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 = 'V2524A5' 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 = 'V2524A5' 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 GTIA1000001Damper · damagedL4 DOOR ASSIST DAMPER MISSING INTERNAL SPRING / REMOVED AND REPLACED L4 DOOR ASSIST DAMPER.SDR SA08040Unknown · malfunctionedFLIGHT 132, SNA-PHX - THE CAPTAIN RECEIVED AN ECAM MESSAGE OF FUEL CONTROL FAULT. THEY PROCEEDED WITH THE TAKEOFF AND THE ECAM STATED TO BRING THE ENGINE BACK TO IDLE. DECLARED AN EMERGENCY AND LANDED IN LAX WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION IS PSDR SA08017Indication Sys · malfunctionedPIT - FLT 257 - PHL TO PHX - DURING CRUISE, FLIGHT EXPERIENCED A HIGH, NUMBER TWO ENGINE VIBRATION INDICATION PROBLEM. AIRFRAME VIBRATION WAS NOT DETECTED OR INDICATED. THE CREW REDUCED POWER ON THE NUMBER TWO ENGINE TO IDLE. SINCE AIRSPEED AND ALTITUDE COUSDR SA08009Solenoid · faultyORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUMBER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE ONE SOLENOID 7B. SDR SA08010Bleed Valve · faultyORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUMBER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE ONE SEVENTH STAGE,SDR SA08011Actuator · failedORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUMBER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE ONE ACC ACTUATOR. SDR YENA2007025Computer · odorFLT 209, APRX 1450Z, DIVERTED, BURNING ODOR IN COCKPIT AND CABIN FOLLOWED BY ANTI-ICE-STBY L STAT, STBY R STAT. PERFORMED T/S TASK 24-00-00-00-810-823, FOUND SELL COMING FROM PROBE HEAT COMPUTER NR3. REMOVED AND REPLACED NR3 PROB HEAT COMPUTER. OPS CHECK OKSDR AWXA200700403Fuel Control · failedSAN - ABTO - CREW ABORTED THE TAKEOFF AT 100 KTS DUE TO LEFT ENGINE FUEL CONTROL FAULT. THE CREW SHUT DOWN THE LEFT ENGINE AND RETURNED TO THE GATE. MX REPLACED THE FUEL METERING UNIT PER AMM 73-22-52-000-01. OPERATIONAL CHECK WAS GOOD.SDR AWXA200700140O-Ring · leakingPHX - DURING INITIAL CLIMB, LOST ALL OIL QUANTITY IN NR 1 ENGINE. OIL PRESS AND ALL OTHER PARAMETERS REMAINED IN THE GREEN. RETURNED TO FIELD AT IDLE THRUST. INSTALLED TEMP THERMOCOUPLE IN NR 1 ENG ACOC WITH NEW O-RING IAW MM 79-32-15 PB401. RAN ENG, LEAK SDR AWXA200700020Eec · out of toleranceFLIGHT 237: DTW - PHX - THE A/C HAD JUST REACHED CRUISE ALTITUDE WHEN THE CREW NOTICED THE NR 1 ENGINE HAD RETARDED TO FLIGHT IDLE FOLLOWED BY AN ENGINE FLAMEOUT/SHUT DOWN. THE CREW ATTEMPTED AN IN-FLIGHT RESTART, THE IN-FLIGHT RESTART WAS NOT SUCCESSFUL. THSDR AWXA200602120Power Supply · failedMCI LOG NR 7241817 - EMERGENCY EXIT SIGNS FLICKER, MX PERFORMED A BITE TEST AND THE EPSU COMM EMER L FAILED. MX REMOVED AND REPLACED LT OVERWING EPSU AND BATTERY, OPS CHECK WAS GOOD.SDR AWXA200602121Smoke Detector · failedLAS LOG NR 7485109. MX REPORTED LAV AND CARGO SMOKE DETECTORS FAULT, SDCU INOP. MX TROUBLESHOT SYSTEM AND FOUND FWD CARGO 2WH INOP. MX REMOVED AND REPLACED FWD CARGO 2WH SMOKE DETECTOR. OPS CHECK WAS GOOD.SDR GTIA200600085Wire · misinstalledR-2 EMERGENCY EXIT SIGN INOP. FOUND R2 DOOR SIGN LIGHT AND EMERGENCY LIGHT MIS-WIRED IAW WDM.SDR GTIA200600084Stator Vane · lack of lubeNR 2 ENG COMPRESSOR VANE ECAM RT AFTER POWER ADVANCE TO FLEX TAKEOFF. LOW SPEED ABORT, NR 2 ENG SHUTDOWN IAW ECAM. MAINTENANCE LUBED VSV SYSTEM.SDR 2006UALA02108Hydraulic System · leakingLANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. AIRCRAFT TOWED TO GATE. GREEN HYDRAULIC INDICATOR JUST ABOVE THE YELLOW BAND. FOUND LEFT YAW DAMP ACTUATOR LEAKING AT ROD SEAL BEYOND 20 DROPS PER MINUTE. REPLACED ACTUATOR.SDR AWXA200601791Floor Support · corrodedBC-4 CHECK - NR 5949844, CORROSION ON MAIN CABIN LONGITUDINAL BEAM, FR 68, -Y1292. REPLACED MAIN CABIN LONGITUDINAL BEAM, FR 68, -Y1292 IAW A319 SRM 51-72-11.SDR AWXA200601792Floor Support · corrodedBC-4 CHECK - NR 5949853, CORROSION ON MAIN CABIN LONGITUDINAL BEAM, FR 67 - 1 INCH, +Y1292. REPLACED MAIN CABIN LONGITUDINAL BEAM, FR 67 - 1 INCH, +Y1292 IAW A319 SRM 51-42-11.SDR AWXA200601847Skin · delaminatedMAJOR REPAIR - BC-4 CHECK -NR 5950024, DELAMINATION FOUND ON RUDDER RT SIDE PANEL, ABOVE BR 7 NEXT TO FASTENER ROW (FASTENER NR 31), DELAMINATED AREA APROX 81/4 X 5.0 INCHES. REPAIRED RUDDER RT SIDE PANEL ABOVE BR 7 IAW A319 SRM 55-41-00 PAR 9Q(9).SDR AWXA200601782Floor Support · corrodedMAJOR REPAIR - BC-4 CHECK - NR 5949835, CORROSION ON MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR20, -Y254. REPAIRED MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR20, -Y254 IAW A319 SRM 53 -00-14 FIG 204 SHEET 2.SDR AWXA200601783Floor Support · corrodedBC-4 CHECK - NR 5949839, CORROSION ON MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR14+7 INCHES - FR16, +Y503.2. REPLACED MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR14+7 INCHES -FR16, +Y503.2 IAW A319 SRM 51-72-11, 51-42-11 AND DRAWING NR D531-12826.SDR AWXA200601784Floor Support · corrodedBC-4 CHECK - NR 5949841, CORROSION ON MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR21, -Y189. REPLACED MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR21, -Y189 IAW A319 SRM 51-72-11.SDR AWXA200601785Floor Support · corrodedBC-4 CHECK - NR 5949846, CORROSION ON MAIN CABIN LONGITUDINAL BEAM, FR 68, -Y765. REPLACED MAIN CABIN LONGITUDINAL BEAM, FR 68, -Y765 IAW A319 SRM 51-42-11 AND 51-72-11.SDR AWXA200601787Floor Support · corrodedBC-4 CHECK - NR 5949838, CORROSION ON MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR16, +Y254. REPAIRED MAIN CABIN DUMMY RAIL (FLOOR SUPPORT), FR16, +Y254 IAW A319 SRM 53-00-14, FIG NR 204 (SHEET 2).SDR AWXA200601757Sill · corrodedCORROSION ON L2 DOOR CUT OUT LOWER SILL, FS 68-5 INCHES, +Y1732. REPAIRED L2 DOOR CUT OUT LOWER SILL, FS 68-5 INCHES, +Y1732 BETWEEN FS 68-7 INCHES TO FS 68-1 INCH IAW A319 SRM 53-41-14 FIG 201.SDR AWXA200601758Sill · corrodedCORROSION ON R2 DOOR CUT OUT LOWER SILL, FS 68 -2.5 INCHES, -Y1732. REPAIRED DOOR CUT OUT LOWER SILL, FS 68 - 2.5 INCHES - FS 68 - 5 INCHES, -Y1732 IAW A319 SRM 53-41-14 FIG 201 SHEET 3.SDR AWXA200601845Wire · damagedSAL - EEL - BC-4 CHECK - NR 5949617, DAMAGED EMERGENCY LIGHT PATH CABLE, SEAT ROW 6 LT. REPLACED EMERGENCY LIGHT PATH CABLE, SEAT ROW 6 LT IAW A319 AMM 33-51-18 AND 33-51-00.SDR AWXA200601746Wire · brokenLOG NR 4046478 - EMERGENCY LIGHT AT ROW 16L INOP. RETERMINATED WIRES AT CONNECTOR 7260VC7-A IAW AWM 33-51-08 P 020 OPS CHECKED GOOD.SDR AWXA200601719Wire · looseLAX - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE AFT ESCAPE PATH LIGHT WAS INOP. MX RESECURED THE WIRE FOR THE AFT EMERGENCY ESCAPE PATH LIGHTS. OPS CHECK WAS GOOD.SDR AWXA200601720Relay · failedCREW REPORTED THE 2R DOOR WILL NOT REMAIN ARMED IN-FLIGHT (INDICATION). MAINTENANCE REPLACED RELAY 12WN AND ADJUSTED THE LOAD CONTROL HANDLE IAW MM 52-13-820-002.SDR AWXA200601716Connector · looseLAS - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE EMERGENCY LIGHT TEST, LEFT EXTERIOR LIGHT FAILED. MX DISCOVERED THE CONNECTOR ON THE LT SIDE NOT FULLY CONNECTED. MX RESECURED THE CONNECTOR. OPS CHECK WAS GOOD.SDR AWXA200601718Smoke Detector · false indicationLAS - FFW - THE PILOT REPORTED A LAV SMOKE AND A CARGO DETECTION FAULT ON THE UPPER ECAM. MAINTENANCE REPLACED LAV (E) AND (D) FILTERS. MAINTENANCE ALSO REPLACED THE FORWARD CARGO DETECTOR (1WH), OPS CHECK WAS GOOD.SDR YENA200672Epsu · inoperativeDURING POWER DOWN, NOTICED EMERGENCY LIGHTS INOP, WILL NOT TURN ON FROM BOTH COCKPIT OR FAP TEST BOTTON. REMOVED AND REPLACED FWD, AFT AND WING EPSU INCLUDING BATTERIES IAW AMM 33-51-00. OPERATIONS CHECK OK.SDR 2006UALA01652Power Supply · faultyEMERGENCY LIGHT TEST FAULTED AFT LEFT POWER SUPPLY. SUPPLEMENTAL DATA UPDATESDR AWXA200601544Connector · dirtyANC - UES - DURING PUSH BACK, THE NR 2 ENGINE AUTO SHUT DOWN WITH AN ASSOCIATED "ENG FAIL" MSG ON ECAM AND FUEL VALVE INOPERATIVE INDICATION ON ECAM. MAINTENANCE INSPECTED AND CLEANED FUEL METERING UNIT CANNON PLUGS. NR 2 ENGINE LOW PRESSURE VALVE WAS TESTEDSDR AWXA200601351Vane · lack of lubeDURING CLIMB OUT OF LAS, THE CREW RECEIVED BOTH COMPRESSOR 1 AND 2 VANE FAULT. N ADDITION, THE CREW RECEIVED ENGINE 1 AND 2 FADEC FAULT. THE CREW DIVERTED TO PHX. A FOLLOW-UP WAS INITIATED TO LUBE THE VSV ACTUATORS. MAINTENANCE LUBED THE VSV ACTUATORS IAW SDR AWXA200600891Engine · malfunctionedSLC - ENGINE SHUTDOWN - DURING NR 1 ENG START, AFTER STARTER CUTOUT, THE NR 1 ENG FAILED TO STABILIZE AND HUNG. AIRCRAFT AUTO CRANKED AND ABORTED. MAINTENANCE HAD CREW PERFORM 1 AUTO AND 1 MAN START. NR 2 ENGINE HUNG ON BOTH ATTEMPTS. MAINTENANCE REMOVED ASDR AWXA200600846Solenoid Valve · malfunctionedLAS - DURING CLIMB THRU FL210, ENG 2 STALL IND RECEIVED ON ECAM WITH ASSOCIATED YAW. NR 2 ENG EPR FLUX FROM 1.37 TO 1.1 SEVERAL TIMES RAPIDLY. 1 MIN LATER RECEIVED ACARS FAULT MSG, "VSV/BLD VLVE/LPC2". MX PERFORMED BORESCOPE OF A5 ENG HPC IAW AWA TASK CARD SDR AWXA200600776Seal · leakingMCI - DIVERSION - FLT 0001 - CREW REPORTED THAT DURING CRUISE, EN ROUTE TO ORD FROM PHX, THE NR 2 ENG OIL QUANTITY HAD DROPPED 5 QUARTS IN 30 MINUTES. CREW THROTTLED BACK ON NR 2 ENGINE THEN DIVERTED TO MCI. NR 2 ENGINE OIL QUANTITY HAD REACHED 0 WHEN ON FINSDR AWXA200600465Actuator · malfunctionedCREW REPORTED THAT DURING TAKEOFF RECEIVED A NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE PRIOR TO 80 KNOTS, ABORTED TAKEOFF. RETURNED TO THE GATE WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED HIGH POWER PERFORMANCE TESTS IAW AIRBUS 319 TSM 75-30-00-810-843. FAUSDR AWXA200600468Warning Light · false activationFLT 841 - CREW REPORTED THAT DURING TAKEOFF RECEIVED NR 1 ENGINE COMPRESSOR VANE FAULT ON ECAM. ABORTED TAKEOFF UNDER 70 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED HIGH POWER ASSURANCE TESTS IAW AWA TASK CARD F5M71302. OPERASDR AWXA200600466Actuator · lack of lubeCREW REPORTED, RECEIVED A NR 1 ENGINE VANE FAULT AND ABORTED TAKEOFF AT 60 KNOTS. CREW REPORTED NO OTHER ABNORMAL ENGINE READINGS AND OBSERVED NO COMPRESSOR FAULTS. CREW RETURNED TO THE GATE WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT IAW AIRBUS TSM 73-0SDR AWXA200600207Valve · malfunctionedDURING CLIMB, REPORTED RECEIVING AN ECAM MESSAGE FOR " ENG1 BEARING 4 OIL SYS - HI PRESS". RETURNED & LANDED WITHOUT FURTHER EVENT. MX R & R NR 4 BEARING SCAVENGE VALVE ON NR 1 ENG IAW MM 79-23-51. COMPLIED WITH HIGH POWER ASSURANCE TEST IAW AWA TC F5M71312SDR AWXA200600133Blade · lack of lubeOAK - ABORTED TAKEOFF - FLT 855 - CREW REPORTED THAT IMMEDIATELY AFTER FLEX POWER WAS SET RECEIVED ENG 2 COMPRESSOR VANE FAULT. CREW ABORTED T/O AT LESS THAN 10 KNOTS. MAINTENANCE TROUBLESHOT AND PERFORMED VSV BLADE LUBE IAW AMM 75-32-42-640-010.SDR AWXA200501614Actuator · malfunctionedLAX - ABORTED TAKEOFF - FLT 36 - CREW REPORTED THAT DURING TAKEOFF RECEIVED NR 1 COMPRESSOR VANE FAULT, ABORTED TAKEOFF UNDER 70 KNOTS. RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VSV ACTUATOR. OPERATIONALSDR AWXA200501605Switch · defectiveCREW REPORTED THAT THE EMERGENCY EXIT LIGHT CAME ON SHORTLY AFTER DEPARTURE. CAPTAIN TURNED THE LIGHTS OFF THEN ARMED THEM AGAIN. THE EMERGENCY EXIT LIGHT RE-ILLUMINATED. CREW SWITCHED THE LIGHTS OFF UNTIL LANDING. MAINTENANCE REMOVED AND REPLACED THE EMERSDR AWXA200501481Warning System · malfunctionedDURING TAKEOFF, CREW REPORTED ECAM MESSAGE (ENG 1 COMPRESSOR VANE). CREW ABORTED TAKEOFF AT ESTIMATED 60 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING IAW SRM 75-30-00-810-843 AND TASKCARD FSM 71312, NO FAULTSSDR GTIA050266Control Unit · malfunctionedFLIGHT CONTROL FLAP FAULT FOLLOWED BY FLIGHT CONTROL FLAPS LOCKED, COULD NOT GET FLAPS TO EXTEND AFTER ENGINE START PRIOR TO TAXI, TAIL SWAP WITH AIRCRAFT N802NK. FOUND FAULT ON SFCC NR1, RESET THE WING TIP BRAKE AND SYSTEM OPS CHECK GOOD. (K)SDR AWXA200501244Radar · failedDURING CRUISE, ENROUTE, THE WEATHER RADAR FAILED. THERE WERE THUNDERSTORMS, AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR TRANSCEIVER UNIT AND THE WEATHER RADAR CONTROL UNIT IAW AMM 34-41-12 AND 34SDR SIMA200528601A/C Pack · contaminatedON CLIMB OUT FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. RECEIVED LAV SMOKE INDICATION ON EICAS. RAN BOTH ENGINES WITH BOTH PACKS ON TO BURN OUT RESIDUAL OIL FROM BLEED DUCTS. RESIDUAL OIL IN DUCTS WAS FROM THE ENGINE THAT WAS PREVIOUSLY MOUNTED ON THE LTSDR AWXA200501196Actuator · faultyDURING TAKEOFF, AT 70 KNOTS, RECEIVED NR 1 ENG COMPRESSOR VANE FAULT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VSV ACTUATOR IAW AMERICA WEST AIRLINES TASK CARD F5M71312. OPERATI
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