Airbus A320-211

Service difficulty reports · 5,271

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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 DALA13046803226Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y81 FWD PAX CABIN BETWEEN FRAMES 12 AND 16. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112828.Sep 23, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA130923003Uplock · failed(CAN) AFTER TAKEOFF THE LT MLG FAILED TO RETRACT AND THE FLIGHT RETURNED LANDING APPROXIMATELY 6000KG OVERWEIGHT. RT MLG UPLOCK PEPLACED IAW AMM 32-31-45-401. OPS TEST C/O. NO FURTHER FAULT.Sep 22, 2013 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR DALA13046313226Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT, +Y765 BETWEEN FRAMES 66+4" AND 70 IN PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Sep 22, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13046303226Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 32 S42-43R FWD CARGO BAY. REPLACED CLEAT IAW SRM AND DWG D53231626.Sep 22, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13046293226Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 31 BETWEEN S40-41L, FWD CARGO BAY. REPLACED CLEAT IAW SRM A320 51-72-11 AND DWG D53231626.Sep 22, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13046283226Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT FRAME 32 BETWEEN S42-43R FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626.Sep 22, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13046273226Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 32 BETWEEN STR 42-43L FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626.Sep 22, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13046223226Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 32 BETWEEN STR 40-41R FWD CARGO BAY. REPLACED CLEAT IAW SRM A320 51-72-11 AND DWG D53231586.Sep 21, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13046213226Cleat · corrodedDURING INSPECTION, CORROSION ON CLEAT LOCATED AT FR 33, BETWEEN STR 41-42R FWD CARGO BAY. REPLACED CLEAT IAW SRM A320 51-72-11 AND DWG D53231586.Sep 21, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13043273217Wire · damagedDURING NON ROUTINE CHECK, FOUND BROKEN BACK SHEET OF ELECTRICAL CONNECTOR ON WIRING CONNECTION 18,19 AND 20 LT BETWEEN SEAT AND ACFT OF PAX CABIN. MX REPLACED ELECTRICAL CONNECTOR AND EPSU. FUNCTIONAL CHECK WAS NORMAL.Sep 8, 2013 · N317US · Airbus A320211 · Light System WiringSDR DALA13042873217Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY BETWEEN FRAMES 62 TO 63 AND S38R. REPLACED WEB AND FASTENER IAW SRM 51-72-11 AND DWG D53470321.Sep 5, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13042863217Structure · corrodedDURING INSPECTION, FOUND CORROSION ON AFT FUSELAGE INTERNAL STRUCTURE BETWEEN FRAMES 65 TO 66 AND S42-43L. REPLACED REINFORCEMENT ON AFT FUSELAGE INTERNAL STRUCTURE BETWEEN FR.65 TO FR.66 AND STR.40L TO STR 43L IAW SRM 51-72-11 AND DWG D53480030.Sep 5, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13042853217Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE IN AFT CABIN FLOOR STRUCTURE BETWEEN FRAMES 69 AND 70 S23R. REPLACED SHEAR PLATE IAW SRM 51-72-11.Sep 5, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13042843217Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB LOCATED AT LEVEL OF FR 16, RT FLOOR STRUCTURE STRG 23R. REPLACED WEB AND FASTENER IAW SRM 51-72-11 AND DWG D53112780.Sep 5, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13042753229Compressor · stalledDURING CRUISE, NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT APPROXIMATELY 50 PERCENT N1. CREW DECLARED EMERGENCY AND FLIGHT WAS DEVERTED. ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED NR 1 ENGINE AND FUNCTIONAL CHECK WAS NORMAL.Sep 5, 2013 · N329NW · Airbus A320211 · Turbine Engine Compressor SectionSDR DALA13042743217Floorbeam · brokenDURING INSPECTION, FOUND BROKEN UPPER FLANGE ON FLOORBEAM, Y254, BETWEEN FRAMES 24 AND 27. PERFORMED PERMANENT REPAIR IAW SRM 53-00-14, PARA 4.G, FIG 207.Sep 4, 2013 · N317US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13042613217Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO COMPARTMENT BETWEEN FR 56 TO FR 57 AND STR 38R. REPLACED WEB IN AFT CARGO COMPARTMENT BETWEEN FR 56 TO FR 57 AND STR 38R IAW SRM A320 51-72-11 AND DWG D53470321.Sep 3, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13042633216Wire Harness · damagedDURING NON-ROUTINE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 18 ABC INOPERATIVE. MX FOUND SEAT HARNESS WIRE PULLED FROM CONNECTOR. INSTALLED NEW CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL.Sep 2, 2013 · N316US · Airbus A320211 · Light System WiringSDR DALA13042603217Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 16 AND FR 20 AT STRG 23L FWD PAX CABIN. REPLACED CENTER FITTING LOCATED BETWEEN FR 16 AND FR 20 AT STRG 23L FWD PAX CABIN IAW SRM 51-72-11.Sep 2, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13044043217Skin · dentedDURING AAI INSPECTION, NOTED THAT AN EXISTING DENT & SCRAPE ON THE RT SIDE OF THE FUSELAGE 22 INCHES FWD OF FR 24. PERFORMED PERMANENT REPAIR IAW SRM 53-21-11, PARA 5.K, FIG 214.Aug 31, 2013 · N317US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13042623277Epsu · faultedDURING NON ROUTINE CHECK, FOUND RT EPSU FAULT ON CIDS PANEL. MX REPLACED RT EPSU AND FUNCTIONAL CHECK WAS NORMAL.Aug 31, 2013 · N377NW · Airbus A320211 · Emergency LightingSDR DALA13042593217Tee Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON LT SECTION TEE LOCATED AT INTERNAL LOWER AREA OF THE OVERWING EMERGENCY EXIT DOOR 833 MEASURES L=1",W=0.400", D=0.020" APPROXIMATELY. REPLACED LT SECTION-T LOCATED AT INTERNAL LOWER AREA OF THE OVERWING EMERGENCY DOOR IAWAug 31, 2013 · N317US · Airbus A320211 · Emergency ExitsSDR CA130830017Wire · chafed(CAN) AFTER DEPARTURE, THE ACFT ENCOUNTERED AN OVERHEATED BLUE HYDRAULIC SYSTEM MESSAGE. THE FLIGHT CREW RETURNED AND HELD BRIEFLY ON RUNWAY FOR CFR TO MEET AND INSPECT THE ACFT. WITH ALL INDICATIONS NORMAL, THE ACFT WAS TAXIIED TO THE GATE UNDER ITS OWN POWAug 30, 2013 · Airbus A320211 · Hydraulic Power System WiringSDR DALA13041913217Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FRAMES 16 AND 20, REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112225.Aug 28, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041643217Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY AT FRAME 29 AND BETWEEN S41- 42R. REPLACED CLEAT IAW SRM 51-72-11.Aug 27, 2013 · N317US · Airbus A320211 · Fuselage Main, Attach FittingsSDR CA130829002Electrical Sys · malfunctioned(CAN) DURING CLIMBOUT, FLIGHT EXPERIENCED AN ELECTRICAL POWER INTERRUPTION LASTING 1-5 SECONDS, THAT RESULTED IN LOSS OF ALL SCREENS, AUTOPILOT, AUTOTHRUST, AND FAC1. ECAM ACTIONS COMPLETED AND ALL SYSTEMS RESTORED. ALL PARAMETERS CHECKED NORMAL, IAW CREW COMAug 26, 2013 · Airbus A320211 · Electrical Power SystemSDR DALA13041633217Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE IN AFT CABIN FLOOR STRUCTURE. FRAMES 69 AND 70. REPLACED SHEAR PLATE IAW SRM 51-72-11.Aug 26, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041463217Floor Support · corrodedDURING INSPECTION, FOUND CORROSION AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 66 AND 68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480019.Aug 25, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041093217Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY FRAME 28 AND BETWEEN S41-42R.Aug 24, 2013 · N317US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13041083217Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY BETWEEN FR 62 TO FR 63 AND STR 38L. REPLACED WEB AND FASTENERS IAW SRM A320 51-72-11 AND DWG D53470321.Aug 24, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041073217Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY BETWEEN FR 58 TO FR 59 AND STR 38L. REPLACED WEB IAW SRM 51-72-11 AND DWG D53470321.Aug 24, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041063217Sill · corrodedDURING INSPECTION, FOUND AFTER CORNER FITTING REMOVAL IAW 200-226, FOUND LOWER SILL WITH CORROSION RT SIDE FWD PAX CABIN, REPLACED LOWER SILL. REPLACED LOWER SILL LOCATED RT SIDE FWD PAX CABIN IAW SRM A320 51-72-11 AND DWG D53110339.Aug 23, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041053217Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING LOCATED AT LEVEL OF FWD FR 20 AND STRG 23R FWD PAX CABIN L=0.50" W=0.25" AND D=0.002". REPLACED CORNER FITTING LOCATED AT LEVEL OF FWD FR 20 AND STRG 23R, FWD PAX CABIN, IAW SRM 51-72-11 AND DWG D53112225.Aug 23, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041043217Structure · corrodedDURING INSPECTION, CORROSION ON BEAM LOCATED IN AFT CARGO COMPARTMENT BETWEEN FR 58 TO FR 59 AND LEVEL STR 44. REPLACED BEAM LOCATED IN AFT CARGO COMPARTMENT BETWEEN FR 58 TO FR 59 AND LEVEL STR 44 IAW SRM A320 51-72-11 AND DWG D53470340 AND D53470014.Aug 23, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041033217Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING AFT OF FRAME 16 STRINGER 23R FWD PAX CABIN. REPLACED CORNER FITTING LOCATED AT LEVEL OF AFT FR 16 AND STRG 23R FWD PAX CABIN IAW SRM 51-72-11 AND DWG D53112225.Aug 23, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13041023217Structure · damagedDURING INSPECTION, FOUND ELONGATED HOLE ON BEAM IN AFT CARGO BAY BETWEEN FR 55 TO FR 56, LEVEL STR 44. REPLACED BEAM AND FASTENERS LOCATED IN AFT CARGO COMPARTMENT BETWEEN FR 55 TO FR 56, LEVEL STR 44 IAW SRM 51-72-11 AND DWG D53470014.Aug 23, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2013082300432Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL AFT CABIN FLOOR STRUCT LOCATION AT FR 68 OUTER FLANGE LT SIDE MEASURED L=0.500", W=0.250" D=0.007" APPROXIMATELY PERFORMED PERMANENT REPAIR ON LOWER SILL AFT CABIN FLOUR STRUCT LOCATION AT FR68 OUTER FLANGE LT SAug 22, 2013 · N317US · Airbus A320211 · Fuselage Floor PanelSDR DALA2013082309332Floor Support · corrodedDURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT FR 67+16" AND FR 69. REPLACED FLOOR SUPPORT IAW A320 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA20130823001Floor Support · corrodedDURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT, FR 67+16" AND FR 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2013082313217Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 IN AFT CABIN FLOOR STRUCTURE LOCATION BETWEEN FR 66+5" AND FR 67+16". REPLACED FLOOR SUPPORT IAW SRM 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2013082303217Support Angle · corrodedDURING INSPECTION, FOUND CORROSION ON SUPPORT ANGLE LOCATION BETWEEN STR 43-44R FR 31+9". REPLACED SUPPORT ANGLE IAW SRM 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2013082393217Support Angle · corrodedDURING INSPECTION, FOUND CORROSION ON SUPPORT ANGLE LOCATED BETWEEN STR 43-44 FR 31+15". REPLACED SUPPORT ANGLE IAW SRM 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2013082383217Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1225 IN AFT CABIN BETWEEN FR 66+5" AND FR 67+16". REPLACED FLOOR SUPPORT IAW SRM 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2013082373217Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPART. FRAME 31 BETWEEN STR 40-41R, REPLACED CLEAT IAW SRM 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2013082363217Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO COMPARTMENT BETWEEN FR 50 TO FR 51 AND STR 38R. REPLACED WEB IAW SRM 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2013082300217Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STR 43L TO STR 43R AT FR 32. REPLACED CLEAT IAW SRM 51-72-11.Aug 22, 2013 · N317US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13040453217Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM Y-1292 LOCATED AT LEVEL OF FR 21. REPLACED FLOORBEAM IAW SRM 51-72-11& DWG D53112812.Aug 20, 2013 · N317US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13040443217Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FWD OF FR 68 AND S23L. REPLACED CORNER FITTING IAW SRM 51-72-11.Aug 20, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13040433217Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING LOCATED AFT FR 16 AND S23L. REPLACED CORNER FITTING LOCATED IAW SRM 51-72-11 AND DWG D53112225.Aug 20, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13039823217Rail · corrodedDURING INSPECTION, FOUND CORROSION ON RAIL DUMMY Y-81 LOCATED BETWEEN FR 12 AND FR 16 FLOOR STRUCTURE FWD PAX CABIN L=0.5" W=0.2" D=0.002" APPROX. REPLACED RAIL DUMMY Y-81 LOCATED BETWEEN FR 12 AND FR 16 FLOOR STRUCTURE FWD PAX CABIN IAW SRM 51-72-11.Aug 18, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous Structure
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