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 2005UALA00987Skin · damagedFUSELAGE SKIN IN AREA AROUND DOOR 2L IS DAMAGED. REPAIRED AREA AROUND DOOR 2L WITH DOUBLER PER SRM 53-00-11 PR 313-314.SDR 2005UALA00988Light · inoperativeEMERGENCY LIGHT TEST FAILED FWD BATTERY LEFT AND COM EMERGENCY AFT L. REPLACED ENERGECY POWER-SUPPLY UNIT 10WL.SDR 2005UALA00979Outflow Valve · malfunctionedAIRCRAFT PRESSURIZATION PROBLEM. CREW STOPPED CLIMB AT 10,000 FT, CABIN ALTITUDE WAS 7,000 FT. AIRCRAFT RETURNED TO FIELD AND LANDED OVERWEIGHT. CREW STOPPED CLIMB AT 10,000 FEET, CABIN ALTITUDE WAS 7,000 FEET. AIRCRAFT RETURNED TO FIELD AND LANDED OVERWEIGSDR 2005UALA00983Lamp · inoperativeEMERGENCY EXIT LIGHT OUT AT SEAT 6ABC. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 6ABCSDR 2005UALA00973Control Panel · inoperativeLEFT AFT MED EMERGENCY LIGHT SWITCH IS INOPERATIVE. REPLACED CIDS AFT PANEL.SDR 2005UALA00974Light · faultyEMERGENCY EXIT LIGHT TEST DOES NOT PASS. REPLACED BATTERY.SDR 2005UALA00961Compressor · stalledNR 2 ENGINE COMPRESSOR STALL. QTY 1 HPC R6 BLADE FRACTURED ON THE AIRFOIL. THIS, ALONG WITH SECONDARY DAMAGE FROM THE RELEASED BLADE, DEGRADED THE COMPRESSOR'S PERFORMANCE WHICH CAUSED THE OPERATIONAL PROBLEMS.SDR 2005UALA00982Battery · failedLEFT EMERGENCY BATTERY WON'T PASS TEST. REPLACED BATTERY.SDR 2005UALA00935Stringer · corrodedSTR 41R HAS CORROSION BETWEEN FS 31-32. CUT-OUT DAMAGED SECTION AND SPLICED IN NEW SECTION OF STRINGER PER SRM 53-21-13 FIG 203.SDR 2005UALA00936Stringer · corrodedSTRINGER 41R HAS CORROSION BETWEEN FRAMES 33-34. CUT-OUT DAMAGED SECTION, SPLICED IN NEW SECTION REF SRM 53-21-13 FIG 203 .SDR 2005UALA00937Stringer · corrodedSTR 43L HAS CORROSION BETWEEN FS 58-59. CUT-OUT DAMAGED SECTION AND SPLICED IN NEW SECTION REF SRM 53-00-13 FIG 201.SDR 2005UALA00938Stringer · corrodedSTR 43L HAS CORROSION BETWEEN FRAMES 54-56. CUT-OUT DAMAGED SECTION ACP SPLICE REPAIR PER SRM 53-00-13 FIG 201.SDR 2005UALA00942Slide · warning lightDURING CABIN EMERGENCY LIGHTS CHECK, FOUND EXT LOAD AFT LEFT ERROR MSG. REPLACED DOOR 2R SLIDE.SDR 2005UALA00910Mount · crackedFWD CARGO DOOR HANDLE MOUNT PLATE WHERE IT ATTACHES TO THE DOOR FRAME IS CRACKED AT THE FRAME.SDR 2005UALA00911Mount · crackedAFT CARGO DOOR HANDLE MOUNT PLATE WHERE IT ATTACHES TO DOOR FRAME IS CRACKED.SDR 2005UALA00912Skin · crackedFWD CARGO DOOR INNER SKIN IS CRACKED AT LWR AFT CORNER.SDR 2005UALA00927Floor Support · corrodedAFT GALLEY FLOOR SUPPORT 66-70 CORRODED. AMIS STATUS SHOWS THAT THE FLOOR SUPPORT WAS REPAIRED. REPAIRED OR REPLACED FLOOR SUPPORT IN ACCORDANCE WITH THE SRM.SDR 2005UALA00833Hydraulic System · failedGREEN HYDRAULIC SYSTEM FAILURE AND YELLOW SYSTEM OVERHEAT.SDR 2005UALA00812Landing Gear · malfunctionedNOSE GEAR WOULD NOT LOCK IN UP POSITION.SDR 2005UALA00813Strap · corrodedPREVIOUS STRAP BETWEEN FS 33 AND FS 34 ON STRINGER 42R IS CORRODED.SDR 2005UALA00794Hydraulic System · leakingFLIGHT EXPERIENCED GREEN HYD QTY LOSS AND ECAM INDICATION.SDR 2005UALA00830Battery Pack · inoperativeSEATS 1C-6C FLOOR PROXIMITY EMERGENCY ESCAPE PATH SYSTEM LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK.SDR 2005UALA00770Compressor · stalledON CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. SHUT DOWN NR 2 ENGINE.SDR 2005UALA00782Battery Pack · inoperativeEMERGENCY LIGHTS FAIL TEST. REPLACED BATTERY PACK AT DOOR 1L.SDR 2005UALA00747Skin · dentedRT FUSELAGE DENTED AFT OF FS 64 AT STR 20R. MAJOR REPAIR TO ADD DOUBLER OVER SKIN.SDR 2005UALA00738Outflow Valve · failedFLIGHT DIVERTED DUE TO AN AIR CONDITIONING FAULT. SKIN AIR OUTLET VALVE FAILED. VALVE WAS REPLACED, SYSTEM OPS CHECKED AND AIRCRAFT WAS RETURNED TO SERVICE. MOTOR WAS FOUND SHORTED.SDR 2005UALA00718Windshield · crackedFIRST OFFICER'S WINDSHIELD CRACKED. REPLACED WINDOW DUE TO CRACKING AND DELAMINATION.SDR 2005UALA00731Pump · leakingLOST GREEN HYDRAULIC SYSTEM. CREW SECURED PUMP AND PTU.SDR 2005UALA00713Radar · malfunctionedFLIGHT DIVERTED DUE TO WEATHER RADAR MALFUNCTION ALONG WITH FUEL AND WEATHER CONSIDERATIONS.SDR 2005UALA00656Epsu · inoperativeSEAT MOUNTED EMERGENCY LIGHTS INOP AT SEATS 12,13, 14, 18, 19 AND 20. POWER SUPPLIES LOW CHARGE, REPLACED.SDR 2005UALA00658Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED IN 5EA PLACES BETWEEN FRAME 66 AND FRAME 68. SUPPORT IS BETWEEN FLOOR PNL 262EF AND 262FF. SEAT TRACK FLOORBEAMS CORRODED AND REPLACED. REPLACEMENT OF A PSE IS CONSIDERED MAJOR REPAIR.SDR 2005UALA00643Light · will not testWHILE PERFORMING EMERGENCY LIGHT TEST FAILED WITH MESSAGE EXT LOADS FWD LEFT. REPLACED SLIDE.SDR 2005UALA00644Controller · failedNR 1 LGCIU FAULT FOLLOWED BY LOSS OF VH2 RADIO AND THRUST REVERSER. LGCIU FAULT DISPLAYED DURING CRUISE. ACP LGCIU SYSTEM GRND TEST REF MM 32-69-00. TEST OKNO FAULTS FOUND.SDR 2005UALA00641Valve · malfunctionedRECEIVED ECAM AND A FIRE ALARM FOR ENG NR 1. SHUT DOWN ENGINE. NR 1 ENGINE PRESSURE REGULATING VALVE FOR LEAKAGE AROUND SPINDLE SHAFT.SDR 2005UALA00737Skin · buckledSKIN BUCKLED AROUND AFT FUSELAGE JACK PAD FITTING. MAJOR REPAIR TO REPLACE SKIN IN AREA OF THE JACK PAD. REPLACED SKIN IN AREA OF THE JACK PAD.SDR 2005UALA00618Battery · dischargedNUMEROUS FLOOR PROX EEL LIGHTS INOP THROUGHOUT CABIN. BPOWER SUPPLIES LOW CHARGE. REPLACED MID AND AFT PWR SUPPLIES.SDR 2005UALA00714Skin · dentedDAMAGE TO FRAME 34 AT BELLY PANEL. DENT IN SKIN 4" FWD OF FS 34 AND JUST OTBD OF STR 43R. MAJOR REPAIR TO ADD DOUBLER OVER SKIN.SDR YENA200536Eec · unserviceableDURING VISUAL APPROACH EXPERIENCED FAILURE OF ENGINE NR 1. DECLARED EMERGENCY AND LANDED. PFR SHOWING FMU CH A AND B FAULTS. PERFORMED TSM TASKS 73-00-00-810-904 AND 906. ALL WIRING CHECKS GOOD IAW 76-12-00. FOUND EEC AT FAULT. REMOVED AND REPLACED EEC IASDR 2005UALA00610Skin · lightning strikeLIGHTNING STRIKE ON VERT FIN RT SIDE BETWEEN RIB 10 AND UPPER LEADING EDGE. MAJOR REPAIR ACCOMPLISHED PER EVA 50378ASDR 2005UALA00609Light · inoperativeCABIN EMERGENCY LIGHTS IN ROW 12-13-14 AND ROWS 18-19 AND 20 INOP.SDR 2005UALA00739Engine · stalledNR 1 ENG STALL ON TAKEOFF ROLL.SDR 2005UALA00608Tube · damaged3 IN LONG SLICE ON LOWER TUBE. SLICE OR LACERATION ON THE INFLATABLE TUBE COULD BE DUE TO MISHANDLING DURING UNIT TRANSPORTATION. THE DAMAGE WAS REPAIRED AND RETESTED OK.SDR 2005UALA00604Transceiver · failedWX RADAR FAILED INFLIGHT. WEATHER RADAR RECEIVER / TRANSMITTER WAS DEFECTIVE. SHOP FINDINGS INDICATED A R/T FAULT. WXR R/T WAS REPLACED, AND NO FURTHER ASSOCIATED PROBLEMS OCCURRED.SDR AWXA200500748Wire · brokenAIR TURN BACK. DURING FLIGHT LOST APU WITH NR 1 GENERATOR ALREADY ON MEL. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED NR 1 IDG IAW AMERICA WEST AIRLINES TASK CARD R5M24301. OPERATIONAL CHECKS WERE GOOD. PLACED THE APU ON MEL. TEARSDR 2005UALA00590Tape · separatedHINGE TAPE ON FLOOR RAMP IS SEPARATED. ADHESIVE FAILURE, RESULTED IN TAPE SEPARATION DURING THE PRESSURIZATION OF THE ASSEMBLY. UNIT WAS SENT TO OEM FOR REPAIR/DISPOSITION.SDR 2005UALA00591Hose · brokenHOSE FOUND BROKEN BY ASPIRATOR. HOSE WAS FOUND BROKEN AT END NEAR ASPIRATOR CONNECTION DURING MAINTENANCE OF THE SLIDE IN THE SHOP. PROBABLE CAUSES COULD BE MISHANDLING DURING TRANSPORTATION OR THAT THE ROUTING OF THE HOSE DURING THE PREVIOUS SLIDE PACKING SDR AWXA200500746Bleed Air Sys · malfunctionedAIR TURN BACK. DURING CLIMB RECEIVED ECAM MESSAGE FOR ENG BLEED 1 FAULT FOLLOWED BY PACK FAULT THEN NR 2 ENG BLEED FAULT FOLLOWED BY PACK FAULT. RETURNED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED NR 1 AND NR 2 BMC. REMOVED AND REPLACED NR 1 ENGINE SDR 2005UALA00587Sensor · malfunctionedNR 2 ENGINE REVERSER FAULT EMAC MESSAGE. ENG 2 REV ECAM MESSAGE AIRCRAFT RETURNED TO FIELD. REVERSER FAULT DUE TO LGCIU DUE TO CHRONIC ECAM ENG 2 REV FAULT IN FLIGHT THAT OCCURS AT THE SAME TIME AS A LGCIU2 FAULT. LANDING GEAR SENSOR 23GA REPLACED PER AMM 3SDR 2005UALA00585Blower · smokeVIBRATIONS & RUMBLING NOISE UNDER FLT DECK ACCOMPANIED BY SMOKE. FOUND AVIONICS BLOWER FAN 20HQ FAILED. REPLACED FAN.SDR 2005UALA00577Line · leakingLEFT WING BLEED LEAK. LEFT WING BLEED LEAK IN CRUISE. FLIGHT RETURNING TO DEN DUE TO ICING AND WX. FOUND VERY LARGE LEAK ON THE RT PACK OZONE CONVERTER AFT CLAMP, REMOVED CLAMP RE-ADJUSTED SEAL AND SECURED CLAMP, LEAK WAS BLOWING AT OVERHEAT LOOP ON KEELBEAM
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