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 AWXA200500903Web · corrodedSAL - DURING C4 CHECK DISCOVERED CORROSION ON WEB IN CABIN LOCATED AT FS 69+16", STRINGER 23L, Y1200. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND REPLACED THE WEB LOCATED AT FR 69+16", STRINGER 23L, Y1200 IAW AIRBUS 3SDR AWXA200500802Landing Gear · malfunctionedAFTER TAKEOFF MLG HANDLE UP, ECAM CAUTION: L/G GEAR NOT UPLOCKED. CYCLED MLG PER ECAM ALL GEAR UP & LOCKED OK. MX CYCLED MLG, OPS CHK GOOD. ACFT RETURNED TO SERVICE. WITHIN 8 CYCLES DISCREPANCY RETURNED. ACFT MX FERRIED BACK TO PHX. SEVERAL SENSORS INSPESDR AWXA200500780Module · failedAFTER TAKEOFF, TRIED TO RAISE MLG, GEAR UNLOCKED ILLUMINATED FOR NLG. CYCLED GEAR PER ECAM, GEAR CAME UP & LOCKED. LANDED IN SEA WITHOUT FURTHER INCIDENT. A/C FERRIED BACK TO PHX. MX R & R MLG CONTROL MODULE IAW AIRBUS MM 32-30-00. TEAR DOWN REPORT CONFISDR AWXA200500757Compressor · dirtyODOR DETECTED. DURING FLIGHT, PACKS CREATING GYM SOCK ODOR WITH PASSENGERS COMPLAINING. MAINTENANCE OPERATED PACKS WITH APU BLEED AIR AND ENGINE BLEED AIR. DISCOVERED ODOR COMING FROM NR 1 ENGINE BLEED AIR SOURCE, ABOVE IDLE. INSPECTED NR 1 ENG AND UNABLE TSDR AWXA200500751Cable · looseDURING 8-DAY CHECK, FOUND R2 DOOR SLIDE CABLE LOOSE. MAINTENANCE REMOVED AND REPLACED R2 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304.SDR AWXA200500750Battery Pack · dischargedDURING 8-DAY CHECK, FOUND BOTH LT AND RT OVERWING SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT (11WL) AND RT (12WL) BATTERY PACKS IAW AIRBUS MM 33-51-38-04. OPERATIONAL TESTS WERE GOOD.SDR AWXA200500727Uplock · malfunctionedDURING GEAR RETRACTION AFTER TAKEOFF, NOSE GEAR STAYED DOWN & ALL GEAR DOORS STAYED DOWN. MX R & R THE NLG DOOR UPLOCK ASSY IAW AWXA TASK CARD F4N32301. OPS CHECKS GOOD. TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL OF NLG DOOR UPLOCK ASSEMBLY. FOUND BINDISDR AWXA200500716Battery · inoperativeDURING 8 DAY CHECK EMERGENCY EXIT LIGHTS FAILED CIDS TEST PANEL (INT LEADS EMER L). MX REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW TASK CARD R1C33303. ALSO, REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW TASK CARD A1C33302. OPS TEST FROM CIDS PANSDR AWXA200500659Battery · dischargedDURING 4-DAY CHECK, FOUND RIGHT EMERGENCY SUPPLY POWER UNIT HAD LOW BATTERY. MAINTENANCE REMOVED AND REPLACED RIGHT ESPU BATTERY IAW AIRBUS MM 33-51-38-04 STEP 7. OPERATIONAL CHECK GOOD.SDR AWXA200500653Pressure Switch · faultyATL - AIR TURN BACK - FLT 617 - ON CLIMB-OUT FROM ATL EN ROUTE TO PHX RECEIVED YELLOW ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE INDICATION, TURNED BACK TO ATL FOR REPAIR. MAINTENANCE FOUND YELLOW HYDRAULIC RESERVOIR OVER SERVICED, SERVICED CORRECTLY IAW TASK SDR AWXA200500657Wire · brokenPHX - EEL - DURING 8-DAY CHECK, FOUND EMERGENCY EXIT ROW LIGHT INOP AT SEAT 26. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT. OPERATIONAL CHECKS GOOD.SDR AWXA200500594Epsu · faultyPHX - EEL - DURING 8-DAY CHECK, A LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK. OPERATIONAL CHECK WAS GOOD. BATTERY PACK INFORMATION: MANUFACTURER: DIEHL GMSDR AWXA200500592Selector Valve · malfunctionedEN ROUTE, PILOTS REPORTED DURING CLIMB & DURING MLG RETRACTION A GRINDING NOISE & ECAM MESSAGE MLG NOT UPLOCKED. CYCLED MLG IAW MX AND UPON RETRACTION SAME NOISE ON RT MLG DOWN. ACFT RETURNED & LANDED WITHOUT INCIDENT. MX R & R MLG SELECTOR VALVE IAW AMM. SDR AWXA200500591Actuator · faultyDURING CLIMB SELECTING GEAR UP & NLG FAILED TO RETRACT & RECEIVED A RED UNLOCK LIGHT. SELECTED GEAR DOWN & GEAR FAILED TO EXTEND (MAINS, NOSE SHOWED GREEN/RED UNLK.) SELECTED GEAR UP & GEAR RETRACTED WITH NORMAL INDICATIONS. SELECTED GEAR DOWN WITH NORMAL ESDR AWXA200500570Wire · brokenPHX - EEL - DURING ROUTINE MX ROW 17 ABC EMERGENCY EXIT ESCAPE PATH LIGHTING WAS INOPERATIVE. TERMINALS CONNECTING WIRES TO SEAT ASSEMBLY INOPERATIVE. MAINTENANCE RETERMINATED TERMINALS AT ROW 17 A,B,C IAW AMM 20-48-14. OPERATIONAL CHECK WAS GOOD.SDR AWXA200500568Interface Unit · faultyEN ROUTE TO EWR PILOTS REPORTED A NR 2 ENGINE EIU FAULT. ACFT RETURNED TO PHX WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ENGINE INTERFACE UNIT IAW AMM 73-25-3-04 AND PERFORMED A POWER ASSURANCE TEST IAW AWA TASKCARD NR F5M71302. OPERSDR AWXA200500559Flashlight · inoperativeLAS - EMERGENCY EQUIPMENT DURING 8-DAY CHECK, THE AFT FLIGHT ATTENDANT FOLD OUT JUMP SEAT EMERGENCY FLASHLIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500560Wire · brokenPHX - EEL - DURING E-03 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE CONNECTOR OF EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500536Wire · brokenSEA - EEL - DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM-A BROKEN WIRE WAS FOUND AT THE WALL CONNECTOR FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT. MAINTENANCE REPINNED THE EMERGENCY ESCAPE PATH LIGHT WIRE TO THE WALL CONNECTOR AT SEAT ROW SDR AWXA200500527Engine · failedON TAKEOFF AT SEA EN ROUTE FOR PHX AFTER APPLYING TAKEOFF THRUST FLIGHT CREW HEARD A LOUD BANG ON LT SIDE OF AIRCRAFT FOLLOWED BY A BURNING ODOR, REJECTED TAKEOFF AT 20 KTS, ANOTHER AIRCRAFT REPORTED SEEING FIRE COMING OUT OF THE NR 1 ENGINE, FIRE FIGHTERS RESSDR AWXA200500501Power Supply · dischargedLAS - EEL - FLIGHT CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.SDR AWXA200500380Generator · damagedON TAKEOFF AT LAS EN ROUTE TO MSP RECEIVED CLASS I ECAM MESSAGE ELECT IDG OIL LOW PRESSURE, REJECTED TAKEOFF AT 50 KTS. ISSUED MEL 24-20-01, COND 2 NR 1 IDG INOP. MAINTENANCE TROUBLESHOT THE NR 1 IDG PER TSM TASK 24-20-00-810 AND FOUND METALIC PARTICLES IN TSDR AWXA200500375Servo · malfunctionedON APPROACH INTO PHX EN ROUTE FROM ATL RECEIVED ECAM MESSAGE FOR NOSE WHEEL STEERING FAULT, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE CENTRALIZED FAULT DISPLAY SYSTEM FAULTED BOTH BRAKE STEERING CONTROL UNIT CHANNELS FOR NLG SSDR AWXA200500351Epsu · failedLAS - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS OVER L-2 AND R-2 DOOR DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED AFT LT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD.SDR CA050321004Compressor · failed(CAN) THE CAPTAIN REPORTED HEARING A LOUD BANG FROM ENG NR 2 WITH INCREASED EGT, 2 RESTARTS WERE ATTEMPTED WITH NO SUCCESS AND THE FIRE HANDLE WAS PULLED (BOTTLES WERE NOT DISCHARGED). DAMAGE TO THE 3RD AND 4TH STAGE HIGH PRESSURE COMPRESSOR WAS CONFIRMED.SDR AWXA200500346Cable · loosePHX - EEL - DURING E-01 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500341Solenoid · ratchetingAPPROACH, SELECTING FLAPS POSITION 1 RECEIVED ECAM SLAT LOCKED WING TIP BRAKE, DECLARED EMERGENCY & LANDED. R&R NR 1 SLAT/FLAP CONTROL COMPUTER. PERF SFCC 1&2 GRD SCAN, SLATS NO FAULTS. T/E FLAPS FAULTED LT PROXIMITY SENSOR 37CV. BITE TEST LGCIU NR 1, FAULSDR AWXA200500339Wire Harness · brokenSEA - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT WALL CONNECTION, REPINNED CONNECTOR, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500337Connector · defectivePHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT WALL SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500260Brake Assy · out of adjustON APPROACH INTO PHX EN ROUTE FROM ATL WHEN SELECTING FLAPS 1 THE SLATS LOCKED OUT AT SLATS 1, FOLLOWED ECAM INSTRUCTIONS AND PERFORMED PRECAUTIONARY LANDING. MAINTENANCE TROUBLESHOT SLAY SYS PER TSM 27-81-00-810-815 AND FOUND LT WING TIP BRAKE ASSY BREAK OUTSDR AWXA200500257Landing Gear · inoperativeAIR TURNBACK, ON CLIMBOUT OF ORD EN ROUTE TO PHX AFTER SELECTING LANDING GEAR TO THE UP POSITION THE NOSE GEAR WOULD NOT RETRACT, TURNED BACK TO ORD FOR REPAIR. AIRCRAFT CURRENTLY OUT OF SERVICE. MAINTENANCE REPACKED NLG SHOCK STRUT IAW T/C R4N32305, ALSO REPSDR AWXA200500208Bar · bindingPHX - EES - DURING 4-DAY CHECK THE L-2 EMERGENCY SLIDE GIRT BAR FAILED RETRACTION TEST. MAINTENANCE REMOVED AND REPLACED L-2 EMERGENCY SLIDE GIRT BAR IAW T/C R1C25304, FUNCTIONAL TEST WAS GOOD.SDR AWXA200500230Actuator · trippedON APPROACH, RECEIVED ECAM MESSAGE FOR F/CTL SLATS FAULT; DECLARED PRECAUTIONARY EMERGENCY LANDING AND LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT SLAT SYS PER TSM 27-81-00-810-810, SLAT SYSTEM OPERATED NORMALLY. INSP OF SLAT ACT FOUND RT OTBD NR 4 SLAT ACTSDR AWXA200500183Sign · inoperativeORD - EMERGENCY EXIT LIGHT INOPERATIVE AT AFT OVERWING EXIT, RIGHT SIDE WALL MOUNTED. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT AFT OVERWING EXIT; OPERATIONAL CHECK WAS GOOD.SDR AWXA200500090Control Unit · faultyON LANDING, RECEIVED ECAM MESSAGE "BRAKING/STEERING CONTROL UNIT (BSCU) FAULT CH. 2 INCHES, WHEN CLEARING RUNWAY BRAKES LOCKED UP MOMENTARILY. MAINTENANCE REMOVED AND REPLACED THE BSCU IAW AMM 32-42-34-04, OPERATIONAL CHECK WAS GOOD. COULD NOT DUPLICATE REASSDR AWXA200500092Cable · brokenCMH - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TERMINAL FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500073Epsu · dischargedSEA - EEL - MX REPORTED LT AFT EPSU WAS FAULTING (INTERNAL LOAD) AND ASSOCIATED FLOOR PATHWAY LIGHTS DID NOT ILLUMINATE. MX REMOVED AND REPLACED THE AFT LT EMERGENCY POWER SUPPLY UNIT (13WL) IAW AWA TASKCARD R1C33303. OPERATIONAL CHECK WAS GOOD.SDR AWXA200500085Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK BETWEEN FR 40 AND FR 42. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 40 TO FR 42; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SDR AWXA200500040Valve · bypassingAFTER TOUCH DOWN, THE BRAKES LOCKED UP ON TAXIWAY, AIRCRAFT UNABLE TO TAXI TO GATE, SHUTDOWN AND DISEMBARKED PASSENGERS ON TAXIWAY. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE SELECTOR VALVE IAW AMM 32-45-51, LEAK AND OPERATIONAL CHECKS WERE GOOD. CONFIRMSDR AWXA200500096Floor Panel · delaminatedSAL - MAJOR REPAIR - DURING C-04 CHECK FOUND PASSENGER CABIN FLOOR PANEL 262FF DELAMINATED. MAINTENANCE REMOVED DAMAGED AREA OF FLOOR PANEL 262FF, PERFORMED BOND REPAIR IAW A320 SRM 53-02-00, FIG 201.SDR AWXA200500094Fitting · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND AROUND HOLE OF L-1 DOOR LOWER SILL SUPPORT ANGLE (FITTING) BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED CORRODED L-1 DOOR LOWER SILL SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT SUPPORT ANGSDR AWXA200500089Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FR 21 AND FR 24. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FR 21 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAWSDR AWXA200500087Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD SEAT TRACK BETWEEN FR 42 AND FR 44. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 42 TO FR 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART ISDR AWXA200500084Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM -Y189 BETWEEN FR 20 AND FR 21. MAINTENANCE REMOVED CORRODED LONGITUDINAL FLOORBEAM -Y189 FROM FR 20 TO FR 21; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED SDR AWXA200500082Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON CABIN FLOOR SEAT TRACK Y765 BETWEEN FR 20 AND FR 23. MAINTENANCE REMOVED AND REPLACED SEAT TRACK Y765 FROM FR 20 TO FR 23 IAW A320 SRM 51-72-11.SDR AWXA200500057Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON CABIN FLOOR STRUCTURE SEAT TRACK Y1292 LT BETWEEN FS 20 AND FS 22. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FS 20 TO FS 22; FABRICATED A NEW REPLACEMENT SEAT TRACK PER DWG D53112812; ISDR AWXA200500054Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-4 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM (DUMMY RAIL) -Y1379.5 RT AT FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL -Y1379.5 RT AT FS 16; FABRICATED A NEW REPLACEMENT DUMMY RAIL; INSTALLED REPAIR PART IAWSDR AWXA200500041Floor Support · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON PASSENGER CABIN LONGITUDINAL FLOOR SUPPORT BEAM Y254 BETWEEN FS 16 AND FS 20. MAINTENANCE CUTOUT DAMAGE IN FLOOR SUPPORT BEAM Y254 FROM FS 16 TO FS 20; FABRICATED A FILLER AND REPAIR ANGLES; INSTALSDR AWXA200500098Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK, CORROSION WAS FOUND ON SEAT RAIL BEAM ASSEMBLY -Y765 AT FR 64+14". MAINTENANCE REMOVED DAMAGED AREA OF SEAT RAIL UPPER FLANGE -Y765 FROM FS 64 TO FS 65; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW ER 26-5341-05SDR AWXA200500088Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM Y1292 AT FR 66. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 AT FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472040; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.
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