N965SW

Service difficulty reports · 165

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 = 'N965SW' 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 SWIA200617876Fitting · crackedFOUND CRACK IN INBOARD CLIP ON PRESSURE FLOOR SKIN AT FS 504.0 AND BL-27 RIGHT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PER STANDARD REPAIR 601R 53-0029B.Dec 25, 2006 · N965SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617875Fitting · crackedFOUND FS 280 LBL 9 1 CLIP ATTACHING TO FLOORBEAM CRACKED AND FLOOR SUPPORT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW LBL 9 CLIP PER REO 601R 53-0054A.Dec 25, 2006 · N965SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617874Floor Support · crackedFOUND FS 621 FLOOR SUPPORT ANGLE IS CRACKED AT LBL32, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AND STRAP AT FS 621 AS PER 601R-53-61-117 -1,-3 .Dec 25, 2006 · N965SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617873Fitting · crackedFOUND CRACK IN CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS624.0 AND STA 15R ON RIGHT SIDE OF FUS DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP ONTO REAR PRESSURE BULKHEAD AT FS 624 AND STA 15R ON RT PER REO 601R 53-64-985.Dec 25, 2006 · N965SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617392Windshield · crackedLEFT WINDSHIELD SHATTERED INFLIGHT. DIVERTED TO SLC. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01 AND RII 56-220-1000.Nov 16, 2006 · N965SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200516055Flutter Damper · leakingINTERMITTENT FLUTTER DAMPER STATUS MESSAGE. REPLACED RT AILERON FLUTTER DAMPER IAW MM 27-15-05. OPERATIONAL CHECK GOOD.Dec 29, 2005 · N965SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA200515685Trim Switch · malfunctionedCAPTAINS ELEVATOR TRIM SWITCH DOES NOT PITCH NOSE DOWN. REPLACED CAPT TRIM SWITCH REF, CRJ MM 27-41-05, OPERATIONAL CHECK GOOD.Oct 13, 2005 · N965SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515568Trim Panel · malfunctionedAILERON TRIM DOESN'T WORK TO THE RIGHT. REPLACED FLIGHT CONTROL TRIM SWITCH PANEL. OPERATIONAL CHECK GOOD.Sep 14, 2005 · N965SW · Cndair CL6002B19 · Aileron Tab Control SystemSDR SWIA200515368Windshield · failedOUTER LAYER OF CAPTAIN WINDSHIELD SHATTERED. REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-11-0.Jun 29, 2005 · N965SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200515166Floor Support · crackedRT FUSELAGE FLOOR SUPPORT ANGLE FS 621 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B" .May 28, 2005 · N965SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200515165Floorbeam · crackedFS 280 AT RBL 9.0 INBOARD AND OUTBOARD FLOORBEAM ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00 .May 28, 2005 · N965SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200515164Floorbeam · crackedFS 280 AT LBL 9.0 OUTBOARD FLOORBEAM ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00.May 28, 2005 · N965SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200414118Nut · looseF/O'S CONTROL YOKE CLICKS WHEN FULL DEFLECTION RIGHT OR LEFT AILERONS. RETORQUED NUT ON F/O'S YOKE AS REQUIRED, OPERATIONAL CHECKS GOOD.Nov 21, 2004 · N965SW · Cndair CL6002B19 · Control Column SectionSDR SWIA200413536Overheat Loop · malfunctionedMAIN LANDING GEAR OVERHEAT MESSAGE INFLIGHT. REPLACED LEFT MAIN LANDING GEAR BAY HARNESS OVERHEAT SENSOR LOOP. OPERATIONAL CHECK GOOD.Jul 3, 2004 · N965SW · Cndair CL6002B19 · Overheat DetectionSDR SWIA200412884Computer · malfunctionedYAW DAMPER (YD) 1 TRIPPED OFF IN CRUISE. RESET (REPEATEDLY), GOT PROGRESSIVELY WORSE DOWN TO 2 SECONDS BETWEEN RESETS AND FAILS. ASSOCIATED: AP TRIPS OFF WITH YD1, AI NR 1 BLANKS OUT AND MAG FLAG APPEARS WITH YD1. VSI NR 1 ERRONEOUS INDICATIONS - SHOWS UP Feb 10, 2004 · N965SW · Cndair CL6002B19 · Attitude and Direction Data System
Back to N965SW