Airbus A320-231
Service difficulty reports · 3,758
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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 AWXA0002173Seat Track · corrodedFR 20 Y765 LT SEAT TRACK CORRODED. REPLACED SEAT TRACK NR 1 FROM FR 16 TO 20 AS PER SRM 53-11-15 PAGE 6.SDR AWXA0002120Skin · dentedDENT IN FUSELAGE AT FRAME 23 BETWEEN STRINGERS 25L & 24L. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED SKIN DOUBLER REPAIR AS PER A320 SRM 53-00+10 FIGURE 203 PAGES 206C TO 208B PAINTED AS PER AMM 51-75-00-001.SDR AWXA0002110Seat Track · corrodedFR Y765 LT SEAT TRACK CORRODED. REPLACED SEAT TRACK NR 1 FROM FR 16 TO FR 20 AS PER SRM 53-11-15 PAGE 6.SDR AWXA0002204Transformer · failedBOS- AIR TURNBACK - FLT 442 - AFTER TAKEOFF FROM BOS EN ROUTE TO PHX THE CREW GOT A TRANSFORMER RECTIFIER 1 (TR1) FAILURE INDICATION AND RETURNED TO BOS. IN BOS MAINTENANCE TROUBLESHOT AND REPLACED TR1 PER AMM 24-32-51-401. THE SYSTEM OPERATIONALLY CHECKED NSDR AWXA0002172Floor Support · corrodedFR 20 TO FR 21 Y-1732 R/11 FLOOR SUPPORT CORRODED. REPAIRED AS PER AWA ER 26-5311-01277-DL1.SDR AWXA0001968B-Nut · loosePHX - AIR TURNBACK - FLT 682 - AFTER TAKEOFF FROM PHX DURING CLIMB EN ROUTE TO EWR THE YELLOW HYDRAULIC SYSTEM QUANTITY STARTED TO DECREASE AND BECAME DEPLETED. THE AIRCRAFT WAS RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND SIGNS OF LEAKASDR AWXA0001966Turbine · damagedSEA - ENGINE FAILURE - DIVERTED FLIGHT. EN ROUTE FROM YVR TO PHX THE NR 2 ENGINE EXCEEDED EGT LIMITS FOLLOWED BY ENGINE STOPPAGE. THE AIRCRAFT DIVERTED TO SEA MAKING AN UNEVENTFUL LANDING. IN SEA THE ENGINE WAS INSPECTED AND FOUND TO HAVE EXTENSIVE TURBINE SDR AWXA0001953Floor Support · corrodedAFT CABIN FLOOR PANEL SUPPORT AT Y-1732R/H FR 66 SCREWS HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .100 (BEYOND LIMITS AS PER A320 SRM 51-72-11 PG 1). REPLACED BEAM AS PER A320 SRM 51-42-11 PAR 6.SDR AWXA0001999Floorbeam · corrodedAFT CABIN FLOOR PANEL SUPPORT AT Y-1732 RT FR 66 SCREW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .100 INCH (BEYOND LIMITS AS PER SRM 51-72-11 PG 1). REPLACED BEAM AS PER A320 SRM 51-42-11 PAR 6.SDR AWXA0001998Floor Support · corrodedAFT CABIN FLOOR PANEL SUPPORT AT Y-765 LT FR 66 TO FR68 SCEW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .035 INCH (BEYOND LIMITS AS PER A320 SRM 53-41-14). REPLACED BEAM AS PER A320 SRM 51-42-11 PG 1.SDR AWXA0001967Proximity Switch · faultyCMH- DIVERTED FLIGHT - FLT 280- EN ROUTE FROM PHL TO LAS THE CREW GOT A CLASS 1 LEVEL 2 FORWARD CARGO DOOR ECAM MESSAGE. AIRCRAFT PRESSURIZATION WAS NORMAL. THE AIRCRAFT DIVERTED TO CMH MAKING AN UNEVENTFUL LANDING. IN CMH MAINTENANCE VERIFIED THE CARGO DOOSDR AWXA0001997Floor Support · corrodedFWD GALLEY FLOOR SUPPORT AT Y-81 FR 14R, 15R AND 16R CORRODED. FWD GALLEY FLOOR SUPPORT AT Y-81 FR12R-16R REPLACED AS PER A320 SRM 53-11-15 FIG 203.SDR AWXA0001996Floor Support · corrodedAFT CABIN FLOOR SUPPORT AT Y1162 FR 66R AND 69R SCREW CLIP ATTACH HOLE CORRODED. AFT GALLEY FLOOR SUPPORT AT Y1162 FR66R-69R REPLACED AS PER A320 SRM 51-42-11 PAGE 1.SDR AWXA0001995Seat Track · corrodedD: Fwd galley floor support at Y1292 Fr 14R and 16R corrodedC: Fwd galley support/seat track at Y1292 FR12R-16R replaced as per A320 SRM 53-11-15 fig. 203SDR AWXA0001994Stringer · misdrilledD: Fr 66 L/H STR 43 has double drilled holesC: Stringer repaired as per SRM 53-00-13 Fig. 201 from sta .3152 to 3167SDR AWXA0001993Floor Support · damagedAFT CABIN FLOOR SUPPORT AT Y1292 RT FR 68 SCREW HOLES DAMAGED. REPLACED FLOOR SUPPORT PER SRM 53-41-11.SDR AWXA0001883Warning System · false activationPHX- AIR TURNBACK - FLT 752- AFTER TAKEOFF, ECAM MESSAGE AFT CARGO DOOR APPEARED AND THE AIRCRAFT WAS RETURNED TO PHX. IN PHX MAINTENANCE INSPECTED THE AFT CARGO DOOR TO ENSURE IT WAS FULLY CLOSED AND LOCKED, WHICH IT WAS. THE AFT CARGO DOOR INDICATION WAS PSDR AWXA0001854Pilot Valve · leakingPHX - AIR TURNBACK - 6/5/01 - FLT 253 - EN ROUTE TO PHL ECAM MSG DISPLAYED HYD YELLOW SYS LOW LEVEL; YELLOW HYD QUANTITY INDICATED IN THE AMBER BAND; CREW COMPLIED W/ THE ECAM ACTIONS & RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MX INSPECTED THE A/C AND FOSDR AWXA0001840Windshield · crackedDTW - unscheduled landing - 6/7/01 - FLT 55 - en route from JFK to LAS the First Officer's NR 1 window outer pane cracked and the aircraft diverted to DTW making an uneventful landing. window changed and aircraft returned to service.SDR AWXA0001826Vor System · malfunctionedPHX - AIR TURNBACK - 6/2/01 - FLT 73 - ON DEPARTURE CLIMBOUT OF PHX THE AIRCRAFT LOST VOR NR 1, VOR NR 2, ILS NR 1 & ILS NR 2; THE AIRCRAFT RETURNED TO PHX. IN PHX MAINTENANCE RESET NR 1 & NR 2 RMP NAV SWITCHES AND CIRCUIT BREAKERS; CYCLED NR 1 & NR 2 FMGC CISDR AWXA0001813Web · gougedFRAME 66 AT UPPER FWD CORNER OF L2 DOOR, WEB AND RIVETS DAMAGED. REPAIRED IAW AWA ER 26-5345-01150-DD1; FINISH RESTORED IAW AMM 55-70-00 PG 1.SDR AWXA0001812Skin · dentedFUSELAGE SKIN DENTED AT LAP JOINT (APPROX FR 28) BELOW AFT EDGE OF C1 DOOR CUTOUT. EVIDENCE OF PRESSURE LEAK. REPAIRED IAW SRM 53-00-11 PARA 4E FIG 211.SDR AWXA0001811Floorbeam · corrodedLIGHT SURFACE CORROSION ON TOP OF FLOORBEAM C20 BL -Y254. CORROSION CLEANED UP, MAT LOSS BEYOND LIMITS. FRAME REPAIRED IAW SRM 53-11-14 FIG 201 PG 203-208; REPAIRED IAW AMM 51-75-00-001.SDR AWXA0001810Seat Track · corrodedLIGHT SURFACE CORROSION ON TOP OF FLOOR TRACK AT FR 20 BL -Y1292. CORROSION CLEANED UP, MAT LOSS BEYOND LIMITS. TRACK FABBED IAW DWG D53112782200; INSTALLED IAW SRM 51-42-11 PG 1.SDR AWXA0001809Floor Support · corrodedLIGHT SURFACE CORROSION ON TOP OF FLOOR SUPPORT AT FR 14 BL -503.2. REPLACED IAW SRM 51-42-11 PG 1.SDR AWXA0001808Fitting · corrodedRT WING NR 2 FLAP CANOE AFT ATTACH LINK LEVER ASSY WORN AT FLAP FITTING AND ATTACH BRACKET. REPAIRED IAW AWA ER 26-5751-01149-KB1 -- ADDITIONAL P/N: D5757055500300.SDR AWXA0001807Floorbeam · corrodedAFT GALLEY AREA AT FR 68 FLOORBEAM Y765 CORRODED AT HOLE (RT INBD FLOOR TRACK BEAM). REPLACED FLOORBEAM IAW A320 DWG D534721932000.SDR AWXA0001695Warning Light · illuminatedMSP - ABORTED TAKEOFF, THE AFT CARGO LIGHT APPEARED AFTER APPLYING T/O POWER ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE DOOR AND OPERATED IT NUMEROUS CYCLES; THE OPERATION AND INDICATIONS WERE NOSDR AWXA0001655Windshield · crackedDEN - DIVERTED FLIGHT - 5/1/01 - FLT 58 - EN ROUTE FROM LAS TO JFK THE CAPTAIN''S NR 1 WINDSHIELD OUTER PANE CRACKED AND THE AIRCRAFT MADE AN UNSCHEDULED LANDING IN DEN. IN DEN MAINTENANCE REMOVED AND REPLACED THE CAPTAIN''S NR 1 WINDSHIELD IAW AMM 56-11-11-4SDR AWXA0001619Rib · crackedNR 2 PYLON RIB NR 14 CRACKED. DAMAGED RIB REPLACED IAW SRM 51-72-11 AND REPAIR ACTION IAW AWA ER 26-5453-01103-JS3.SDR AWXA0001618Floor Support · corrodedFLOOR PANEL SUPPORT Y 254 RT FR 16-20 CORRODED. CORROSION REMOVED IAW SRM 51-74-00 - FOUND TO BE OUT OF LIMITS; FABBED AND INSTALLED FLOOR PANEL SUPPORT IAW SRM 53-11-14 AND DWG D53110858.SDR AWXA0001617Floor Support · corrodedFLOOR PANEL SUPPORT Y 254 LT FR 16-20 CORRODED. FABBED AND INSTALLED NEW FLOOR SUPPORT IAW DWG 531128182.SDR AWXA0001616Seat Track · corrodedNR 3 SEAT TRACK FRAME 20 CORRODED. SEAT TRACK FABBED IAW DWG NR 53112782; INSTALLED IAW SRM 51-72-11.SDR AWXA0001615Plate · crackedLT CABIN FR 68 O/B SHEAR PLATE CRACKED. FABBED AND INSTALLED SHEAR PLATE IAW DWG 53480020.SDR AWXA0001612Warning Light · illuminatedPHX - EMERGENCY LANDING - 4/10/01 - EN ROUTE FROM ORD TO PHX THE FLIGHT CREW GOT AN ECAM WARNING AND CAUTION LIGHT FOR THE GREEN HYD SYSTEM RESERVOIR OVERHEAT. THE CREW CALLED AN EMERGENCY LANDING; THE CREW CYCLED THE GREEN HYD SYSTEM SWITCH AND THE GREEN SYSSDR AWXA0001601Power Supply · faultyPHX - 4/5/01 - DURING MAINTENANCE OPERATIONAL CHECK ESCAPE PATH LIGHTS AT SEAT ROW 3L, 7L & 26L AS WELL AS OVERHEAD LIGHT AT 11L FAILED TO ILLUMINATE. THE EMERGENCY LIGHT POWER SUPPLY UNIT AT POSITION NR 4 WAS REPLACED AND FUNCTIONAL CHECKS WERE GOOD.SDR AWXA0001598Fmu · failedSEA - ABORTED TAKEOFF - 4/2/01 - NR 2 ENGINE FLAMEOUT. ON TAKEOFF AFTER SETTING TAKEOFF POWER AND ABOUT 60 KTS THERE WAS A SURGE ON NR 2 ENGINE AND IT SHUT DOWN; THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. THE POST FLIGHT REPORT FAULTED THE NR 2 ENGINSDR AWXA0001568Actuator · leakingD: PHX - AIR TURNBACK - 3/31/01 - EN ROUTE FROM PHX TO BOS THE AIRCRAFT LOST GREEN HYDRAULIC SYSTEM QUANTITY AND RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE LT YAW DAMP SERVO ACTUATOR LEAKING AT THE OUTPUT SHAFT; THE SERVO ACTUATOR WASSDR CA010426008Terminal Block · melted(CAN) THE FORWARD GALLEY OVENS WERE FOUND TO BE INOPERATIVE BY THE FLIGHT ATENDANTS ON THE FLIGHT. THE ENGINEERS TROUBLESHOOTING THE DEFECT FOUND FWD GALLEY FEEDER D BREAKER POPPED. FURTHER INVESTIGATION FOUND TERMINAL BLOCK 2752VT STUD 8 MELTED, AND THE TERMISDR AWXA0001566Handle · misalignedC1 DOOR UPPER LOCKING SHAFT AFT SUPPORT FITTING BORE FOUND IN MISALIGNMENT TO SHAFT. REPAIRED IAW AWA ER 26-5231-01087-5-S51.SDR 20010430AP002Slide · deployedFLT 962 - MSP - R1 DOOR EMERGENCY EVACUATION SLIDE WAS INADVERTENTLY DEPLOYED WHILE ACCOMPLISHING OTHER MAINTENANCE. REMOVED AND REPLACED R1 DOOR EMERGENCY EVAUCATION SLIDE. SYSTEM OPERATES NORMAL. (M)SDR AWXA0001508Battery · dischargedD: EMERGENCY LIGHT TEST FAILS FOWARD LEFT BATTERYC: 10 WL BATTERY REPLACED IAW AMM 33-51-48-401 AND CHECKED SERV. IAW T/C R1C33301SDR AWXA0001507Fitting · damagedLEFT FR 40 INNER FITTING FOUND DAMAGED. REPAIRED IAW AWA ER 26-5711-01072-JS5.SDR AWXA0001506Fitting · gougedRT WING NR 1 SLAT OUTBOARD T/E LOWER SURFACE GOUGED. REPAIRED IAW AWA ER 26-5711-01072-JS2.SDR AWXA0001505Skin · scratchedLT FUSELAGE BETWEEN FR 60 AND 61 STR 26 SKIN HAS SEVERAL SCRATCHES AND NICKS. REPAIRED DAMAGE IAW SRM 53-00-11.SDR AWXA0001504Floor Support · corrodedFLOOR SUPPORT AT FR 16 Y-503.2 LT CORRODED. FABBED AND REPLACED FLOOR SUPPORT IAW AIRBUS DWG D533112600200 AND ASSY DWG D53112005 AND D53117005 AND SRM 53-11-14 PAGE 41.SDR AWXA0001503Floor Support · corrodedFLOOR SUPPORT AT FR 16-20 Y-254 LT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-11-14 3A FIG 202.SDR AWXA0001502Floor Support · corrodedFLOOR SUPPORT AT FR 16 TO FR 20 TO FR 20 Y-254 RT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-11-14 3A FIG 202.SDR AWXA0001497Floor Support · corrodedFLOOR SUPPORT AT FR 16-20 Y-765 RT CORRODED. FLOOR SUPPORT FABBED IAW A320 DWG 53112091203 AND INSTALLED IAW SRM 51-42-00.SDR AWXA0001496Seat Track · corrodedNR 4 SEAT TRACK FRAME 20 CORRODED FR 220 Y-1292 TO FR 16 Y-1252. FABBED AND INSTALLED NEW SEAT TRACK IAW AIRBUS DWG 53112092206 AND SRM 51-42-00.
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