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 AWXA200500086Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM -Y1292 BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y1292 FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472800; INSTALLED REPAIR PARTSDR AWXA200500083Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD SEAT TRACK BETWEEN FR 38 AND FR 40. MAINTENANCE REMOVED AND REPLACED LT INBOARD SEAT TRACK FROM FR 38 TO FR 40 IAW A320 SRM 51-72-11 PG 1 & 2.SDR AWXA200500063Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 LT BETWEEN FR 65 AND FR 66. MAINTENANCE REMOVED CORRODED BEAM Y1732 LT FROM FR 65 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM PER DWG D53474250; INSTALLED REPAIR PART IAW A32SDR AWXA200500061Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FR 44 AND FR 46. MAINTENANCE REMOVED CORRODED SECTION OF RT OUTBOARD SEAT TRACK FROM FR 40 TO FR 46; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTSDR AWXA200500058Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 42 AND FS 44. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 42 TO FS 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A3SDR AWXA200500055Beam · corrodedDURING C-4 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR LOWER SILL BEAM AT FS 68 - 4 INCHES. MAINTENANCE REPAIRED R-2 DOOR LOWER SILL BEAM AT FS 68 - 4" IAW A320 SRM 53-41-14, FIG 201.SDR AWXA200500053Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C-4 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR BEAM Y1292 LT, BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM INSTALLED REPAIR PART IAW A320 SRM SDR AWXA200500052Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C-4 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 LT, BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT FLOORBEAM INSTALLED REPAIR PART IAW A320 SRM 5SDR AWXA200500044Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y920 AT FR 66 + 4". MAINTENANCE REMOVED DAMAGED FLOORBEAM Y920 FROM FS 66 TO FS 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.SDR AWXA200500043Shear Plate · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON WEB (SHEAR PLATE) -Y1732 BETWEEN FS 69 AND FS 70. MAINTENANCE REMOVED DAMAGED SHEAR PLATE -Y1732 FROM FS 69 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART ISDR AWXA200500042Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y510 AT FS 66 - 2 IN. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y510 AT FS 66 - 2; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.SDR AWXA200500097Floor Panel · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK, CORROSION WAS FOUND ON FACESHEET OF AFT CARGO COMPARTMENT FLOOR PANEL 161AF. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 161AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPLACEMENT PART IAW A320 SRM 53-02-00, FIGSDR AWXA200500095Doubler · corrodedSAL - MAJOR REPAIR - DURING C-04 CHECK, INTERGRANULAR CORROSION WAS FOUND BETWEEN INTERNAL DOUBLER AND BASE OF AFT POTABLE WATER DOOR FS 65-66, STR 40 LT. MAINTENANCE REMOVED CORRODED INTERNAL DOUBLER AT BASE OF AFT POTABLE WATER DOOR FROM FS 65 TO FS 66, STRSDR AWXA200500065Floor Panel · delaminatedDURING C-04 CHECK AFT CARGO COMPARTMENT FLOOR PANEL 151DF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 151DF FROM FR 47 TO FR 59; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPLACEMENT PARTS IAW EO 5326-01007.SDR AWXA200500064Floor Panel · delaminatedSAL - MAJOR REPAIR - DURING C-04 CHECK FORWARD CARGO COMPARTMENT FLOOR PANEL 131AF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 131AF FROM FR 24 TO FR 34; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPLACEMENT PARTS SDR AWXA200500018Power Supply · failedLAS - EEL - DURING 8-DAY CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) FAILED TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.SDR AWXA200500016Bleed Valve · malfunctionedCLIMBOUT 8000 FT LOUD BANG LT SIDE, ALL ENG IND NORM. TURNED BACK. A SECTION OF NR 1 ENG I/B C-DUCT INNER LINER FOUND MISSING IN AREA OF 10TH STAGE BLEED VALVE. FOUND SMALL DENT IN L/E OF STAB 10 INCHES FROM OB END. R&R LT HORIZONTAL STAB END CAP, NR 1 ENGSDR AWXA200500014Light · inoperativePHX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF THE EMERGENCY LIGHT SYSTEM, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 22 LT, OPERATIONAL CHECK WSDR AWXA200500005Light · inoperativePHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT SIDEWALL WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500066Floor Panel · delaminatedSAL - MAJOR REPAIR - DURING C-04 CHECK AFT CARGO COMPARTMENT FLOOR PANEL 151GF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 151GF FROM FR 47 TO FR 49; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPLACEMENT PARTS IAW SDR AWXA200500004Packing · rupturedPHX - EMERGENCY LANDING - FLT 0270 - EN ROUTE FROM IAH TO PHX RECEIVED CLASS 1 ECAM MESSAGE FOR GREEN HYDRAULIC LOW RESERVOIR THAT WAS FOLLOWED BY GREEN LOW PRESSURE, AS A PRECAUTION DECLARED EMERGENCY LANDING. MAINTENANCE REPLACED A RUPTURED PACKING ON PLUG,SDR AWXA200401434Power Supply · dischargedPHX - EEL - FLIGHT CREW REPORTED THE RT CENTER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.SDR AWXA200401419Control Unit · faultyON SHORT FINAL AFTER MLG SELECTED DOWN, RECEIVED NLG STEERING FAULT, ABORTED APPROACH & FLEW BY TOWER. CYCLED ANTI-SKID & NLG STEERING SWITCH & FAULT CLEARED, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT SYS, BITE CODES INDICATED INTERNASDR AWXA200401407Filter Element · contaminatedAT TAKEOFF, RECEIVED ECAM MESSAGE FOR NR 1 ENG FUEL FILTER CLOGGED, REJECTED TAKEOFF AT 60 KTS, MESSAGE DISAPPEARED AFTER A FEW SECONDS. MADE SEVERAL ATTEMPTS TO TRY & DUPLICATE MESSAGE WITH NO SUCCESS, TAXIED BACK TO RUNWAY & TOOK OFF. AFTER TAKEOFF AT APPRSDR AWXA200401403Proximity Sensor · intermittentDTW - EMERGENCY LANDING - FLT 0096 - WHILE PREPARING FOR LANDING AT DTW EN ROUTE FROM LAS AFTER LANDING GEAR WAS LOWERED RECEIVED A LANDING GEAR SYSTEM DISAGREE MESSAGE WITH LANDING GEAR CONTROL INTERFACE UNIT NR 2 INDICATING THE NOSE GEAR WAS UNSAFE. ABORTEDSDR AWXA200401354Fitting · out of adjustPHX - EES - DURING 4-DAY CHECK AND SCHEDULED SLIDE DEPLOYMENT, THE R-1 DOOR SLIDE DID NOT DEPLOY UPON INITIAL OPENING OF DOOR, DOOR REQUIRED SLIGHT ADDITIONAL PRESSURE TO DEPLOY SLIDE. WHEN SLIDE FINALLY DID DEPLOY, IT DID SO NORMALLY. MAINTENANCE FOUND R-1 SDR AWXA200401353Slide · delaminatedPHX - EES - DURING 4-DAY CHECK THE LOWER AFT CORNER OF THE RT OVERWING SLIDE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING SLIDE ASSEMBLY IAW T/C R1A25301.SDR AWXA200401341Slide · faultyPHX - EEL / EES - FLT 0005 - DURING FLIGHT, EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13, 17, 19, AND 24 ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ASSEMBLY IAW T/C R1C25304, OPERATIONAL CHECK OF EMERGENCY LIGHTING AND SLIDE WAS GOOD.SDR AWXA200401339Proximity Switch · malfunctionedORD - ABORTED TAKEOFF - FLT 0010 - PILOT REJECTED TAKEOFF AT 60 KTS DUE TO FORWARD CARGO DOOR OPEN INDICATION. MAINTENANCE REMOVED AND REPLACED THE FORWARD CARGO DOOR PROX SWITCH 30WV IAW AMM 52-31-00-05. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE DOOSDR AWXA200401332Power Supply · faultyORD - EEL - DURING 8-DAY CHECK TEST OF EMERGENCY LIGHT SYSTEM FOUND THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL) INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401310Computer · malfunctionedON APPROACH, AFTER SETTING FLAPS TO 1 THE SLATS LOCKED OUT. FOLLOWED ECAM INSTRUCTIONS AND ACCOMPLISHED FLAPS 3 APPROACH / LANDING. WHEN GEAR LOWERED AIRCRAFT WENT ALTERNATE LAW THEN DIRECT LAW, AUTO PILOT, FLT DIRECTOR 2, AND AUTO THROTTLES ALL FAILED. MX SDR AWXA200401305Epsu · faultyLAS - EEL - DURING 8-DAY CHECK EMERGENCY EXIT LIGHT TEST FAULTED FOR RT EXTERNAL. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.SDR AWXA200401302Terminal · defectivePHX - EEL - DURING 4-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHTING SYSTEM FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 11 RT. MAINTENANCE REPLACED TERMINAL 10N EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401346Floor Panel · delaminatedSAL - MAJOR REPAIR - DURING C-02 CHECK, CABIN FLOOR PANEL 241EF WAS FOUND DELAMINATED BETWEEN FS 30 AND FS 42. MAINTENANCE PERFORMED BOND REPAIR ON FLOOR PANEL 241EF IAW A320 SRM 53-02-00, FIG 201 AND 202.SDR AWXA200401333Floor Panel · crackedSAL - MAJOR REPAIR - DURING C-02 CHECK A 16 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 251RF BETWEEN FR 58 AND FR 62. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 251RF IAW A320 SRM 53-02-00.SDR AWXA200401329Seat Track · corrodedSAL - MAJOR REPAIR - DURING C-02 CHECK CORROSION WAS FOUND ON SEAT TRACK -Y765 AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK -Y765 FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 53-00-15 FIG 202.SDR AWXA200401334Floor Panel · crackedSAL - MAJOR REPAIR - DURING C-02 CHECK A 16 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 231QF BETWEEN FR 28 AND FR 32. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 231QF IAW A320 SRM 53-02-00.SDR AWXA200401328Floor Panel · tornSAL - MAJOR REPAIR - DURING C-02 CHECK FOUND AFT CARGO COMPARTMENT ALUMINUM FLOOR PANEL PLATE TORN BETWEEN FR 49 AND FR 50. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR PANEL PLATE; FABRICATED A NEW REPLACEMENT PLATE FROM 2024T3.071; AND INSTALLEDSDR AWXA200401279Outflow Valve · inoperativeON TAKEOFF, WHEN APPROACHING V1 UPPER ECAM INDICATED VENT SKIN VALVE FAULT. FOLLOWED ECAM INSTRUCTIONS, AIRCRAFT WOULD NOT PRESSURIZE, TURNED BACK TO STL AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED SKIN AIR VALVE IAW T/C R2A21301, OPERSDR AWXA200401278Idg · failed3 SHARP JOLTS OCCURRED IN YAW APPROX 45 SEC TO 1 MIN APART. AFTER 2ND JOLT RECEIVED ECAM INDICATION NR 1 GEN FAULT, AFTER 3RD JOLT ECAM INDICATED AUTO/FLT YAW DAMP NR 1 INOP, DIVERTED, LANDED W/O EVENT. MX ISSUED MELS. YAW DAMP NR 1 INOP. NR 1 IDG INOP. MSDR AWXA200401237Wire · brokenDURING 8-DAY CHECK, OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM FOUND THE EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 11 LT. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401225Filter · cloggedON TAKEOFF AT LAS EN ROUTE TO PHX, WHEN TAKEOFF POWER WAS APPLIED RECEIVED NR 2 ENGINE OIL FILTER CLOG MESSAGE ON ECAM, OIL PRESSURE WAS VERY HIGH, REJECTED TAKEOFF LESS THAN 40 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL SCAVENGE FILTER IAW AMMSDR AWXA200401231Floor Panel · corrodedDURING C-04 CHECK, CORROSION WAS FOUND ON AFT SIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 151AF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 151AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW A320 SRM 53-02-00, FIG 209.SDR AWXA200401277Power Supply · dischargedSAL - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13 LT, 17 LT, 19 LT, 24 LT AND 26 LT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.SDR AWXA200401190Pressure Switch · faultyONT - ABORTED TAKEOFF - FLT 0083 - ON TAKEOFF ROLL AT ONT EN ROUTE FOR PHX RECEIVED ECAM MESSAGE HYDRAULIC GREEN ENGINE 1 PUMP LOW PRESSURE, REJECTED TAKEOFF AT 70 KTS AND RETURNED TO GATE. VERIFIED GREEN HYDRAULIC SYSTEM QUANTITY AND PRESSURE, ISSUED MEL 29-3SDR AWXA200401221Floor Panel · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A 6 INCH CRACK WAS FOUND IN FLOOR PANEL 221AF. MAINTENANCE REMOVED CRACKED FLOOR PANEL FROM FS 12 TO FS 16 AND -Y81 TO -Y512; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG B5D53610125AND A320 SRM 53-02-00, FIG. 209.SDR AWXA200401230Wire · brokenDURING C-04 CHECK, FOUND BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROWS 5, 7, 13, AND 24 LEFT. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROWS 5, 7, 13, AND 24 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401210Damper · leakingDURING C-04 CHECK, THE L-1 DOOR ASSIST DAMPER PRESSURE WAS LOW. MAINTENANCE REMOVED L-1 DOOR ASSIST DAMPER PERCUSSION MECHANISM AND REPLACED TWO EACH PACKINGS. REINSTALLED L-1 DOOR ASSIST DAMPER IAW A320 AMM 52-10-00, LEAK AND OPERATIONAL CHECK WAS GOOD.SDR AWXA200401269Floor Panel · delaminatedSAL - MAJOR REPAIR - DURING C-04 CHECK A 2 X 7 INCH AREA OF DELAMINATION WAS FOUND ON FLOOR PANEL 222CF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 222CF IAW A320 SRM 53-02-00 FIG 209.SDR AWXA200401272Web · crackedSAL - MAJOR REPAIR - DURING C-04 CHECK A 2 INCH CRACK WAS FOUND IN WEB TRAY LT SIDE OF FUSELAGE BETWEEN FR 68 AND FR 69, WL Z240. MAINTENANCE REMOVED CRACKED WEB TRAY ON LT SIDE FROM FR 68 TO FR 69. FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IA
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