N469AW

Service difficulty reports · 206

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 = 'N469AW' 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 A6WA200740484Switch · faultedIN FLIGHT STAB CHANNEL 1 DISENGAGED, ABLE TO REENGAGE NO PROBLEM DURING APPROACH BOTH STAB TRIM AND MACH TRIM FAILED, UNABLE TO REENGAGE. AIRCRAFT CONFIGURATION WAS AUTOPILOT OFF, FLAPS 20 AND TRIM 3.8 COMPLIED WITH QRH AND LANDED. FIRST OFFICERS STAB TRIM DIAug 29, 2007 · N469AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200740083Potentiometer · out of adjustFLAPS FAIL CAS MSG AT ZERO DEGREES, LANDING WEIGHT 40,000 LBS, TOUCHDOWN SPEED 160 KNOTS, MAX BRAKE TEMP = 6.0 FLAP LANDING PERFORMED RIG CHECK OF BPSU`S, IAW AMM 27-51-10, FOUND NR 6 AND NR 7 POTENTIOMETERS OUT OF ADJUSTMENT. ADJUSTED POTENTIOMETERS AND PERFeb 23, 2007 · N469AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640009Loop · failedDURING CLIMB (ANTI-ICE DUCT OVERHEAT) MESSAGE ILLUMINATED ALSO ON OVERHEAD PANEL WING (OVHT) CAPTION (ON) ON SYNOPTIC PAGE (ANTI-ICE) INDICATED FUSELAGE IN RED. REMOVAL AND REPLACED AFT LT LOOP IAW AMM ON W/O 92640 GROUND RAN AIRCRAFT, OPS CHECKED ANTI-ICE DUJan 17, 2006 · N469AW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR A6WA200540114Coalescer Bag · dirtySTRONG FUEL SMELL IN COCKPIT AT CRUISE. SMELL INCREASED WITH TEMP SELECTED IN MANUAL MODE. SELECTED LT PACK OFF, SMELL WENT AWAY. INSPECTED APU AREA, PACK NR 1 AND NR 2, NO LEAKS NOTED. NO EVIDENCE OF FUEL AROUND ENGINES OR APU. REAM ENGINE AND BOTH PACKSMar 20, 2005 · N469AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200440192Flap · malfunctionedFLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREE ON APPROACH. RESET FLAP SYSTEM IAW AWAC SUPPLEMENT 98-18. NO FURTHER DISCREPANCIES.Nov 17, 2004 · N469AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200440187Flap · stuckFLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREES ON APPROACH. RESET FLAPS SYSTEM IAW SUPPLEMENT 98-18, NO FURTHER DISCREPANCIES.Nov 17, 2004 · N469AW · Cndair CL6002B19 · Trailing Edge Flap Control System
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