N827AW

Service difficulty reports · 277

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 = 'N827AW' 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 USAA2009030290476Ballast · defectiveFLT 632 - PHX-PIT - SMOKE - PRIOR TO LANDING, CABIN LIGHTS FLICKERING. UPON LANDING IN PIT, SMOKE WAS REPORTED IN THE CABIN (POWDERY SMOKE), SOURCE WAS AROUND ROW 4. CREW DECLARED EMERGENCY, FIRE AND RESCUE EQUIPMENT RESPONDED. INSTALLED NEW BALLAST. OPERAFeb 28, 2009 · N827AW · Airbus A319132 · Passenger Compartment LightingSDR USAA920081531Wire Harness · faultyFLT 655 - SNA-PHX- EEL - EMERGENCY PATH LIGHT AT SEAT 22C INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT HARNESS ON SEAT 22C. OPERATIONAL CHECK WAS GOOD. (S)Aug 17, 2008 · N827AW · Airbus A319132 · Light System WiringSDR USAA920081252Actuator · failedFLT 687 - PHX - EWR - RETF - DURING CLIMB THE LT SPOILER REMAINED DEPLOYED 2 INCHES CAUSING EXCESSIVE VIBRATION. CABIN VERIFIED CONDITION. CAPTAIN RETURNED TO THE FIELD. MX REPLACED THE NR3 SPOILER ACTUATOR IAW WITH AIRCRAFT MAINTENANCE MANUAL 27-64-51. OPJun 20, 2008 · N827AW · Airbus A319132 · Drag Control ActuatorSDR AWXA200700802Smoke Detector · failedPHX - EES - LOG NR 7848154 - CREW REPORTED SMOKE LAV AND CRG DET FAULT. MX REMOVED AND REPLACED SDCU IAW AMM 26-17-34, OPERATIONAL CHECK WAS GOOD.Jul 6, 2007 · N827AW · Airbus A319132 · Smoke DetectionSDR AWXA200700140O-Ring · leakingPHX - DURING INITIAL CLIMB, LOST ALL OIL QUANTITY IN NR 1 ENGINE. OIL PRESS AND ALL OTHER PARAMETERS REMAINED IN THE GREEN. RETURNED TO FIELD AT IDLE THRUST. INSTALLED TEMP THERMOCOUPLE IN NR 1 ENG ACOC WITH NEW O-RING IAW MM 79-32-15 PB401. RAN ENG, LEAK Jan 31, 2007 · N827AW · Airbus A319132 · Turbine Engine Oil SystemSDR AWXA200601929Floorbeam · corrodedSAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 67 + 11" - FS 70, -Y765. REPLACED MAIN CABIN FLOORBEAM, FS 67 + 11" - FS 70, -Y765 IAW A319 SRM 51-72-11 AND 51-42-11.Nov 11, 2006 · N827AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601928Floorbeam · corrodedSAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 64 - FS 66, + Y1292. REPLACED MAIN CABIN FLOORBEAM, FS 64 - FS 66, + Y1292 IAW A319 SRM 51-72-11 AND 51-42-11.Nov 11, 2006 · N827AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601909Sill · corrodedSAL - MAJOR REPAIR - BC-4 CHECK, CORROSION ON R2 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 66 TO FS 68, S23R. REPLACED R2 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 66 TO FS 68, S23R IAW A319 SRM 51-72-11.Nov 9, 2006 · N827AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601900Shear Web · corrodedSAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN SHEAR WEB, FS 69 TO FS 70, -Y1732. REPLACED MAIN CABIN SHEAR WEB, FS 69 TO FS 70, -Y1732 IAW A319 SRM 51-72-11.Nov 9, 2006 · N827AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601927Floorbeam · corrodedSAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 68 - FS 70, + Y765. REPLACED MAIN CABIN FLOORBEAM, FS 68 - FS 70, + Y765 IAW A319 SRM 51-72-11 AND 51-42-11.Nov 8, 2006 · N827AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601926Sill · corrodedSAL - CORROSION ON L2 DOOR CUT OUT LOWER SILL, FS 67+16" - FS 68, -Y1732. REPAIRED L2 DOOR CUT OUT LOWER SILL, FS 67+16" - FS 68, -Y1732 IAW A319 SRM 53-41-14.Nov 8, 2006 · N827AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601899Dummy Rail · corrodedSAL - MAJOR REPAIR - BC -4 CHECK - CORROSION ON MAIN CABIN DUMMY RAIL, FS 20 AND -Y254. REPAIRED MAIN CABIN DUMMY RAIL, FS 20 AND -Y254 IAW A319 SRM 53-00-14 FIGURE 204.Nov 8, 2006 · N827AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601898Floorbeam · corrodedSAL - MAJOR REPAIR - BC-4 CHECK, CORROSION ON MAIN CABIN FLOORBEAM, FS 66, -Y1292. REPLACED MAIN CABIN FLOORBEAM, FS 66, -Y1292 IAW A319 SRM 51-72-11.Nov 8, 2006 · N827AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601925Floorbeam · corrodedSAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 66 - FS 68, -Y1292. REPLACED MAIN CABIN FLOORBEAM, FS 66 - FS 68, -Y1292 IAW A319 SRM 51-42-11 AND 51-72-11.Nov 7, 2006 · N827AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601939Shear Web · corrodedSAL - CORROSION ON SHEAR WEB IN AFT PASSENGER CABIN, FROM FS 69 TO FS 70, +Y1732. REPLACED SHEAR WEB IN AFT PASSENGER CABIN, FROM FS 69 TO FS 70, +Y1732, IAW A320 SRM 51-72-11 AND 51-42-11.Nov 4, 2006 · N827AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601908Dummy Rail · corrodedSAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN DUMMY RAIL, FS 20 - FS 24, -Y189. REPLACED MAIN CABIN DUMMY RAIL, FS 20 - FS 24, -Y189 IAW A319 51-72-11.Nov 4, 2006 · N827AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601897Floorbeam · corrodedSAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN FLOORBEAM, FS 67 + 16" TO FS 69 + 4", -Y1162. REPLACED MAIN CABIN FLOORBEAM, FS 67 + 16" TO FS 69 + 4", -Y1162 IAW A319 SRM 51-72-11.Nov 4, 2006 · N827AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601896Floorbeam · corrodedSAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN FLOORBEAM, FS 66 + 5", -Y1162. REPLACED MAIN CABIN FLOORBEAM, FS 66 + 5", -Y1162 IAW A319 SRM 51-72-11.Nov 4, 2006 · N827AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601887Dummy Rail · corrodedSAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN DUMMY RAIL, FS 16+7", -Y1292. REPAIRED MAIN CABIN DUMMY RAIL, FS 16+7", -Y1292 IAW A319 SRM 53-11-15 FIGURE 203.Nov 4, 2006 · N827AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601938Seat Track · corrodedSAL - CORROSION ON MAIN CABIN SEAT TRACK, +Y765, FS 41 + 7", FS 44 + 5" AND FS 45 + 16". REPLACED MAIN CABIN SEAT TRACK, +Y765, FS 41 - FS 47 IAW A319 SRM 51-72-11.Nov 3, 2006 · N827AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200501519Condenser · failedCREW REPORTED THAT THE NR 1 PACK WOULD NOT HOLD CABIN PRESSURE WHILE EN ROUTE TO LAS AT FL 270 CABIN CLIMBED TO 9650 FL. CREW PERFORMED EMERGENCY DESCENT TO 10,000 FLT. AT 10,000 FLT CABIN ALT WAS 5500FT. AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT. MXDec 15, 2005 · N827AW · Airbus A319132 · Cabin Pressure Control SystemSDR AWXA200501184Battery · inoperativePHX - EEL - ON THE GROUND REPORTED THAT THE AFT FLIGHT ATTENDANT RT EMERGENCY FLASHLIGHT DOES NOT BLINK. MAINTENANCE REMOVED AND REPLACED THE RT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS GOOD.Oct 8, 2005 · N827AW · Airbus A319132 · Emergency EquipmentSDR AWXA200401406Battery · dischargedPHX - EMERGENCY EQUIPMENT - DURING THROUGH FLIGHT INSPECTION THE FORWARD INBOARD EMERGENCY FLASHLIGHT WAS NOT FLASHING. MAINTENANCE REMOVED AND REPLACED THE FORWARD INBOARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.Dec 16, 2004 · N827AW · Airbus A319132 · Emergency EquipmentSDR AWXA200400243Pressure Switch · crackedPHX - EMERGENCY LANDING - FLT 0154 - EN ROUTE FROM SFO TO PHX RECEIVED GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL INDICATION. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND NR 1 ENGINE (GREEN SYSTEM) HYDRAULIC PRESSURE SWITCH CRACKED Mar 6, 2004 · N827AW · Airbus A319132 · Hydraulic Pressure SensorSDR AWXA200301504Iru · faultyLAX - ABORTED TAKEOFF - FLT 0408 - ON TAKEOFF ROLL AT LAX EN ROUTE FOR BOS THE CAPTAINS AIRSPEED INDICATOR SHOWED 40 KTS AT THE 80 KTS CROSS CHECK. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 AIR DATA INERTIAL REFERENCE UNIT Nov 29, 2003 · N827AW · Airbus A319132 · Inertial Guidance SystemSDR AWXA200201205Warning Horn · false activationON TAKEOFF ROLL ENROUTE FOR SET N1 THRUST AT 80 KTS AND HEARD REPETITIVE "RETARD" OVER THE LOUD SPEAKER; REJECTED TAKEOFF AND RETURNED TO GATE. MAX SPEED INDICATED WAS 87 KTS. MAINTENANCE REVIEWED POST FLIGHT REPORT THAT INDICATED AIRCRAFT WENT FROM PHASE 2 TODec 16, 2002 · N827AW · Airbus A319132 · Central WarningSDR AWXA200201193Circuit Board · failedON CLIMB FROM LAX EN ROUTE FOR CMH WITH AIR DATA SWITCH IN FIRST OFFICER 3 POSITION; FIRST OFFICERS AIR SPEED INDICATOR RED LINE DECREASED TO APPROXIMATELY 240 KTS. SWITCHED BACK TO AIR DATA NORMAL POSITION AND INDICATIONS WENT BACK TO NORMAL. DUE TO FIRST OFFDec 12, 2002 · N827AW · Airbus A319132 · Air Data Computer
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