N8665A

Service difficulty reports · 61

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 = 'N8665A' 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 REXA201000289Bulkhead · crackedCRACKED FS 559.00 BULKHEAD WEB REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB LAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B, DEVIATION "E".Dec 5, 2010 · N8665A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000276Receptacle · damagedTHE GROUND POWER UNIT (GPU) ACCESS POWER RECEPTACLE WAS DAMAGED. THE DAMAGE CONSISTS OF THE POWER RECEPTACLE BEING PULLED FROM THE INSTALLED POSITION IN THE RECESSED PAN AREA. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-280. REPEAT INSPECTIONS DAILY, FLYNov 22, 2010 · N8665A · Cndair CL6002B19 · External Power SystemSDR REXA200900083Ecu · failedFLAPS FAIL CAUTION MESSAGE AFTER START WITH ZERO DEGREE INDICATION. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I) PER AMOC DATED MARCH 27-2009 AND PA 27-052C. REMOVED FECU, CODES-51A REPLACED WITH SERVICEABLE FECAug 1, 2009 · N8665A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200900065Bulkhead · cracked3 CRACKS FOUND ON FWD PRESSURE BULKHEAD FS 202.75 AT BL 23.71 AT THE PARKING BRAKE CABLE CUT OUT DURING AN "A" CHECK INSPECTION. THE CRACKS MEASURES IN LENGTH .50 INCH AT THE 5:00 POSITION, .250 INCH AT 7:00 POSITION AND .625 INCH AT 11:00 POSITION. MAJOR REJun 11, 2009 · N8665A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2009F00028Engine · flamed outON APPROACH, ATC ISSUED DESCENT CLEARANCE TO 9000. BOTH THRUST LEVERS WERE REDUCED TO IDLE AT WHICH POINT THE FLIGHT CREW NOTICED A SEVERE YAW IN THE ACFT AND RT ENG OIL PRESSURE MASTER WARNING. ECIAS INDICATED A FLAMEOUT OF THE RT ENGINE. THE FLIGHT CREW DFeb 28, 2009 · N8665A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA200700036Flap System · unknownFLAPS FAIL ON APPROACH. RESET FLAPS AND PLACED ON 72 HOUR MONITORING PER AD 2006-12-21.Feb 4, 2007 · N8665A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200600089Computer · malfunctionedFLAP FAILURE MESSAGE. SYSTEM TROUBLESHOT DETERMINE TO BE THE SKEW DETECTION COMPUTER FAILURE. COMPUTER CHANGED PER BOMBARDIER AMM, OPERATIONAL CHECKED GOOD.Oct 8, 2006 · N8665A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200600080Flap System · failedFLAPS FAIL AT 0 DEGREES ON APPROACH. LANDING UNEVENTFUL. RESET SYSTEM AND PLACED ON 72 HOUR MONITORING PER AD 2006-12-21.Sep 3, 2006 · N8665A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200600081Fcu · failedFLAPS FAILED AT 8 DEGREES ON APPROACH. LANDING UNEVENTFUL. REMOVED AND REPLACED FECU PER BOMBARDIER AEROSPACE AIRCRAFT MAINTENANCE MANUAL. OPERATIONALLY CHECKS GOOD.Sep 3, 2006 · N8665A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200600011Pump · defectiveUPON CLIMBOUT WHEN SELECTING GEAR UP RECEIVED GEAR DISAGREE MESSAGE. QRH FOLLOWED, RETURNED TO MEM WITH UNEVENTFUL LANDING. MAINT FOUND NR 3 HYDRAULIC PUMP LOW PRESSURE, REMOVED AND REPLACED PUMP OPERATIONAL CHECK PER AMM.Feb 10, 2006 · N8665A · Cndair CL6002B19 · Hydraulic System, AuxiliarySDR REXA200500113Handle · corrodedDURING ROUTINE INSPECTION TASK, CREW ESCAPE HATCH OUTER HANDLE DID NOT EJECT WHEN OPENING ESCAPE HATCH WHEN UTILIZING INSIDE HANDLE. OUTER HANDLE IS RECESSED INTO HATCH FOR AERODYNAMIC PURPOSES. UPON INSPECTION, OUTER HANDLE WAS FOUND FROZEN IN PLACE (FLUSH)Sep 9, 2005 · N8665A · Cndair CL6002B19 · Emergency Exits
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