N809AW
Service difficulty reports · 211
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 = 'N809AW' 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.
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 = 'N809AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AWXA200401013Coupling · corrodedDURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON LOWER SURFACE OF UPPER COUPLING (BEAM SPLICE) AT Y1292 RT, FORWARD OF FS 68. MAINTENANCE REMOVED CORRODED COUPLING AT Y1292 RT, FS 68; FABRICATED A NEW REPLACEMENT COUPLING; INSTALLED REPAIR PART IAW A319 SRMSDR AWXA200401006Seat Track · corrodedDURING BC-4 CHECK, CORROSION WAS FOUND ON DUMMY RAIL Y503 LT AT FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 LT AT FS 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG 9-12, PG. 23-28.SDR AWXA200401005Floorbeam · corrodedDURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y765 LT AT FS 66. MAINTENANCE REMOVED CORRODED BEAM Y765 LT AT FS 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11.SDR AWXA200401004Floorbeam · corrodedDURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 RT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11.SDR AWXA200400990Floor Panel · crackedDURING BC-4 CHECK A .5 INCH CRACK WAS FOUND IN AFT GALLEY FLOOR PANEL 262 EF. MAINTENANCE PERFORMED BOND REPAIR OF CRACKED FLOOR PANEL 262 EF IAW A319 SRM 53-02-00, FIG. 201, PG. 203-204, AND 206.SDR AWXA200401016Battery · dischargedDURING BC-4 CHECK, THE FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERIES WOULD NOT CHARGE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK OF FLASHLIGHT WAS GOOD.SDR AWXA200400404Servo · failedEN ROUTE AT FL 220, 340 KTS, FELT A VERY STRONG VIBRATION THROUGHOUT ENTIRE AIRFRAME, VIBRATION STRONGER IN REAR, SLOWED TO 240 KTS & VIBRATION WENT AWAY. REMAINDER OF FLT NORMAL, DID NOT EXCEED 290 KTS. MX PERFORMED ELEVATOR FREE PLAY CHECK IAW T/C 16C55304, SDR AWXA200300714Windshield · crackedAT CRUISE ALTITUDE EN ROUTE FROM BOS TO PHX THE FIRST OFFICERS WINDSHIELD CRACKED, DIVERTED TO CMH AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM 56-11-11-401. CENTRAL FAULT DISPLAY SYSTEM TEST OF WINSDR AWXA200300019Warning Light · false activationON CLIMB OUT AT FL 180 NR 2 ENGINE, NR 2 DISCHARGE LIGHT ILLUMINATED, NO OTHER INDICATIONS. DIVERTED TO MCI AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE AT MCI PLACED THE SYSTEM ON MEL, COND. 1, "ENG 2 AGENT 2 DISCHARGE LIGHT SYSTEM INOP", AND PERFORMED MAINTSDR AWXA200201018Battery · dischargedFLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200099Fmc · out of adjustBUR - ABORTED TAKEOFF - FLT 0536 - C - DURING TAKEOFF ROLL OUT OF BUR EN ROUTE TO PHX WHEN ADVANCING THROTTLE IN BLUE FLEX TEMPERATURE DROPPED OUT OF FMGC CAUSING THE MASTER CAUTION LIGHT TO ILLUMINATE AT APPROXIMATELY 40-50 KNOTS. TAKEOFF WAS ABORTED AND AIR
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