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.

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)Mar 2, 2009 · N459AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR 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)May 28, 2007 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 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)May 28, 2007 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 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)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740276Floorbeam · crackedRT FS 621.00 FLOOR ATTACHMENT SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR 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)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR 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)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 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)May 27, 2007 · N459AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 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 MMNov 15, 2006 · N459AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR 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 THIOct 24, 2005 · N459AW · Cndair CL6002B19 · Drag Control SystemSDR 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)Aug 16, 2005 · N459AW · Cndair CL6002B19 · Airspeed/Mach IndicatorSDR 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)Jul 19, 2005 · N459AW · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR 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)Jun 10, 2005 · N459AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR 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.Nov 22, 2004 · N459AW · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR 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.Nov 21, 2004 · N459AW · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR 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 BLJan 5, 2004 · N459AW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR 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 BLENDIJan 5, 2004 · N459AW · Cndair CL6002B19 · Turbine Engine Compressor Section
Back to N459AW