N814AW

Service difficulty reports · 271

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 = 'N814AW' 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 AWXA200600026Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR36 TO FR 41 AND Y765. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 51-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y765 IAW AIRBUS 319 SRM 51-Dec 23, 2005 · N814AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600022Seat Track · corrodedMCN - DURING BC-4 CHECK DISCOVERED CORROSION ON FLOORBEAM SEAT RAIL AT FR 66 AND Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 64 TO FR 66 AND Y-1292 IAW AIRBUS 319 SRM 51-72-11.Dec 23, 2005 · N814AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600025Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR 37+1 TO FR 40+2 AND Y1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y1292 IAW AIRBUS 319 Dec 21, 2005 · N814AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600024Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FR 42+7" AND Y-765. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR42 TO FR51 AND Y-765 IAW AIRBUS 319 SRM 51-72-11Dec 21, 2005 · N814AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600023Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR 38 TO FR 40 AND Y-1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 51-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y-1292 IAW AIRBUS 319 SRDec 21, 2005 · N814AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200500538Iru · malfunctionedEN ROUTE, AFTER REACHING CRUISE ALTITUDE RECEIVED ECAM MESSAGE ADR 1 FAULT FOLLOWED BY NR 1 IR FAILURE. APPROXIMATELY 2 HRS 45 MINUTES LATER AUTOPILOT, AUTO THROTTLES, AND FLIGHT DIRECTORS DISCONNECTED AND WOULD NOT RE-ENGAGE, NR 2 IR FAULT INDICATED ON ADIRUMay 5, 2005 · N814AW · Airbus A319132 · Inertial Guidance SystemSDR AWXA200400849Seat · leakingAFTER TAKEOFF AT JFK EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "AIR ENG 1 BLEED ABNORMAL PRESSURE", NR 1 ENGINE BLEED VALVE WOULD NOT OPEN, DIVERTED TO BWI FOR REPAIR. MX T/S PER TSM 36-11-00-810-809A, BLEED PRESSURE REGULATOR VALVE FAILED 20 PSI TEST PER STEP 2Aug 3, 2004 · N814AW · Airbus A319132 · Pneumatic Distribution SystemSDR AWXA200400055Fuel Control · malfunctionedPHX - ABORTED TAKEOFF - FLT 0820 - ON TAKEOFF AT PHX EN ROUTE FOR BOS THE NR 1 ENGINE FAILED TO ACCELERATE, REJECTED TAKEOFF AT 60 KTS. TAXIED CLEAR OF RUNWAY AND RAN UP NR 1 ENGINE, ENGINE AGAIN FAILED TO ACCELERATE ABOVE 1.1 EPR, RETURNED TO GATE. MAINTENAJan 19, 2004 · N814AW · Airbus A319132 · Fuel Controlling SystemSDR AWXA200301383Apu · malfunctionedNR 1 GENERATOR INOPERATIVE AND ON (MEL), APU AUTO SHUTDOWN AT 330 FT, ATTEMPTED 1 RESTART, NO LUCK, DIVERTED & LANDED WITHOUT FURTHER EVENT. MAINT R & R NR 1 IDG, OPS CHK GOOD. MAINT FOUND APU BEARINGS GRINDING & DAMAGE TO BLADES, R & R APU, OPS CHECK GOOD. Nov 9, 2003 · N814AW · Airbus A319132 · APU Core EngineSDR AWXA200300971Actuator · malfunctionedON TAKEOFF ROLL AT SMF EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75306, OPERATIONAL AND LEAK CHECK WERE GOOD PER T/C F5MAug 21, 2003 · N814AW · Airbus A319132 · Engine Air Intake SystemSDR AWXA200300970Engine · malfunctionedON TAKEOFF ROLL AT ORD EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE INSPECTED ENGINE INLET AREA, NO DAMAGE NOTED. PERFORMED FULL AUTHORITY DIGITAL ENGINE CONTROL TEST ON THE NR 2 ENGINE PER TSM 75-30-0Aug 21, 2003 · N814AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR AWXA200300776Bleed Actuator · faultyON TAKE OFF ROLL AT PHX EN ROUTE TO YYC, EGT LIMIT EXCEEDED (645) DEGREES. ABORTED TAKEOFF AND RETURNED TO GATE. MECHANIC REMOVED AND REPLACED THE 2.5 BLEED (LPC MASTER) ACTUATOR IAW AWA T/C R5M75307 AND PERFORMED POWER ASSURANCE TESTS IAW AWA T/C F5M71312 ASJul 4, 2003 · N814AW · Airbus A319132 · Compressor Bleed ControlSDR AWXA200300530Pressure Sensor · faultyCMH - DIVERSION - FLT 0045 - AFTER CLIMBOUT OF DCA EN ROUTE FOR PHX NOTICED HYDRAULIC POWER TRANSFER UNIT ON ECAM AFTER THRUST REDUCTION. ALSO DISPLAYED ECAM MESSAGE NR 1 ENGINE HYDRAULIC PUMP. DIVERTED TO CMH AS PRECAUTION. MAINTENANCE REMOVED AND REPLACEDMay 12, 2003 · N814AW · Airbus A319132 · Hydraulic Pressure SensorSDR AWXA200300213Seal · tornPHX - DIVERSION - FLT 0251 - ON CLIMB OUT FROM LAS EN ROUTE FOR PHL A NOISE WAS HEARD COMING FROM THE LEFT LOWER CORNER OF THE CAPTAINS WINDSHIELD. NOISE WAS INTERMITTENT AT FIRST, BUT AS DIFFERENTIAL INCREASED THE NOISE INCREASED AND THEN BECAME STEADY. DIVERFeb 27, 2003 · N814AW · Airbus A319132 · Flight Compartment WindowsSDR AWXA200300003Slat · crackedMCN - MAJOR REPAIR - DURING B-02 CHECK A 1/2" CRACK AND 1/2" X 1/2" SECTION OF #2 SLAT WAS FOUND MISSING AT THE UPPER TRAILING EDGE 8" FROM THE INBOARD END. MAINTENANCE BLENDED OUT DAMAGED AREA ON #2 SLAT AT UPPER TRAILING EDGE INBOARD END; PERFORMED A HFEC INDec 26, 2002 · N814AW · Airbus A319132 · Leading Edge DevicesSDR AWXA200200958Computer · failedFLT 0843 DURING CRUISE RECEIVED ECAM WARNING AP AUTOTHRUST YAW DAMPER 2 FAULT A/C "ALT LAW", DIVERTED TO ABQ. MAINTENANCE DOWNLOADED PREFLIGHT REPORT AND FOUND BOTH THE NR 2 AND 3 AIR DATA INERTIAL REFERENCE UNITS (ADIRU) FAILED. REMOVED AND REPLACED THE NR 3Sep 30, 2002 · N814AW · Airbus A319132 · Inertial Guidance SystemSDR AWXA200200912Power Supply · malfunctionedLAS - EEL - EMERGENCY POWER SUPPLY UNIT INDICATED LOAD MESSAGE ON FORWARD FLIGHT ATTENDANT PANEL AFTER EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED FORWARD LT EMERGENCY POWER SUPPLY UNIT (11WL) IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD.Sep 23, 2002 · N814AW · Airbus A319132 · Emergency LightingSDR AWXA200100615Sign · brokenPHX - EEL - C - EMERGENCY EXIT SIGN HOUSING AND LENS BROKEN AT L1 DOOR. MAINTENANCE REMOVED AND REPLACED L1 EMERGENCY EXIT SIGN HOUSING AND LENS IAW AMM 33-51-16-401A.Dec 4, 2001 · N814AW · Airbus A319132 · Emergency LightingSDR AWXA200100565Bearing · fracturedEN ROUTE ECAM MESSAGE FOR NR 1 ENG OIL FILTER CLOG APPEARED, FOLLOWED BY NR 1 ENG OIL PRESSURE RISE INTO THE RED AREA, NR 1 ENG HIGH VIBRATION & SMOKE IN THE CABIN. EXECUTED EMERGENCY DESCENT & LANDED AT MAF. MX REMOVED MAIN OIL FILTER & CHIP DETECTORS AND FNov 2, 2001 · N814AW · Airbus A319132 · Turbine Engine Compressor SectionSDR AWXA200100567Cylinder · failedMAF - EMERGENCY EVACUATION - FLT 786 -O- REFERENCE SDR AWXA200100565, DURING EMERGENCY EVACUATION THE R-1 DOOR DAMPER CYLINDER (POWER ASSIST) FAILED TO FULLY OPEN THE R-1 DOOR AND THE ESCAPE SLIDE FAILED TO DEPLOY. THE L-1 & L-2 DOORS WERE USED FOR EVACUATIONNov 2, 2001 · N814AW · Airbus A319132 · Passenger/Crew DoorsSDR AWXA200100449Circuit Board · faultyPHX - AIR TURNBACK - FLT 803 - C - DURING CLIMBOUT OF PHX TO SFO, THE NR 1 ENG FIRE LIGHT AT THE START SWITCH AND OVERHEAD INDICATION CAME ON TWICE, (NO ECAM INDICATION OR CRC). THE AIRCRAFT WAS RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE TROUBSep 18, 2001 · N814AW · Airbus A319132 · Fire Detection
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