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 DALA13056933212Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT Y765 FRAME 66. REPLACED FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 IAW SRM 51-72-11 AND DWG D53472090 AND D53472000.Oct 31, 2013 · N312US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13056273212Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT LOCATED BETWEEN FRAMES 20 TO 22 -Y189 FWD PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.Oct 28, 2013 · N312US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13054143218Relay · malfunctionedDOOR LIGHTS ON AFTER GEAR UP. CABIN LIGHT UNCONTROLLABLE FROM F/A PANEL. R & R RELAY 8WL IAW ASM 33-51. OPS TESTED GOOD, OK FOR CONTINUED SERVICE.Oct 20, 2013 · N318US · Airbus A320211 · Lighting SystemSDR CA131017006Filter · dirty(CAN) THE FLIGHT CREW REPORTED AN ODOR IN THE CABIN ON DEPARTURE FROM 3000 FT TO CRUISE. THE ODOR SEEMED TO DISSIPATE AFTER SELECTION OF PACK FLOW. AFTER ARRIVAL, STATION REPORTED THAT THE ENTIRE IFS CREW HAD IRRITATION IN THEIR EYES AND THROAT. THERE WAS NO Oct 16, 2013 · Airbus A320211 · Air Distribution SystemSDR DALA13052953221Wire · damagedIN-SEAT EMERGENCY LIGHTS INOPERATIVE AT ROWS 2, 6, 21, 22 AND 25. REPLACED LAMPS AND REPAIRED WIRING. OPS CHECKED GOOD IAW AMM 33-51-00.Oct 16, 2013 · N321US · Airbus A320211 · Light System WiringSDR DALA13052963231Battery Pack · inoperativeFOUND ON SERVICE CHECK. EMERGENCY LIGHTS TEST FAILS. FAULTS "BATTERY AFT L". FOUND 13WL EPSU BATTERY BAD. REPLACED IAW AMM 33-51. OPS OK AND EMERGENCY LIGHTS TEST PASSES.Oct 15, 2013 · N331NW · Airbus A320211 · Emergency LightingSDR DALA13052023226Plate · corrodedDURING INSPECTION, FOUND CORROSION ON AREA SURROUNDING THE FWD LT PASSENGER DOOR CUT OUT LOCATED AT LEVEL OF FWD FACE FRAME 20 AND STR 23L, REPLACED REINFORCEMENT PLATE IAW SRM 51-72-11, DWG D53112174, D53112350 AND ER/A NR 518745-14,REV ORIGINAL.Oct 13, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13052013226Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE LOCATED BETWEEN FRAMES 69 AND 70 AT S23R IN PAX CABIN. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D53470100.Oct 13, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13052003226Plate · corrodedDURING INSPECTION, FOUND CORROSION ON REFORCING PLATE IN BULK CARGO COMPART. LOCATED BETWEEN FRAMES 65 TO 66 AND STRINGERS 37-43L REPLACED REFORCING PLATE IAW SRM 51-72-11.Oct 13, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13052033230Battery Pack · inoperativeDURING EMERGENCY LIGHTS CHECK, FOUND AFT LT BATTERY PACK FAULT. REPLACED BATTERY AND FUNCTION WAS NORMAL.Oct 12, 2013 · N330NW · Airbus A320211 · Emergency LightingSDR DALA13051993226Plate · corrodedDURING INSPECTION, FOUND CORROSION ON PLATE LOCATED AT FRAME 24A THRESHOLD SHEET AREA FWD CARGO COMPARTMENT. REPLACED PLATE IAW SRM 51-72-11.Oct 10, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13051093227Battery Pack · failedDURING NON ROUTINE CHECK, FOUND FWD LT EMERGENCY BATTERY FAILED. REPLACED BATTERY AND FUNCTIONAL CHECKED NORMAL.Oct 8, 2013 · N327NW · Airbus A320211 · Emergency LightingSDR DALA13049823226Rod · corrodedDURING INSPECTION, FOUND CORROSION ON TARGET AND PLAY ON ACTUATOR ROD AND PLAY ON BEARING AT INTERCONNECTING STRUT. LT SIDE. REPLACED INTERCONNECTING STRUT LT SIDE. IS DOCUMENTED ON AMDS CARD 2751-9202/101.Oct 6, 2013 · N326US · Airbus A320211 · Flight Control SystemSDR DALA13049813226Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 44 IN AFT CARGO BAY FRAMES 61. PERFORMED PERMANENT REPAIR ON STRINGER 44 IAW SRM 53-00-13, PARA 4A, FIG 201 (SHEET 2) PAG 213/214.Oct 6, 2013 · N326US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13050653226Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN AFT CARGO BAY BETWEEN FRAMES 56 TO 57. REPAIRED STRINGER.Oct 5, 2013 · N326US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13050643226Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL REAR FUSELAGE SKIN LOCATED FRAME 79+2" AND BETWEEN STR 4 - 5L. PERFORMED PERMANENT REPAIR ON EXTERNAL REAR FUSELAGE SKIN IAW SRM A320 53-00-11, PARA 4W, PAG 579/580, FIG 239.Oct 5, 2013 · N326US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13050633226Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE LOCATED BETWEEN FRAMES 69 AND 70 AT STR 23L IN PAX CABIN. REPLACED SHEAR PLATE IAW SRM A320 51-72-11 AND DWG D53470100.Oct 5, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13050623226Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY, LOCATED BETWEEN FRAMES 58 TO 59 AT STR 38R, REPLACED WEB IN AFT CARGO COMPARTMENT LOCATED BETWEEN FR 58 TO FR 59 AT STR 38R IAW SRM 51-72-11 AND DWG D53470320.Oct 5, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049783226Structure · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION CONNECTING IN BULK CARGO COMPART LOCATION. AT STR 27L AND AT FR 67 MEASURE L=0.900", W=0.250", D=0.004". REPLACED SECTION CONNECTING LOCATED AT FR 67 AND STR 27L IN BULK CARGO COMPARTMENT IAW SRM 51-72-11.Oct 5, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049773226Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FRAMES 66 AND 68 STRINGER 23L. REPLACED LOWER SILL IAW SRM 51-72-11.Oct 4, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049763226Structure · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION CONNECTING IN BULK CARGO BAY, STRINGER 29L AND FRAME 67 MEASURE. REPLACED SECTION CONNECTING IN BULK CARGO BAY IAW SRM 51-72-11.Oct 4, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049753226Structure · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION CONNECTING IN BULK CARGO BAY STRINGER 26L FRAME 67. REPLACED SECTION IAW SRM 58-72-11 AND DWG D53480505.Oct 4, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049793275Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE IN AFT CABIN FLOOR STRUCTURE LOCATED FR 69 AND FR 70 AT LEVEL STR 23L. MEASURES APPROX: L=3"; W=2"; D=0.003". REPLACED SHEAR PLATE LOCATION BETWEEN FR 69 AND FR 70 AT LEVEL STR 23L AFT CABIN FLOOR STRUCTURE SROct 2, 2013 · N375NC · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049313226Fitting · corrodedCORROSION ON CENTER FITTING BETWEEN FRAMES 66 AND 68 STR 23L. REPLACED FITTING.Oct 2, 2013 · N326US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13049013226Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1292 LOCATED BETWEEN FRAMES 64 AND 66+4". REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472230.Oct 1, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049003226Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 LOCATED BETWEEN FRAMES 67+15" AND 69+3". REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472000.Oct 1, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048993226Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT +Y1225 BETWEEN FRAMES 66+4" AND 67+15". REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472000 AND REPLACED SPLICE IAW SRM 51-72-11, LOCATION FR 66+4" UPPER INBD POSITION IAW DWG D53472230.Oct 1, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048983226Fitting · corrodedCORROSION ON LOWER CORNER FITTING AT FRAME 68 LEVEL OF STR 23R IN PAX CABIN. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53480505.Oct 1, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048973226Floor Support · corrodedIMPROPERLY HOLE ON FLOOR SUPPORT +Y1292 LOCATED AT FRAME 66 IN PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472230.Oct 1, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048963226Upper Sheet · corrodedCORROSION ON COVER SHEET LOCATED BETWEEN FRAMES 24A TO 28 FWD CARGO BAY. REPLACED COVER SHEET IAW SRM 51-72-11 AND DWG D53230315.Oct 1, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA131001003Wire Harness · failed(CAN) SHORTLY AFTER TAKEOFF THE CREW REPORTED THE NR 2 GENERATOR FAILED AND RESET WAS NOT SUCCESSFUL. PAN WAS DECLARED AND THE FLIGHT RETURNED AND LANDED OVERWEIGHT. NR 2 IDG REPLACED IAW AMM 24-21-51. NR 2 GCU REPLACED IAW AMM 24-22-34 ANB BTC NR 1 11VU1 RESep 30, 2013 · Airbus A320211 · Electrical Power System WiringSDR DALA13048953226Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1162 LOCATED BETWEEN FRAMES 67+15" - 69+3". REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000 AND REPLACED SPLICE IAW SRM 51-72-11 AND DWG D53472000.Sep 30, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048943226Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT -Y1225 LOCATED BETWEEN FRAMES 66+4" - 67+15" IN PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Sep 30, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048353226Threshold · corrodedDURING INSPECTION, FOUND CORROSION ON THRESHOLD SHEET LOCATED BETWEEN FR 24A TO FR 28 FWD CARGO COMP SSI 532180. MEASURES ARE: L=0.890", W=0.425", D=0.001". REPLACED THRESHOLD SHEET LOCATED BETWEEN FR 24A TO FR 28 FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWSep 30, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048223226Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER L1 DOOR SILL LOCATED BETWEEN FR 16 TO FR 20 AND STR 23L. REPLACED LOWER SILL IAW SRM 51-72-11.Sep 29, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048183226Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FWD FACE FR 20 AT LEVEL OF STRG 23R. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53112225 JOB COMPLETE.Sep 28, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048173226Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING AFT FACE FR 16 AT LEVEL OF STRG 23R. REPLACED CONER FITTING IAW SRM 51-72-11.Sep 28, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048163226Web · corrodedDURING INPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY BETWEEN FR 58 TO FR 59 AT STR 38L. REPLACED WEB AND FASTENER IAW SRM 51-72-11 AND DWG D53470321.Sep 28, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13048153226Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 LEVEL OF STR 23R IN PAX CABIN. REPLACED CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 LEVEL OF STR 23R IN PAX CABIN IAW SRM 51-72-11 AND DWG D53480505.Sep 28, 2013 · N326US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13049383226Cleat · corrodedCORROSION ON CLEAT AT FRAME 31, BETWEEN STRINGERS 39 AND 40L IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626.Sep 26, 2013 · N326US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13049373226Cleat · corrodedCORROSION ON CLEAT AT FRAME 28 BETWEEN STRINGERS 42 AND 43R IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626.Sep 26, 2013 · N326US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13049363226Web · corrodedCORROSION FOUND ON WEB IN AFT CARGO BAY, BETWEEN FRAMES 54 - 55 STRINGER 38L. REPLACED WEB IAW SRM 51-72-12 AND DWG D53470321.Sep 26, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049353226Cleat · corrodedCORROSION ON CLEAT AT FRAME 28 BETWEEN STRINGERS 41-42R IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231586.Sep 26, 2013 · N326US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13047283226Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 32, BETWEEN S40-41L FWD CARGO BAY. REPLACED CLEAT IAW SRM A320 51-72-11 AND DWG D53231626.Sep 26, 2013 · N326US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13047273226Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN BULK CARGO BAY BETWEEN FRAMES 69 & 70 S23L. REPLACED WEB IAW SRM 51-72-11.Sep 25, 2013 · N326US · Airbus A320211 · Fuselage Floor PanelSDR DALA13047263226Splice · corrodedDURING INSPECTION, FOUND CORROSION ON SPLICE LOCATED BETWEEN FRAMES 30 AND 31, STRINGER 41L FWD CARGO BAY. REPLACED SPLICE IAW SRM 51-72-11 AND DWG D53231375.Sep 25, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13047253226Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN BULK CARGO BAY BETWEEN FRAMES 69 TO 70 AT S23R. REPLACED WEB IAW SRM 51-72-11 AND DWG D53470100.Sep 25, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13047073217Connector · disconnectedDURING NON-ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT ON SEAT 23 ABC INOPERATIVE. FOUND CONNECTION UNDER CARPET DISCONNECTED. REINSTALLED CONNECTION AND OPS CHECKED NORMAL.Sep 25, 2013 · N317US · Airbus A320211 · Light System WiringSDR CA130927004Alternator · contaminated(CAN) AFTER ROTATION, THERE WAS A FUEL FILTER CLOGGED ECAM MESSAGE. THE MESSAGE THEN CLEARED AFTER THRUST REDUCTION. IMMEDIATELY AFTER THRUST REDUCTION THERE WAS AN INTERMITTENT ENGINE 2 THRUST LEVER TLA DISAGREE. ECAM ACTIONS WERE COMPLETED HOWEVER MAINTENSep 24, 2013 · Airbus A320211 · DC Generating SystemSDR DALA13047053226Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FRAME 32 BETWEEN S41-42R FWD CARGO BAY. . REPLACED CLEAT IAW SRM 51-72-11.Sep 24, 2013 · N326US · Airbus A320211 · Fuselage Miscellaneous Structure
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