N118US

Service difficulty reports · 266

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N118US' AND registry_match = 'registration'
  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 USAA2012011700013Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 231MF BETWEEN FR24 TO FR28 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 231MF IAW A320 SRM 53-02-00 FIG 209 IRM 9701 REV G.Jan 10, 2012 · N118US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012012300016Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR64, -Y1292. REPLACED SEAT TRACK AT FR64, -Y1292 IAW A320 SRM 51-72-11, 53-72-11 & 53-41-15 PAGE 215.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012012300015Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING SEAT RAIL AT FR64, -Y1292. REPLACED COUPLING SEAT RAIL AT FR64, -Y1292 IAW A320 SRM 51-72-11.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012012300013Fitting · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON AFT CORNER FITTING AT FR67+18", S23L. REPLACED AFT CORNER FITTING AT FR67+18", S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012012300012Sill · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR68, S23R. REPAIRED LOWER SILL BETWEEN 65+18 INCHES TO FR68, S23R IAW EA 133980.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012012300011Sill · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR68, S23L. REPAIRED LOWER SILL BEAM BETWEEN FR66 TO FR68, S23L IAW EA 133984.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011800023Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT BEAM RAIL BETWEEN FR64 TO FR66, Y765. REPLACED SEAT BEAM RAIL BETWEEN FR64 TO FR66, Y765 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53472815.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012011800021Fitting · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR67+18 INCHES, S23R. REPLACED CORNER FITTING AT FR67+18 INCHES, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011300014Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR67, -Y318. REPLACED FLOORBEAM BETWEEN FR65 TO FR67, -Y318 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472814.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011300008Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y765. REPLACED FLOORBEAM AT FR20, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812 & D53110920.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011200017Dummy Rail · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY AT FR14+11 INCHES, S23R, -Y81. REPLACED RAIL DUMMY AT FR14+11 INCHES, S23R, -Y81 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112828.Jan 8, 2012 · N118US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012012300019Shear Plate · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-72-11, AIRBUS DRAWING D53474180 & TYPICAL REPAIR # TR320-2528-10-0011.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012012300018Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR64+8 INCHES, -Y765. REPLACED FLOORBEAM AT FR64+8 INCHES, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472832.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012012300017Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y189. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y189 IAW A320 SRM 51-72-11, EA 133963 & AIRBUS DRAWING D53111406.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012012300014Skin Panel · corrodedC11 CHECK - CORROSION ON FUSELAGE SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41R TO S42R. REPAIRED FUSELAGE SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41R TO S42R IAW EA 133982.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Plate/SkinSDR USAA2012012300010Sill · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+17 INCHES, S23L. REPLACED SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+17 INCHES, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012012300005Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 262BF BETWEEN FR64 TO FR66, BETWEEN -Y1732 TO -Y254. REPLACED FLOOR PANEL 262BF IAW A320 SRM 53-02-00 FIGURE 209, IRM 9701 REV G AND EA 133968.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012012300004Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68, BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 261DF IAW A320 SRM 53-02-00 FIGURE 209, IRM 9701 REV G & EA 133967.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012012000015Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, -Y1732 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53470150.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012012000014Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472832.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011800032Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162 IAW A320 SRM 51-72-11, AIRBUS DRAWINGS D53472780.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011800031Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, Y1292. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, Y1292 IAW A320 SRM 51-72-11, AIRBUS DRAWINGS D53472780.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011800030Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR68, Y1292 IAW A320 SRM 51-72-11, AIRBUS DRAWINGS 53472815.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011800029Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR 67+16 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR 67+16 INCHES, -Y1292 IAW A320 SRM 51-72-11, AIRBUS DRAWINGS D53472816 & D53472815.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011800028Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR64, Y1292. REPLACED COUPLING AT FR64, Y1292 IAW A320 SRM 51-72-11, AIRBUS DRAWINGS D53472831 & D53472815.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011800027Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR68, Y1162. REPLACED COUPLING AT FR68, Y1162 IAW A320 SRM 51-72-11.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011800026Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, -Y1162. REPLACED COUPLING AT FR67+16 INCHES, -Y1162 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53472780.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011800025Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, -Y1162. REPLACED COUPLING AT FR67+16 INCHES, -Y1162 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53472780.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011800024Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR66+5 INCHES, Y1292. REPLACED COUPLING AT FR66+5 INCHES, Y1292 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53472815.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011800022Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66+ 5 INCHES, Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66+ 5 INCHES, Y1292 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53472831 & D53472815.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012011700014Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261BF BETWEEN FR64 TO FR66 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL 261BF IAW A320 SRM 53-02-00 FIGURE 209 & IRM 9701 REV G.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012011700012Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN Y1292 TO -Y1292. REPLACED FLOOR PANEL 261PF IAW A320 SRM 53-02-00 TABLE 105 & IRM 9701 REV G.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012011300013Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y765. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812, D53112813 & D531109202.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012011300010Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011300009Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011300003Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y254 IAW A320 SRM 51-72-11 & DRAWING D53111462.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011300002Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+10 INCHES TO FR70, Y512. REPLACED FLOORBEAM BETWEEN FR67+10 INCHES TO FR70, Y512 IAW A320 SRM 51-72-11 & DRAWING D53472815.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011300001Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11 & DRAWING D53472780 & D53472093.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011200019Floor Support · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254. REPLACED FLOOR SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53112816 & D53110406.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011200016Web · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, -Y1732. REPLACED WEB BETWEEN FR20 TO FR24, -Y1732 IAW A320 SRM 51-72-11.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012011100022Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION IN FLOORBEAM BETWEEN FR12 TO FR16, Y503. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, Y503 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53112825 & D53110984.Jan 7, 2012 · N118US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011122700034Pump · failedAFTER ENGINE START, AND POSSIBLY DURING POWER CHANGE OVER, NR 2 ENGINE FAILURE ECAM MESSAGE WITH AUTO SHUTDOWN OF NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE HYDRO-MECHANICAL UNIT AND FUEL PUMP/FILTER ASSEMBLY IAW AIRBUS MAINTENANCE MANUAL 73-11Dec 24, 2011 · N118US · Airbus A320214 · Engine Fuel PumpSDR USAA2011122700018Hydromech Unit · failedAFTER ENGINE START, AND POSSIBLY DURING POWER CHANGE OVER, NR 2 ENGINE FAILURE ECAM MESSAGE WITH AUTO SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENG HYDROMECHANICAL UNIT AND FUEL PUMP/FILTER ASSEMBLY IAW AIRBUS MAINTENANCE MANUAL 73-11-10 & 73-21-10.Dec 24, 2011 · N118US · Airbus A320214 · Fuel Control/Turbine EnginesSDR USAA2011100700003Valve · faultyAIR - ENG 2 BLEED FAULT IN CRUISE ACCOMPANIED BY A HOT BURNING SMELL IN CABIN & COCKPIT. CREW ACCOMPLISHED ECAM - QRH PROCEDURES - SHUTDOWN ENG 2 BLEED FOR REMAINDER OF FLIGHT. MAINTENANCE REPLACED OVERPRESSURE VALVE IAW AIRBUS MAINTENANCE MANUAL 36-11-53.Oct 5, 2011 · N118US · Airbus A320214 · Pneumatic Distribution SystemSDR USAA2010030190461Lens · missingFLT 894 - ATL - EEL - EMERGENCY LIGHT EXIT LENS MISSING R-2 DOOR. MAINTENANCE INSTALLED EXIT LENS AT R-2 DOOR.Feb 27, 2010 · N118US · Airbus A320214 · Emergency LightingSDR USAA2009121493334Pin · corrodedPIT - MAJOR REPAIR - GEAR CHANGE - CORROSION ON REAR PINTLE PIN FLANGE ON THE RIGHT MAIN LANDING GEAR. REPLACED THE RIGHT MAIN LANDING GEAR PINTLE PIN IAW TASK CARD 26T00032001.Dec 7, 2009 · N118US · Airbus A320214 · Main Landing Gear Attach SectionSDR USAA2009101592773Lens · missingFLT 729 - DEN - EEL - SEAT 3C EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED LENS AS REQUIRED.Oct 14, 2009 · N118US · Airbus A320214 · Emergency LightingSDR USAA2008122692329Hose · chafedLOG PAGE 8316449 - FLT 1584 PHX-PIT - EMERGENCY LANDING - CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM. FLIGHT CONTINUED TO PIT AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO GATE DUE TO LOSS OF NOSE WHEEL STEERING. MAINTEDec 25, 2008 · N118US · Airbus A320214 · Hydraulic System, MainSDR USAA920081212Manifold · failedFLT NR 973. CREW REPORTED HIGH ENGINE VIBRATION ON CLIMB OUT. DECLARED AN EMERGENCY & RTF MAKING AN OVERWEIGHT LANDING. PILOT REPORTED SMOKE COMING FROM NR 1 ENGINE ON SHUTDOWN, WHICH STOPPED AFTER FIRE BUTTON RELEASE. R&R LPT ACTIVE CLEARANCE CONTROL SYS FUEJun 15, 2008 · N118US · Airbus A320214 · Engine Fuel DistributionSDR SA06082Battery Pack · dischargedPIT - THE AFT, LEFT EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS OPERATIONAL TEST. MAINTENANCE REPLACED THE AFT, LEFT EMERGENCY POWER SUPPLY UNIT BATTERY PACK. OPERATIONALLY CHECKS OK.Oct 17, 2006 · N118US · Airbus A320214 · Emergency Lighting
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