N919SW

Service difficulty reports · 166

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 = 'N919SW' 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 SWIA200515155Fitting · crackedFS 460 RT FLOOR RBL 9.0 OUTBOARD FITTING CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06 & 51-42-21.Jun 4, 2005 · N919SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200515154Clip · crackedFS 280 LEFT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH CLIPS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00.Jun 4, 2005 · N919SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200515153Clip · crackedFS 280 RT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 & 51-23-00.Jun 4, 2005 · N919SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200515080Bpsu · malfunctionedFLAPS FAIL IN 20 DEGREE POSITION UPON TAKEOFF. RIGGED LEFT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD.May 24, 2005 · N919SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200514642Control Unit · malfunctionedSELECTED FLAPS TO 8 DEGREES, THEN FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED FECU IAW CRJ 200 MM CHAPTER 27-51-05, OPERATIONAL CHECK GOOD.Feb 24, 2005 · N919SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200514646Sensor · malfunctioned"FLAPS FAIL" MSG WHEN SELECTING FLAPS OUT OF 0 DEGREES. REMOVED AND REPLACED RIGHT BPSU IAW CRJ27-51-10, OPERATIONAL CHECK GOOD.Feb 23, 2005 · N919SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200514486Lamp · burned outEMERGENCY LIGHT CEILING AT ROW 5 INOPERATIVE. REPLACED LAMP IAW AMM 33-51-16. OPERATIONAL CHECK GOOD.Jan 30, 2005 · N919SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200414315Ecu · malfunctionedSPOILERON FAULT STATUS MSG ON ED2 DURING TAXI OUT. REPLACED SECU NR 2 IAW 27-60-00. REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-61-00, OPERATIONAL CHECK GOOD.Dec 23, 2004 · N919SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200414300Control Unit · malfunctionedON TAXI OUT FLIGHT SPOILER STATUS MESSAGE. REPLACED NR 1 AND NR 2 SECU IAW AMM 27-60-00, REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-61-00. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF 01533, P/N 49-164-06, S/N OFF 01598, P/N 27000-7, S/N OFF 5494.Dec 23, 2004 · N919SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413408Bulb · burned outRIGHT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EXTERIOR EMERGENCY LIGHT BULB, OPERATIONAL CHECK GOOD.Jun 5, 2004 · N919SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200413060Switch · failedSTAB CHANNEL NR 2 WILL NOT ENGAGE. REPLACED STAB DISCONNECT SWITCH ON F/O'S YOKE. REPLACED HSTCU. OPS CHECKS GOOD IAW MM 27-41-00. S/N OFF: 1384.Mar 18, 2004 · N919SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413018Sensor · malfunctionedWHILE ON APPROACH TO DEN LEFT JETPIPE OVERHEAT WARNING CAME ON. SHUTDOWN LEFT ENGINE AS PER THE QRH. REMOVED AND REPLACED LEFT ENGINE JETPIPE OVERHEAT SENSING ELEMENTS ON BOTH A AND B SYSTEMS IAW CRJ MM ATA CHPT 26-11-00 AND 26-11-01. P/N: 26212000.Mar 7, 2004 · N919SW · Cndair CL6002B19 · Overheat DetectionSDR SWIA200412954Control Unit · malfunctionedSTAB CHANNEL 1 WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW CL600 MM 27-41-01, OPS CHECK GOOD.Feb 29, 2004 · N919SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200412852Attach Angle · crackedDURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS OUTBOARD ATTACH ANGLE CRACKED AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM.Feb 3, 2004 · N919SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200412851Attach Angle · crackedDURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT RBL 9.0 HAS INBOARD AND OUTBOARD ATTACH ANGLES CRACKED AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM.Feb 3, 2004 · N919SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200412850Attach Angle · crackedDURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS A CRACKED INBOARD ATTACH ANGLE AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM.Feb 3, 2004 · N919SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
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