N802AW

Service difficulty reports · 325

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 = 'N802AW' 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 AWXA200300951Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF RT OUTBOARD FLOOR SHEAR PLATE WEB BETWEEN FR 69 AND FR 70, AFT OF FLOORBEAM Y1792. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED SHEAR PLATE WEB BETWEEN FR Aug 5, 2003 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300946Angle · crackedDURING C-04 CHECK A 1/2) CRACK WAS FOUND ON RT UPPER SIDE OF ANGLE, AFT OF FR 34, UNDER PANEL 192AT. MAINTENANCE REMOVED CRACKED ANGLE; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG C3 D53230281; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG. 22, 23, 25, & 28, Aug 5, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300943Floorbeam · corrodedDURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF Y1292 FLOORBEAM AT FR 16. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOORBEAM FR 16 TO FR 18; FABRICATED A NEW SECTION OF FLOORBEAAug 5, 2003 · N802AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200300958Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 58, STR 39 L/H - 39 R/H. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 58, STR 39 L/H - 39 R/H; FABRICATED A NEW REAug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300955Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 53, STR 39 LT - 39 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 53, STR 39 L/H - 39 R/H; FABRICATED A NEW REPLAug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300954Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 56, STR 39 LT - 39 R/H. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 56, STR 39 LT - 39 RT; FABRICATED A NEW REPLAAug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300953Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 59, STR 39 LT - 39 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 59, STR 39 LT - 39 RT; FABRICATED A NEW REPLACAug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300950Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON LT TRANSITION PROFILE IN AFT CARGO COMPARTMENT BETWEEN FR 56 AND FR 58. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED TRANSITION PROFILE BETWEEN FR 56 AND FR 58; FABRICATED A NEW REPAug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300949Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON LT TRANSITION PROFILE IN AFT CARGO COMPARTMENT BETWEEN FR 52 AND FR 55. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED LT TRANSITION PROFILE BETWEEN FR 52 AND FR 55; FABRICATED A NEW Aug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300948Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 61, BETWEEN STR 39 LT AND 39 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 61, BETWEEN STR 39 LT AND 39 RT ; FAAug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300947Profile · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON CENTER PROFILE IN AFT CARGO COMPARTMENT AT FR 63, BETWEEN STR 39 LT AND 39 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CENTER PROFILE AT FR 63, BETWEEN STR 39 LT AND 39 RT; FABAug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300913Bracket · crackedMCN - MINOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON UPPER ATTACH BRACKET (CLOSING PLATE) UNDER LT FUSELAGE PANEL 191AT AT FR 34, BS 1438. MAINTENANCE REMOVED CRACKED CLOSING PLATE AT FR 34, BS 1438; FABRICATED A NEW REPLACEMENT CLOSING PLATE; IAug 4, 2003 · N802AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200300459Battery · dischargedFLIGHT CREW REPORTED THE AFT LT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.May 1, 2003 · N802AW · Airbus A319132 · Emergency EquipmentSDR AWXA200300460Power Supply · dischargedDURING INSPECTION THE LT FORWARD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-38-400.Apr 29, 2003 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200300210Cable · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BROKEN CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H IAW ESPM 20-25-21; OPERATIONAL CHECK WAS GOOD.Feb 26, 2003 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA200201162Check Valve · bypassingSNA - APU TAIL PIPE FIRE - APU FIRE REPORTED BY GROUND PERSONNEL, APU FIRE EXTINGUISHER WAS DISCHARGED. MAINTENANCE VISUALLY INSPECTED THE APU COMPARTMENT, TAIL PIPE, AND SURROUNDING AREA, NO DAMAGE WAS NOTED. SYSTEM WAS PLACED ON MEL 26-22-00, COND. 1 (APU FIDec 3, 2002 · N802AW · Airbus A319132 · APU Engine Fuel and ControlSDR AWXA200201060Computer · malfunctionedFLT 0472 - ON TAXI OUT AT PHX RECEIVED ECAM MESSAGE FOR AVIONICS VENT FAULT, A BURNING ODOR WAS ALSO NOTICED IN THE CABIN AREA. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER IAW AMM 21-26-34, OPERATIONAOct 28, 2002 · N802AW · Airbus A319132 · Air Distribution SystemSDR AWXA200200762Selector Valve · failedAFTER TAKEOFF WITH GEAR RETRACTED, ECAM IND L/G NOT UPLOCKED & L/G DOOR NOT CLOSED MESSAGE. RECYCLED, RECEIVED MESSAGE, RECYCLED AGAIN & GEAR RETRACTED NORMALLY, TURNED BACK. PFR FAILURES IND NLG UPLOCK PROXIMITY SENSORS (12GA & 13GA), DOWNLOCK (18GA & 19GA)Aug 18, 2002 · N802AW · Airbus A319132 · Landing Gear SelectorSDR AWXA200200435Computer · malfunctionedIN CRUISE FLIGHT AT FL390 ECAM SHOWED YELLOW HYD RESERVOIR OVERHEAT FOLLOWED BY ECAM ACTION OVERHEAT ON LOWER DISPLAY UNIT, INDICATION FLASHED ON AND OFF THEN WENT AWAY, DIVERTED TO MCI. MX RECALLED EVENT THAT INDICATED YELLOW ELECTRIC HYD PUMP CAUSED RESERVMay 19, 2002 · N802AW · Airbus A319132 · Hydraulic Indicating SystemSDR AWXA200200434Switch · malfunctionedICT - DIVERSION - FLT 0472 - DURING CRUISE EN ROUTE FROM DCA TO PHX ECAM INDICATED AN INTERMITTENT YELLOW HYDRAULIC RESERVOIR CLASS 1 OVERHEAT MESSAGE, AIRCRAFT DIVERTED TO ICT. MAINTENANCE TROUBLESHOT PER TSM 29-13-00-810-802 AND FOUND NO OVERHEAT OR FAULTS.May 18, 2002 · N802AW · Airbus A319132 · Hydraulic Indicating SystemSDR AWXA200200383Filter · contaminatedON CLIMBOUT, CREW RECEIVED ECAM MESSAGE FOR NR 1 ENG BLEED FAULT; BLEED TEMP REACHED 280 DEG & CROSSFEED VALVE OPENED; ACFT RETURNED. MX REPLACED FAN AIR THERMOSTAT & OPERATIONALLY CHECKED OUT SYS BY RUNNING ENG FOR AN EXTENDED PERIOD OF TIME AT POWER, CHECKEApr 29, 2002 · N802AW · Airbus A319132 · Pneumatic Distribution SystemSDR AWXA200200340Proximity Switch · out of adjustPHX - AIR TURNBACK - FLT 0590 - WHILE CLIMBING OUT OF PHX EN ROUTE TO MCI AT 10,000 FEET ECAM INDICATED THE RT AFT AVIONICS DOOR WAS OPEN. AIRCRAFT TURNED BACK AND LANDED SAFELY AT PHX. MAINTENANCE VERIFIED THE DOOR WAS CLOSED. ADJUSTED THE GAP ON THE RT AFApr 13, 2002 · N802AW · Airbus A319132 · Door Warning SystemSDR AWXA200200008Battery · dischargedPHX - EEL - C - DURING INSPECTION EMERGENCY POWER SUPPLY BATTERY WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY BATTERY IAW AMM-33-51-38.Jan 6, 2002 · N802AW · Airbus A319132 · Emergency LightingSDR AWXA0000024Controller · malfunctionedAFTER TAKEOFF, RECEIVED CAPTAINS ANTI-ICE/PITOT MESSAGE (REPEAT). REPLACED NR 1 AND NR 2 LGCIU COMPUTERS AND NLG PROX SENSOR 25GA. NR 1 LGCIU WAS REPLACED FOR SAME DISCREPANCY TT 0097701 SN 1905. PITOT HEAT COMPUTER REPLACED FLIGHT PRIOR. REPLACED FOR NR Jan 25, 2000 · N802AW · Airbus A319132 · Pitot/Static Anti-Ice SystemSDR AWXA9900395Regulator · leakingDIVERT FOR CREW OXYGEN LOSS. CREW O2 750 PSI, DECREASED TO 570 IN FLT. REMOVED AND REPLACED O2 REGULATOR FOR LEAKS PER MM 35-13-15-401. NO LEAKS NOTED. SEE ALSO LPS 7349112, 113, 116, PLUS 110. ATA 35 NUMEROUS WRITE-UPS SINCE APRIL 99, 9 MONTH LOOK BACK Nov 3, 1999 · N802AW · Airbus A319132 · Crew Oxygen System
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