N459AW
Service difficulty reports · 217
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 = 'N459AW' 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 = 'N459AW' 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 A6WA200940116Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT FS 621.00 AFT LINTEL FITTING AREA. AFT PRESSURE BULKHEAD AT FS 621.00 AT LINTEL FITTING AREA REPAIRED IAW REO 601R-53-61-1230, REV D. (K)SDR A6WA200740279Angle · crackedLT 625, OBLIQUE ANGLE IS CRACKED APPROX 1 INCH LONG. (K) [07-12-07] MAINATENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-06. (K)SDR A6WA200740278Angle · crackedRT 625, OBLIQUE ANGLE IS CRACKED APPROX 1 INCH LONG. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-06. (K)SDR A6WA200740277Floorbeam · crackedLT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW REO 601R-53-61-117, REV C. (K)SDR A6WA200740276Floorbeam · crackedRT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K)SDR A6WA200740275Floorbeam · crackedRT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW REO 601R-53-61-117 REV C. (K)SDR A6WA200740274Angle · crackedRT 484 ANGLE IS CRACKED AT RBL 27 APPROX .2500 INCH LONG. (K) [07-12-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW REO 601R-53-41-059, REV A AND BSC STANDARD REPAIR 601R-53-0029B. (K)SDR A6WA200740273Angle · crackedLT 484 ANGLE IS CRACKED AT LBL 36 AND LBL 27 APPROX .2500 INCH LONG. (K) [07-12-07] MAINTENANCE REPAIRED LT 484 ANGLE AT LBL 36 AND 27 IAW REO 601R-53-41-059 REV A, STANDARD REPAIR 601R-53-0029B AND STANDARD REPAIR 601R-53-0030A. (K)SDR ATWA200640386Carbon Seal · leakingON CLIMBOUT, ENGINE NR 1 LOW OIL PRESSURE WARNING, AT FLIGHT IDLE OIL PRESSURE AT 45 PSI. TEMP 84. AIRCRAFT DIVERTED. DURING CONSUMPTION TEST, FOUND ENGINE NR 1 AXIS F HYDRAULIC PUMP CARBON SEAL LEAKING. REPLACED AXIS (F) CARBON SEAL AND MATING RING IAW MMSDR A6WA200540315Ecu · faultyIN LEVEL FLIGHT AT 240, RECEIVED SPOILERON FAULT, ALSO RECEIVED ROLLING MOVEMENT 5-8 DEGREES TO THE RT. AIRCRAFT RETURNED TO NORMAL FLIGHT CHARACTERISTICS, SPOILERON FAULT EXTINGUISHED ON GROUND. REMOVED AND REPLACED SECU NR 2 IAW AMM, OPS CHECCK GOOD AT THISDR A6WA200540284Indicator · inoperativeTAKEOFF ABORTED DUE TO STANDBY AIRSPEED INDICATION READING ZERO AT 80 KNOTS. TAKEOFF ABORTED AT 90 KNOTS, BRAKE TEMPS 8,8,6,5, NORMAL BRAKING. REMOVED AND REPLACED STANDBY AIRSPEED INDICATOR. (K)SDR A6WA200540259Sensor · inoperativeRT FUEL HIGH LEVEL SENSOR INOPERATIVE PLACARD AND PLACED ON MEL. CODE ON COMPUTER SHOWS 140 (LT TANK HIGH LEVEL SENSOR). REMOVED AND REPLACED RT FUEL LEVEL SENSOR IAW AMM. OPS AND LEAK CHECK GOOD. (K)SDR A6WA200540194Skin · dentedREPAIR DENT IN FUSELAGE SKIN AT FS 409 TO FS 409+16 BETWEEN STR 13L AND STR 15L. PERFORMED EXTERNAL FLUSH PERMANENT REPAIR IN FUSELAGE SKIN AT FS 409 TO FS 409+16 BETWEEN STR 13L AND STR 15L IAW SRM. (K)SDR A6WA200440190Outflow Valve · stuckREF LOG PG 124783, BLOCK 1, ON CLIMB-OUT, RECEIVED (CABIN ALT) MESSAGE AT 10K FEET. COMPLIED WITH QRH. FOUND PRIMARY OUTFLOW VALVE STUCK IN OPEN POSITION. REPLACED PRIMARY VALVE IAW AMM 21-32-01. OPS CHECK COMPLIED WITH. AUTO OK, MANUAL FAILED.SDR A6WA20040191Outflow Valve · failedREF LOG 124783, BLOCK 1, ON CLIMB-OUT, RECEIVED (CABIN ALT) MESSAGE. COMPLIED WITH QRH. REPLACED SECONDARY OUTFLOW VALVE IAW AMM 21-32-01. OPS CHECK COMPLIED WITH, AUTO AND MANUAL CHECK GOOD AT THIS TIME.SDR A6WA2003400ZZBlade · nickedAFTER TAKEOFF, RIGHT ENGINE VIBRATION WENT TO 3.9, FELT AIRFRAME VIBRATION, WITH THRUST REDUCED VIBRATION INDICATION REDUCED TO GREEN RANGE. AIR RETURN, INSPECTED FAN IAW 72-20-00. BLENDED NICKS FROM SEVERAL BLADES IAW AMM TASK 72-20-00-300-801, ALL MINOR BLSDR A6WA200440002Blade · nickedAFTER TAKEOFF RT ENGINE VIBRATION WENT TO 3.9, FLET AIRFRAME VIBRATION, WITH THRUST REDUCED VIBRATION INDICATION REDUCED TO GREEN RANGE. AIR RETURN, INSPECTED FAN IAW 72-20-00. BLENDED NICKS FROM SEVERAL BLADES IAW AMM TASK 72-20-00-300-801, ALL MINOR BLENDI
Back to N459AW