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.

SDR USAA2011011890242Splice · damagedMCN - BC6 - EEL - EMERGENCY EXIT LIGHT INOP AT ROW 9ABC. REPLACED SPLICE UNDER SEAT AT ROW 9 ABC, EMERGENCY LIGHT OPS CHECKS GOOD IAW AIRBUS ESPM 20-43-11 & A320 AMM 33-51-00.Jan 13, 2011 · N644AW · Airbus A320231 · Light System WiringSDR USAA2011021490746Dampener · low pressureSAL - EES - S5 CHECK - THE PRESSURE WAS LOW ON THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FOR DOOR 842 AND WOULD NOT OPERATE CORRECTLY. REPLACED THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FOR DOOR 842 IAW A320 AMM 52-13-14.Jan 9, 2011 · N621AW · Airbus A320231 · Passenger/Crew DoorsSDR USAA2011011890247Door · crackedSAL - S5 - MAJOR REPAIR - CRACK ON RIGHT AFT EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN S14R TO S21R. REPLACED RIGHT AFT EMERGENCY EXIT DOOR 844 IAW JOB CARD 26C83352006 & A320 SRM 52-21-11.Jan 4, 2011 · N624AW · Airbus A320231 · Emergency ExitsSDR USAA2011010390022Angle · crackedPIT - C1 - MAJOR REPAIR - 4 &.125 INCH CRACKS IN ANGLE SEGMENT OF LEFT FORWARD EMERGENCY EXIT DOOR AT FORWARD SIDE OF WINDOW. REPLACED ANGLE SEGMENT OF LEFT FORWARD EMERGENCY EXIT DOOR AT FORWARD SIDE OF WINDOW IAW EO 5210Y228.Dec 31, 2010 · N632AW · Airbus A320231 · Emergency ExitsSDR USAA2011010390021Angle · crackedPIT - C1 - MAJOR REPAIR - 4 &.125 INCH CRACKS IN ANGLE SEGMENT OF LEFT FORWARD EMERGENCY EXIT DOOR AT AFT SIDE OF WINDOW. REPLACED ANGLE SEGMENT OF LEFT FORWARD EMERGENCY EXIT DOOR AT AFT SIDE OF WINDOW IAW AIRWAYS EO 5210Y228.Dec 31, 2010 · N632AW · Airbus A320231 · Emergency ExitsSDR USAA2011010390020Angle · crackedPIT - C1 - MAJOR REPAIR - 4 & 1 INCH CRACKS IN ANGLE SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR AT AFT SIDE OF WINDOW. REPLACED ANGLE SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR AT AFT SIDE OF WINDOW IAW AIRWAYS EO 5210Y228.Dec 31, 2010 · N632AW · Airbus A320231 · Emergency ExitsSDR USAA2011010390019Angle · crackedPIT - C1 - MAJOR REPAIR - .125 INCH CRACK IN ANGLE SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR AT FORWARD SIDE OF WINDOW. REPLACED ANGLE SEGMENT OF RIGHT AFT EMERGENCY EXIT DOOR AT FORWARD SIDE OF WINDOW IAW EO 5210Y228.Dec 31, 2010 · N632AW · Airbus A320231 · Emergency ExitsSDR USAA2011010390018Angle · crackedPIT - C1 - MAJOR REPAIR - 4 INCH CRACK IN ANGLE SEGMENT OF RIGHT FORWARD EMERGENCY EXIT DOOR AT FORWARD SIDE OF WINDOW. REPLACED ANGLE SEGMENT OF RIGHT FORWARD EMERGENCY EXIT DOOR AT FORWARD SIDE OF WINDOW IAW EO 5210Y228.Dec 31, 2010 · N632AW · Airbus A320231 · Emergency ExitsSDR USAA2011010390017Angle · crackedPIT - C1 - MAJOR REPAIR - 4.25 INCH CRACK IN ANGLE SEGMENT OF LEFT AFT EMERGENCY EXIT DOOR ON AFT SIDE OF WINDOW. REPLACED ANGLE SEGMENT OF LEFT AFT EMERGENCY EXIT DOOR ON AFT SIDE OF WINDOW IAW EO 5210Y228.Dec 31, 2010 · N632AW · Airbus A320231 · Emergency ExitsSDR USAA2011010390016Angle · crackedPIT - C1 - MAJOR REPAIR - 3 INCH CRACK IN ANGLE SEGMENT OF LEFT AFT EMERGENCY EXIT DOOR FORWARD OF WINDOW. REPLACED ANGLE SEGMENT OF LEFT AFT EMERGENCY EXIT DOOR FORWARD OF WINDOW IAW EO 5210Y228.Dec 31, 2010 · N632AW · Airbus A320231 · Emergency ExitsSDR USAA2010123093268Lens · missingFLT 614 - ATL - EEL - EMERGENCY LIGHT LENS MISSING ON SEAT 9-L. MAINTENANCE INSTALLED LENS ON SEAT 9-L.Dec 30, 2010 · N644AW · Airbus A320231 · Emergency LightingSDR USAA2010123093272Web · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON WEB LOCATED BETWEEN FR33 TO FR34, S38R. REPLACED WEB LOCATED BETWEEN FR33 TO FR34, S38R IAW A320 SRM 51-72-11.Dec 29, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011011090148Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO -Y765. REPLACED FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO -Y765 IAW A320 SRM 53-02-00 & IRM 9701 REV G.Dec 28, 2010 · N624AW · Airbus A320231 · Fuselage Floor PanelSDR USAA2010123093275Pin · corrodedMAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER OUTBOARD POSITION ENG 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER OUTBOARD POSITION ENG 2 IAW A320 AMM 71-22-11.Dec 28, 2010 · N624AW · Airbus A320231 · Engine Mount SectionSDR USAA2010123093274Pin · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER INBOARD POSITION ENGINE NR 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER INBOARD POSITION ENGINE NR 2 IAW A320 AMM 71-22-11.Dec 28, 2010 · N624AW · Airbus A320231 · Engine Mount SectionSDR USAA2010123093273Pin · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER CENTER POSITION ENGINE NR 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER CENTER POSITION ENGINE NR 2 IAW A320 AMM 71-22-11.Dec 28, 2010 · N624AW · Airbus A320231 · Engine Mount SectionSDR USAA2010123093271Web · crackedSAL -MAJOR REPAIR - S5 CHECK - CRACKED WEB LOCATED Y765 BTW FR 8 TO FR 11 IN COCKPIT. REPLACED WEB LOCATED Y765 BETWEEN FR 8 TO FR 11 IN COCKPIT IAW A320 SRM 51-72-11.Dec 26, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2010123093276Attach Fitting · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON THE RIGHT WING TO PYLON AFT ATTACH FITTING AT RIB 10. REPLACED THE RIGHT WING TO PYLON AFT ATTACH FITTING AT RIB 10 IAW TASK CARD 26C40054026.Dec 22, 2010 · N624AW · Airbus A320231 · Nacelle/Pylon, Attach FittingsSDR USAA2011011990262Pin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON PIN OF NR 2 ENGINE AFT ENGINE MOUNT LOWER OUTBOARD POSITION BETWEEN PYLON STA 6465 TO STA 7063 & BETWEEN RIB 3 TO RIB 5. REPLACED PIN OF NR 2 ENGINE AFT ENGINE MOUNT LOWER OUTBOARD POSITION IAW A320 AMM 71-22-11-0401.Dec 21, 2010 · N624AW · Airbus A320231 · Engine Mount SectionSDR USAA2011011090154Seat Track · corrodedS5 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK AT FR25, -Y1292. REPAIRED SEAT TRACK AT FR27 + 10 INCHES, -Y1292 IAW SRM 53-21-15 & AIRBUS DRAWING D53112812.Dec 21, 2010 · N624AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011011090156Fitting · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LEFT PYLON SPIGOT FITTING BORE BETWEEN LEFT PYLON STA 6465 TO STA063. REPLACED LEFT PYLON SPIGOT FITTING BETWEEN LEFT PYLON STA 6465 TO STA 063 IAW A320 SRM 54-51-12.Dec 20, 2010 · N624AW · Airbus A320231 · Nacelle/Pylon, Attach FittingsSDR USAA2010122393233Floor Panel · delaminatedSAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 251LF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 251LF.Dec 17, 2010 · N624AW · Airbus A320231 · Fuselage Floor PanelSDR USAA2010121793113Profile · crackedSAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTRAL FUSELAGE IAWDec 17, 2010 · N628AW · Airbus A320231 · Emergency ExitsSDR USAA2010121793112Profile · crackedSAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (833) AT CENTRAL FUSDec 17, 2010 · N628AW · Airbus A320231 · Emergency ExitsSDR USAA2010121793111Profile · crackedSAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTIG PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSDec 17, 2010 · N628AW · Airbus A320231 · Emergency ExitsSDR USAA2011011890260Shear Plate · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON SHEAR PLATE BETWEEN FR58 TO FR59, S38L. REPLACED SHEAR PLATE BETWEEN FR58 TO FR59, S38L IAW A320 SRM 51-72-11.Dec 16, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2010121793125Sill · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LOWER SILL AROUND GIRT BAR FITTING AT FR 66, S23L. REPAIRED LOWER SILL AROUND GIRT BAR FITTING AT FR 66, S23L IAW EA 133170.Dec 16, 2010 · N628AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2010121793124Sill · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LOWER SILL AROUND GIRT BAR FITTING AT FR 68, S23R. REPAIRED LOWER SILL AROUND GIRT BAR FITTING AT FR 68, S23R IAW EA 133170.Dec 16, 2010 · N628AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2010121793118Floorbeam · crackedSAL - S5 - MAJOR REPAIR - CRACK ON FLOORBEAM BETWEEN FR46 TO FR47, -Y254. REPAIRED FLOORBEAM BETWEEN FR46 TO FR47, -Y254 IAW EA 133198.Dec 16, 2010 · N628AW · Airbus A320231 · Fuselage Main, Floor BeamSDR USAA2010121793117Profile · crackedSAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTER FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTER FUSELAGE IAW EA Dec 16, 2010 · N628AW · Airbus A320231 · Emergency ExitsSDR USAA2010121793116Profile · crackedSAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE RIGHT AFT EMERGENCY EXIT (844) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE RIGHT AFT EMERGENCY EXIT (844) AT CENTRAL FUSELAGE IDec 16, 2010 · N628AW · Airbus A320231 · Emergency ExitsSDR USAA2010121793115Profile · crackedSAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELADec 16, 2010 · N628AW · Airbus A320231 · Emergency ExitsSDR USAA2010121793114Profile · crackedSAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSEDec 16, 2010 · N628AW · Airbus A320231 · Emergency ExitsSDR USAA2011012190314Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR56 TO FR57, S44. REPLACED FLOORBEAM BETWEEN FR56 TO FR57, S44 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53470001.Dec 15, 2010 · N624AW · Airbus A320231 · Fuselage Main, Floor BeamSDR USAA2011011890259Shear Plate · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON SHEAR PLATE WEB BETWEEN FR54 TO FR55, S38L. REPLACED SHEAR PLATE WEB BETWEEN FR54 TO FR55, S38L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53470320.Dec 15, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011011890258Fitting · corrodedS5 - MAJOR REPAIR - LEVEL 2 CORROSION ON CLEAT AT FR31 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR31 BETWEEN S41R TO S42R IAW SRM 51-72-11 & DRAWING D53231582.Dec 15, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011011090151Crossbeam · corrodedS5 CHECK - MAJOR REPAIR - CORROSION ON CROSSBEAM AT FR33 BETWEEN S38L TO S38R. REPLACED CROSSBEAM AT FR33 BETWEEN S38L TO S38R IAW SRM 51-72-11.Dec 15, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011011090150Shear Tie · corrodedS5 CHECK- MAJOR REPAIR - CORROSION ON SHEAR TIE CLEAT AT FR31 BETWEEN S40R TO S41R. REPLACED SHEAR TIE CLEAT AT FR31 BETWEEN S40R TO S41R IAW SRM 51-72-11.Dec 15, 2010 · N624AW · Airbus A320231 · Fuselage Internal Mounting StructureSDR USAA2011010390013Fitting · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON AFT LOWER CORNER FITTING OF L-1 DOOR AT FR20, S23L. REPLACED AFT LOWER CORNER FITTING OF L-1 DOOR AT FR20, S23L IAW A320 SRM 51-72-11.Dec 15, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011012190313Stringer · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR28 TO FR28 + 19 INCHES, S40L. REPAIRED STRINGER BETWEEN FR28 TO FR28 + 19 INCHES, S40L IAW A320 SRM 53-21-13.Dec 14, 2010 · N624AW · Airbus A320231 · Fuselage Main, Longeron/StringerSDR USAA2011011990266Hinge Pin · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON NR 3 SPOILER INNER HINGE PIN AT LEFT WING STA 7792, RIB 14. REPLACED NR 3 SPOILER INNER HINGE PIN AT LEFT WING STA 7792, RIB 14 IAW A320 AMM 27-64-43.Dec 14, 2010 · N624AW · Airbus A320231 · SpoilersSDR USAA2011011990264Fitting · crackedSAL - S5 - MAJOR REPAIR - CRACK ON FITTING AT FR24A BETWEEN S34L TO S35L. REPLACED FITTING AT FR24A BETWEEN S34L TO S35L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53911160.Dec 14, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011011990263Web · crackedSAL - S5 - MAJOR REPAIR - CRACK ON WEB OF FLOOR STRUCTURE AT FR6, Y869. REPAIRED WEB OF FLOOR STRUCTURE AT FR6, Y869 IAW EA 133257.Dec 14, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011011090149Web · crackedSAL - S5 - MAJOR REPAIR - CRACK IN WEB AT FR14 BETWEEN S1R TO S1L. REPLACED WEB AT FR14 BETWEEN S1R TO S1L IAW A320 SRM 51-72-11.Dec 14, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011010390012Fitting · corrodedS5 CHECK - MAJOR REPAIR - CORROSION ON CLEAT AT FR28 BETWEEN S42R TO S43R. REPLACED CLEAT AT FR28 BETWEEN S42R TO S43R IAW SRM 51-72-11.Dec 14, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2010121793123Skin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON INTERNAL SKIN AT FR58 + 15 INCHES BETWEEN S43R & S44R AFT CARGO COMPARTMENT. REPAIRED INTERNAL SKIN AT FR58 + 15 INCHES BETWEEN S43R & S44R IAW EA 133191.Dec 14, 2010 · N628AW · Airbus A320231 · Fuselage Main, Plate/SkinSDR USAA2010121793122Frame · crackedSAL - S5 - MAJOR REPAIR - CRACK ON UPPER FLANGE OF FRAME 25 AT LEVEL S31L FWD C.C. REPAIRED UPPER FRAME FLANGE AT FR25, S31L IAW A320 SRM 53-00-12.Dec 13, 2010 · N628AW · Airbus A320231 · Fuselage Main, FrameSDR USAA2010121793120Angle · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON ANGLE AT FR71 CUTOUT ACCESS DOOR 312AR BETWEEN S27R TO S30R TAIL SECTION AFT FUSELAGE. REPLACED ANGLE AT FR71 CUTOUT ACCESS DOOR 312AR BETWEEN S27R TO S30R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53571500.Dec 13, 2010 · N628AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011011990265Fitting · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FORWARD LOWER CORNER FITTING OF R-1 DOOR CUTOUT AT FR16, S23R. REPLACED FORWARD LOWER CORNER FITTING OF R-1 DOOR CUTOUT AT FR16, S23R IAW A320 SRM 51-72-11 & EA 133272.Dec 12, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR USAA2011011090155Fitting · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR20, S23R. REPLACED CORNER FITTING AT FR20, S23R IAW A320 SRM 51-72-11.Dec 12, 2010 · N624AW · Airbus A320231 · Fuselage Miscellaneous Structure
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