAIR PART ISDR AWXA200401087Beam · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D53472133; INSTALLED REPAIR PART IAW A320 SRM 51-72-SDR AWXA200401090Floorbeam · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11.SDR AWXA200401091Seat Track · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 3 EACH SPLICE ANGLES; INSTALLED REPAIR PSDR AWXA200401092Floor Panel · corrodedDURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 261FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 261FF IAW T/C C1D25310.SDR AWXA200401093Floor Panel · corrodedDURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 262FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 262FF IAW T/C C1D25310.SDR AWXA200401130Floorbeam · corrodedDURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM Y1292, UNDER LT AFT LAVATORY AT FR 66. MAINTENANCE REMOVED FLOORBEAM Y1292 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-71-11.SDR 2004UALA00896Lamp · inoperativeRED EMERGENCY ESCAPE PATH LIGHT ON BULKHEAD FORWARD OF SEAT ROW 1ABC INOPERATIVE. REPLACED LAMPS.SDR AWXA200401042Tire · failedEMERGENCY LANDING, ON TAKEOFF, EN ROUTE, THE NR 2 TIRE BLEW OUT CAUSING DAMAGE IN WHEEL WELL, LT WING, AND LT FLAPS, AIRCRAFT OUT OF SERVICE. EXAMINATION OF CASING FOUND TREAD MISSING 360º AROUND TIRE FROM SERIAL SIDE UPPER SIDEWALL TO OPPOSITE SERIAL SIDE SHSDR AWXA200401058Seat Track · corrodedDURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK RAIL Y254 LT AT FR 16. MAINTENANCE CUTOUT THE DAMAGE ON SEAT TRACK RAIL Y254 LT AT FR 16; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW SRM 53-00-14, FIG. 206.SDR 2004UALA00838Symbol Generator · failedFLIGHT INSTRUMENT DISPLAY PROBLEM. CAPTAINS NAV DISPLAY BLANKED OUT. BLANKING CAUSED BY CAPT NAV DISPLAY UNIT. DISPLAY UNIT REPLACED. SHOP TEST OF THE DISPLAY UNIT FOUND INTERMITTENT BLANKING CONDITION SUSPECT SYMBOL GENERATOR CARD.SDR AWXA200401012Engine · failedON TAKEOFF AT ORD EN ROUTE FOR PHX, WHEN FLEX THRUST APPLIED HEARD A LOUD BANG WITH MOMENTARY STALL INDICATED ON ECAM, REJECTED TAKEOFF AND UPON CLEARING RUNWAY NOTICED NR 1 ENGINE N2 VIB AT 7.4, SHUTDOWN ENGINE AND RETURNED TO GATE. MAINTENANCE PERFORMED A VSDR AWXA200401056Floorbeam · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 RT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 9-18.SDR AWXA200401057Sill · corrodedDURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SILL FORWARD IB CORNER AT FR 66. MAINTENANCE REMOVED CORRODED R-2 DOOR SILL FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF SILL; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 8-12, ANDSDR AWXA200400989Battery · discharged8-DAY CHECK - DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM THE RT OVER WING EMERGENCY LIGHT BATTERY PACK FAULTED. MAINTENANCE REMOVED AND REPLACED THE RT EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.SDR 2004UALA00893Structure · dentedDENT ON AFT RT CORNER OF 811 AVIONICS DOOR STRUCTURE. DOUBLER AND TRIPLER REPAIR INSTALLED IN ACCORDANCE WITH AIRBUS RAS/031172/019/2004 (MAJOR REPAIR).SDR AWXA200400972Battery Pack · dischargedDURING 4-DAY CHECK THE AFT SECTION OF SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FAILED TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (11WL), FUNCTIONAL CHECK WAS GOOD.SDR AWXA200400973Epsu · faultyDURING E-06 CHECK THE RT FORWARD RED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVER WING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.SDR YENA200446Electrical Box · smokeELECTRIC ODOR COMING FROM 26D. INFO NOTICE 2004-T023TR PERFORMED IN SAN AND FOUND SEB AT 26D WITH ELECTRICAL ODOR. LIVE TV PLACED ON MEL 25-22-03 CAT D, C/N L01825. REMOVED AND REPLACED SEB AT 26D IAW LTV MM 23-39-00, OPS CHECK NORMAL. MEL CLEARED.SDR 2004UALA00793Cap · wrong partFLIGHT DIVERTED DUE TO POSSIBLE FUEL LEAK. INCORRECT CAP ASSEMBLY INSTALLED. REPLACED CAP WITH CORRECT PART NUMBER.SDR 2004UALA00789Control Unit · faultyNR 2 GENERATOR FAULT ECAM MESSAGE. *S/D* NR 2 GENERATOR CONTROL UNIT REPLACED.SDR AWXA200400954Floor Panel · corrodedDURING BC-4 CHECK CORROSION WAS FOUND LOWER SIDE OF FLOOR PANEL 222 FF, FR 16, FR 20, RBL 45, RBL 60. MAINTENANCE REMOVED CORROSION ON LOWER SURFACE OF FLOOR PANEL 222 FF; FABRICATED A REPAIR DOUBLER; INSTALLED DOUBLER ON LOWER SURFACE OF FLOOR PANEL IAW AWA SDR AWXA200400955Web · crackedDURING BC-4 CHECK A 1 INCH CRACK WAS FOUND LT AFT TRAY (WEB) OB OF Y1292 LT, AFT OF FR 68. MAINTENANCE REMOVED CRACKED LT AFT TRAY AT Y1292 LT, FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.SDR AWXA200400956Web · crackedDURING BC-4 CHECK A 4 INCH CRACK WAS FOUND IN RT AFT TRAY (WEB) OB OF Y1292 RT, AFT OF FR 68. MAINTENANCE REMOVED CRACKED RT AFT TRAY AT Y1292 RT, FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.
Back to IAE V2527-A5