N760US

Service difficulty reports · 197

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 = 'N760US' 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 USAA2012070900027Floor Support · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53110920 & D53111462.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012070900026Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR24, -Y1292. REPLACED SEAT TRACK AT FR24, -Y1292 IAW A319 SRM 53-21-15 & AIRBUS DRAWING D53110920.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012070900025Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR16 TO FR21, Y1292. REPLACED SEAT TRACK BETWEEN FR16 TO FR21, Y1292 IAW A319 SRM 51-72-11.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012070900024Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR16 TO FR21, Y765. REPLACED SEAT TRACK BETWEEN FR16 TO FR21, Y765 IAW A319 SRM 51-72-11.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012070900023Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR25+5 INCHES, -Y765. REPLACED SEAT TRACK AT FR25+5" INCHES, -Y765 IAW A319 SRM 53-21-15 FIG 204 PAGE 239/240.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012070900022Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070900021Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070900020Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+4 INCHES, -Y1165. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+4 INCHES, -Y1165 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070900019Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+4 INCHES, Y1165. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+4 INCHES, Y1165 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070900015Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, -Y1165. REPLACED COUPLING AT FR67+16 INCHES, -Y1165 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012070900013Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, -Y1165. REPLACED COUPLING AT FR67+16 INCHES, -Y1165 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012070900012Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, Y1165. REPLACED COUPLING AT FR67+16 INCHES, Y1165 IAW A319 SRM 51-72-11.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012070900011Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR66+5 INCHES, Y1292. REPLACED COUPLING AT FR66+5 INCHES, Y1292 IAW A319 SRM 51-72-11.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012070900010Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR66, S23L. REPLACED COUPLING AT FR66, S23L IAW A319 SRM 51-72-11.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012070900008Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW A319 SRM 53-02-00 AND IRM 9701 REV G.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012070600012Seat Track · corrodedC11 CHECK - CABIN SEAT TRACK CORRODED BETWEEN FR 64 AND FR 66+5" AT Y -1292. REMOVED AND REPLACED SEAT TRACK IAW A319 SRM 51-72-11 AND DRAWING D53472815.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012070600011Floorbeam · corrodedC11 CHECK - FLOORBEAM AUXILIARY RAIL CORRODED FROM FR 65 TO FR 66 AT Y 1732. REMOVED AND REPLACED FLOORBEAM AUXILIARY RAIL IAW A319 SRM 51-72-11 AND DRAWING D53474250.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070600010Floorbeam · corrodedC11 CHECK - FLOORBEAM WEB CORRODED BETWEEN FR 20 AND FR 24 AT Y -1732. REMOVED AND REPLACED WEB IAW A320 SRM 51-72-11AND DRAWING D53112783.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070600009Floorbeam · corrodedC11 CHECK - FLOORBEAM AUXILIARY RAIL CORRODED BETWEEN FR 12 AND FR 16 AT Y 503.2. REMOVED AND REPLACED FLOORBEAM AUXILIARY RAIL IAW A319 SRM 51-72-11 AND DRAWING D53112825.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070500032Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED FR 16 AND FR 24 AT Y-1292. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND DRAWING D53112812.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070500030Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 20 AND FR 24 AT Y -765. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND DRAWING D53112812.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070500029Fitting · corrodedC11 CHECK - LOWER AFT STRINGER TO FRAME CORNER FITTING OF L2 DOOR CUTOUT CORRODED AT FR 68, S23L. REMOVED AND REPLACED CORNER FITTING IAW A319 SRM 51-72-11 AND DRAWING D53480505.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Attach FittingsSDR USAA2012070500012Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 64 AND FR 66+5" AT Y -765. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND DRAWING D53472816.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070500011Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 66+5" AND FR 70 AT Y -765. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND DRAWING D53472780.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070500009Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN BS 808 AND BS 950 AT Y -189. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND DRAWING D53111406.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070500008Floorbeam · corrodedC11 CHECK - FLOORBEAM AUXILIARY RAIL CORRODED BETWEEN BS 605 AND BS 709 AT Y -81. REMOVED AND REPLACED FLOORBEAM AUXILIARY RAIL IAW A319 SRM 51-72-11 AND DRAWING D53112828.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070500007Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN BS 2798.7 AND BS 2992 AT Y 765. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND DRAWING D53472780.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012070500006Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN BS 2670 AND BS 2798.7 AT Y 765. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-72-11 AND DRAWING D53472815.Jun 29, 2012 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011033191287Power Supply · inoperativeFLT 1649 - DCA-TPA - EMERGENCY LIGHTS - OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED PER JOB CARD 26L0005005, STEP 12. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU). OPERATIONAL CHECK WAS GOOD.Mar 29, 2011 · N760US · Airbus A319112 · Emergency LightingSDR USAA2010110192463Cylinder · low pressureFLT 1176 - CLT-BOS - EMERGENCY EGRESS SYSTEM - RIGHT AFT PASSENGER DOOR (R2) EMERGENCY CYLINDER PRESSURE LOW. SERVICED R2 DOOR CYLINDER IAW AMM 52-10-00-614.Oct 31, 2010 · N760US · Airbus A319112 · Service DoorsSDR USAA2010081691668Epsu · failedFLT 2046 - DCA-BOS - EMERGENCY LIGHTS - EMERGENCY LIGHT TEST FAILED, FORWARD LEFT EMERGENCY POWER SUPPLY UNIT (EPSU). REMOVED AND REPLACED FORWARD LEFT EMERGENCY POWER SUPPLY UNIT AND BATTERY PER AMM 33-51-38. OPERATIONAL CHECK WAS GOOD.Aug 14, 2010 · N760US · Airbus A319112 · Emergency LightingSDR USAA2010081691666Carbon Seal · leakingFLT 2043 - AIRCRAFT CABIN HAS A "LOCKER ROOM" ODOR THROUGHOUT WHICH DID NOT DISSIPATE DURING ENTIRE FLIGHT. FOUND APU AT FAULT. REMOVED AND REPLACED APU PER 26L31049006, LEAKS CHECK & OPERATIONAL CHECK WAS GOOD. COMPRESSOR CARBON SEAL WAS CHIPPED AND LEAKIAug 12, 2010 · N760US · Airbus A319112 · APU Core EngineSDR USAA2009091192474Power Supply · faultyFLT 822 - CLT-BOS - EMERGENCY LIGHTS - EMERGENCY LIGHT TEST SHOWS "INT LOAD AFT L" FAULT. TEST OF POWER SUPPLY SHOWS INTERIOR LIGHT FAULT, BUT ALL LIGHTS ILLUMINATE WHEN TURNED ON. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) PER MAINTENANCE MANUASep 8, 2009 · N760US · Airbus A319112 · Emergency LightingSDR USAA2009080692028Diaphragm · leakingPIT - C11 - EES - NR # 26C80012004/001 - FOUND FORWARD SERVICE DOOR ASSIST BOTTLE AT 0 PSI. REPLACED DIAPHRAM IN FORWARD SERVICE DOOR ASSIST BOTTLE IAW A319 AMM 52-10-00-03-610-01.Aug 5, 2009 · N760US · Airbus A319112 · Service DoorsSDR USAA2009012690157Connector · brokenFLT 544 - CLT-DEN - EEL - ROW 10 AIRCRAFT LEFT EMERGENCY LIGHTING INOPERATIVE. FOUND CONNECTOR BACKSHELL BROKEN OFF AND WIRE DISCONNECTED FROM WALL INPUT. REMOVED AND REPLACED BACKSHELL AND RE-CRIMPED WIRE FROM WALL INPUT PER ESPM 20-48-21. OPERATIONAL CHECJan 24, 2009 · N760US · Airbus A319112 · Light System WiringSDR USAA061045Skin · crackedL1 DOOR LOWER AFT CORNER CRACKED. DAMAGE CUT OUT, REPAIR DOUBLER INSTALLED PER SRM 52-10-00 & EA 57732A, DEFECT SIZE: 3 INCHES.Aug 15, 2006 · N760US · Airbus A319112 · Passenger/Crew DoorsSDR USAA061046Beam · corrodedFRAME 16 AND Y -81 CORROSION. REMOVED & REPLACED BEAM PER DWG B2 D53112829, DEFECT SIZE: 2 INCH DIA.Aug 15, 2006 · N760US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061047Floorbeam · corrodedFLOORBEAM Y1292 LT AT FR 66 FLOOR PANEL, UPPER FACE CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER AIRBUS SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 INCH DIA.Aug 15, 2006 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061048Floorbeam · corrodedFLOORBEAM Y1292 (LT) CORRODED BETWEEN FR 66 & 68 CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11, DEFECT SIZE: 2 X 24 INCHES.Aug 15, 2006 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061049Floorbeam · corrodedFLOORBEAM Y1292 (LT) BETWEEN FR 68 & 69 CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11, DEFECT SIZE: 2 X 24 INCHES.Aug 15, 2006 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061034Sill · corrodedL2 DOOR BETWEEN FR 66 & 68 AT FLOOR LEVEL CORROSION. DEFECTIVE PART REPLACED WITH IDENT PART PER AIRBUS DWG D53480048202; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1 X 24 INCHES.Aug 9, 2006 · N760US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061032Floorbeam · corrodedFLOORBEAM - Y1292 AT FRAME 68 & 66 CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 X 1 & 1 X 1 INCH (2 AREAS).Aug 9, 2006 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061035Floorbeam · corrodedFRAME 23 & Y254, TOP SIDE OF BEAM CORROSION. REMOVED BEAM, INSTALLED FILLER W/ 2 EA 10 INCHES ANGLES PER SRM 53-00-14; CORR TASK JA-220-53500.Aug 9, 2006 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR SA04104Girt Bar · out of positionCLT - THE SLIDE GIRT BAR FELL FROM THE FORWARD ENTRY DOOR DURING PUSHBACK. AIRCRAFT RETURNED TO GATE. MAINTENANCE RE-ATTACHED THE GIRT BAR TO THE FORWARD ENTRY DOOR SLIDE. OK FOR SERVICE.Nov 4, 2004 · N760US · Airbus A319112 · Emergency EquipmentSDR USAASA03092Release Cable · wrong partTHE FORWARD RIGHT EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLDIE AND RETURNED THE SLIDAug 17, 2003 · N760US · Airbus A319112 · Escape SlideSDR USAASA03093Release Cable · wrong partTHE AFT RT EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SEAug 17, 2003 · N760US · Airbus A319112 · Escape SlideSDR USAA011293Skin · dentedCLT - FOUND SKIN DENTED 4 INCHES BY 4 INCHES, 3 FT FORWARD OF LEFT AFT DOOR ON FUSELAGE. INSTALLED DOUBLER. (M)Sep 13, 2001 · N760US · Airbus A319112 · Fuselage Main, Plate/Skin
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