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 AWXA200401206Seat Track · corrodedDURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON LT CABIN SEAT TRACK Y1292 BETWEEN FS 41 AND FS 47. MAINTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y1292 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALSDR AWXA200401242Shear Plate · corrodedDURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE BETWEEN FS 69 AND FS 70, OUTBOARD OF BEAM Y1292. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FS 69 TO FS 70, AT Y1292; FABRICATED A NEW REPLACEMENT SHEARSDR AWXA200401216Floorbeam · corrodedDURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED SECTION BEAM Y1292 LT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.SDR AWXA200401211Floor Panel · corrodedDURING C-04 CHECK, FOUND CORROSION ON L-2 DOOR ENTRY WAY FLOOR PANEL 221FF. MAINTENANCE REMOVED AND REPLACED L-2 DOOR ENTRY WAY FLOOR PANEL 221FF IAW T/C C1D25306.SDR AWXA200401205Web · corrodedDURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT OUTBOARD WEB Y1698 BETWEEN FS 20 AND FS 21. MAINTENANCE REMOVED CORRODED SECTION OF RT OUTBOARD WEB Y1698 FROM FS 20 TO FS 21; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPASDR AWXA200401204Floorbeam · corrodedDURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FS 16 TO FS 20; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14, FIG 102.SDR AWXA200401203Floor Support · corrodedDURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT Y254 RT BETWEEN FS 16 AND FS 20. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT Y254 RT FROM FS 16 TO FS 20; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND 4 EACH SPLICE ANGLESDR AWXA200401202Sill · corrodedDURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF L-2 DOOR SILL AT Y1350 BETWEEN FR 66 AND FR 68. MAINTENANCE CUTOUT DAMAGE IN L-2 DOOR SILL AT Y1350 FROM FS 66 TO FS 68; FABRICATED A REPAIR ANGLE, FILLER, AND PLATE; INSTALLED RSDR AWXA200401201Floorbeam · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11.SDR AWXA200401198Sill · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER OB EDGE OF R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546, FROM FR 66 TO FR 6SDR AWXA200401197Shear Plate · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE, OB OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT Y1292 FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSDR AWXA200401196Seat Track · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON OB SEAT TRACK Y1292 RT FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-42SDR AWXA200401195Seat Track · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT IB SEAT TRACK Y765 FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-72-11SDR AWXA200401194Seat Track · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9-12.SDR AWXA200401193Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 9-12.SDR AWXA200401214Floor Panel · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON CORNER OF AFT CARGO COMPARTMENT FLOOR PANEL 161AF UNDER PADDING. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR PANEL 161AF, FABRICATED A NEW REPLACEMENT FLOOR PANEL, INSTALLED PANEL IAW SDR AWXA200401209Floor Panel · delaminatedDURING C-04 CHECK, FOUND R-1 DOOR ENTRY FLOOR PANEL DELAMINATED. MAINTENANCE REMOVED AND REPLACED R-1 DOOR ENTRY FLOOR PANEL IAW T/C C1D25306.SDR CA041015007Blade · failed(CAN) ON TAKE OFF WITH THROTTLES BETWEEN IDLE AND FLEX MCT. LOUD BANG FROM LT ENGINE HEARD IN THE COCKPIT. TAKE OFF ABANDONED AT 115 KTS. ACRFT RETURNED WITH ENGINE RETARDED TO IDLE. NO UNUSUAL PARAMETERS. BORESCOPE INSPECTION REVEALED ONE FAILED HPC STAGE 4 BSDR AWXA200401119Computer · malfunctionedON TAKEOFF, NR 1 ENG DID NOT PRODUCE TAKEOFF THRUST, EPR ONLY AT 1.31, REQUIRED EPR 1.42, REJECTED TAKEOFF AT 95 KTS. MX TROUBLESHOT SYS, WITH ENGINES NOT RUNNING FOUND EPR MISMATCH BETWEEN ENGINE NR 1 & 2 AT FLEX MAXIMUM CONTINUOUS THRUST (MCT) AND TOGA POSITSDR AWXA200401111Wire Harness · damagedON CLIMB-OUT AT FL 300, CLIMBING 1200 FPM, 290 KTS ECAM INDICATED ENG 2 COMP VANE WITH INSTRUCTION AVOID THRUST CHANGE, IF ENGINE STALL, ENG MASTER 2 OFF. REDUCED VERT SPEED AS ACRFT CLIMBED THRU FL 310 TO MINIMIZE LEVEL OFF THRUST CHANGES. WITHIN 100 FT OFSDR AWXA200401041Wire · brokenDURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN GROUND WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401039Wire · brokenDURING 4-DAY CHECK, A BROKEN WIRE WAS FOUND ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401034Swivel · brokenON LANDING AT CMH EN ROUTE FROM LAS, WHEN LANDING GEAR EXTENDED LOST GREEN HYDRAULIC FLUID, MANUALLY EXTENDED GEAR, LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE RT MAIN LANDING GEAR DOOR ACTUATING CYLINDER FORWARD FLEX HOSE SWIVEL JOINT ASSEMBLY BROKENSDR AWXA200401033Fmu · malfunctionedON DESCENT INTO LAS EN ROUTE FROM ORD AT APPROXIMATELY 17,000 FT, RECEIVED ECAM MESSAGE NR 2 ENGINE VANE FAILURE, ENGINE THEN SPOOLED DOWN AND ECAM INDICATED NR 2 ENGINE FAILED. FOLLOWED ECAM INSTRUCTIONS AND SECURED NR 2 ENGINE; DECLARED EMERGENCY AND LANDEDSDR AWXA200401027Wire · shortedARCHING / SMOKE, FLIGHT CREW REPORTED WIRES IN CAPTAINS SLIDING WINDOW POST CONNECTED TO READING LIGHT SHORED OUT WITH VISIBLE ARCHING AND SMOKE, A SMALL HOLE BURNED THROUGH PLASTIC COVER. MAINTENANCE PULLED AND COLLARED CAPTAINS READING LIGHT CIRCUIT BREAKERSDR AWXA200401002Wire · openFLIGHT CREW REPORTED EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, AND 5 REMAIN ON AND WILL NOT RESET. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), PROBLEM STILL EXISTS, OHMED L-1 DOOR SLIDE WIRING AND FOUND OPEN READING. SDR AWXA200400970Spur Gear · galledABORT T/O, NR 1 ENG ROLLED BACK TO IDLE WHEN BRAKES RELEASED. PRIOR, NR 1 ENG SHUTDOWN WHEN THROTTLES ADV & BRAKES RELEASED. INSP INLET & EXHAUST, BITE TEST OF CFDS & FADEC 1A&1B, HI PWR ENG RUN GOOD. *S/D* 10TH STG SOLENOID VLV INPUT LINE HAND TIGHT, TORQSDR AWXA200400941Epsu · failedFLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS IN AFT GALLEY WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT GALLEY EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD.SDR AWXA200400983Floor Panel · corrodedDURING C-04 CHECK, CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151DF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 151DF, FS 50 TO FS 53, Y1292 LT TO Y1292 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER IAW A320 SRM 53-02SDR AWXA200400937Battery · dischargedCMH - EEL - DURING 8-DAY CHECK THE LEFT FORWARD EMERGENCY LIGHT BATTERY PACK FAULTED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400936Bearing · failedEN ROUTE FROM PHX TO MCO, SMELLED A BURNING ELECTRICAL ODOR WITH VISIBLE SMOKE IN COCKPIT, WHILE DIVERTING TO DFW APPROXIMATELY 2 MILES LATER VENT EXTRACT FAULT LIGHT ILLUMINATED. MAINTENANCE PLACED SYSTEM ON MEL AND DEACTIVATED EXTRACT FAN. UPON ARRIVAL AT SDR AWXA200400935Battery · dischargedCMH - EEL - DURING 4-DAY CHECK THE LEFT OVERWING EMERGENCY LIGHT BATTERY FAULTED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LEFT OVERWING EMERGENCY POWER SUPPLY UNIT 11WL, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400934Odor · detectedON CLIMB OUT, AN ELECTRICAL BURNING ODOR NOTICED IN COCKPIT FOLLOWED BY SMOKE COMING FROM AIR CON VENTS IN COCKPIT & CABIN, DONNED O2 MASKS & TURNED BACK, WHEN EXITING RUNWAY RECEIVED PACK 1 OVRHT IND. A/C OUT OF SERVICE. MX FOUND ACM FROZEN, R & R ACM IAW ASDR AWXA200400922Epsu · faultyDURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY BULLNOSE LIGHT AT SEAT ROW 4 RT INOPERATIVE. REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.SDR AWXA200400917Slide · inoperativePHX - EES - DURING 4-DAY CHECK THE L-2 DOOR SLIDE FAILED EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE, EMERGENCY LIGHT TEST WAS GOOD.SDR AWXA200400951Floor Panel · crackedDURING C-04 CHECK A 4 INCH CRACK WAS FOUND IN FLOOR PANEL 251 AF, FR 47 - FR 51, Y254 LT - Y254 RT. MAINTENANCE REMOVED CRACKED FLOOR PANEL 251 AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670022 AND A320 SRM 53-02-00, FIG. 209.SDR AWXA200400944Sill · corrodedDURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SHAPE SILL ASSEMBLY AT Y1750 RT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SHAPE SILL AT Y1750 RT, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IASDR AWXA200401001Web · crackedDURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN RT AFT OB TRAY (WEB) BETWEEN FR 68 AND FR 69, OB OF BEAM Y1292 RT. MAINTENANCE REMOVED CRACKED RT AFT OB TRAY FROM FR 68 TO FR 69, Y1292 RT; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRSDR AWXA200400998Shear Plate · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, AT STR 24 LT. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE FROM FR 69 TO FR 70, AT STR 24 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW SDR AWXA200400997Web · crackedDURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN LT AFT OB TRAY (WEB) BETWEEN FR 68 AND FR 69, OB OF BEAM Y1292 LT. MAINTENANCE REMOVED CRACKED LT AFT OB TRAY FROM FR 68 TO FR 69, Y1732 LT TO Y1792 LT; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART SDR AWXA200400994Floor Panel · delaminatedDURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 151 PF DELAMINATED ON AFT SIDE. MAINTENANCE REMOVED DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 151 PF FROM FR 58 TO FR 59; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00, FIG. 209, PG. 233-SDR AWXA200400986Floorbeam · corrodedDURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.SDR AWXA200400985Gusset · corrodedDURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON GUSSET STRINGER 26 RT AT FORWARD SIDE OF FS 66. MAINTENANCE REMOVED CORRODED GUSSET STRINGER 26 RT AT FORWARD SIDE OF FS 66; FABRICATED A NEW REPLACEMENT GUSSET PER DWG 18D53480062; INSTALLED REPAIR PART ISDR AWXA200400984Sill · corrodedDURING C-04 CHECK, CORROSION WAS FOUND ON R-2 DOOR LOWER SHAPE SILL BETWEEN FS 66 AND FS 68. MAINTENANCE CUTOUT DAMAGED AREA OF R-2 DOOR SHAPE SILL AT Y1732 RT, FROM FS 66 TO FS 68; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-SDR AWXA200400981Sill · corrodedDURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON FORWARD INBOARD END OF L-2 DOOR SILL AT FS 66. MAINTENANCE CUTOUT DAMAGED AREA OF L-2 DOOR SILL AT Y1732 LT, FROM FS 66 TO FS 68; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SDR AWXA200400980Floorbeam · corrodedDURING C-04 CHECK, CORROSION WAS FOUND ON Y1292 RT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM PER DWG 18D53472172; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.SDR AWXA200400979Floorbeam · corrodedDURING C-04 CHECK, CORROSION WAS FOUND ON BEAM Y1292 RT AT FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FS 68 TO FS 69; FABRICATED A NEW SECTION OF REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.SDR AWXA200400976Floorbeam · corrodedDURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y919 LT AT FS 66. MAINTENANCE REMOVED CORRODED BEAM Y919 LT AT FS 66, INSTALLED NEW REPLACEMENT BEAM IAW A320 SRM 51-72-11.SDR AWXA200400971Beam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y512 LT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y512 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8.SDR AWXA200400958Seat Track · corrodedDURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 RT, FORWARD OF FS 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 RT AT FS 66; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, F
Back to Airbus A320-231