Airbus A320-231
Service difficulty reports · 3,758
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 aircraft_model_key = 'A320231' 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 aircraft_model_key = 'A320231' 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 AWXA200200499Flashlight · inoperativeLAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE LT FORWARD EMERGENCY FLASHLIGHT WAS NOT BLINKING. MAINTENANCE REPLACED THE LT FORWARD EMERGENCY FLASHLIGHT.SDR AWXA200200498Light · inoperativeCMH - EEL - DURING INSPECTION THE L1 DOOR LOWER EMERGENCY LIGHT WAS FOUND TO BE INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR LOWER EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200489Filter · cloggedON CLIMBOUT, CREW RECEIVED ECAM MESSAGE FOR NR 1 ENG BLEED FAULT; BLEED TEMP REACHED 280 DEGREES & CROSSFEED VALVE OPENED; ACFT TURNED BACK TO PHX. MX REPLACED THE FAN AIR THERMOSTAT AND OPERATIONALLY CHECKED OUT SYS BY RUNNING ENG FOR AN EXTENDED PERIOD OF TSDR AWXA200200443Connector · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 L/H WAS FOUND INOPERATIVE. MAINTENANCE FOUND A WALL CONNECTOR DAMAGED WITH A WIRE PULLED OUT FROM BACKSHELL, REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT WALL OF SEAT ROW 22 L/H,SDR AWXA200200439O-Ring · deterioratedLAS - DIVERSION - FLT 0470 - EN ROUTE FROM PHX TO BUR ECAM INDICATED YELLOW HYDRAULIC SYSTEM LOW QUANTITY, AIRCRAFT DIVERTED TO LAS. MAINTENANCE FOUND HYDRAULIC LEAK AT QUICK DISCONNECT (3701GM) ON YELLOW HYDRAULIC SYSTEM MAIN POWER MODULE, REMOVED AND REPLACESDR AWXA200200433Proximity Sensor · malfunctionedPHX - AIR TURNBACK - FLT 0807 - AFTER TAKEOFF FROM PHX EN ROUTE TO SFO PASSING APPROXIMATELY 500 AGL THE FWD CARGO DOOR UNLOCK WARNING CAME ON. AIRCRAFT TURNED BACK TO PHX AND ON DOWNWIND RETURN FOR LANDING THE WARNING LIGHT WENT OUT. MAINTENANCE REPLACED THSDR AWXA200200432Connector · brokenATL - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG AT THE WALL PLUG IN, SEAT ROW 19 L/H, OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-00-710-001.SDR AWXA200200415Outflow Valve · inoperativePHX - AIR TURNBACK - FLT 0239 - AFTER TAKEOFF FROM PHX EN ROUTE TO DTW SKIN AIR VALVE FAULTED WITH AVIONICS VENT ALREADY ON MEL 21-26-02 AND EXTRACT FAN OVERRIDE. ECAM INDICATED MAXIMUM ALTITUDE 10,000 MEA, TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACESDR AWXA200200404Valve · malfunctionedLAX - AIR TURNBACK - FLT 0315 - AFTER TAKEOFF FROM LAX EN ROUTE TO PHX RECEIVED VENT SKIN VALVE AND VENT AVIONICS SYSTEM FAULT ON ECAM, NO CABIN PRESSURE, TURNED BACK TO LAX. MAINTENANCE AT LAX ISSUED MEL 21-26-04, COND. NR 1 (EXTRACT VALVE INOPERATIVE); THISDR AWXA200200379Computer · faultyEN ROUTE FLT CREW RECEIVED ECAM MESSAGE FOR NR 2 ENG BLEED FAULT TEMP AT 70 C AND 70 PSI; DUE TO ICING CONDITIONS AT IND, ACFT TURNED BACK TO PHX. MX TROUBLESHOT & REPLACED NR 2 BLEED MONITORING COMPUTER, BITE CHECK GOOD, NR 2 ENG PRESSURE TRANSDUCER REPLACEDSDR AWXA200200365Ballast · defectivePHX - BURNING SMELL - FLT 0652 - FLIGHT ATTENDANTS NOTICED AN ELECTRICAL BURNING SMELL AT MID CABIN NEAR OVERWING AREA. MAINTENANCE DISCOVERED AND REPLACED A BAD CABIN SIDEWALL LIGHTING BALLAST AT SEAT ROW 7 RT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200359Ballast · faultyPHX - BURNING SMELL - FLT 0467 - DURING FLIGHT, FLIGHT CREW NOTICED A BURNING SMELL SIMILAR TO HOT WIRES AT SEAT ROW 13 LT. MAINTENANCE TROUBLESHOT AND FOUND A BAD CEILING LIGHT BALLAST AT SEAT ROW 13 LT. REPLACED BALLAST IAW AMM 33-21-11-401, OPERATIONAL CHSDR AWXA200200339Ballast · inoperativeABQ - DIVERSION - FLT 0081 - WHILE ENROUTE FROM PHX TO BWI FLIGHT CREW RECEIVED MULTIPLE REPORTS (6+) OF AN INTENSE ELECTRICAL BURNING SMELL IN THE CABIN CENTERED AROUND SEAT ROWS 15-18, SMELL PERSISTED FOR 5-7 MINUTES, PASSENGER ENTERTAINMENT SYSTEM WAS DEACTSDR AWXA200200337Anti-Ice Valve · closedYKM - DIVERSION - EN ROUTE FROM PHX TO SEA LT ENGINE ANTI-ICE VALVE CLOSED, ECAM WARNING OCCURRED AFTER SELECTION OF ANTI-ICE TO ON. TRIED VARIOUS POWER SETTINGS UP TO FULL CLIMB POWER TO OPEN THE ANTI-ICE VALVE, ATTEMPTS WERE UNSUCCESSFUL, DUE TO ICING CONDISDR AWXA200200307Sensor · failedEN ROUTE FROM PHX A WARNING FOR GREEN HYD SYS LOW LEVEL APPEARED ON ECAM. FLT CREW REQUESTED EMERGENCY EQUIP STANDBY AT LANDING, ACFT LANDED WITHOUT EVENT. MX REPLACED THE GREEN HYD SYS LOW LEVEL SENSOR. REPLACED WAS THE GREEN HYD SYS DRAIN VALVE, AND THE QSDR AWXA200200265Seal · leakingPHX - AIR TURNBACK - FLT 0001 - ON CLIMBOUT FROM PHX EN ROUTE TO ORD LT ENGINE OIL PRESSURE INDICATED 300 PSI, AIRCRAFT TURNED BACK TO PHX. MAINTENANCE TROUBLESHOT THE HIGH OIL PRESSURE INDICATION PER AWA ER 26-7920-02091-KL1, THE DIFFERENTIAL PRESSURE TRANSDSDR AWXA200200291Seat Track · corrodedMAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND ON OUTBOARD UPPER LIP OF SEAT TRACK NR2, 2 INCH AFT OF FR 20, Y 765. MAINTENANCE REMOVED CORROSION AND CUTOUT DAMAGED SECTION OF SEAT TRACK, FABRICATED A REPAIR DOUBLER AND PLUG, AND INSTALLED REPAIR PARTS.SDR AWXA200200282Damper · failedYWG - EMERGENCY EVACUATION - DURING C-08 CHECK THE L1 DOOR DAMPER WOULD NOT SNUB. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR DAMPER IAW AMM 52-11-14-401, PRESSURE CHECKED IAW AMM 52-11-14-210-056.SDR AWXA200200281Damper · failedYWG - EMERGENCY EVACUATION - DURING C-08 CHECK THE R1 DOOR DAMPER WOULD NOT SNUB. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR DAMPER IAW AMM 52-11-14-401, PRESSURE CHECKED IAW AMM 52-11-14-210-056.SDR AWXA200200305Floor Support · corrodedYWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON NUTPLATES AND FLOOR SUPPORT AT Y254L, BETWEEN FR 20 AND FR 21. MAINTENANCE REMOVED FLOOR SUPPORT BETWEEN FR 12 TO FR 24. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-72-11, PG. 1 & 2.SDR AWXA200200313Rib · crackedYWG - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND ON LT WING GEAR SUPPORT RIB 5, HOLE NR 82. MAINTENANCE OVERSIZED HOLE TO AND INSTALLED NEW FASTENER IAW AWA ER 26-5721-02093-TB2.SDR AWXA200200321Sill · corrodedYWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON THE L2 DOOR SILL AT FR 68. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM.SDR AWXA200200320Sill · corrodedYWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON THE R2 DOOR SILL AT FR 68. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM.SDR AWXA200200197Indicator · failedLAS - DIVERSION - FLT 790 - "S" - DURING CRUISE STANDBY HORIZON INDICATOR FAILED, AIRCRAFT DIVERTED TO LAS. MAINTENANCE REPLACED STANDBY HORIZON INDICATOR AND PERFORMED AN OPERATIONAL CHECK IAW T/C 34-22-24-04. AIRCRAFT CONTINUED TO PDX WITH OUT INCIDENT. BENCSDR AWXA200200198Skin · dentedPHX - GROUND DAMAGE - "S" - WHILE AIRCRAFT WAS PARKED AT GATE A BAGGAGE CART WAS BLOWN INTO THE AIRCRAFT BY A GUST OF WIND STRIKING THE AIRCRAFT JUST AFT OF THE AFT CARGO DOOR DAMAGING EXTERNAL SKIN AND FRAME FLANGE BETWEEN STR 37 R/H AND STR 38 R/H, FR 30. **SDR AWXA200200348Floor Support · corrodedYWG - MAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AT Y1292 RT, FR 68 TO FR 69. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1, PARA 5.SDR AWXA200200347Floor Support · corrodedYWG - MAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND IN 7 PLACES ON FLOOR SUPPORT RAIL AT Y254, FR 16 TO FR 20, INCLUDING THE SPLICE REPAIR. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2.SDR AWXA200200310Plate · crackedYWG - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND ON THE LT AFT L2 DOOR SHEAR PLATE. MAINTENANCE REMOVED SHEAR PLATE, FABRICATED A NEW SHEAR PLATE AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1 AND SRM 51-72-11 PG 1 & 2.SDR AWXA200200309Plate · crackedYWG - MAJOR REPAIR - DURING C-08 CHECK A 6 INCH CRACK WAS FOUND ON THE RT AFT SIDE OF THE R2 DOOR SHEAR PLATE. MAINTENANCE REMOVED SHEAR PLATE, FABRICATED A NEW SHEAR PLATE AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1, SRM 51-72-11 PG 1 & 2.SDR AWXA200200328Flange · crackedYWG - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND ON THE RT HORIZONTAL STABILIZER L/E 3 FROM OUTBOARD END ON LOWER L/E PANEL MATING SURFACE. MAINTENANCE REMOVED DAMAGED AREA AT STAB STA 6009, RIB 14, FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 26-SDR CA020308002Pump · failed(CAN) DURING INITIAL ROLL AT 1.2 EPR THE ECAM MESSAGE "COMP VANE NR 2" APPEARED ON THE UPPER ECAM SCREEN. THE ENGINE EXPERIENCED A LIGHT COMPRESSOR STALL. THE TAKE-OFF WAS REJECTED AT 50 KTS AND THE AIRCRAFT RETURNED TO THE GATE WITH BOTH ENGINES RUNNING. MAINSDR AWXA200200312Seat Track · corrodedYWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND AT RECESSED NUT HOLES ON SEAT RAIL Y1292 RT, FR 64 TO FR 66. MAINTENANCE REMOVED SEAT RAIL Y1292 RT BETWEEN FR 64 AND FR 66, FABRICATED A NEW SEAT RAIL AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2, SDR AWXA200200311Seat Track · corrodedYWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON RECESSED NUT HOLE OF SEAT RAIL AT FR 64, Y765. MAINTENANCE REMOVED SEAT RAIL AT FR 64, Y765 RT, FABRICATED A NEW SEAT RAIL, AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2 AND SRM 51-42-11 PG 1.SDR AWXA200200190B-Nut · looseIAH - DIVERSION - FLT 555 - C - EN ROUTE FROM MIA TO LAS AT FL 350 ECAM MESSAGE FOR GREEN HYDRAULIC SYSTEM LOW PRESSURE INFLIGHT, POWER TRANSFER UNIT AND NR 1 ENGINE HYDRAULIC PUMP WERE TURNED OFF AND AIRCRAFT DIVERTED SAFELY INTO IAH. MAINTENANCE FOUND 2 EACSDR AWXA200200189Dampener · leakingYWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE L1 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. MAINTENANCE REMOVED, REPLACED, AND RIGGED THE L1 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200188Dampener · leakingYWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE R2 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. MAINTENANCE REMOVED, REPLACED, AND RIGGED THE R2 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200185Dampener · leakingYWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE L2 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. MAINTENANCE REMOVED, REPLACED AND RIGGED THE L2 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200182Hydraulic Line · burstON FINAL TURN INTO PHX WHEN LANDING GEAR WAS EXTENDED ECAM INDICATED A LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED UNEVENTFULLY WITH ALTERNATE HYDRAULIC SYSTEM OPERATING NORMALLY. NOSE WHEEL STEERING INOPERATIVE AFTER SDR AWXA200200178Power Supply · dischargedYWG - EEL -C- DURING C-08 CHECK EMERGENCY ESCAPE PATH LIGHTING AT ROWS 13, 17, 19, 24 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-401, OPERATIONAL CHECK PERFORMED IAW T/C F1C33301.SDR AWXA200200161Housing · brokenPHX - EEL - "C" - DURING INSPECTION EMERGENCY ESCAPE LIGHT WAS FOUND BROKEN AT SEAT ROW 7 L/H. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE LIGHT HOUSING AT SEAT ROW 7, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200187Fitting · wornYWG - MAJOR REPAIR - "C" - DURING C-02 INSPECTION CENTER JOINT FITTINGS FOR THE TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WERE FOUND WORN BEYOND DRAWING LIMITATIONS. L/H DIMENSIONS RANGE FROM 2.4746' TO 2.4751", R/H SIDE DIMENSIONS RANGE FROM 2.6007" TO 2.6009"SDR AWXA200200129Floor Support · corrodedYWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 66 AND FR 67. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 51-74-00, PG 1. REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRICSDR AWXA200200133Seat Track · corrodedYWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT SEAT TRACK Y254 L/H FR 20. MAINTENANCE REMOVED CORROSION FROM FLOOR SUPPORT SEAT TRACK AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPORTSDR AWXA200200132Seat Track · corrodedYWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SEAT TRACK Y765 R/H FR 16. MAINTENANCE REMOVED FLOOR SEAT TRACK Y765 R/H, FABRICATED NEW FLOOR SEAT TRACK AND INSTALLED REPAIR IAW DWG 53112782.SDR AWXA200200131Floor Support · corrodedYWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 15 AND FR 19. MAINTENANCE REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53112782.SDR AWXA200200130Floor Support · corrodedYWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y254 LT BETWEEN FR 15 AND FR 21. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPORT BEAM Y254 LT, FABRSDR AWXA200200181Frame · damagedYWG - MAJOR REPAIR - C - DURING C-08 CHECK TOOLING HOLES AT FR 38-40 LT TO RT WERE FOUND TO BE OVERSIZED. COLD EXPANDED THE HOLES PER SRM 51-48-00, MAINTENANCE DRILLED HOLES TO APPLICABLE DIAMETER, COUNTERSUNK HOLES TO A MAXIMUM OF 0.4MM, INSTALLED FASTENERS SDR AWXA200200217Web · crackedYWG - MAJOR REPAIR - C - DURING C-02 CHECK A CRACK WAS FOUND ON LT OUTBOARD WEB BELOW THE AFT GALLEY, FR 68-69.SDR AWXA200200146Web · crackedYVR - MAJOR REPAIR - C - DURING C-02 CHECK A CRACK WAS FOUND ON THE LT OUTBOARD WEB JUST BELOW THE AFT GALLEY FR 68-69. MAINTENANCE REMOVED CRACKED WEB, FABRICATED NEW WEB, AND INSTALLED REPAIR IAW SRM 51-72-00, AND SRM 53-41-14, PG 37 & 41.SDR 2002F00267Smoke Detector · activatedAFT CARGO AND LAVATORY SMOKE WARNING ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT FROM MSP TO MCO. (M)
Back to Airbus A320-231