N955SW

Service difficulty reports · 224

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 = 'N955SW' 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 SWIA200617304Intercostal · crackedSTA 625 INTERCOSTAL CRACKED AT LT SIDE AT STR 14 (CLIP) DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP AT STA 625 AT STRINGER 14 LT WITH NEW CLIP IAW CRJ200 SRM 51-42-21 PG 1-21.Aug 26, 2006 · N955SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617303Support Bracket · crackedPAX DOOR AFT SIDE CRACK AT AFT SIDE AT HANDRAIL SUPPORT BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND ANGLES IAW CRJ200 REO 601R-52-11-702.Aug 26, 2006 · N955SW · Cndair CL6002B19 · Entrance StairsSDR SWIA200617302Support Bracket · crackedPAX DOOR FWD SIDE HAS CRACK AT HANDRAIL SUPPORT BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS DOUBLER, ANGLES AND HANDRAIL SUPPORT BRACKET TO FWD SIDE PANEL ON PAX DOOR PER CRJ200 SRM 51-42-06 PG 11, 12, 13 AND 51-42-21 PG 17.Aug 26, 2006 · N955SW · Cndair CL6002B19 · Entrance StairsSDR SWIA200617301Structure · crackedSTA 621, LOWER LEFT CORNER ADJACENT TO AFT PRESSURE BULKHEAD IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE, REPAIR ANGLE AND STRAP ON STA 621 LWR LT IAW CRJ200 REO 601R-53-61-117 REV C.Aug 26, 2006 · N955SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617300Structure · crackedSTA 621 LOWER RIGHT CORNER ADJACENT TO PRESSURE (AFT) BULKHEAD IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AND STRAP ON LWR RT 621 IAW CRJ200 REO 601R-53-61-117 REV C.Aug 26, 2006 · N955SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617299Floor Support · crackedFS 280 RBL9 FLOOR SUPPORT BEAM CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR AT FS 280 RBL9 FLOOR SUPPORT BEAM PER REO 601R-53-11-10159.Aug 26, 2006 · N955SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617298Angle · cracked280 ANGLES CRACKED AT LBL9 INBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS AT LBL9 IAW CRJ200 SRM 51-42-06 PG 11 PARAGRAPH 9 AND RII53-911-1001.Aug 26, 2006 · N955SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200616795Windshield · crackedCAPTAIN'S WINDSHIELD SHATTERED DURING DESCENT AT APPROXIMATELY 28,000'. REPLACED CAPTAIN'S WINDSHIELD IAW CRJ 200 MM 56-00-00, 56-11-01, 56-12-01 AND RII 56-402. OPERATIONAL CHECKS GOOD, PN OFF: 601K33033-17, SN OFF: 03070H8328.Jun 23, 2006 · N955SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200616682Window · crackedCAPTAIN SIDE WINDOW SPLIT ON DESCENT. REPLACED CAPTAIN'S COCKPIT SIDE WINDOW IAW MM 56-00-00, 56-11-01 AND MM 56-12-01 AND RII 56-402, PN: NP-139322-11 SN OFF: 03084H9545.May 6, 2006 · N955SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200616633Beam · damagedDAMAGE TO BEAM ASSY AT LOCATION FS 529.0 CAUSED BY RIGHT MLG DOOR PUSH PULL ROD. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER IAW CRJ REO 601R-53-41-417 AND REO 601R-53-41-418.Apr 27, 2006 · N955SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200616583Bpsu · malfunctionedFLAPS FAIL MSG ON GROUND. REPLACED RIGHT BPSU PER CRJ MM 27-51-10. OPERATIONAL CHECK GOOD.Apr 17, 2006 · N955SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200616541Pcu · malfunctionedRIGHT FLIGHT SPOILER BOX GOES WHITE ALONG WITH FLIGHT SPOILERS. WHITE STATUS MESSAGE. REPLACED RIGHT FLIGHT SPOILER O/B PCU. OPERATIONAL CHECK GOOD.Apr 7, 2006 · N955SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200616059Control Unit · malfunctionedFLT SPLRS FAULT MESSAGE RECEIVED. REPLACED RT OB FLIGHT SPOILER PCU IAW MM 27-61-01. OPERATIONAL CHECK GOOD.Jan 1, 2006 · N955SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200515026Trim Switch · inoperativeCAPT STAB TRIM ONLY WORK IN THE NOSE DOWN, NOSE UP IT IS INOPERATIVE. REPLACED CAPTAINS STAB TRIM SWITCH AS REQUIRED IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD.May 21, 2005 · N955SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200514759Control Panel · malfunctionedAILERON TRIM WILL NOT GO LEFT; TRIM ONLY GOES RIGHT. REPLACED AILERON/RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD IAW 27-12-10 CRJ AMM.Mar 20, 2005 · N955SW · Cndair CL6002B19 · Aileron Tab Control SystemSDR SWIA200514578Floorbeam · crackedMAIN FUSELAGE FLOORBEAM AT RBL 9.0 ATTACH ANGLES CRACKED AT FS 280.00. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-23-00.Feb 2, 2005 · N955SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200514577Floorbeam · crackedMAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS OUTBOARD ATTACH ANGLE CRACKED AT FS 280.00. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00.Feb 2, 2005 · N955SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200514413Pcu · malfunctionedSPOILERONS FAULT STATUS MESSAGE COULD NOT CLEAR. REPLACED LEFT OUTBOARD SPOILERON (NR 3) PCU WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. ALL WORK PERFORMED IAW CRJ MM CH 27. P/N 27000-7, S/N OFF 6976.Jan 14, 2005 · N955SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200414161Detector · malfunctionedWHEN FLAPS 45 DEGREES SELECTED AIRPLANE ROLLS TO THE LEFT. FLAPS FAIL AND FLAPS DEGRADED MESSAGE. REMOVED AND REPLACED SKEW SENSOR ON RIGHT OUTBAORD FLAP OUTBOARD ACTUATOR IAW CRJ MM 27-51-15. OPERATIONAL CHECK GOOD. P/N 601R59014-1, S/N R431.Nov 19, 2004 · N955SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA200414086Actuator · lack of lubeFLAPS DEGRADED STATUS MESSAGE IN FLIGHT. LUBRICATED FLAP ACTUATORS IAW AMM 12-20-27. OPERATIONAL TEST OF SKEW DETECTION SYSTEM GOOD IAW AMM 27-51-15.Nov 4, 2004 · N955SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR SWIA200413982Detector · malfunctionedFLAPS DEGRADED WHEN FLAPS SELECTED TO TAKEOFF SETTING. FLAPS DEGRADED STATUS MESSAGE. REMOVED AND REPLACED SKEW DETECTION UNIT IAW CHAPTER 27-51-15 CRJ MM. OPERATIONAL CHECK GOOD.Oct 15, 2004 · N955SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200413477Control Unit · malfunctionedSTAB TRIM CHANNEL 1 INOP STATUS MESSAGE DISPLAYED. REPLACED HSTA AND MOTOR CONTROL UNIT (MCU). OPERATIONAL CHECK GOOD. P/N: 8396-3, S/N OFF: 1087.Jun 17, 2004 · N955SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413420Control Unit · malfunctionedSTAB TRIM CHANNEL 1 FAIL OFFLINE. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD.Jun 8, 2004 · N955SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200312730Power Supply · inoperativeAFT FACING AISLE OVERWING EXIT SIGN DOES NOT ILLUMINATE DURING EMERGENCY EXIT LIGHT TEST. REPLACED NR 3 BATTERY PACK. OPS CHECK GOOD.Dec 26, 2003 · N955SW · Cndair CL6002B19 · Emergency Lighting
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