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 DALA14017213220Bracket · corrodedDURING INSPECTION, FOUND CORROSION ON BRACKET LOCATION LOWER CURVED EDGE RT THE E/E HATCH RT 843. REPLACED BRACKET IAW SRM 51-72-11 AND DWG D52279040.Mar 18, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14017703219Frame · corrodedDURING INSPECTION, FOUND CORROSION ON LATERAL FRAME 19 IN RT AVIONIC BAY S39R. REPLACED FRAME IAW SRM 51-72-11 AND DWG D53114433, D53113542.Mar 16, 2014 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA14017693219Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL FUSELAGE, FRAME 68 AT S29L. REPAIRED IAW ER/A 522856-14, REV ORIGINAL AND PRI 522856-14, REV 0, 1, 2 .Mar 15, 2014 · N319US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA14016823220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FWD PAX CABIN LOCATED Y1292 BETWEEN FRAMES 16 AND 21. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53110920.Mar 14, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14016813220Support · corrodedDURING INSPECTION, FOUND CORROSION ON SUPPORT ON LOWER CURVE EDGE LT SIDE THE E/E HATCH DOOR 844 . REPLACED SUPPORT IAW SRM 51-72-11 AND DWG D52279040.Mar 14, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA2016103108034Floorbeam · corrodedCORROSION ON FLOORBEAM -Y254 IN FWD PAX CABIN FLOOR STRUCTURE. LOC BTW FR 12 TO FR 24, REPAIR ON FLOORBEAM -Y254 IN FWD PAX CABIN FLOOR STRUCTURE LOC BTW FR 12 TO FR 24 AS PER ER/A 523452-14 REVISION 0 AND REVISION ORIGINAL.Mar 13, 2014 · N319US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA14016583220Angle · crackedDURING INSPECTION, FOUND SEVERAL CRACKS IN BOTH SEGMENT ANGLES BETWEEN NR 1 AND 3 BEAMS OF E/E HATCH DOOR 844. REPLACED BOTH SEGMENT ANGLES IAW SRM 51-72-11 AND DWG D52279040.Mar 13, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14016573220Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL OF R2 DOOR LOCATION BETWEEN FRAMES 66 - 68 IN PAX CABIN. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480505.Mar 13, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14016103220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT FRAME 65+22 Y254. REPLACED FLOOR SUPPORT BETWEEN FRAMES 58-66 IAW SRM 51-72-11 AND DWG D53472000.Mar 12, 2014 · N320US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA14016113220Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CURVED EDGE LT THE E/E HATCH DOOR LT 833. REPLACED LOWER CURVED EDGE LT THE E/E HATCH DOOR IAW SRM A320 51-72-11 AND DWG D52279010.Mar 12, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14016093220Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CURVE EDGE RT THE E/E HATCH DOOR LT 833. REPLACED LOWER CURVE EDGE RT THE E/E HATCH DOOR IAW SRM A320 51-72-11 AND DWG D52279010.Mar 12, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14016083220Structure · dentedDURING INSPECTION, FOUND DENT ON LOWER CURVED EDGE LT, THE E/E HATCH LT 834. REPLACED LOWER CURVED EDGE LT THE E/E HATCH, IAW SRM 51-72-11 AND DWG D52279010.Mar 12, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14016073220Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CURVED EDGE RT THE E/E HATCH LT 834. REPLACED LOWER CURVED EDGE RT THE E/E HATCH IAW SRM 51-72-11 AND DWG D52279010.Mar 12, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14016033224Connector · unsecureDURING NON ROUTINE CHECK, FOUND SEAT EMERGENCY ESCAPE LIGHT AT 17C INOPERATIVE. MAINTENANCE FOUND SEAT HARNESS CONNECTOR LOOSE. SECURED CONNECTOR AND HARNESS. OPS CHECKED GOOD.Mar 11, 2014 · N324US · Airbus A320211 · Light System WiringSDR DALA2016103108033Web · corrodedCORROSION ON WEB LOCATED AFT CARGO COMPARTMENT BETWEEN FR 50 AND FR 51 LEVEL STR 38L OF LOWER SURFACE. REPLACED WEB AND FASTENERS LOC AFT CARGO COMPARTMENT FR 50 TO FR 51 LEVEL STR 38L IAW SRM 51-72-11 AND DWG D534-70320.Mar 10, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016103108032Web · corrodedCORROSION ON WEB LOCATED AFT CARGO COMPARTMENT BETWEEN FR 50 AND FR 51 LEVEL STR 38R. REPLACED WEB AND FASTENERS LOC AFT CARGO COMPARTMENT FR 50 TO FR 51 LEVEL STR 38R SRM 51-72-11 AND DWG D534-70320.Mar 10, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14015603248Module · inoperativeDURING INSPECTION, FOUND ESCAPE PATH LIGHT MODULE MISSING. MAINTENANCE REPLACED ESCAPE PATH LIGHT MODULE AND FUNCTIONAL CHECKED NORMAL.Mar 10, 2014 · N348NW · Airbus A320211 · Emergency LightingSDR DALA14015593220Panel · corrodedDURING INSPECTION, FOUND CORROSION ON STAMPING PANEL BETWEEN FRAMES 28-29 S42-44, IN FWD CARGO BAY. REPLACED PANEL IAW SRM 51-72-11 AND DWG D53230861.Mar 10, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14015583220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN LOWER FLOOR SUPPORT BETWEEN FRAMES 16 - 20 S23L. REPLACED IAW SRM 51-72-11 AND DWG D53110339.Mar 10, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14015573220Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT C/C. LOCATED BETWEEN FRAMES 62-63 AT S38R. REPLACED WEB IAW SRM 51-72-11AND DWG D53570320.Mar 10, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14015563220Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON S42L BETWEEN FRAMES 28 - 29 FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER IAW SRM 53-00-13, PARA 4.A 6.Mar 9, 2014 · N320US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14015553220Tee Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON TEE FITTING LOWER CURVE EDGE RIGHT SIDE THE E/E HATCH DOOR 833. REPLACED TEE FITTING IAW SRM A320 51-72-11 AND DWG D52279040.Mar 9, 2014 · N320US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA14015543220Floor Panel · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SURFACE OF FLOOR PANEL 152KF AFT CARGO BAY. REPLACED FLOOR PANEL IAW SRM 51-72-11.Mar 9, 2014 · N320US · Airbus A320211 · Fuselage Floor PanelSDR DALA14015283220Floor Panel · damagedDURING INSPECTION, FOUND DAMAGED FLOOR PANEL 261EF. REPLACED FLOOR PANEL.Mar 8, 2014 · N320US · Airbus A320211 · Fuselage Floor PanelSDR DALA14015273220Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL L2 DOOR LOCATION BETWEEN FRAME 66-FRAME 68 IN AFT PAX CABIN. MEASURES, L = 1.300", W= 0.800", D= 0.004", APPROXIMATELY, SSI 534147. REPLACED LOWER SILL L2 DOOR LOCATED BETWEEN FRAME 66-FRAME 68 IN AFT PAX CABMar 8, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14015263220Structure · gougedDURING INSPECTION, FOUND GOUGE ON LT WING NR 4 SPOILER LOCATED AT LOWER SURFACE CENTER HINGE FITTING STOP BOLT. PERFORMED PERMANENT REPAIR ON LT WING SPOILER NR 4 LOCATED AT LOWER SURFACE CENTER HINGE FITTING STOP BOLT IAW SRM 57-70-00, PARA 5.C, FIG 201.Mar 8, 2014 · N320US · Airbus A320211 · SpoilersSDR DALA2016103108031Lug · corrodedCORROSION ON INBOARD ACTUATOR FITTING INBOARD LUG LT ELEVATOR. REPAIRED I/B ACTUATOR FITTING I/B LUG AND REPLACED BUSHING ON LT ELEVATOR AS PER SRM 55-26-47.Mar 7, 2014 · N320US · Airbus A320211 · Elevator StructureSDR DALA2016103108030Bushing · corrodedCORROSION ON PLAIN BUSHING OF HINGE FITTING N 2 AT LT ELEVATOR. REPAIRED LT ELEVATOR HINGE FITTING N.2 O/B LUG AND REPLACED BUSHING AS PER SRM 55-26-41.Mar 7, 2014 · N320US · Airbus A320211 · Elevator StructureSDR CA140310002Flap System · failed(CAN) FLIGHT CONTROL FAULT ON APPROACH, FLAPS JAMMED AT FLAPS 1, UNABLE TO EXTEND. PERFORMED QRH, RETRACTED GEAR, CIRCLED FOR APPROXIMATELY 15 MINUTES AND SUBSEQUENTLY LANDED AT PARTIAL FLAPS. DID NOT DECLARE PAN PAN WITH ATC, BUT ATC ADVISED THEY WOULD HAVE CMar 6, 2014 · Airbus A320211 · Trailing Edge Flap Control SystemSDR DALA14015213220Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM FRAME 68, Y160. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472000.Mar 6, 2014 · N320US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA14015203219Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 26R BETWEEN FRAMES 65-66. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480019.Mar 6, 2014 · N319US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14015193219Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 25R BETWEEN FRAMES 65-66. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480019.Mar 6, 2014 · N319US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14015183220Structure · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN AFT LOWER CORNER FRAME 20 BETWEEN S22-23R. REPLACED LOWER CORNER IAW SRM 51-72-11 AND DWG D53112109.Mar 6, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14015173220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN LOWER SILL LOCATED BETWEEN FRAMES 16 AND 20 S23R. REPLACED SILL IAW SRM 51-72-11 AND DWG D53112191.Mar 6, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14015163220Cleat · corrodedDURING INSPECTION, FOUND FWD CARGO BAY CLEAT FRAME 32 BETWEEN S40-41R CORRODED. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231582.Mar 6, 2014 · N320US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA14014903219Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 44 LOCATED BETWEEN FRAMES 33-34. REPAIRED STRINGER IAW SRM 53-00-39, PARA 4A, FIG 201, PAGES 201-212 AND DWG D532-10093.Mar 5, 2014 · N319US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14014893220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1732 FRAME 65+20" AFT PAX CABIN . REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53470150.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014883220Structure · corrodedDURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER AT FRAME 68 ABOVE OF STRINGER 23L. REPLACED AFT LOWER CORNER AT FRAME 68 ABOVE OF STR 23L IAW SRM 51-72-11 AND DWG D53480505.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014873220Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 25R BETWEEN FRAMES 65 - 66 AFT PAX CABIN. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480505.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14014863220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292, FRAME 66" IN AFT PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000 AND D53472815.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014853220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 67+15 - 69 IN AFT PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014843220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 66+5-67+15 AFT PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014833220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765 FRAME 68 IN AFT PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D534720000.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014823220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 66+5 - 67+15 IN AFT PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014813220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162, BETWEEN FRAMES 67+15- 69 AFT PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014803220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1292 BETWEEN FRAMES 64-66+5 AFT PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014793220Stringer Splice · corrodedDURING INSPECTION, FOUND CORROSION ON COUPLING OF STRINGER 41R, BETWEEN FRAMES 30-31 FWD CARGO BAY. REPLACED COUPLING IAW SRM 51-72-11 AND DWG D53231586.Mar 5, 2014 · N320US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14014543219Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED AT FR 20 AT LEVEL STR 23LT FWD PAX CABIN. REPLACED LOWER SILL LOCATED ON FR 16 TO FR 20 FWD PAX CABIN IAW SRM 51-72-11 AND DWG D53110339.Mar 4, 2014 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014563220Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN SEAT TRACK -Y765, BETWEEN FRAMES 20-23. REPLACED SEAT TRACK BETWEEN FRAMES 12 - 23 IAW SRM 51-72-11 AND DWG D53112812.Mar 3, 2014 · N320US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA14014553220Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765 BETWEEN FRAMES 47-64 AND FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Mar 3, 2014 · N320US · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
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