Airbus A320-211

Service difficulty reports · 5,271

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 = 'A320211'
  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 DALA2014081804647Web · corrodedCORROSION FOUND ON WEB - Y1732 FRAME 20. REPLACED WEB IAW SRM 51-72-11 AND DWG D53114392.Aug 17, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081804646Seat Track · corrodedCORROSION ON SEAT TRACK Y765 BETWEEN FRAMES 36 - 41, FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Aug 17, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081804645Seat Track · corrodedCORROSION ON SEAT TRACK Y765 BETWEEN FRAMES 47 - 64, FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Aug 17, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081804627Seat Track · corrodedCORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 41 - 47. FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG 53370500.Aug 17, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081704626Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y512 BETWEEN FRAMES 64 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472000, & D53474250.Aug 16, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081704625Door Sill · corrodedCORROSION ON LOWER L1 DOOR SILL BETWEEN FRAMES 16 - 20. REPLACED LOWER L1 DOOR SILL IAW SRM 51-72-11 AND DWG D53110339.Aug 16, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081704624Floor Support · corrodedCORROSION ON AFT PAX CABIN FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 16, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081604597Stringer · corrodedCORROSION ON STRINGER 33L BETWEEN FRAMES 65 - 66. REPAIRED STRINGER IAW SRM 53-00-13 PARAGRAPH 4A, FIG 201, SHEET 2, 3, 4 AND 5, PAGES 202-218.Aug 16, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082004664Frame · corrodedCORROSION ON FRAME 16 STR 23R. WORKED CORROSION IAW SRM 51-74-00. FOUND WITHIN LIMITS IAW SRM 53-11-12, FIG 104, SHEET 1, AND FIGURE 105, SHEET 1.Aug 15, 2014 · N324US · Airbus A320211 · Fuselage Main, FrameSDR DALA2014082004663Window Frame · crackedDURING M2-CHECK, A CRACK WAS FOUND ON THE FRAME SECTION AT LT SLIDING WINDOW IAW ALI 53-11-35-PB6. REPAIRED IAW ER/A 527498-14AD, REV ORIGINAL.Aug 15, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014081604599Frame · corrodedCORROSION ON AFT LOWER CORNER OF FRAME 20 BETWEEN STRINGERS 22 - 23L. REPLACED LOWER CORNER LOCATED ON FRAME IAW SRM 51-72-11 AND DWG D53112109.Aug 15, 2014 · N324US · Airbus A320211 · Fuselage Main, FrameSDR DALA2014081504598Plate · corrodedAFTER REMOVING LOWER CORNER FITTING PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON REINFORCEMENT PLATE FRAME 20 STRINGER 23L. REPLACED LOWER REINFORCEMENT PLATE AND FASTENER IAW SRM 51-72-11 AND ENGINEERING REPAIR AUTHORIZATION, 527501-14, REV ORIGINAL ANAug 15, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081604596Floor Support · corrodedCORROSION ON AFT PAX CABIN FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66+5 AND 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWGS D53472000, D53472816.Aug 15, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081804586Frame · corrodedCORROSION ON FWD FACE LATERAL FRAME 20 STRINGER 23R. PERFORMED TIME LIMITED REPAIR ON FWD FACE LATERAL FRAME 20 LOCATED FWD PASSENGER ENTRY DOOR LEVEL STR 23 RT INTERNAL STRUCTURE IAW ER/A 527494-14, REVISION ORIGINAL AND PRELIMINARY REPAIR INSTRUCTIONS 52749Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Main, FrameSDR DALA2014081504585Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAME 16 AND 20 Y-254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND ENGINEERING REPAIR , AUTHORIZATION N 527502-14, REV: ORIGINAL.Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081504584Floor Support · corrodedCORROSION ON FWD PAX CABIN FLOOR SUPPORT -Y765 BETWEEN FRAMES 16-20. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.Aug 14, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081504583Floor Support · corrodedCORROSION ON LOWER SILL IN AFT PAX CABIN LOCATED BETWEEN FRAMES 66 AND 68 AT STRINGER 23R. REPLACED LOWER SILL IN AFT PAX CABIN LOCATED BETWEEN FR 66-FR 68 AT LEVEL STR 23R IAW SRM 51-72-11 AND DWG D53480019; JOB COMPLETE.Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081404578Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CORNER ON FWD LEFT PASSENGER DOOR AT FRAME 16, STINGER 23. REPLACED LOWER CORNER IAW SRM 51-72-11 AND DWG D53112109;Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014081404577Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING, FWD OF LEFT PASSENGER ENTRY DOOR, BETWEEN FRAMES 16 - 20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112109.Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014081404576Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD OF LEFT PASSENGER ENTRY DOOR AT FRAME 20, STRINGER 23L. REPLACED LOWER CORNER STRUCTURE IAW SRM 51-72-11 AND DWG 53112109.Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014081404575Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN FLOOR SUPPORT Y1292 BETWEEN FRAMES 16-20. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D531-10920 AND D531-12812.Aug 13, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081404579Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN SEAT TRACK -Y1292 BETWEEN FRAMES 20-24. REPLACED SEAT TRACK IAW SRM 51-72-11, DWGS D53112812 AND D53110920.Aug 12, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081304574Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN FWD PAX CABIN, Y1732 FRAME 20. REPLACED WEB IAW SRM 51-72-11, DWG D53114392 AND DWG D53110920.Aug 12, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081304573Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 31 BETWEEN STRINGERS 41 - 42R IN FWD CARGO BAY. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231582.Aug 12, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014081304572Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE IN FWD CARGO BAY FRAME 32 BETWEEN STRINGERS 42 - 43R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231212.Aug 12, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014081304571Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE IN FWD CARGO BAY AT FRAME 33 BETWEEN STRINGERS 40 - 41R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231582.Aug 12, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014081304570Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON AFT PAX CABIN FLOOR SUPPORT Y765 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815; D53472831.Aug 12, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081304569Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON AFT PAX CABIN FLOOR SUPPORT Y765 BETWEEN FRAMES 66+ 5 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472000 & D53472815.Aug 12, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081304568Bearing · corrodedDURING INSPECTION, FOUND CORROSION ON BEARING AT LT WING INBD FLAP. REPLACED BEARING IAW CMM 57-52-21-410-011-A01. .Aug 12, 2014 · N324US · Airbus A320211 · Trailing Edge FlapsSDR DALA2014081304567Fitting · corrodedDURING INSPECTION, FOUND CORROSION IN FWD PAX CABIN FWD LOWER CORNER FRAME 16 BETWEEN STRINGERS 22 - 23L. REPLACED CORNER FITTING AND FASTENERS IAW SRM 51-72-11 AND DWG D531-12109.Aug 12, 2014 · N324US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014081304566Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 12, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081304565Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 12, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081304563Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y-1292, BETWEEN FRAMES 64 - 66+5". REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Aug 12, 2014 · N322US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016112309219Floor Support · corrodedCORROSION ON AFT PAX CABIN FLOOR SUPPORT -Y765 BETWEEN FRAMES 66+5" TO 70. REPLACED THE FLOOR SUPPORT IAW SRM.Aug 11, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081104423B-Nut · leakingAFTER LANDING, THE CREW CONTACTED MAINTENANCE AND ADVISED THAT THEY HAD DONNED THEIR OXYGEN MASKS DUE TO AN OIL ODOR. REPORTED PASSENGERS WERE GETTING SICK DUE TO THE ODOR. MAINTENANCE FOUND HYDRUALIC FLUID IN INTAKE DUCT AND PLENUM OF APU. ALSO FOUND LT GEAAug 11, 2014 · N314US · Airbus A320211 · Hydraulic System, MainSDR DALA2014081204422Battery Pack · no testDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS TEST FAULTED BATTERY AFT LT OF CABIN. MAINTENANCE REPLACED AFT LT BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Aug 11, 2014 · N325US · Airbus A320211 · Emergency LightingSDR DALA2014081204421Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON AFT PAX CABIN FLOOR SUPPORT -Y318 BETWEEN FRAMES 65 - 67. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472305.Aug 11, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081204420Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y512 BETWEEN FRAMES 64 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081204419Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 42L IN FWD CARGO BAY BETWEEN FRAMES 33 - 34. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53231212.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014081204418Frame · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN AFT LOWER CORNER OF FRAME 20 BETWEEN STRINGERS 22-23R. REPLACED LOWER CORNER OF FRAME 20 IAW SRM 51-42-11 AND DWG NR D53112109.Aug 11, 2014 · N324US · Airbus A320211 · Fuselage Main, FrameSDR DALA2014081104394Angle · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE INTERNAL AREA EMERGENCY DOOR 843. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522 79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104393Angle · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING ANGLE INTERNAL AREA EMERGENCY DOOR 843. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104392Angle · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING ANGLE LOCATED INTERNAL AREA EMERGENCY DOOR 844. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104391Angle · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATED INTERNAL AREA EMERGENCY EXIT DOOR 833. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104390Angle · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATION INTERNAL AREA EMERGENCY DOOR 834. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D52279010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104389Angle · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATION INTERNAL AREA EMERGENCY DOOR 844. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522 79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104388Structure · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE LOCATED INTERNAL AREA EMERGENCY DOOR 833. REPLACED SEGMENT ANGLE LOCATED ON INTERNAL AREA EMERGENCY DOOR AFT POSITION IAW SRM 51-72-11 AND DWG D522 79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104386Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081104385Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN FWD CARGO BAY BETWEEN FRAMES 32 - 34. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53231626.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014081104384Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-464.5 LOCATED BETWEEN FRAMES 64 - 67+10. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72305.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
Back to Airbus A320-211