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 CA140918008Computer · failed(CAN) APPROXIMATELY 1 HOUR INTO THE FLIGHT THE CREW REPORTED AN AVIONICS SMOKE ECAM WARNING AND AFTER A DISCUSSION WITH MAINTENANCE A PANPAN WAS DECLARED AND THE FLIGHT DIVERTED. LANDING WEIGHT WAS UNDER MAXIMUM. RESOLUTION T/S CARRIED AS PER FIM 26-15-00-8Sep 18, 2014 · Airbus A320211 · Air Distribution SystemSDR CA140915007Computer · failed(CAN) ON APPROACH, THE AIRCRAFT DEVELOPED A SLAT ISSUE. WITH THE RUNWAY BEING SHORTER, THE CREW ELECTED TO DIVERT. AN EMERGENCY WAS DECLARED WITH A NORMAL LANDING BEING CARRIED OUT. NR 1 SFCC REPLACED AS PER AMM 27-51-34-400-001-A & TESTED IAW AMM 27-54-00-71Sep 10, 2014 · Airbus A320211 · Leading Edge Slat Control SystemSDR CA140910004Hydraulic Line · failed(CAN) SLOW DEPLETION OF GREEN HYDRAULIC FLUID IN CRUISE ABOUT 1 HOUR FROM DESTINATION. ECAM ACTIONS COMPLETED. ARRIVAL AND LANDING UNEVENTFUL. MAINTENANCE MET FLIGHT AT GATE. RESOLUTION REPAIRED GREEN SYSTEM PX SUPPLY LINE P/N : D2904004809601OUTBD OF RIB 5Sep 3, 2014 · Airbus A320211 · Hydraulic System, MainSDR DALA2014090404911Light · missingDURING NON-ROUTINE CHECK, FOUND SEAT 20A MISSING AISLE EMERGENCY LIGHT. MAINTENANCE REPLACED EMERGENCY LIGHT AND FUNCTIONAL CHECKED NORMAL.Sep 1, 2014 · N313US · Airbus A320211 · Emergency LightingSDR DALA2014090104884Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB -Y1732 FRAME 16. REPLACED WEB IAW SRM 51-72-11 AND DWG D53114392.Aug 31, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016112309217Web · corrodedCORROSION ON WEB LOCATED IN AFT CARGO BAY BETWEEN FRAMES 48 AND 49 STRINGER 38R. REPAIRED THE WEB IAW PRI ER/A.Aug 29, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2017100407292Frame · crackedA CRACK WAS FOUND IN FRAME 20, ONLY AT THE NR 6 FASTENER HOLE, ABOVE DOOR STOP NR 7, REPAIRED IAW ER/A 528127-14.Aug 28, 2014 · N324US · Airbus A320211 · Fuselage Main, FrameSDR DALA2014082904835Stringer Splice · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE LOCATED BETWEEN FRAMES 30 - 31 STRINGER 41R. REPLACED STRINGER SPLICE IAW SRM 51-72-11 AND DWG D53231586.Aug 28, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082804803Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FRAME 13. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D531-13515.Aug 27, 2014 · N324US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014082804802Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 42R BETWEEN FRAMES 64 - 65. REPAIRED IAW SRM 53-00-13, PARA 4 A, FIG 201, SHEET 2 AND DWG D53480030.Aug 27, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082804801Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 66 BETWEEN STRINGERS 43 - 44R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53480210.Aug 27, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014082804805Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FRAMES 51 - 52 STR 38R. REPLACED WEB IAW SRM 51-72-11 AND DWG D53470320.Aug 26, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014082804804Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FRAMES 50 - 51, STRINGER 38R. REPLACED WEB IAW SRM 51-72-11 AND DWG D53470320.Aug 26, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014082704775Skin · corrodedDURING INSPECTION, FOUND CORROSION ON INTERNAL SKIN BETWEEN STRINGERS 43-44R BETWEEN FRAMES 64 - 65. REWORKED AREA IAW 51-74-00.Aug 26, 2014 · N324US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2014082704774Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 42R BETWEEN FRAMES 31 - 32. REPLACED THE STRINGE IAW SRM 51-72-11 AND DWG D53231626.Aug 26, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082704773Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE LOCATED IN FWD CC AT LEVEL OF FRAME 34 AND BETWEEN STR 42R TO STR 43R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231215.Aug 26, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014082704772Skin · dentedDURING INSPECTION, FOUND A DENT ON EXTERNAL FUSELAGE SKIN AT FRAME 24A+9 BETWEEN STRINGERS 42 AND 43R. REPAIRED THE SKIN IAW SRM 53-00-11; PARAGRAPH 4. W, FIG 238, PAGE 571/572.Aug 26, 2014 · N324US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2014082604756Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE LOCATED FWD CARGO COMPARTMENT AT LEVEL OF FR32 AND BETWEEN STR 41R AND STR 42R. REPLACED SHEAR TIE, CLEAT, LOCATED FWD CARGO COMPARTMENT AT LEVEL OF FR 32 AND BETWEEN STR 41R TO STR 42R IAW SRM 51-72-11 AND DWG DAug 25, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014082604755Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE LOCATED AT LEVEL OF FRAME 31 BETWEEN STR 39R TO STR 40R FWD CC. REPLACED SHEAR TIE, CLEAT LOCATED AT LEVEL OF FRAME 31, BETWEEN STR 39R TO STR 40R FWD CC IAW SRM 51-72-11 AND DWG D53231568.Aug 25, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014082604754Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE LOCATED AT LEVEL OF FRAME 26 BETWEEN STR 42L TO STR 43L FWD CC. REPLACED SHEAR TIE, CLEAT, LOCATED AT LEVEL OF FRAME 26, BETWEEN STR 42L TO STR 43L FWD CC AS IAW SRM 51-72-11 AND DWG D53230324.Aug 25, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014082604753Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL OF AFT PAX CABIN LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL OF STR 23L, SSI 534147, L=1.00", W=0.500", D=0.003" APPROXIMATELY. REPLACED LOWER SILL L2 OF AFT PAX CABIN LOCATED BETWEEN FRAME 66 AND FRAME 68 AT LEAug 25, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014082604752Profile · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE IN EMERGENCY EXIT DOOR 834 INTERNAL STRUCTURE. REPLACED AFT LOAD TRANSMITTING PROFILE IN EMERGENCY EXIT DOOR 834. INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG D52279010.Aug 25, 2014 · N324US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014082604751Profile · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING PROFILE LOCATED ON INTERNAL STRUCTURE OF EMERGENCY EXIT DOOR 844. REPLACED FWD LOAD TRANSMITTING PROFILE LOCATED ON INTERNAL STRUCTURE OF EMERGENCY EXIT DOOR 844 IAW SRM 51-72-11 AND DWG D52279040.Aug 25, 2014 · N324US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014082604750Profile · crackedDURING INSPECTION, FOUND CRACK ON FWD AND AFT LOAD TRANSMITING PROFILE OF LT FWD E/E DOOR 833. REPLACED FWD AND AFT LOAD TRANSMITTING PROFILE OF LT E/E DOOR, 833, SRM 51-72-11 AND DWG D52279040.Aug 25, 2014 · N324US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014082604749Profile · crackedDURING INSPECTION, FOUND CRACK ON FWD AND AFT LOAD TRANSMITING PROFILE OF RT FWD E/E DOOR (843). REPLACED FWD AND AFT LOAD TRANSMITTING PROFILE OF RT E/E DOOR (843) IAW SRM 51-72-11 AND DWG D52279010.Aug 25, 2014 · N324US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014082604748Skin · corrodedDURING INSPECTION, FOUND CORROSION ON INTERNAL SKIN AT FRAME 65 BETWEEN STR 43R TO STR 44 . REWORKED & EVALUATED WITH N/R 5320-5010/174, ZONE 100 AND FOUND OUT LIMITS MUST BE REPAIR . PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW FRAME 64 TO Aug 25, 2014 · N324US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2014082504701Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 44 BETWEEN FRAMES 64 - 65 IN THE AFT CARGO BAY. REPAIRED THE STRINGER IAW SRM 53-00-13, FIG 201, SHEET 2.Aug 24, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082504700Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 42L BETWEEN FRAMES 64 - 65 IN THE AFT CARGO BAY. REPAIRED THE STRINGER IAW SRM 53-00-13, FIG 201, SHEET 2.Aug 24, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082504699Stringer · corrodedDURING INSPECTION, PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON STRINGER 33L BETWEEN FRAMES 65 - 66. REPAIRED THE STRINGER IAW SRM 53-00-13, FIG 201.Aug 24, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082404698Seat Track · corrodedDURING INSPECTION, CORROSION FOUND ON SEAT TRACK -Y1292 BETWEEN FRAMES 24 - 35, FOUND TO BE OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DWG D53231181, DWG D53110920 AND DWG D53210005.Aug 23, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014082304697Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 47 - 64, FOUND TO BE OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND SRM 53-41-15.Aug 22, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014082304696Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 47 - 64, FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11.Aug 22, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017100407291Frame · corrodedTHREE CORRODED SPOTS WERE FOUND ON THE FWD FLANGE OF FRAME 20, STRINGER 23L. REWORKED IAW SRM 51-74-00 AND FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS, REPAIRED IAW ERA 528120-14.Aug 21, 2014 · N324US · Airbus A320211 · Fuselage Main, FrameSDR DALA2014082204677Stringer · corrodedCORROSION ON STRINGER 43L AFT CARGO BAY BETWEEN FRAMES 63 - 64. WORKED CORROSION IAW SRM 51-74-00. FOUND WITHIN TOLERANCES IAW DAN 50, TABLE 4, FIG 1.Aug 21, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082204676Stringer · corrodedCORROSION ON STRINGER 31R FRAME 65. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480009.Aug 21, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082004662Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 42R IN FWD CARGO BAY BETWEEN FRAMES 28 - 31. REPLACED STRINGER SPLICE IAW SRM 51-42-11, 51-72-11, DWG D53231248200, ERA 528125-14, ORIGINAL REVISION AND PRI 528125-14 REV 0.Aug 19, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082004661Frame · corrodedCORROSION FOUND ON FRAME 66 S23L. FOUND WITHIN LIMITS IAW SRM 53-41-12, FIG 102, PAGE 104, PARAGRAPH 4.A.Aug 19, 2014 · N324US · Airbus A320211 · Fuselage Main, FrameSDR DALA2014082004659Stringer · corrodedCORROSION ON STRINGER 43R IN FWD CARGO BAY BETWEEN FRAMES 32 - 33. REPAIRED STRINGER IAW SRM 53-00-13, PARA 4.A ITEM 7, FIG 201, SHEET 1, PAGE 211-212. .Aug 19, 2014 · N324US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082004658Seat Track · corrodedCORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 47 - 64 FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Aug 19, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014082004657Fitting · corrodedCORROSION ON CENTER FITTING AT AFT PASSENGER ENTRY DOOR BETWEEN FRAMES 66 - 68. REPLACED THE CENTER FITTING IAW SRM 57-72-11 AND DWG D534-80505.Aug 19, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014082004656Floor Support · corrodedCORROSION ON AFT PAX CABIN FLOOR SUPPORT Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 19, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014082004655Floor Support · corrodedCORROSION ON AFT PAX CABIN FLOOR SUPPORT Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 19, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014082004654Floor Support · corrodedCORROSION ON AFT PAX CABIN FLOOR SUPPORT Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 19, 2014 · N324US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014082004653Shear Tie · corrodedCORROSION ON SHEAR TIE FRAME 26 BETWEEN S41 - 42L IN FWD CARGO BAY. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53230324.Aug 19, 2014 · N324US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2014081904652Seat Track · corrodedCORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 36 - 41 FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11.Aug 18, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081904651Seat Track · corrodedCORROSION ON SEAT TRACK, -Y765, BETWEEN FRAMES 41 - 47 FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Aug 18, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081904650Seat Track · corrodedCORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 24 - 35 FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53231181.Aug 18, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016112309218Stringer · corrodedCORROSION FOUND UNDER AFT CARGO BIN FLOOR FRAMES 56 & 57 AND AT STRINGER 42L. REMOVED CORROSION, MANUFACTURED A DOUBLER, TREATED AND PRIMED. INSTALLED THE STRINGER REPAIR IAW SRM.Aug 17, 2014 · N378NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082004660Seat Track · corrodedCORROSION ON SEAT TRACK Y765 BETWEEN FRAMES 41 - 47 FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D533370500.Aug 17, 2014 · N324US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081804648Skin · corrodedCORROSION ON INTERNAL SKIN OF FWD CARGO BAY FRAME 34+2 BETWEEN S42 - 43R. FOUND WITHIN LIMITS IAW SRM 53-21-11, PARAGRAPH 4-E, FIG 115, DIAGRAM 105, SHEET 2.Aug 17, 2014 · N324US · Airbus A320211 · Fuselage Main, Plate/Skin
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