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 AWXA200600286Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON Y1292 BEAM AT FS 66. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y1292 AND FS 66 IAW AIRBUS 320 SRM 51-72-11.SDR AWXA200600284Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON Y1292 BEAM, BETWEEN FS 67 AND FS 68. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y1292 FROM FS 68 TO FS 69 IAW AIRBUS 320 SRM 51SDR AWXA200600281Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON THE CABIN FLOOR AT Y512 BEAM, FROM FS 66 TO FS 67. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y512 FROM FS 66 TO FS 67 IAW AIRBSDR AWXA200600280Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON CABIN FLOORBEAM AT Y1732 AND FR68. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14 FIG 101. MAINTENANCE CUT OUT DAMAGED AREA AT Y1732 BEAM IAW AIRBUS 320 SRM 53-41-14 FIG 201. RECEIVESDR AWXA200600371Attach Angle · crackedMCN - DURING C4 CHECK DISCOVERED VERTICAL STIFFENER UPPER ATTACH ANGLE AT THE LT AIR CONDITIONING BAY CRACKED, 1.6 INCHES IN LENGTH. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPAIR ATTACH ANGLE ON THE LT A/C BAY WTB VERTICAL STIFFENER IAW AIRBUS 320 SRM SDR AWXA200600285Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON Y-1292 BEAM, BETWEEN FR66 AND FR68. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y-1292 FROM FS 66 TO FS 68 IAW AIRBUS 320 SRM 51SDR AWXA200600283Floorbeam · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON Y-1162 BEAM, FROM FS 68 AND FS 69. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT Y-1162 FROM FS 68 TO FS 69 IAW AIRBUS 320 SRM 51-SDR AWXA200600277Plate · corrodedMCN - DURING C4 CHECK DISCOVERED LEVEL 2 CORROSION ON THE RT AFT SHEAR PLATE FROM FS 69 TO FS 70 AND Y-1295. NO CORROSION REMOVAL LIMITS AVAILABLE IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR PLATE FROM FR69 TO FR70 AND Y-1295 IAW AIRBUS 32SDR AWXA200600272Attach Fitting · corrodedMCN - DURING C4 CHECK DISCOVERED CORROSION ON Y-1162 BEAM, INBOARD ATTACH COUPLING ON THE FORWARD SIDE OF FS 68. CORROSION WAS FOUND OF OUT OF LIMITS IAW A320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW COUPLING AT Y-1162 BEAM AT FR 68 IAW AISDR AWXA200600373Attach Angle · crackedMCN - DURING C4 CHECK IT WAS DISCOVERED THAT THE LEFT FORWARD WING TO BODY SUPPORT STRUCTURE ATTACH ANGLE WAS CRACKED, 2.1 INCHES IN LENGTH, AT FR34 OUTBOARD OF STR30L AND STR 31L. MAINTENANCE REMOVED AND INSTALLED NEW LEFT HAND FORWARD WING TO BODY SUPPORT SDR AWXA200600279Attach Angle · crackedMCN - DURING C4 CHECK DISCOVERED THE RT FORWARD WING TO BODY SUPPORT STRUCTURE, INNER VERTICAL ATTACH ANGLE CRACKED, .75 INCHES, AT FS 34 AND STR 32R. MAINTENANCE REMOVED AND INSTALLED NEW ANGLE AT THE RT FORWARD WING TO BODY SUPPORT STRUCTURE AT FS 34 AND STSDR AWXA200600278Attach Angle · crackedMCN - DURING C4 CHECK DISCOVERED THE LT FORWARD WING TO BODY SUPPORT STRUCTURE, INNER VERTICAL ATTACH ANGLE CRACKED, .75 INCHES, AT FS 34 AND STR 32L. MAINTENANCE REMOVED AND INSTALLED NEW ANGLE AT THE LT FORWARD WING TO BODY SUPPORT STRUCTURE AT FS 34 AND STSDR AWXA200600370Attach Angle · crackedMCN - DURING C4 CHECK DISCOVERED ATTACH ANGLE CRACKED, 7.5 INCHES, AT FR 42 AND STR 35L, JUST OUTBOARD OF THE RAM AIR TURBINE. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPAIR ATTACH ANGLE AT FS 42 AND STR 35L IAW AIRBUS 320 SRM 53-35-11 AND SRM 51-72-11 SDR AWXA200600150Cabin Pressure · malfunctionedLAS - AIR TURN BACK - FLT 0374 - CREW REPORTED THAT AT FL 300 CABIN ALTITUDE KEPT CLIMBING TO 10000', STARTED DESCENT AND CABIN WAS CLIMBING AT 700' PER MIN. MAINTENANCE PRESSURIZED AIRCRAFT IAW TASK CARD F1B21308 WITH AIRFLOW IN HIGH FLOW. OPERATIONAL CHECKSDR AWXA200600237Sill · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON THE R2 LOWER SILL AROUND GIRT BAR FITTING AT FS 68 AND Y-1732. NO ALLOWABLE DAMAGE LIMITS WAS FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW R2 LOWER SILL AT THE GIRT BAR FITTING FRSDR AWXA200600236Sill · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON THE R2 LOWER SILL AT THE CENTER FITTING FROM FS 66 TO FS 68 AT Y-1732. NO ALLOWABLE DAMAGE WAS FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW R2 LOWER SILL AT THE CENTER FITTING FROSDR AWXA200600234Sill · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON UPPER SHEET METAL AT FORWARD CARGO DOOR SILL STRUCTURE FROM FR27 TO FS 28 AT Y-590. NO ALLOWABLE LIMITS WERE FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW UPPER SHEET METAL FROM FSSDR AWXA200600232Floor Support · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON FLOOR SUPPORT, LOWER FLANGE, LOCATED BETWEEN FS 16-1" AND FS 16+5" AT Y-254. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR SUPPORT FROM FS 12 TSDR AWXA200600227Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON DUMMY RAIL LOCATED AT FS 16 AND Y503.2. CORROSION WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14 FIG 104. MAINTENANCE REMOVED AND INSTALLED NEW DUMMY RAIL AT FS 16 AND Y503.2 IAW AIRBUS 320 SRSDR AWXA200600226Sill · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON THE L2 LOWER SILL AT FS 68, AROUND GIRT BAR AREA. CORROSION WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14 FIG 101. LOWER SILL WAS REMOVED IAW AIRBUS 320 SRM 51-42-11. NEW LOWER SILL WAS INSTSDR AWXA200600222Fitting · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON FITTING SUPPORT LOCATED AT L2 DOOR BETWEEN BEAM 1 AND BEAM 2 AT XP820.6. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND INSTALLED NEW FITTING ASSEMBLY AT THE LSDR AWXA200600221Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-1292, FROM FS 66 TO FS 68. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. FLOORBEAM WAS REMOVED AND NEW BEAM WAS INSTALLED FROM FS 6SDR AWXA200600220Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-1292, FROM FS 68 TO FS 69. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. FLOORBEAM WAS REMOVED AND NEW BEAM WAS INSTALLED FROM FS 6SDR AWXA200600219Floorbeam · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT Y-464, FROM FS 65 TO FS 67. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. FLOORBEAM WAS REMOVED AND NEW BEAM WAS INSTALLED FROM FS 64SDR AWXA200600224Support Fitting · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON FITTING SUPPORT LOCATED AT R1 DOOR BETWEEN AT BEAM 2, XP712.9. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND INSTALLED NEW FITTING ASSEMBLY AT R1 DOOR XP712.9SDR AWXA200600223Support Fitting · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON FITTING SUPPORT LOCATED AT L1 DOOR, BEAM 2 AT XP712.9. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND INSTALLED NEW FITTING ASSEMBLY AT THE L1 DOOR, BEAM 2 AT SDR AWXA200600217Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ALONG THE RT INBOARD SEAT TRACK AT Y-765, FROM FS 41 TO FS 47. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED FROM SDR AWXA200600216Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED AT Y-765, BETWEEN FS 20 AND FS 23+9". MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED FROM FS SDR AWXA200600215Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED AT Y-1292, FROM FS 20 TO FS 22+4" AND FROM FS 23+3" TO FS 24. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACSDR AWXA200600214Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ALONG LT OUTBOARD SEAT TRACK AT Y1292, FROM FS 41 TO FS 47 IN 8 LOCATIONS. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSSDR AWXA200600210Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ALONG LT INBOARD SEAT TRACK AT Y765, FROM FS 41 TO FS 47 IN 8 LOCATIONS. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTASDR AWXA200600235Channel · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON THE RT AILERON TRAILING EDGE LOWER SURFACE CHANNEL. NO ALLOWABLE DAMAGE WAS FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW AILERON TRAILING EDGE LOWER SURFACE CHANNEL IAW AIRBUS 320SDR AWXA200600225Angle · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON ANGLE AT FS 71, BETWEEN STRINGER 26R AND STRINGER 30R. CORROSION WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-50-00 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW ANGLE AT FS 71, BETWEEN STR 26R ASDR AWXA200600218Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON RT OUTBOARD SEAT TRACK LOCATED AT Y-1292, FROM FS 41 TO FS 47. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED FRSDR AWXA200600213Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ALONG R/H OUTBOARD SEAT TRACK AT Y-1292, FROM FS 36 TO FS 41. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED FROM FSDR AWXA200600212Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ALONG LT INBOARD SEAT TRACK AT Y765, FROM FS 36 TO FS 41 IN 6 LOCATIONS. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTASDR AWXA200600211Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ALONG LT OUTBOARD SEAT TRACK AT Y1292, FROM FS 35 TO FS 36. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED FROM FS SDR AWXA200600209Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ALONG LT OUTBOARD SEAT TRACK AT Y1292, FROM FS 36 TO FS 41 IN 5 LOCATIONS. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSSDR AWXA200600208Seat Track · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ALONG RT INBOARD SEAT TRACK AT Y-765, FROM FS 36 TO FS 41 IN 6 LOCATIONS. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. SEAT TRACK WAS REMOVED AND NEW TRACK WAS INSTSDR AWXA200600018Slide · faultyDURING OVERNIGHT INSPECTION THE L2 DOOR SLIDE FAILED STEP 5 OF THE 4-DAY TASK CARD. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR SLIDE IAW TASK CARD R1C25304.SDR AWXA200501571Windshield · failedCREW REPORTED THAT AT FL 360, THE CAPT WINDSHIELD OUTER PANE SHATTERED & LT WINDSHIELD ANTI-ICE FAILED. LANDED WITHOUT FURTHER EVENT. MX R & R CAPT WINDSHIELD & NR 1 WINDSHILED HEAT COMPUTER. OPS CHECKS GOOD. PERFORMED FUNCTIONAL TESTS OF CAPT WINDSHIELD HSDR AWXA200501520Battery · inoperativeDTW - EEL - DURING INSPECTION DISCOVERED THE FORWARD F/A JUMSEAT INBOARD EMERGENCY FLASHLIGHT BATTERY DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD F/A FLASHLIGHT BATTERY PACK IAW AIRBUS 320 MM 25-65-52. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200501511Power Supply · inoperativePHX - EEL - DURING INSPECTION DISCOVERED THE AFT THREE ROWS OF SEATS THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT POWER SUPPLY. OPERATIONAL TESTS WERE GOOD. VENDOR CONFIRMED FAULT. REPLACED F2 FUSE. UNIT REPAIRED AND SDR AWXA200501500Battery · inoperativePHX - EEL - CREW REPORTED THAT THE AFT LEFT GALLEY EMERGENCY FLASHLIGHT WAS LOSING ITS CHARGE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200501486Battery · dischargedEEL - CREW REPORTED THAT THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY IS DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT BATTERY. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200501485Connector · defectiveEEL-DURING OVERNIGHT INSPECTION DISCOVERED THE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 24L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR PLUG FOR THE EMERGENCY LIGHT ASSEMBLY AT ROW 24L IAW MM. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200501478Handle · unsecureFLT 859 - DURING TAKEOFF, CREW RECEIVED AFT CARGO DOOR CLASS 1 MAINTENANCE MESSAGE. ABORTED TAKEOFF AT 60 KNOTS. RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RE-SECURED AFT CARGO DOOR HANDLE, FOUND HANDLE NOT COMPLETELY IN DETENT. OPERATIONAL CHESDR AWXA200501456Power Supply · failedOVERNIGHT MAINTENANCE DISCOVERED EMERGENCY LIGHT TEST FAILING, FAULT (115 VAC AFT L) PRESENT. MAINTENANCE REMOVED AND REPLACED THE LT AFT POWER SUPPLY IAW MM 33-51-38-04. VENDOR CONFIRMED FAULT. UNIT WAS REPAIRED AND TESTED IAW CMM 33-51-09 REV.2SDR AWXA200501424Battery · inoperativeLAS - EEL - DURING OVERNIGHT INSPECTION DISCOVERED THE EMERGENCY EXIT LIGHT BATTERY, AT ROW 11R, WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY AT ROW 11R. OPERATIONAL TESTS WERE GOOD.SDR AWXA200501376Blades · failedCREW REPORTED ON CLIMB-OUT ECAM MSG ENG 2 STALL. PILOTS RAN QRH PROCEDURE & RAN ENGINE AT IDLE. STALL RETURNED WHEN THEY ADVANCED THRUST LEVER ABOVE IDLE. RETURNED & LANDED WITHOUT FURTHER EVENT. NR 2 ENGINE BOROSCOPED. HPC NR 6, BLADES BENT & OUT OF LIMIT
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