N769US

Service difficulty reports · 253

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 = 'N769US' 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 USAA2012112700008Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, Y1732 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472750.Nov 2, 2012 · N769US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112700007Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, -Y1732 IAW A319 SRM 51-72-11.Nov 2, 2012 · N769US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112700003Tray · cracked2S CHECK - CRACK ON WEB TRAY ON FLOOR STRUCTURE BETWEEN FR68 TO FR69, -Y1732. REPLACED WEB TRAY ON FLOOR STRUCTURE BETWEEN FR68 TO FR69, -Y1732 IAW A319 SRM 51-72-11.Nov 2, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012120400018Flap · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON 2 POINTS OF INTERNAL AREA OF LEFT WING OUTBOARD FLAP AT RIB 14A. REPLACED LEFT WING OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001-A.Nov 1, 2012 · N769US · Airbus A319112 · Trailing Edge FlapsSDR USAA2012120400015Flap · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON 4 POINTS OF INTERNAL AREA OF RIGHT WING OUTBOARD FLAP BETWEEN STRINGERS 7 TO 8 & BETWEEN RIB 13 TO RIB 14. REPLACED RIGHT WING OUTBOARD FLAP IAW A319 AMM 27-54-62.Nov 1, 2012 · N769US · Airbus A319112 · Trailing Edge FlapsSDR USAA2012112900002Splice · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK SPLICES AT FR24, -Y655. REPLACED SEAT TRACK SPLICES AT FR24, -Y655 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110920.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112800009Splice · damaged2S CHECK - ELONGATED HOLES ON SPLICES OF RIGHT AFT PASS/CREW LOWER DOOR SILL AREA AT FR66, S23R, -Y1450. REPLACED SPLICES OF RIGHT AFT PASS/CREW LOWER DOOR SILL AREA AT FR66, S23R, -Y1450 IAW A319 SRM 51-72-11.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112800017Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66 & BETWEEN -Y1732 TO -Y765. REPLACED FLOOR PANEL 262BG IAW A319 SRM 53-02-00, IRM 9701 REV G & EA 503548.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112800016Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR WEB AT FR20, S23R, -Y1732. REPLACED FLOOR WEB AT FR20, S23R, -Y1732 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53114392 & D53110920.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112800013Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AFT PASS/CREW LOWER DOOR SILL BETWEEN FR66 TO FR68, S23L, Y1732. REPLACED LEFT AFT PASS/CREW LOWER DOOR SILL BETWEEN FR66 TO FR68, S23L, Y1732 IAW A319 SRM 51-72-11 & EA 503550.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112800012Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT AFT PASS/CREW LOWER DOOR SILL BETWEEN FR66 TO FR68, S23R, -Y1732. REPLACED RIGHT AFT PASS/CREW LOWER DOOR SILL BETWEEN FR66 TO FR68, S23R, -Y1732 IAW A319 SRM 51-72-11 & EA 503549.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112800011Splice · damaged2S CHECK - ELONGATED HOLES ON SPLICES OF LEFT AFT PASS/CREW LOWER DOOR SILL AREA AT FR66, S23L, Y1450. REPLACED SPLICES OF LEFT AFT PASS/CREW LOWER DOOR SILL AREA AT FR66, S23L, Y1450 IAW A319 SRM 51-72-11.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112800010Sill · damaged2S CHECK - ELONGATED HOLES ON SPLICES OF LEFT AFT PASS/CREW LOWER DOOR SILL AREA AT FR66, S23L, Y1450. REPLACED SPLICES OF LEFT AFT PASS/CREW LOWER DOOR SILL AREA AT FR66, S23L, Y1450 IAW A319 SRM 51-72-11.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112800008Splice · damaged2S CHECK - ELONGATED HOLES ON SPLICES OF RIGHT AFT PASS/CREW LOWER DOOR SILL AREA AT FR66, S23R, -Y1450. REPLACED SPLICES OF RIGHT AFT PASS/CREW LOWER DOOR SILL AREA AT FR66, S23R, -Y1450 IAW A319 SRM 51-72-11.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112800007Angle · cracked2S CHECK - CRACK ON ANGLE SEGMENT OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN S15R TO S16R. REPLACED ANGLE SEGMENT OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN S15R TO S16R IAW EO 5210Y228.Nov 1, 2012 · N769US · Airbus A319112 · Emergency ExitsSDR USAA2012112800006Angle · cracked2S CHECK - CRACK ON ANGLE SEGMENT OF EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED ANGLE SEGMENT OF EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3 IAW EO # 5210Y228.Nov 1, 2012 · N769US · Airbus A319112 · Emergency ExitsSDR USAA2012112700022Coupling · damaged2S CHECK - ELONGATED HOLE ON SPLICE COUPLING AT FR66, S23R, -Y1450. REPLACED SPLICE COUPLING AT FR66, S23R, -Y1450 IAW A319 SRM 51-72-11.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112700021Coupling · damaged2S CHECK - ELONGATED HOLE ON SPLICE COUPLING AT FR66, S23R, -Y1450. REPLACED SPLICE COUPLING AT FR66, S23R, -Y1450 IAW A319 SRM 51-72-11.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112700020Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812, D53110984 & D53110920.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112700006Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW IRM 9701 REV G & A319 SRM 53-02-00 FIG 209.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112700005Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221LF BETWEEN FR16 TO FR20 & BETWEEN -Y254 TO Y765. REPLACED FLOOR PANEL 221LF IAW IRM 9701 REV G & A319 SRM 53-02-00.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112700004Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 222CF BETWEEN FR16 TO FR20 & BETWEEN -Y254 TO -Y1732. REPLACED FLOOR PANEL 222CF IAW IRM 9701 REV G & A319 SRM 53-02-00.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112000030Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT THRESHOLD AREA BETWEEN FR16 TO FR20, S23R. REPLACED CENTER FITTING AT THRESHOLD AREA BETWEEN FR16 TO FR20, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112109.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112000029Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT THRESHOLD AREA BETWEEN FR16 TO FR20, S23L. REPLACED CENTER FITTING AT THRESHOLD AREA BETWEEN FR16 TO FR20, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112109.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112000028Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812, D53110984.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112000027Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT THRESHOLD AREA BETWEEN FR66 TO FR68, S23L OF AFT LEFT PASS/CREW DOOR. REPLACED CENTER FITTING AT THRESHOLD AREA BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112000026Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR20 TO FR23, Y254. REPLACED FLOOR SUPPORT BETWEEN FR20 TO FR23, Y254 IAW A319 SRM 51-72-11.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112000025Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR18 TO FR20, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR18 TO FR20, -Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING 53111462.Nov 1, 2012 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112800019Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 4 RUDDER HINGE FITTING BETWEEN RIB 6 TO RIB 7. REPLACED NR 4 RUDDER HINGE FITTING BETWEEN RIB 6 TO RIB 7 IAW A319 SRM 51-72-11.Oct 31, 2012 · N769US · Airbus A319112 · Rudder StructureSDR USAA2012112800018Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 1 RUDDER HINGE FITTING BETWEEN RIB 2 TO RIB 3. REPLACED NR 1 RUDDER HINGE FITTING BETWEEN RIB 2 TO RIB 3 IAW A319 SRM 51-72-11.Oct 31, 2012 · N769US · Airbus A319112 · Rudder StructureSDR USAA2011122700019Fcu · leakingCREW REPORTED A DIRTY SOCK SMELL THROUGHOUT AIRCRAFT UPON BOARDING AND DID NOT FEEL IT ALLOWED FOR PASSENGER BOARDING. MAINTENANCE REMOVED AND REPLACED APU FUEL CONTROL UNIT IAW AIRBUS MAINTENANCE MANUAL 49-32-11-401.Dec 24, 2011 · N769US · Airbus A319112 · APU Engine Fuel and ControlSDR USAA2011122300018Oil System · overservicedSTRONG ODOR STARTED IN CABIN AND FLIGHT DECK ON DESCENT THROUGH APPROXIMATELY 3000FT. ALL CREW MEMBERS AND MANY PASSENGERS NOTICED THE ODOR. MAINTENANCE FOUND APU TO BE OVER-SERVICED. RE-SERVICED TO PROPER LEVEL WITH NO LEAKS NOTED.Dec 22, 2011 · N769US · Airbus A319112 · APU Oil SystemSDR USAA2011122200008Slide · low pressureL-2 DOOR SLIDE BOTTLE PRESSURE LOW (OUT OF GREEN BAND). REMOVED AND REPLACED L-2 DOOR SLIDE ASSEMBLY.Dec 20, 2011 · N769US · Airbus A319112 · Escape SlideSDR USAA2011111800009Drain Valve · leakingFLIGHT ATTENDANT REPORTED FUMES IN AFT CABIN. REMOVED AND REPLACED LEAKING BLUE SYSTEM HYDRAULIC DRAIN VALVE PER AMM 29-12-35, OPS CHECKED GOOD.Nov 17, 2011 · N769US · Airbus A319112 · Hydraulic System, MainSDR USAA2010092992137Lens · missingFLT 1649 - DCA-TPA - EMERGENCY LIGHTS - AFT ENTRY DOOR EMERGENCY EXIT LENS MISSING. REPLACED MISSING LENS FOR EXIT LIGHT AFT ENTRY DOOR.Sep 28, 2010 · N769US · Airbus A319112 · Emergency LightingSDR USAA2010080391575Lens · missingFLT 1897 - CLT-ATL - EMERGENCY LIGHTS - AFT R2 DOOR LOWER EMERGENCY LIGHT LENS MISSING "EXIT". REMOVED AND REPLACED R2 DOOR LOWER EMERGENCY LIGHT LENS "EXIT". OPERATIONAL CHECK WAS GOOD.Aug 2, 2010 · N769US · Airbus A319112 · Emergency LightingSDR USAA2009082892279Chiller · odorFLT 2182 - DCA-LGA - BURNING SMELL - LOUD NOISE IN AFT GALLEY FOLLOWED BY BURNING RUBBER SMELL. FOUND CHILLER FAN MAKING NOISE AND ODOR. REMOVED AND REPLACED CHILLER PER 25-30-00. OPERATIONAL CHECK WAS GOOD. NO SMELL.Aug 26, 2009 · N769US · Airbus A319112 · Buffet/GalleysSDR USAA2009072291897Proximity Switch · malfunctionedFLT 1911 - PHL - NAS - EMERGENCY EQUIPMENT - CLIMBING THROUGH 11000, GOT ECAM DOOR LEFT EMERGENCY EXIT FALSE INDICATION. CHECKED ADJUSTMENT OF PROXIMITY SWITCH, PRESSURIZED AND VERIFIED ECAM WARNING DIDN'T COME ON PER MAINTENANCE MANUAL 52-71-13. OPERATIONALJul 21, 2009 · N769US · Airbus A319112 · Door Warning SystemSDR USAASA07082Computer · intermittentCLT - FLT 1480 EN ROUTE MSP TO CLT. DURING THE FLIGHT, AUTOPILOT 2 DISENGAGED. THE CREW RE-ENGAGED THE AUTOPILOT, AND IT DISCONNECTED AGAIN, ALONG WITH AUTOPILOT 1. AFTER HAND FLYING FOR ABOUT 20 SECONDS, THE STAB TRIM WHEEL JERKED WHILE AUTO-TRIMMING, THEDec 11, 2007 · N769US · Airbus A319112 · Autopilot ComputerSDR SA06087Fan · burned outPHL - FLT 1737 EN ROUTE RDU TO PHL. THE CREW NOTICED A SLIGHT ODOR AT 15,000 FT DURING CLIMB. AFTER LEVEL OFF, THE ODOR BECAME SLIGHTLY MORE NOTICEABLE. AS THE DESCENT STARTED, AN ELECTRICAL SMOKE ODOR BECAME APPARENT. THE FLIGHT CREW DECLARED AN EMERGENCYNov 21, 2006 · N769US · Airbus A319112 · Air Distribution FanSDR USAA061337Floor Support · corrodedFLOORBEAM AT LBL 10 FR C16 CORRODED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER & FILLER PER SRM 53-00-14; CORR TASK JA-220-535, LEVEL 1, DEFECT SIZE: 2 X 2 INCHES.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061338Floor Support · corrodedTOP SIDE OF FLOORBEAM AT FR 66 (FWD OF LT DOOR SILL) CORRODED. ROUTED OUT CORROSION, INSTALLED FILLER PIECE PER SRM 53-41-14 FIG 201; CORR TASK JA-260-53500, DEFECT SIZE: 1 X 1 INCH.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061339Floor Support · corrodedY765 FRAME 66 CORRODED. REPLACED FLOORBEAM PER DWG D53472815; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1" X .5" X .250" DEEP.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061340Floor Support · corrodedFLOORBEAM Y1292 FR 12-24 CORRODED. REMOVED & REPLACED FLOORBEAM IAW SRM 51-72-11; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1" X 3-/2" AND 1" X 6" AND 1/2" GOUGE.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061341Floor Support · corrodedFR 66 AT -Y1162 CORRODED. REPLACED FLOORBEAM PER SRM 72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 3 INCHES.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061342Floor Support · corrodedFR 66 & 68 OF FLOORBEAM Y1162 CORRODED. REMOVED & REPLACED FLOORBEAM PER SRM 51-70-00; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 1 X 6 INCH & 1 X 4 INCH.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061343Floorbeam · corrodedC16 AT RBL 4 CORRODED. REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-220-53500, LEVEL 1, DEFECT SIZE: 2 SQ INCHES.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061344Floorbeam · corrodedFLOORBEAM AT RBL 11 + 4 INCHES FWD OF FR C18 CORRODED. REMOVED DAMAGE & FABRICATED REPAIR PARTS PER SRM 53-00-14; LEVEL 1, DEFECT SIZE: 1 X 2 INCHES.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061345Floorbeam · corrodedFLOORBEAM ADJACENT TO RT SERVICE DOOR FWD GIRT BAR MOUNT CORRODED. MODIFIED PART INSTALLED PER SRM 53-41-14, DEFECT SIZE: 1 X 1.5 INCH.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061346Floor Panel · delaminatedFRAME 14-16 DELAMINATED. FABRICATED NEW FLOOR PANEL PER MCGILL IRM 9701 REV F. DEFECT SIZE: 2 X 4 INCHES AT 2 AREAS.Nov 14, 2006 · N769US · Airbus A319112 · Fuselage Floor Panel
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