N463SW

Service difficulty reports · 233

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 = 'N463SW' 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 SWIA200617341Panel · crackedPAX DOOR AFT SIDE PANEL HAS CRACK AT CORNER BETWEEN STEP THREE AND FOUR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON AFT SIDE PANEL AT STEP 3, 4 AS PER REO 601R-52-11-1102.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Entrance StairsSDR SWIA200617340Floor Support · crackedLBL 10 STG 280 BELOW FORWARD WARDROBE FLOOR SUPPORT BEAM HAS CRACK COMING FROM RIVET, DISCOVERED DURING C-CHECK INSPECTION. SPLICE ANGLE INSTALLED IAW REO 601R-53-11-138NC.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617339Angle · crackedFS 484 RBL 27 AND RBL 36 ANGLES CRACKED AT BOTH ENDS OF PULLEY BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AT FS 484, RBL 27 AND RBL 36 IAW REO 601R-53-41-059 REV A.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617338Intercostal · crackedSTA 625STR 14 LT SIDE INTERCOSTAL CRACKED (CLIP), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP ON STA 625 AT STR 14 IAW CRJ 200 SRM REF 51-42-06 PG 11.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617337Intercostal · crackedSTA 625 RIGHT SIDE STR 14 INTERCOSTAL CRACKED (CLIP), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP ON RHS STR 14 STA 625 IAW CRJ 200 SRM REF 51-42-06 PG 11.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617336Angle · crackedPAX DOOR - ANGLE CRACKED UPPER OUTBOARD ANGLE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE PER CRJ 200 SRM 51-42-20 PG 23. OPERATIONAL CHECKS GOOD.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200617335Web · crackedPAX DOOR CRACK AT WEB BETWEEN TOP AND SECOND STEP FWD SIDE AT HANDRAIL SUPPORT FITTING, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, AND ANGLES PER REO 601R-52-11-702. OPERATIONAL CHECKS GOOD.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Entrance StairsSDR SWIA200617334Web · crackedPAX DOOR CRACK AT WEB BETWEEN TOP AND SECOND STEP AFT SIDE, AT HANDRAIL SUPPORT FITTING, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, AND ANGLES PER REO 601R-52-11-702. OPERATIONAL CHECKS GOOD.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Entrance StairsSDR SWIA200617333Handle · crackedPAX DOOR OUTER HANDLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SERVICEABLE PAX DOOR OUTER HANDLE IAW CRJ200 AMM 52-11-03-400-802. OPERATIONAL CHECKS GOOD.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200617332Bracket · crackedLBL 9 STA 280 OUTBOARD ANGLE BRACKET CRACKED AT TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT LBL 9 STA 280 OUTBOARD IAW REO 601R-53-11-138 NC.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617331Angle · crackedRBL 9 STA 280 INBOARD ANGLE CRACKED AT TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT RBL 9 STA 280 INBOARD IAW CRJ SRM 51-42-21.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617330Angle · crackedRBL 9 STA 280 OUTBOARD ANGLE CRACKED AT TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW CRJ 200 SRM 51-42-21.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200617329Bracket · crackedLBL 9 STA 280 INBD ANGLE BRACKET CRACKED AT TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW REO 601R-53-11-138 NC.Sep 9, 2006 · N463SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200616941Light · inoperativeFLOOR EMERGENCY LIGHTS FROM EMERGENCY EXIT TO LAV INOP. REPLACED AFT SECTION OF EMERGENCY LIGHT POWER STRIP. OPERATIONAL CHECKS GOOD, PN: 6464-5.Aug 6, 2006 · N463SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200616531Computer · malfunctionedON FINAL WHILE WINGS LEVEL, ON SPEED, FLAPS 45 DEGREES, RECEIVED STALL SHAKER. REPLACED EGPWS COMPUTER REF AMM 34-42-01. OPERATIONAL CHECK GOOD.Apr 6, 2006 · N463SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA200616370Window · crackedCAPT SIDE WINDOW CRACKED ON TAXI. REPLACED CAPTAINS SIDE WINDOW IAW AMM 56-12-01. P/N NP-139322-5; S/N OFF 0392H1080.Mar 6, 2006 · N463SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200515948Actuator · malfunctionedON FINAL SELECTED FLAPS 8 DEGREES. RECEIVED FLAPS FAIL MESSAGE. REPLACED FLAP ACTUATORS ON LT AND RT OUTBOARD FLAPS IAW 27-53-05. REPLACED FLEX SHAFT. REPLACED SKEW DETECTION UNIT IAW MM 27-51-15. OPERATIONAL CHECK GOOD.Dec 5, 2005 · N463SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR SWIA200515721Control Unit · malfunctionedA -STAB CH 1 STATUS MESSAGE-, AFTER TAKEOFF. REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW MM 27-41-01.Oct 23, 2005 · N463SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515527Trim Switch · inoperativeFO SIDE STAB TRIM INOP. REPLACED FO'S STAB TRIM SWITCH IAW 27-41-05. OPERATIONAL CHECK GOOD.Sep 7, 2005 · N463SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515334Lamp · burned out2ND AFT OVHD EMERGENCY LIGHT INOP. RELAMPED 2ND AFT OVHD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.Jul 29, 2005 · N463SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200515229Windshield · crackedCAPT SIDE WINDSHIELD CRACKED IN FLIGHT. REPLACED CAPT SIDE WINDSHIELD IAW MM 56-00-00 AND 56-11-01, PN NR-139321-5; SN OFF 03081H9374.Jul 4, 2005 · N463SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200514904Actuator · malfunctionedRECEIVED FLAPS FAIL CAUTION MSGS ON FINAL APPROACH. FAILED AT 41 DEGREES. REPLACED FLAP ACTUATORS R1, R2, R3, R4, L1, L2, L3, AND L4. OPERATIONAL CHECK GOOD AMM 27-53-01, AMM 27-53-05. P/N 852D100-19, S/N OFF 4982, 5039, 4609, 4941, P/N 853D100-20, S/N OFApr 24, 2005 · N463SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR SWIA200514925Connector · contaminatedFRONT SECTION OF EMERGENCY LIGHTING SYSTEM INOPERATIVE. CLEANED FORWARD EMERGENCY LIGHT STRIP CONNECTIONS OF WATER. OPERATIONAL CHECK GOOD.Apr 19, 2005 · N463SW · Cndair CL6002B19 · Light System WiringSDR SWIA200514758Detector · malfunctionedAFTER T/O, THE GEAR AND FLAP INDICATORS REMAINED ILLUMINATED ON ED1 FOR APPROX 20 MINUTES. GEAR AND FLAPS INDICATED NORMAL (UP & 0 DEGREES). REPLACED SKEW DETECTOR UNIT IAW MM 27-51-15, OPERATIONAL CHECK GOOD.Mar 22, 2005 · N463SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200514566Floorbeam · crackedFLOORBEAM ANGLE CRACKED AT FS 621.00 LBL 41.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV B.Feb 9, 2005 · N463SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200514565Floorbeam · crackedFLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RBL 41.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT IAW CRJ REO 601R-53-61-117.Feb 9, 2005 · N463SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200514564Frame · crackedTHREE SUPPORT CRACKS FOUND ON FRAME JUST AFT OF ELECTRONICS BAY DOOR, MARKED. ITEM FOUND AT C-CHECK INSPECTION. HFEC INSPECTION ON 3 SUSPECT CRACKS AS REQUESTED ON E & E BAY DOOR FRAME STRUCTURE, NO CRACKS FOUND. NDTM PT1 51-20-06.Feb 9, 2005 · N463SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200514563Floorbeam · crackedMAIN FUSELAGE FLOORBEAM AT RBL 9.0 HAS 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, 51-21-11, 51-25-16, 51-23-00Feb 9, 2005 · N463SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200414238Light · inoperative2ND OVERHEAD EMERGENCY FLOOD LIGHT AND AFT OF PAX DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.Dec 4, 2004 · N463SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200414129Unknown · unknownJUST AFTER TAKEOFF WITH FLAPS 20 AND TRIMS CENTERED THE AIRCRAFT ROLLS TO THE RIGHT. THIS HAPPENS IMMEDIATELY AFTER WEIGHT OFF WHEELS AND BECOMES LESS PRONOUNCED AFTER FLAP RETRACTION AND/OR INCREASE IN SPEED. SANDED ABRASION RESISTANT TEFLON FILM TO SPECIFINov 23, 2004 · N463SW · Cndair CL6002B19 · Aircraft StructuresSDR SWIA200414001Actuator · malfunctionedINTERMITTENT STAB TRIM CH 1 STATUS MESSAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. PN 4062-3 SN OFF 1102Oct 22, 2004 · N463SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413371Control Unit · malfunctionedGEAR/FLAP EICAS INDICATIONS CAME ON INTERMITTANTLY FROM TAKEOFF THROUGH CLIMBOUT. REMOVED AND REPLACED FECU IAW 27-51-05. OPS CHECK GOOD AT THIS TIME.May 31, 2004 · N463SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200412765Battery Pack · dischargedFIRST CABIN CEILING EMERGENCY LIGHT IS INOP. REPLACED NR 1 ELBP IAW 33-51-04, OPS CHECK GOOD.Jan 9, 2004 · N463SW · Cndair CL6002B19 · Emergency Lighting
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