N454AW

Service difficulty reports · 156

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 = 'N454AW' 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 A6WA200640001Bracket · bentGEARS UP DISAGREE CAS, AFTER TAKEOFF. MLG`S INDICATED UP AND LOCKED. NLG REMAINED DOWN. FOUND PROXIMITY SENSOR BRACKET BENT REMOVED AND REPLACED PROXIMITY SENSOR BRACKET IAW MM. REINSTALLED SENSOR TO WITHIN LIMITS IAW MM. PERFORMED GEAR SWING IAW MM. GEARJan 2, 2006 · N454AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540355Computer · failedRT AOA HEAT FAIL MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED ADHC NR 2 (AIR DATA HEAT CONTROLLER) IAW AMM. OPS TEST GOOD. (K)Dec 18, 2005 · N454AW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR A6WA200540220Duct · cloggedELECTRIC SMELL IN CABIN FROM ROW 9 AFT. FOUND CABIN FAN DUCT CLOGGED WITH DUST AND DEBRIS. CLEANED FAN AND DUCT ABOVE ROW 8. OPS CHECK GOOD. ALSO, FOUND BALLAST B130 ABOVE ROW 11 GROUND PIN IN CONNECTOR NOT SEATED CAUSING BALLAST INTERMITTENTLY FLICKERING.Jun 24, 2005 · N454AW · Cndair CL6002B19 · Air Distribution FanSDR A6WA200540170Bushing · migratedLEFT MLG FORWARD TRUNNION AFT BUSHING MIGRATED ON OUTBOARD EDGE .0015. INSTALLED NEW BUSHINGS, P/N 601R-57-21-003-41, IN FORWARD TRUNNION IAW BOMBARDIER, INC REO 601R-57-21-003-REV B. (M)May 15, 2005 · N454AW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR A6WA200540183Skin · dented2 DENTS RT SIDE AF FS409 + 32 BETWEEN STR 21R AND 22R. 3.5 INCHES LONG X 1.65 INCHES WIDE X 0.39 INCHES DEEP. 2.5 INCHES LONG X 1.5 INCHES WIDE X .022 INCHES DEEP. REPAIRED DAMAGE AT FS 409 +32 BETWEEN STR 21R AND 22R IAW SRM. (K)May 9, 2005 · N454AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200340148Flap · misriggedFLAP FAIL CAS MESSAGE AT ZERO FLAPS ON CLIMB, DECLARED EMERGENCY. RE-RIGGED, FLAPS. (M)Oct 20, 2003 · N454AW · Cndair CL6002B19 · Trailing Edge Flap Control System
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