N803AW

Service difficulty reports · 190

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 = 'N803AW' 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 USAA920081483Pin · corrodedSAL-C7 -MAJOR REPAIR- CORROSION ON REAR PINTLE PIN OF LT MAIN LANDING GEAR. REPLACED REAR PINTLE PIN OF LT MAIN LANDING GEAR IAW TASK CARD R4M32311. (S)Jul 26, 2008 · N803AW · Airbus A319132 · Main Landing GearSDR USAA920081481Seat Track · corrodedSAL-C7 -MAJOR REPAIR- CORROSION ON RAIL SEAT LOCATION AT FR66 AND Y1292. REPLACED RAIL SEAT LOCATION AT FR66 AND Y1292 IAW A319 SRM 51-72-11. (S)Jul 26, 2008 · N803AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA920081432Floorbeam · corrodedSAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR66 TO FR70, Y765. REPLACED FLOORBEAM AT FR66 TO FR70, Y765 IAW SRM A319 51-72-11. (S)Jul 25, 2008 · N803AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA920081433Floorbeam · corrodedSAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR67 TO FR70, -Y765. REPLACED FLOORBEAM AT FR67 TO FR70, -Y765 IAW SRM A319 51-72-11. (S)Jul 25, 2008 · N803AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA920081434Floorbeam · corrodedSAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR67 TO FR69, -Y1292. REPLACED FLOORBEAM AT FR67 TO FR69, -Y1292 IAW SRM A319 51-72-11. (S)Jul 24, 2008 · N803AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA920081466Shear Plate · corrodedSAL-C7- MAJOR REPAIR - SHEAR PLATE CORRODED FR69 TO FR70, -Y1732, S23R. REPLACED SHEAR PLATE FR60 TO FR70, -Y1732, S23R IAW A319 SRM 51-72-11. (S)Jul 22, 2008 · N803AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA920081465Shear Plate · corrodedSAL-C7- MAJOR REPAIR - SHEAR PLATE CORRODED BETWEEN FR69 TO FR70, Y1738. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1738 IAW A319 SRM 51-42-11 AND 51-72-11. (S)Jul 22, 2008 · N803AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA920081464Floorbeam · corrodedSAL-C7- MAJOR REPAIR - BEAM RAIL CORRODED AT FR66, Y1292. REPLACED BEAM RAIL AT FR66, Y1292 IAW A319 SRM 51-72-11. (S)Jul 22, 2008 · N803AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA920081462Dummy Rail · corrodedSAL-C7-MAJOR REPAIR - DUMMY RAIL CORRODED AT BS FR16 BL Y503. REPLACED DUMMY RAIL AT BS FR16 BL Y503 IAW A319 SRM 57-72-11. (S)Jul 22, 2008 · N803AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA920081467Shear Plate · crackedSAL-C7-MAJOR REPAIR - CRACKED TRAY PLATE AT FR68 TO FR69, -Y1738. REPLACED -TRAY PLATE AT FR68 TO FR69, -Y1738 IAW A319 SRN 51-72-11. (S)Jul 22, 2008 · N803AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA920081442Seat Track · corrodedSAL-C7- MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR 16, BL-Y1292. REPLACED SEAT TRACK AT FR 16, BL-Y1292 IAW A319 SRM 51-72-11. (A)Jul 22, 2008 · N803AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA920081441Seat Track · corrodedSAL-C7- MAJOR REPAIR- CORROSION ON SEAT TRACK AT FR16, BL-Y765. REPLACED SEAT TRACK AT FR16, BL-Y765 IAW A319 SRM 51-72-11. (A)Jul 22, 2008 · N803AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA920081472Hinge Fitting · excess playSAL-C7- MAJOR REPAIR - EXCESSIVE PLAY ON HINGE NR 4 OF RUDDER. REPLACED NR 4 HINGE FITTING NR 4 AT RIB NR 6, HORIZONTAL STABILIZER STATION 2632 IAW A319 AMM27-21-00. (S)Jul 21, 2008 · N803AW · Airbus A319132 · Rudder StructureSDR USAA920081463Hinge Fitting · excess playSAL-CY- MAJOR REPAIR - EXCESSIVE PLAY ON NR 1 HINGE OF RUDDER AT RIB 2 VERTICAL STABILIZER STA 760. REPLACED FITTING ASSEMBLY AT RIB 2 VERTICAL STABILIZER STA 760 IAW A319 AMM 55-36-41. (S)Jul 21, 2008 · N803AW · Airbus A319132 · Rudder StructureSDR USAA920081455Seat Track · corrodedSAL-C7- MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK FR20, -Y1292. REPLACED CABIN SEAT TRACK FR20, -Y1292 IAW A319 SRM 51-72-11. (S)Jul 15, 2008 · N803AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR SA08016Proximity Switch · faultedLAS - FLT 268 - YYZ TO LAS - AFTER TAKEOFF, RECEIVED ECAM MESSAGE "L/G DOORS NOT LOCKED". CREW RECYCLED THE GEAR AND RECEIVED A SATISFACTORY INDICATION. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSOR FIN 23GA. OPERATIONALLMar 21, 2008 · N803AW · Airbus A319132 · Landing Gear Position and WarningSDR AWXA200700324Sill · corrodedSAL - FOUND CORROSION ON L2 DOOR CUT OUT LOWER SILL, FR 67 + 19", +Y1250. REPAIRED L2 DOOR CUT OUT LOWER SILL, FR 67 + 19", +Y1250 IAW A319 SRM 53-41-14.Mar 2, 2007 · N803AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700322Sill · corrodedSAL - FOUND CORROSION ON L2 DOOR CUT OUT SILL BEAM SHAPE SILL, FR 60 - FR 68, S23L. REPLACED L2 DOOR CUT OUT SILL BEAM SHAPE SILL, FR 60 - FR 68, S23L IAW B737-300 SRM 51-72-11.Feb 27, 2007 · N803AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700326Fitting · corrodedSAL - FOUND CORROSION ON R1 DOOR SILL CENTER FITTING, FR16 + 6". REPLACED R1 DOOR SILL CENTER FITTING, FR16 - FR 20 IAW A319 SRM 51-72-11.Feb 21, 2007 · N803AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200700336Fitting · corrodedSAL - FOUND CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT OUT THRESHOLD CORNER FITTING, FR 24A, S37R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUT OUT THRESHOLD CORNER FITTING, FR 24A, S37R IAW A319 SRM 51-72-11.Feb 20, 2007 · N803AW · Airbus A319132 · Fuselage Main, Attach FittingsSDR AWXA200700319Seat Track · corrodedSAL - FOUND CORROSION ON MAIN CABIN SEAT TRACK, FR 41 - FR 47, -Y1292. REPLACED MAIN CABIN SEAT TRACK, FR 41 - FR 47, -Y1292 IAW A319 SRM 51-72-11.Feb 20, 2007 · N803AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500610Actuator · bypassingFLT 605 EN ROUTE TO DEN PILOT REPORTED THE NOSE LANDING GEAR WAS SLOW TO RETRACT AT APPROXIMATELY 20 SECONDS ECAM MESSAGE LANDING GEAR NOT UPLOCKED AND LANDING GEAR DOORS NOT CLOSED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR ACTUATING CYLINDER PEMay 25, 2005 · N803AW · Airbus A319132 · Landing Gear ActuatorSDR AWXA200400584Outflow Valve · faultyAIR TURN BACK - FLT 0051 - ON CLIMB OUT OF LAS EN ROUTE, RECEIVED AVIONICS VENT SYSTEM FAULT, AIRCRAFT PRESSURIZED NORMALLY, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE ISSUED MEL 21-26-04 COND 1, "SKIN AIR OUTLET VALVE INOP". ON 05/31/200May 29, 2004 · N803AW · Airbus A319132 · Pressure Regulator/Outflow ValveSDR AWXA200400201Proximity Sensor · defectiveLAX - LANDING GEAR - FLT 0409 - ON DESCENT INTO LAX EN ROUTE FROM BOS WHEN LANDING GEAR WAS SELECTED DOWN, RECEIVED ECAM MESSAGE FOR LANDING GEAR NOT DOWN AND LOCKED. ALSO HAD 3 RED LIGHTS & LANDING GEAR DOOR OPEN INDICATIONS. RECYCLED LANDING GEAR HANDLE WIFeb 22, 2004 · N803AW · Airbus A319132 · Landing Gear Position and WarningSDR AWXA200301558Floor Panel · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LOWER SIDE OF FLOOR PANEL 261FF FROM BS 31577 TO BS 32571, Y1600 TO Y1898, Z240. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261FF FROM BS 31577 TO BS 32571, Y1600 TO Y1898, Z240 IAW AWA T/C C1D253Dec 11, 2003 · N803AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200301571Floor Panel · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT LOWER SURFACE OF FLOOR PANEL 262FF. MAINTENANCE REMOVED CORROSION AND TRIMMED AWAY CORRODED AREA ON AFT LOWER SURFACE OF FLOOR PANEL 262FF; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IADec 9, 2003 · N803AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200301564Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1219, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM AT FR 68, Y1219, Z240; FABRICATED A NEW REPLACEMENT FLOOR BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7.Dec 9, 2003 · N803AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200301563Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK 4 AREAS OF GALVANIC CORROSION WERE FOUND ON FLOORBEAM 279MM AFT OF FR 67 AT Y1219, 431MM AFT OF FR 67 AT Y1143, 330MM AFT OF FR 67 AT Y1143, AND 220MM AFT OF FR 66 AT Y1292, Z240. MAINTENANCE REMOVED AND REPLACED FLOORBEDec 9, 2003 · N803AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200301562Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1193, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM AT FR 68, Y1193, Z240; RECEIVED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7.Dec 9, 2003 · N803AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200301557Seat Track · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF FLOORBEAM AT FR 66, Y1292, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM FROM FR 64 TO FR 66, Y1292, Z240; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D534-72209; INSTALLED REPDec 9, 2003 · N803AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200301531Rib · crackedDURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON AFT FIXED FAIRING RIB 14 AT PYLON STATION 908. MAINTENANCE REMOVED AND REPLACED CRACKED NR 2 ENGINE PYLON AFT FIXED FAIRING RIB 14 AT PYLON STATION 908 IAW A319 SRM 51-42-11, FIG 2, 3, & 8, PGDec 9, 2003 · N803AW · Airbus A319132 · Nacelle/Pylon, Frame/Spar/RibSDR AWXA200301538Angle · crackedDURING C-04 CHECK A .5 INCH CRACK WAS FOUND IN LOWER RADIUS OF L-ANGLE ON RT AFT SIDE OF FR 34 UNDER PANEL 192AT, BS 14836. MAINTENANCE REMOVED CRACKED -L- ANGLE ON RT AFT SIDE OF FR 34; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A319 SRM 5Dec 8, 2003 · N803AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200301537Angle · crackedDURING C-04 CHECK A .5 INCH CRACK WAS FOUND IN LOWER RADIUS OF L- ANGLE ON LT SIDE OF FR 34 UNDER PANEL 191A, BS 14836. MAINTENANCE REMOVED CRACKED -L- ANGLE ON LT SIDE OF FR 34; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11,Dec 8, 2003 · N803AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300299Door · out of rigEN ROUTE FROM LAS TO MIA THE FLIGHT DECK DOOR WAS EXTREMELY HARD TO OPEN. DOOR WOULD NOT CLOSE PROPERLY AND THE UPPER & CENTER LATCH WOULD NOT ENGAGE. MAINTENANCE RIGGED THE FLIGHT DECK DOOR IAW AMM 52-51-11, OPERATIONAL CHECK WAS GOOD.Mar 22, 2003 · N803AW · Airbus A319132 · Passenger/Crew DoorsSDR AWXA200200646Cover · delaminatedPHX - EMERGENCY ESCAPE EQUIPMENT - DURING POST FLIGHT INSPECTION THE EDGE OF THE LT OVERWING DUAL LANE SLIDE COVER WAS FOUND DELAMINATING. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING ESCAPE SLIDE PACK ASSEMBLY IAW T/C R1A25301.Jul 22, 2002 · N803AW · Airbus A319132 · Escape SlideSDR AWXA200200425Restrictor Valve · obstructedT/O ROLL APPROX 90 KTS, CAPT NOTICED NR 2 ENG HIGH OIL PRESSURE IND 332 PSI. AIRCRAFT RETURNED. MX REPLACED NR 2 ENG PRESSURE PUMP, NR 4 BEARING SCAVENGE VALVE & OIL FILTERS. PROBLEM PERSISTS, BUT OIL PRESSURE REDUCED TO ACCEPTABLE LIMITS FOR FERRY TO PHX. May 14, 2002 · N803AW · Airbus A319132 · Engine Oil Distribution (Airframe Furnished)SDR AWXA0001602Panel · unsecureLAS - ABORTED TAKEOFF - 4/7/01 - AT APPROX 40 KIAS ECAM MESSAGE FOR THE LEFT EMERGENCY OVERWING EXIT DOOR OPEN ILLUMINATED AND THE TAKEOFF WAS ABORTED. A PAX REPORTED THE EMERGENCY DOOR HANDLE ACCESS COVER FELL OFF DURING INITIAL TAKEOFF ROLL. MAINTENANCE INApr 9, 2001 · N803AW · Airbus A319132 · Emergency ExitsSDR AWXA0001154Contactor · failedPHX - AIR TURNBACK - ON DEPARTURE AT APPROX 3000FT MSL THE CENTER ESSENTIAL BUS LOST POWER; CREW COMPLIED WITH ECAM ACTION AND RETURNED TO PHX; ND NR 1 WAS NOT POWERED, PFD NR 1 OPERATED NORMAL; AN OVERWEIGHT LANDING WAS MADE, SINK RATE WAS LESS THAN 200 FPM ODec 29, 2000 · N803AW · Airbus A319132 · AC Power Distribution SystemSDR AWXA0000795Unknown · odorMELTING PLASTIC OR WIRING SMELL WAS NOTICED AT THE TOP OF CLIMB AND DISSIPATED AFTER TWO MINUTES. SMELL RETURNED DURING DESCENT WHILE PASSING THROUGH 140 FT, AGAIN DISSIPATING AFTER TWO MINUTES. SMELL WAS COMING FROM ROW EIGHT FORWARD. INSPECTED FWD COMPAROct 24, 2000 · N803AW · Airbus A319132 · Air Distribution SystemSDR AWXA0000184Slide · deployedON ARRIVAL AT TUS, SLIDE WAS DEPLOYED (DID NOT INFLATE). REPLACED ESCAPE SLIDE IAW CARD R1C25305. TT 0064631 RECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT. NO HISTORY.Mar 28, 2000 · N803AW · Airbus A319132 · Escape Slide
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