N805AW

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 = 'N805AW' 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 USAA2008123092351Hinge Fitting · wornSAL - MAJOR REPAIR - C7 CHECK - NR 6141112, NR 5 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2985 / RIB7 HAS EXCESSIVE PLAY. REPLACED NR 5 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2985 / RIB7 IAW A319 AMM 55-36-41.Dec 10, 2008 · N805AW · Airbus A319132 · Vertical StabilizerSDR USAA2008123092350Hinge Fitting · wornSAL - MAJOR REPAIR - C7 CHECK - NR 6141111, NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2632 / RIB6 HAS EXCESSIVE PLAY. REPLACED NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2632 / RIB6 I/A/W A319 AMM 55-36-41.Dec 10, 2008 · N805AW · Airbus A319132 · Vertical StabilizerSDR USAA2008123092348Seat Track · corrodedSAL MAJOR REPAIR C7 CHECK NR 6141071, CORROSION ON CABIN SEAT TRACK AT FR 32 - FR 35, +Y765. REPAIRED CABIN SEAT TRACK AT FR 32 - FR 35, +Y765 IAW A319 SRM 53-21-15.Dec 10, 2008 · N805AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2008112692128Battery · dischargedFLT 160 - PHX-LAS - EEL - AFT RECHARGEABLE EMERGENCY FLASHLIGHT HAS DEAD BATTERY. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.Nov 25, 2008 · N805AW · Airbus A319132 · Emergency EquipmentSDR USAA2008111492063Connector · disconnectedLOGPAGE:4327505 - FLT#700 - PHX-SEA - EEL - AISLE EMERGENCY LIGHT AT ROW 10R IS INOPERATIVE. FOUND EMERGENCY LIGHT AT ROW 10R TO BE UNPLUGGED. RECONNECTED PLUG. OPERATIONAL CHECK WAS GOOD.Nov 13, 2008 · N805AW · Airbus A319132 · Light System WiringSDR USAA920081506Power Supply · inoperativeFLT 0573-SFO-LAS-EEL - EMERGENCY EXIT LIGHT OVERWING CEILING (AFT FACING) AND ACFT LT SIDEWALL INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD. (S)Aug 8, 2008 · N805AW · Airbus A319132 · Emergency LightingSDR AWXA200700736Damper · brokenSAL - EES - BROKEN ASSIST DAMPER ASSEMBLY ON R1 DOOR, FR 16 - FR 20. REPLACED ASSIST DAMPER ASSEMBLY ON R1 DOOR, FR 16 - FR 20 IAW A319 AMM 52-11-14. [06-19-07] REMOVED INFORMATION FROM STRUCTURE CAUSING DIFFICULTY SECTION SINCE DEFECTIVE ITEM IS NOT A STRUJun 8, 2007 · N805AW · Airbus A319132 · Passenger/Crew DoorsSDR AWXA200700710Floorbeam · corrodedSAL - CORROSION ON CABIN FLOORBEAM, FR 67 + 18", -Y1162. REPLACED CABIN FLOOR BEAM, FR 68 - FR 69, -Y1162 IAW A319 SRM 51-72-11.Jun 8, 2007 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200700709Floorbeam · corrodedSAL - CORROSION ON CABIN FLOORBEAM, FR 67 + 13", -Y1192. REPLACED CABIN FLOOR BEAM, FR 66 - FR 68, -Y1192 IAW A319 SRM 51-72-11.Jun 8, 2007 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200700712Floorbeam · corrodedSAL - CORROSION ON CABIN FLOORBEAM, FR 69 + 19", -Y254. REPLACED CABIN FLOOR BEAM, FR 68 - FR 70, -Y254 IAW A319 SRM 51-72-11.Jun 4, 2007 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200700707Shear Plate · corrodedSAL - FOUND CORROSION ON CABIN SHEAR PLATE, FR 69 - FR 70, -Y1162. REPLACED CABIN SHEAR PLATE, FR 69 - FR 70, -Y1162 IAW A319 SRM 51-72-11.Jun 4, 2007 · N805AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700708Sill · corrodedSAL - CORROSION ON R2 DOOR LOWER SILL, FR 67 + 19", -Y1230. REPAIRED R2 DOOR LOWER SILL, FR 67 + 19", -Y1230 IAW A319 SRM 53-41-14.Jun 3, 2007 · N805AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700701Fitting · corrodedSAL - CORROSION ON L1 DOOR LOWER SILL CENTER FITTING, FR 16 - FR 20, -Y1732. REPLACED L1 DOOR LOWER SILL CENTER FITTING, FR 16 - FR 20, -Y1732 IAW A319 SRM 51-72-11.Jun 3, 2007 · N805AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700722Sleeve · crackedSAL - EES - RIGHT OVERWING EMERGENCY EXIT SLIDE RESERVOIR CONNECTION SLEEVE CRACKED. REPLACED AND OPERATIONAL CHECKED RIGHT OVERWING EMERGENCY EXIT SLIDE RESERVOIR IAW A319 AMM 25-62-46.Jun 2, 2007 · N805AW · Airbus A319132 · Escape SlideSDR AWXA200602065Bleed Valve · failedLAS - IN CRUISE, AT FLT LEVEL 390 IN LIGHT OCCASIONAL MODERATE TURBULENCE. THE CREW HEARD A LOUD COMPRESSOR STALL, ACCOMPANIED BY ECAM ENG 2 STALL MSG. NO ABNORMAL ENGINE PARAMETERS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SEA. THE LANDING WAS UNEVEDec 13, 2006 · N805AW · Airbus A319132 · Compressor Bleed ValveSDR AWXA200501007Battery · inoperativeLAS - EEL - DURING GROUND HANDLING IN LAS, TECH DISCOVERED THE FORWARD FLIGHT ATTENDANT'S JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY AS REQUIRED.Aug 25, 2005 · N805AW · Airbus A319132 · Emergency EquipmentSDR AWXA200500827Adiru · failedDURING TAKEOFF RECEIVED MULTIPLE FAULTS BEGINNING TAKE OFF ROLL. ACFT ABORTED T/O & RETURNED TO GATE WITHOUT INCIDENT. MX R & R FAC 1 IAW AMWEST TASK CARD R2A22301. OPS TESTS GOOD. ATTEMPTED ANOTHER TAKEOFF & RECEIVED AUTO FLT RUD TRV LIM SYS ECAM MSG DURIJul 16, 2005 · N805AW · Airbus A319132 · Attitude and Direction Data SystemSDR AWXA200401402Power Supply · failedPHX - EEL - DURING E-04 CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND TO HAVE AN INTERNAL FAILURE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.Dec 15, 2004 · N805AW · Airbus A319132 · Emergency LightingSDR AWXA200401359Power Supply · dischargedLAX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.Dec 6, 2004 · N805AW · Airbus A319132 · Emergency LightingSDR AWXA200401236Power Supply · faultyDURING 4-DAY CHECK, OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.Nov 6, 2004 · N805AW · Airbus A319132 · Emergency LightingSDR AWXA200400887Computer · malfunctionedEN ROUTE, FLT MANAGEMENT GUIDANCE COMPUTER NR 1 FAILED AND FMGC NR 2 FAULTED, FIRST OFFICER LOST MAP DISPLAY 3 TIMES, DIVERTED TO CMH & LANDED WITHOUT FURTHER DIFFICULTY. MX R & R FMGC NR 1 IAW T/C R2A22302, PERFORMED OPS TEST OF FMGC NR 1 & 2, BOTH CHECK GOOAug 15, 2004 · N805AW · Airbus A319132 · Flight ControllerSDR AWXA200400883Epsu · failedPHX - EEL - DURING E-01 CHECK THE FORWARD LT EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED FORWARD LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.Aug 13, 2004 · N805AW · Airbus A319132 · Emergency LightingSDR AWXA200400744Floor Panel · delaminatedDURING B-04 CHECK FOUND FLOOR PANEL 262BG MISSING AN INSERT WITH DELAMINATION TO BOTTOM OF LAMINATE. MAINTENANCE REPLACED INSERT AND PERFORMED BOND REPAIR TO BOTTOM LAMINATE OF FLOOR PANEL 262BG IAW SRM 53-02-00, FIG. 201.Jun 28, 2004 · N805AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200400743Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AFT OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 LT FROM FR 66 TO FR 68 IAW A319 SRM 51-42-11, FIG. 2, 3, & 18.Jun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400742Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AFT OF FR 66. MAINTENANCE REMOVED BEAM Y1292 RT FROM FR 64 TO FR 66+5 INCH; FABRICATED A NEW REPLACEMENT BEAM; DRILLED SPLICE COUPLING TO FORWARD END OF NEW BEAM; INSTALLED NEW BEAM NR COUPLINGJun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400734Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 FROM FR 67 TO FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y765 FROM FR 67 TO FR 68 IAW SRM 51-42-11 FIG. 9-12, AND 18.Jun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400733Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 AT FR 66 IAW A319 SRM 51-72-11 PG. 1 AND 2.Jun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400732Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW SRM 51-42-11 FIG. 2, 3, AND 18.Jun 27, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400727Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 66 IAW A319 SRM 51-42-11 PG. 6, 7, & 41, FIG. 18. REGISTRATION NR WAS CHANGED TO REFLECT THE CORRECT AIRCRAFT, THIS EVENT DID NOT OCCUR Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400746Floor Panel · crackedMAJOR REPAIR, DURING B-04 CHECK FOUND 2 EACH 1INCH CRACKS IN FLOOR PANEL 221EF. MAINTENANCE CUTOUT DAMAGE IN FLOOR PANEL 221EF, AND PERFORMED BOND REPAIR IAW A319 SRM 53-02-00, FIG. 202.Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200400731Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 BETWEEN FR 64 AND FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 FROM FR 64 TO FR 66 IAW A319 SRM 51-42-11 PG. 39 AND 41 FIG. 18.Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400730Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 (2 PLACES) AT FR 64 AND FR 65. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 FROM FR 64 TO FR 65 IAW A319 SRM 51-42-11 FIG. 2, 3, 8, 18.Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400729Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 AT FR 66. MAINTENANCE REPAIRED BEAM Y1732 DOOR SILL AT FR 66 IAW A319 SRM 53-41-14 FIG. 201.Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400728Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW A319 SRM 51-42-11 FIGURES 2-18.Jun 26, 2004 · N805AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200400745Floor Panel · corrodedDURING B-04 CHECK FOUND CORROSION ON AFT SIDE CORNER OF FLOOR PANEL 261FF FROM FR 66 TO FR 68, AND Y1292 LT TO 1732 LT. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261FF IAW AWA T/C C1D25310.Jun 25, 2004 · N805AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200400726Plate · corrodedDURING B-04 CHECK CORROSION (4 SPOTS) WAS FOUND ON AFT CARGO DOOR SILL PLATE. MAINTENANCE REMOVED AND FABRICATED A NEW AFT CARGO DOOR SILL PLATE IAW A319 SRM 51-42-11 FIGURES 3,4,5,9 AND MFG DRAWING 17D53477153.Jun 25, 2004 · N805AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200400654Battery Pack · dischargedPHX - EEL - DURING 4-DAY CHECK THE LT OVERWING EMERGENCY BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (11WL) FAILS PUSH BUTTON TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.Jun 16, 2004 · N805AW · Airbus A319132 · Emergency LightingSDR AWXA200400469Computer · faultyEN ROUTE, RECEIVED ECAM MESSAGE FOR ANTI-ICE LT WINDOW THEN HEARD A LOAD NOISE AS LT AFT SIDE WINDOW SHATTERED, PRESSURE WAS NOT LOST, DIVERTED TO GJT. MAINT R & R LT AFT SIDE WINDOW IAW AMM 56-11-12, & REPLACED LT WINDOW HEAT COMPUTER IAW AMM 30-42-34. OPS CHMay 3, 2004 · N805AW · Airbus A319132 · Flight Compartment WindowsSDR AWXA200301212Solenoid Valve · looseDURING CLIMB OUT OF CMH EN ROUTE FOR LAS RECEIVED NR 1 ENGINE SYSTEM FAULT AT 6000 FT, EGT AT 617 DEGREES, PLACED NR 1 ENGINE THRUST LEVER TO IDLE AND MAINTAINED 567 DEG EGT UNTIL LANDING AND SHUTDOWN. MAINTENANCE FOUND THE 10TH STAGE BLEED SOLENOID VALVE BOTTOct 11, 2003 · N805AW · Airbus A319132 · Engine Ignition Analyzer SystemSDR AWXA200301124Battery · dischargedEMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT LT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.Oct 5, 2003 · N805AW · Airbus A319132 · Emergency EquipmentSDR AWXA200300629Battery · inoperativeFLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.May 30, 2003 · N805AW · Airbus A319132 · Emergency EquipmentSDR AWXA200300403Battery · dischargedPHX - EEL - FLIGHT CREW REPORTED THE RT OVERWING EMERGENCY EXIT LIGHT WAS FLASHING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.Apr 21, 2003 · N805AW · Airbus A319132 · Emergency LightingSDR AWXA200300394Bottle · dischargedOMA - DIVERSION - FLT 0012 - APPROXIMATELY 1 HOUR AND 30 MINUTES INTO FLIGHT EN ROUTE FROM PHX TO JFK CREW OXYGEN WENT DOWN TO 20 PSI AND REGULATOR PRESSURE WAS LOW, FLIGHT DIVERTED TO OMA. EMERGENCY OXYGEN SWITCH WAS STUCK IN 100 PERCENT POSITION AFTER GROUNApr 19, 2003 · N805AW · Airbus A319132 · Crew Oxygen SystemSDR AWXA200300296Battery · dischargedDURING INSPECTION THE FORWARD LT EMERGENCY POWER SUPPLY LOAD WAS FOUND INOPERATIVE ON FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT FORWARD LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.Mar 20, 2003 · N805AW · Airbus A319132 · Emergency LightingSDR AWXA200300097Filter · contaminatedPHX - AIR TURN BACK - FLT 0001 - ON TAKEOFF FROM PHX EN ROUTE FOR ORD FUMES WERE NOTICED IN MID-CABIN, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED POWER RUN AT ALL SETTINGS ISOLATING THE NO.1 AND NO. 2 ENGINES BLEEDS AND APU BLEEJan 31, 2003 · N805AW · Airbus A319132 · Air Distribution FanSDR AWXA200300089Bottle · dischargedFLT 0820 - WHILE EN ROUTE FROM BOS TO PHX CREW OXYGEN WENT TO ZERO, DIVERTED TO ROC. MAINTENANCE REMOVED AND REPLACED THE CREW OXYGEN BOTTLE IAW AWA T/C R2A35301. PERFORMED LEAK CHECK OF ALL CONNECTIONS AT BOTTLE, ALSO CHECK ALL MASKS FOR CORRECT STOWAGE AND LJan 28, 2003 · N805AW · Airbus A319132 · Crew Oxygen SystemSDR AWXA200201208Apu · malfunctionedTAILPIPE FIRE, AFTER (APU) SHUT DOWN, A TAILPIPE FIRE WAS NOTICED BY GROUND CREW. MAINTENANCE INSPECTED THE APU AND FOUND NO DAMAGE TO TAILPIPE OR SURROUNDING AREA. PLACED SYSTEM ON MEL, COND. 1.Dec 17, 2002 · N805AW · Airbus A319132 · APU Engine Fuel and ControlSDR AWXA200201111Fmc · malfunctionedFLT 0822 - EN ROUTE FROM PHX TO BOS FT MANAGEMENT GUIDANCE COMPUTER (FMGC) NR 2 FAILED, DIVERTED TO CMH AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FMGC NR 2 IAW AWA; NAV DATA UPLOADED IAW T/C A1B34321. FUNCTIONAL TEST GOOD. UNIT CHENov 12, 2002 · N805AW · Airbus A319132 · Flight Management Computing Hardware SystemSDR AWXA200200678Wire · brokenLAS - EMERGENCY LIGHT HARNESS SEAT ROW 9 RT HAS A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 9 RT, OPERATIONAL CHECK OF LIGHTING SYSTEM CHECKED GOOD.Jul 29, 2002 · N805AW · Airbus A319132 · Light System WiringSDR AWXA200200422Battery · dischargedPHX - EMERGENCY EQUIPMENT - F/A REPORTED THAT THE AFT EMERGENCY FLASHLIGHT NEAR THE RIGHT AFT F/A JUMPSEAT IS INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN THE EMERGENCY FLASHLIGHT AT THE AFT F/A JUMPSEAT.May 12, 2002 · N805AW · Airbus A319132 · Emergency Equipment
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