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 DALA2014081104387Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON AFT PAX CABIN FLOOR SUPPORT -Y512 BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472229.Aug 10, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081004383Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT AT FRAME 33 AND BETWEEN STR 40L TO STR 41L MEASURES APPROXIMATELY L=0.110", W=0.105", D=0.002" SSI 532180. REPLACED CLEAT AND FASTENERS LOCATED IN FWD CARGO COMPARTMENT AT FR 33 AND BETWEEN Aug 10, 2014 · N322US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014081004382Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DG D53472000.Aug 9, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081004381Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y-765 BETWEEN FRAMES 64 - 66. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Aug 9, 2014 · N322US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081004380Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-464.5 BETWEEN FRAMES 67+10 - 70 . REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472400.Aug 9, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081004379Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOG AT FR 34 AND BETWEEN STR 43L TO STR 44 REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231212.Aug 9, 2014 · N322US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014080904378Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT AT FR 30 AND BETWEEN STR 40R TO STR 41R MEASURES 532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT AT FRAME 30 AND BETWEEN STR 40R TO STR 41R IAW SRM A320 51-72-11 AND DWG D53231582.Aug 8, 2014 · N322US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014080904377Cargo Track · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT AT FR 33 AND BETWEEN STRG 41L TO STRG 42L REPLACED CLEAF IN FWD IAW SRM 51-72-11 AND DWG D53231212, D53230337.Aug 8, 2014 · N322US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014080804373Wire · brokenDURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 3B AFT LIGHT ASSY. MAINTENANCE FOUND BROKEN WIRE UNDER SEAT. RECONNECTED WIRE AND FUNCTIONAL CHECK WAS NORMAL.Aug 7, 2014 · N363NW · Airbus A320211 · Light System WiringSDR DALA2014080804372Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD PASSENGER ENTRY DOOR RT AT FRAME 16, LEVEL STR23, INTERNAL STRUCTURE WITH MEASUREMENT OF L=0.500", W= 0.238" AND D=0.003" APPROXIMATELY, SSI 531163. REPLACED LOWER CORNER LOCATED FWD PASSENGER ENTAug 7, 2014 · N322US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2014080804371Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD PASSENGER ENTRY DOOR RT AT FRAME 16, LEVEL STR23, INTERNAL STRUCTURE WITH MEASUREMENT OF L=0.500", W=0.238" AND D=0.003" APPROXIMATELY, SSI 531163. REPLACED LOWER CORNER LOCATED FWD PASSENGER ENTRAug 7, 2014 · N322US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2014080804370Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD PASSENGER ENTRY DOOR RT AT FRAME 20 STR 23 INTERNAL STRUCTURE. REPLACED LOWER CORNER OF FWD PASSENGER ENTRY DOOR IAW SRM 51-72-11 AND DWG NRD53112109.Aug 7, 2014 · N322US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2014080804369Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-160.5, BETWEEN FRAMES 68 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 7, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080804368Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FRAMES 66 - 68 AND STRINGER 23R. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53480505.Aug 7, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080804367Structure · corrodedDURING INSPECTION, FOUND CORROSION ON AFT PAX DOOR CUTOUT LOWER CORNER BETWEEN, STRINGERS 22 - 23L FRAME 68. REPLACED DOOR CUTOUT LOWER CONER IAW SRM 51-72-11 AND DWG D53480505.Aug 7, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014080704353Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 LOCATED BETWEEN FRAMES 67+17 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.Aug 6, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080704352Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON UPPER SPLICE INBD SIDE Y1162 AT FRAME 67+17. REPLACED UPPER SPLICE IAW SRM 51-72-11 AND DWG D53472000.Aug 6, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080704351Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765 LOCATED BETWEEN FRAME 64 - 66. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG NR D53472000.Aug 6, 2014 · N322US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014080704350Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT FRAME 20, Y-1292 . REPLACED FLOOR SUPPORT FRAMES 12 - 24 IAW SRM 51-72-11 AND DWG D53112812.Aug 6, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080704349Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN FLOOR SUPPORT -Y189 BETWEEN FRAMES 20 - 21. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.Aug 6, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080704348Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FRAME 20, Y-765. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IAW SRM 51-72-11 AND DWG D53112812.Aug 6, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080704347Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 32 - 33. REPLACED STRINGER.Aug 6, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014080704346Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 33 - 34. REPLACED STRINGER.Aug 6, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014080604322Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 20 - 23 Y-189. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.Aug 5, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080404302Cover · corrodedDURING INSPECTION, FOUND CORROSION ON JOINT COVER IN FWD PAX CABIN AT FRAME 14 Y-1.234. REPLACED JOINT COVER IAW SRM 51-72-11, DWG D53112619, D53110984 AND D53112829.Aug 3, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080404301Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY FRAME 30 BETWEEN STRINGERS 41 - 42R. REPLACED CLEAT IAW SRM 51-72-11, DWGS D532-31582 AND S532-30320.Aug 3, 2014 · N322US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014080204298Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY AT FRAME 29 BETWEEN STRINGERS 42-43L. REPLACED CLEAT IAW 51-72-11, DWGS D532 31212 AND D532 30319.Aug 2, 2014 · N322US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014080204297Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY AT FRAME 32 BETWEEN STRINGERS 42-43R. REPLACED THE CLEAT IAW SRM 51-72-11, DWGS D532 31212 AND D532 31486.Aug 2, 2014 · N322US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014080204296Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY AT FRAME 33 AND BETWEEN STRINGERS 43-44R. REPLACED THE CLEAT IAW SRM 51-72-11, DWG D532 31212 AND D532 30337.Aug 2, 2014 · N322US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014080204295Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000.Aug 2, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014080204294Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 16 - 21 Y254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWGS D53112816 , D53110422 , & D53110984.Aug 1, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014073004270Floor Panel · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR PANEL 231AF. FOUND OUT OF LIMITS. REPLACED FLOOR PANEL .Jul 29, 2014 · N323US · Airbus A320211 · Fuselage Floor PanelSDR CA140728003Sensor · failed(CAN) FLIGHT DIVERTED DUE TO YELLOW HYDRAULIC SYS FAILURE. CFR WAS CALLED OUT FOR ARRIVAL. YELLOW HYD TEMP SENSOR 3381GR REPLACED IAW AMM 29-33-11-400-003-A DUE TO CONTAMINATION, DAMAGE FOUNDED INSIDE TRANSMITTER.Jul 27, 2014 · Airbus A320211 · Hydraulic Indicating SystemSDR DALA2014072804223Battery Pack · inoperativeDURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHTS FAULTING AT LT BATTERY. MAINTENANCE REPLACED BATTERY PACK AND FUNCTIONAL CHECKED NORMAL.Jul 27, 2014 · N337NW · Airbus A320211 · Emergency LightingSDR DALA2014072704222Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FRAMES 69-70 STR 23R IN AFT PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D534 70100.Jul 27, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014072704221Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB LOCATED BETWEEN FRAMES 69-70 STR 23L IN AFT PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D53470100.Jul 27, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016112509224Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y254 LOC. BETWEEN FRAMES 24 - 35. REPLACED THE FLOOR SUPPORT.Jul 24, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014072504220Door Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL THE R2 DOOR. REPLACED LOWER SILL BETWEEN FRAMES 66-68 AT LEVEL STRINGER 23R IAW SRM 51-72-11 AND DWG D53480505.Jul 24, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014072404219Structure · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION TEE LOCATED ON LOWER CURVED EDGE LT SIDE THE E/E HATCH DOOR. REPLACED SECTION TEE IAW SRM 51-72-11 AND DWG D52279040 .Jul 23, 2014 · N323US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA2014072404218Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CURVED EDGE LT OF THE E/E HATCH DOOR. REPLACED LOWER CURVED EDGE IAW SRM 51-72-11 AND DWG D52279010.Jul 23, 2014 · N323US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA2014072404217Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CURVED EGDE RT SIDE THE E/E HATCH DOOR. REPLACED SECTION TEE IAW SRM 51-72-11 AND DWG D52279040.Jul 23, 2014 · N323US · Airbus A320211 · Emergency ExitsSDR DALA2016112509225Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT.Jul 22, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014072304178Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER40R REPAIR, IN AFT CARGO BAY BETWEEN FRAMES 62-64. REPAIRED STRINGER IAW SRM 53-00-13, PARA 4.A FIG 201, DWGS E53470330 AND D53470338.Jul 22, 2014 · N323US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014072304177Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 36 - 41. EVALUATED AND FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Jul 22, 2014 · N323US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014072304176Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK, Y1292 BETWEEN FRAMES 41-47. EVALUATED AND FOUND OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53377500.Jul 22, 2014 · N323US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014072304175Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 FRAME 47+8 ON UPPER FLANGE. EVALUATED AND FOUND OUT LIMITS. REPLACED SEAT TRACK BETWEEN FRAMES 47 - 64 IAW SRM 51-72-11 AND DWG D53472000.Jul 22, 2014 · N323US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR CA140721021Actuator · failed(CAN) NO AUTOPILOT AND FLIGHT CONTROL PROBLEMS, MAYDAY DECLARED. ACFT CIRCLED, TRYING TO RESOLVE FLIGHT CONTROL PROBLEMS. REPLACED RT SLAT 2, OTBD TRACK ACTUATOR IAW AMM 27-84-49-401.Jul 20, 2014 · Airbus A320211 · Leading Edge Slat ActuatorSDR DALA2014072104166Skin · dentedDURING INSPECTION, FOUND A DENT ON EXTERNAL FUSELAGE SKIN AT FRAME 69 STRINGERS 27-28R. REPAIRED SKIN IAW SRM 53-41-11 PARA 5.M, FIG 216.Jul 20, 2014 · N323US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2014072104165Floor Support · brokenDURING INSPECTION, FOUND FLOOR SUPPORT BROKEN AT Y254 BETWEEN FRAMES 24-35. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53231181.Jul 20, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014072004164Angle · crackedDURING INSPECTION, FOUND SEVERAL CRACKS WERE FOUND IN AFT SEGMENT ANGLE BETWEEN BEAMS NR 1 AND 3 INTERNAL STRUCTURE OF EMERGENCY EXIT DOOR. REPLACED AFT SEGMENT ANGLE IAW SRM 51-72-11 AND DWG.Jul 19, 2014 · N323US · Airbus A320211 · Emergency Exits
Back to Airbus A320-211