N818AW

Service difficulty reports · 267

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 = 'N818AW' 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 AWXA200600993Seat Track · corrodedMCN - DURING BC4 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON LT INBOARD SEAT TRACK AT FS 41. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW LT INBOARD SEAT TRACK AT FS 36 TO FS 41 IAW AIRBUS 319 SRM 51-72-11.May 25, 2006 · N818AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600992Seat Track · corrodedMCN - DURING BC4 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON LT OUTBOARD SEAT TRACK AT FS 41. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW LT OUTBOARD SEAT TRACK AT FS 36 TO FS 41 IAW AIRBUS 319 SRM 51-72-11.May 25, 2006 · N818AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600995Plate · crackedMCN - DURING BC4 CHECK DISCOVERED LT WING TO BODY FAIRING SUPPORT STRUCTURE LOSING PLATE CRACKED, .5 INCHES, AT FS 31. MAINTENANCE REMOVED AND REPLACED THE LT WING TO BODY SUPPORT CLOSING PLATE AT FS 31 IAW AIRBUS 319 SRM 51-72-11.May 24, 2006 · N818AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200600994Support Angle · crackedMCN - DURING BC4 CHECK DISCOVERED, THE LT WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT FS 31. MAINTENANCE REMOVED AND INSTALLED FABRICATED LT WING TO BODY FARING SUPPORT ANGLE AT FS 31 IAW AIRBUS 319 SRM 51-72-11.May 24, 2006 · N818AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200600443Connector · contaminatedCREW REPORTED THAT RT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT AND BATTERY IAW AWA TC A1C33302 & R1C33303. OPS CHECKS GOOD. CONFIRMED FAILURE. REMOVED CONNECTOR A3P3, CLEANED WATEMar 8, 2006 · N818AW · Airbus A319132 · Light System WiringSDR AWXA200600021Slide · malfunctionedTHE R1 DOOR WAS DEPLOYED DURING CLEANING SERVICE, THE SLIDE DID NOT FULLY DEPLOY. AIRCRAFT WAS FERRIED BACK TO PHX FOR REPAIR, R1 DOOR RESERVOIR BOTTLE WAS FOUND DEPLETED. MAINTENANCE REMOVED AND REPLACED THE R1 SLIDE. VENDOR TESTED THE UNIT AND WAS NOT ABLJan 6, 2006 · N818AW · Airbus A319132 · Escape SlideSDR AWXA200500910Battery · faultyPHX - EEL - DURING 4 DAY CHECK DISCOVERED EPSU COMM EMER L MESSAGE ON CIDS PANEL DURING FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY FROM THE FORWARD LEFT EMERGENCY PACK. OPERATIONAL CHECKS WERE GOOD.Aug 7, 2005 · N818AW · Airbus A319132 · Emergency LightingSDR AWXA200401397Battery · dischargedDURING THRU FLIGHT CHECK THE FORWARD LT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN FORWARD LT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Dec 14, 2004 · N818AW · Airbus A319132 · Emergency EquipmentSDR AWXA200400370Valve · malfunctionedAT FL 310 COULD NOT CONTROL CABIN PRESSURE, 250 FPM TO 10000, DESCENDED DOWN TO 12000 FT AND DIVERTED. PREVIOUS FLT A MEL WAS ISSUED FOR AFT CABIN TEMP & RT PACK FLOW CONTROL VALVE DE-ACTIVATED & LOCKED IN CLOSED POSITION. MEL ALSO REQUIRES FLOW SWITCH BE PLApr 15, 2004 · N818AW · Airbus A319132 · Cabin Pressure ControllerSDR AWXA200400312Bleed Valve · inoperativeEN ROUTE FROM PHX TO SFO AT FL 350 DURING MODERATE TURBULENCE ECAM INDICATED NR 2 ENG STALL & FLT ATTENDANT REPORTED HEARING A LOUD THUMP. PERFORMED FCOM 3 PROCEDURE, ENG OPS NORMAL, DID NOT DECLARE EMERGENCY. MAINT COMPLIED WITH AMM 72-22-49, EEC TEST & VISMar 27, 2004 · N818AW · Airbus A319132 · Compressor Bleed ValveSDR AWXA200301000Battery · dischargedFLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.Aug 28, 2003 · N818AW · Airbus A319132 · Emergency EquipmentSDR AWXA200300708Shear Pin · defectiveDURING 8-DAY CHECK FOUND THE R-1 DOOR ASSIST BOTTLE WOULD NOT HOLD PRESSURE. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR DAMPER CYLINDER SHEAR PIN AND PUNCTURE DISK IAW 52-11-14-401, OPERATIONAL CHECK WAS GOOD.Jun 18, 2003 · N818AW · Airbus A319132 · Passenger/Crew DoorsSDR AWXA200300711Packing · failedON APPROACH INTO PHX EN ROUTE FROM PHL RECEIVED GREEN HYDRAULIC SYSTEM LOW LEVEL INDICATION ON LIGHT PANEL. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE SERVICED 6 QUARTS IN GREEN HYDRAULIC SYSTEM AND INSPECTED AIRCRAFT FOR EVIDENCE OF HYDRJun 17, 2003 · N818AW · Airbus A319132 · Hydraulic Pump (Electric/Engine), MainSDR AWXA200300293Cartridge · contaminatedON DESCENT INTO PHX EN ROUTE FROM PHL AT APPROXIMATELY 12000 FT THE FLIGHT ATTENDANT AND PASSENGERS COMPLAINED OF A STRONG ODOR SIMILAR TO BURNING RUBBER. MAINTENANCE REMOVED AND REPLACED RECIRCULATION FILTER CARTRIDGE IAW AMM TASK 21-21-000-001. RAN BOTH ENGIMar 18, 2003 · N818AW · Airbus A319132 · Air Distribution SystemSDR AWXA200300204Anti-Ice System · inoperativeEN ROUTE FROM PIT TO PHX WING ANTI-ICE WENT INOPERATIVE AFTER NR 1 BLEED TRIP, DIVERTED TO CMH. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF WING ANTI-ICE SYSTEM PER AMM 30-11-00-05, ALL CHECKS WERE NORMAL.Feb 23, 2003 · N818AW · Airbus A319132 · Airfoil Anti/De-ice SystemSDR AWXA200201202Actuator · failedABORTED TAKEOFF, FLT 0045, REJECTED TAKEOFF AT APPROXIMATELY 50 KTS DUE TO NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE. MESSAGE FOLLOWED MOMENTARY SURGE OF NR1 EPR ABOVE FLEX THRUST TARGET. NO OTHER ANOMALIES NOTED, RETURNED TO GATE. REVIEWED THE LAST LOG REPODec 13, 2002 · N818AW · Airbus A319132 · Compressor Bleed ControlSDR AWXA0002166Engine · failedDEN - IN FLIGHT SHUTDOWN / UNSCHEDULED LANDING - FLT 534 - ORIG OPEN - EN ROUTE FROM PHX TO CLE THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND WENT TO IDLE, UPPER ECAM DISPLAYED ENG OIL FILTER (1) AND WAS SHUT DOWN. THE FLIGHT WAS DIVERTED TO DEN AND ON DAug 16, 2001 · N818AW · Airbus A319132 · Engine (Turbine/Turboprop)
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