N749US

Service difficulty reports · 238

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 = 'N749US' 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 USAA2012013100015Seat Track · corrodedC11 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.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012013100013Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53111462.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012013100011Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-42-11 & AIRBUS DRAWING D53112812.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012013100010Web · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, -Y1732. REPLACED WEB BETWEEN FR20 TO FR24, -Y1732 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112783.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020800013Sill · corrodedC11 CHECK - GALVANIC CORROSION ON SILL BETWEEN FR66 TO FR68, S23L. REPAIRED SILL BETWEEN FR66 TO FR68, S23L IAW EA 500514.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020700021Sill · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON R2 DOORWAY LOWER SILL BETWEEN FR66 TO FR68, S23R. REPLACED R2 DOORWAY LOWER SILL BETWEEN FR66 TO FR68, S23R IAW EA # 133838.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020700020Shear Plate · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 51-72-11, AIRBUS DRAWING # D53474180 & TYPICAL REPAIR # TR 320-2528-10-0011C.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020700019Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66+5 INCHES, -Y765. REPLACED SEAT TRACK BETWEEN FR64 TO FR66+5 INCHES, -Y765 IAW A319 SRM 51-72-11.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012020700007Sill · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING (SHAPE, SILL) BETWEEN FR66 TO FR68, S23R. REPLACED CENTER FITTING (SHAPE, SILL) BETWEEN FR66 TO FR68, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING # D53480048.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020700006Coupling · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR66, -Y1292. REPLACED COUPLING AT FR66, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING # D53472816.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020700005Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66+5 INCHES, -Y1292. REPLACED SEAT TRACK BETWEEN FR64 TO FR66+5 INCHES, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING # D53472832.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012020600015Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+15 INCHES TO FR69, -Y1162.5. REPLACED FLOORBEAM BETWEEN FR67+15 INCHES TO FR69, -Y1162.5 IAW A319 SRM 51-72-11 & AIRBUS DRAWING # D53472780.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012020600014Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+15 INCHES, -Y1227. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+15 INCHES, -Y1227 IAW A319 SRM 51-72-11 & AIRBUS DRAWING # D53472816.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012020600013Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR68, Y1162.5. REPLACED FLOORBEAM AT FR68, Y1162.5 IAW A319 SRM 51-72-11 & AIRBUS DRAWING # D53472780.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012020600012Shear Plate · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L, Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L, Y1732 IAW TYPICAL REPAIR 320-2528-10-0011C AND A319 SRM 51-72-11.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020600010Coupling · corrodedC11 CHECK - ON UPPER INBOARD SIDE COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5. REPLACED UPPER INBOARD SIDE COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5 IAW A319 SRM 51-72-11.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020600009Coupling · corrodedC11 CHECK - ON LOWER OUTBOARD SIDE COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5. REPLACED LOWER OUTBOARD SIDE COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5 IAW A319 SRM 51-72-11.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020600008Fitting · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING CORNER AT FR68, S23L. REPLACED FITTING CORNER AT FR68, S23L IAW A319 SRM 51-42-11 AND AIRBUS DRAWING D53480505.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020600007Fitting · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING CORNER AT FR68, S23R. REPLACED FITTING CORNER AT FR68, S23R IAW A319 SRM 51-42-11 AND AIRBUS DRAWING D53480505.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012020600006Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR64 PLUS 10 INCHES, S23L, Y1292. REPLACED SEAT TRACK AT FR64 PLUS 10 INCHES, S23L, Y1292 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472831.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012020600005Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR67 PLUS 7 INCHES, S23L, Y1227. REPLACED SEAT TRACK AT FR67 PLUS 7 INCHES, S23L, Y1227 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472815.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012020100011Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR67+10 INCHES, -Y464.8. REPLACED FLOORBEAM AT FR67+10 INCHES, -Y464.8 IAW A319 SRM 51-72-11, AIRBUS DRAWING # D53472816, D53474250 & D53478309.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012020100010Floorbeam · 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 A319 SRM 51-72-11.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012020100009Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY AT FR66+5 INCHES, -Y464.8. REPLACED FLOORBEAM ASSEMBLY AT FR66+5 INCHES, -Y464.8 IAW A319 SRM 51-72-11 & AIRBUS DRAWING # D53472816.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012013100012Floorbeam · 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 A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012013100009Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL SEAT BEAM (SEAT TRACK) BETWEEN FR64 TO FR66+5 INCHES, Y765. REPLACED RAIL SEAT BEAM (SEAT TRACK) BETWEEN FR64 TO FR66+5 INCHES, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472815.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012013100008Dummy Rail · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, Y503. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, Y503 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110984.Jan 25, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011031791088Seal · leakingFLT 9466 - CLT - ODOR - ON CLIMBOUT SMELLED DIRTY SOCK GYM ROOM ODOR IN CABIN AND COCKPIT. STOPPED CLIMB AT 25,000 FT. RETURNED TO FIELD. ENTIRE CREW SMELLED AND TASTED ODOR - FIRST OFFICER COUGHING, AFT FLIGHT ATTENDANT MOVED FROM JUMPSEAT TO GET AWAY FROMMar 15, 2011 · N749US · Airbus A319112 · Turbine SectionSDR USAA2010071691434Strap · missingFLT 1794 - MSY-CLT - EMERGENCY EQUIPMENT - FLIGHT ATTENDANT REPORTS ESCAPE STRAPS MISSING IN FROM OVERHEAD BINS IN CABIN OVERWING AREA. REPLACED OVERWING ESCAPE LIFE LINES.Jul 15, 2010 · N749US · Airbus A319112 · Emergency EquipmentSDR USAA2010070191319Tru · malfunctionedCLT - FLT 1214 - EMERGENCY LANDING - IN FLIGHT, CAPTAIN PRIMARY FLIGHT DISPLAY (PFD), NAVIGATIONAL DISPLAY (ND), AND UPPER ECAM DISPLAY WENT BLANK. FOLLOWED QRM PROCEDURES, ECAM PROCEDURES LOSS OF GEN 1, APU WOULD NOT POWER AC BUS 1. ALSO HAD AN INOPERATIVE Jun 30, 2010 · N749US · Airbus A319112 · DC Rectifier/ConverterSDR USAA2010020890296Battery · dischargedFLT 1543 - CLT-MSY - FLIGHT ATTENDANT REPORTS AT PUSH TIME LEFT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.Feb 5, 2010 · N749US · Airbus A319112 · Emergency EquipmentSDR USAA2009080692030Lanyard · out of positionFLT 1678 - TPA-DCA - EMERGENCY EQUIPMENT - DOOR 1L ON TAKEOFF ROLL, THE "RED" CABIN PRESSURE LIGHT & DOOR SLIDE UNARMED BEGAN FLASHING. AT CRUISE, ALL WENT BACK TO NORMAL. ON DESCENT, CABIN PRESSURE LIGHT & DOOR SLIDE NOT ARMED STARTED FLASHING. FOUND RAFT Aug 4, 2009 · N749US · Airbus A319112 · Life RaftSDR USAA920081437Pin · stalledFLT 792, ACFT EXPERIENCED NR 1 ENG FAILURE AFTER TAKEOFF. CAPTAIN REPORTED A LOUD BANG PRIOR TO FINAL FLAP RETRACTION PROBABLY FROM A COMPRESSOR STALL. THEN EXPERIENCED ENG SURGING, VIBRATION AND A MAX ENG TEMP READING. THE CREW SHUTDOWN ENG AND RETURNED TO Jul 28, 2008 · N749US · Airbus A319112 · Turbine Engine Compressor SectionSDR USAA060468Floorbeam · corrodedFLOORBEAM Y-765 STA 16-24; CORR LEVEL 1; TASK JA-220-53500. REMOVED & REPLACED PER SRM 51-72-11, DEFECT SIZE: .25" X .25".Mar 21, 2006 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA060469Floorbeam · corrodedFLOORBEAM BETWEEN FR 68 & 66 CORROSION. REMOVED & REPLACED PER SRM 51-72-11; CORR LEVEL 1; TASK JA-260-53500 DEFECT SIZE: 2" X 6'.Mar 21, 2006 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA060470Floorbeam · corrodedBEAM AT -Y1160 AT FR 68 CORROSION. REMOVED & REPLACED PER SRM 51-72-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 2" X 4'.Mar 21, 2006 · N749US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA060444Sill · corrodedRIGHT SILL PLATE AT FRAME 66 CORRODED. INSTALLED ANGLE PER SRM 53-41-14 REPAIR 6; CORROSION TASK JA-260-53500.Mar 7, 2006 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAASA03089Release Cable · incorrectCLT - THE 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 SLIDE AND RETURNED THJul 27, 2003 · N749US · Airbus A319112 · Emergency Equipment
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