N413SW

Service difficulty reports · 147

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 = 'N413SW' 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 SWIA200718111Seat Back · crackedPILOTS UPPER SEAT BACK PANEL IS CRACKED, DISCOVERED AT C-CHECK. REPLACED PILOTS UPPER SEAT BACK PANEL P/N 1B3003-5R PER SRM 51-42-13.Mar 16, 2007 · N413SW · Cndair CL6002B19 · Flight Compartment EquipmentSDR SWIA200718109Track · crackedRIGHT THRUST REVERSER INBOARD LOWER TRACK CRACKED AT STOP ATTACHMENT HOLE, DISCOVERED AT C-CHECK. REPLACED RIGHT THRUST REVERSER INBD LOWER TRACK P/N 228-50809-801 PER CRJ200 AMM 78-34-11-000-801.Mar 16, 2007 · N413SW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA200718108Track · crackedRIGHT THRUST REVERSER INBOARD UPPER TRACK CRACKED AT FORWARD STOP ATTACHMENT HOLE, DISCOVERED AT C-CHECK. REPLACED RIGHT THRUST REVERSER INBOARD UPPER TRACK P/N 228-50809-801 PER CRJ200 AMM 78-34-11-000-801.Mar 16, 2007 · N413SW · Cndair CL6002B19 · Engine Oil Indicating SystemSDR SWIA200718106Stringer Clip · crackedOUTBOARD CLIP AT FS280 RBL 9 IS CRACKED, DISCOVERED DURING C-CHECK. REPLACED DAMAGED OUTBOARD CLIP P/N 601R311011-57 AT FS280 RBL9 IAW CRJ200 SRM 51-42-21.Mar 16, 2007 · N413SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200718104Bracket · corrodedROLLER BRACKET ON AFT SIDE OF SERVICE DOOR HAS CORRODED HARDWARE, DISCOVERED ON C-CHECK. REPLACED HARDWARE ON SERVICE DOOR ROLLER BRACKET IAW CRJ200 AMM 20-21-00-910-801.Mar 16, 2007 · N413SW · Cndair CL6002B19 · Service DoorsSDR SWIA200718103Support Fitting · corrodedFORWARD AND AFT HINGE SUPPORT FITTING PINS ARE CORRODED ON LEFT EMERGENCY EXIT DOOR, DISCOVERED ON C-CHECK. REPLACED FORWARD AND AFT PINS ON EMERGENCY EXIT DOOR IAW CRJ200 AMM 20-24-00-910-801 PN MS20392-4C19.Mar 16, 2007 · N413SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA200616936Light · inoperativeTHE THIRD CEILING EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED THIRD CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.Jul 31, 2006 · N413SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200616292Windshield · crackedCAPT WINDSHIELD CRACKED. REPLACED CAPT'S WINDSHIELD PER MM 56-11-01.Feb 18, 2006 · N413SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200616180Control Unit · malfunctionedTHE "FLAPS HALFSPEED" MESSAGE WHEN RETRACTING FROM 45 TO 30 DEGREES. REPLACED FLAP ELECTORNIC CONTROL UNIT IAW CRJ 200 MM 27-51-05, OPERATIONAL CHECK GOOD.Jan 24, 2006 · N413SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200515995Pcu · malfunctionedDURING DESCENT, RIGHT SPOILER WOULD NOT FULLY DISPLAY CAUSING A ROLL TO THE LEFT. REPLACED RT FLIGHT SPOILERON OUTBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.Dec 9, 2005 · N413SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200515570Oxygen Mask · deployedO2 MASKS DROPPED (UNCOMMANDED). RESTOWED ALL O2 MASKS. NO DEFECTS NOTED OF PAX O2 SYSTEM. OPERATIONAL CHECK SYSTEM PER CRJ MM 35-20-00.Sep 18, 2005 · N413SW · Cndair CL6002B19 · Passenger Oxygen SystemSDR SWIA200515550Frame · crackedFRAME FLANGE CRACKED AT FS 605 STR 9L - BELOW STRINGER CRACK EMINATING FROM TOP FASTENER HOLE ABOVE & BELOW. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLANGE IAW CRJ REO 601R-53-61-1507.Aug 25, 2005 · N413SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200515549Frame · crackedFRAME FLANGE CRACKED AT FS 605 STR 9L ABOVE STRINGER FROM LOWER FASTENER HOLE TO EDGE OF FLANGE. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLANGE IAW CRJ REO 601R-53-61-1507.Aug 25, 2005 · N413SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200516195Attach Fitting · crackedAFT EQUIPMENT COMPARTMENT; INTERCOSTAL TO SKIN ATTACH CLIP IS CRACKED; FS 635.0; STR 12R, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-25-16, 51-42-21.Aug 24, 2005 · N413SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200516194Seat Track · corrodedFUSELAGE; FLOOR SEAT TRACK IS CORRODED; FS 559.00 + 40; RBL - 9.0, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SEAT TRACK FS 559.00 + 40; RBL - 9.0 IAW CRJ 200 AMM 53-01-11-400-802.Aug 24, 2005 · N413SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200514824Oxygen Mask · unwanted deployTHE O2 MASKS IN SEATS 1C AND D DEPLOYED AND WILL NOT STOW. REPLACED PSU AT 2C AND D. STOWED O2 MASKS AT 1C AND D. OPERATIONAL CHECK GOOD IAW 25-20-00.Apr 1, 2005 · N413SW · Cndair CL6002B19 · Passenger Compartment EquipmentSDR SWIA200514535Control Unit · out of rigAIRCRAFT REQUIRE'S LEFT RUDDER TRIM 1/2 WAY BETWEEN CENTER AND FIRST HASH MARK AND RIGHT AILERON TRIM 1/2 WAY BETWEEN CENTER AND FIRST HASH MARK. RE-RIGGED ALL FLAP IAW MM 27-53-05 AND RIGGED RIGHT AILERON PCU'S IAW CRJ MM 27-11-00. PERFORMED INFLIGHT FUNFeb 10, 2005 · N413SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200414333Trim Panel · faultyRUDDER TRIM FFOD TEST. REMOVED AND REPLACED RUDDER TRIM PANEL IAW CRJ MM 27-12-6, OPERATIONAL CHECK GOOD.Dec 30, 2004 · N413SW · Cndair CL6002B19 · Rudder Tab Control SystemSDR SWIA200414176Yoke · corrodedLEFT ENGINE FORWARD MOUNT YOKE CORROSION FOUND ON BEARING SURFACES. REMOVED AND REPLACED FORWARD LEFT ENGINE YOKE MOUNT ASSEMBLY REF 71-21-01.Nov 30, 2004 · N413SW · Cndair CL6002B19 · Engine Mount SectionSDR SWIA200414027Controller · malfunctionedATTEMPT APU START AIRBORNE, RECEIVED APU FIRE MESSAGE AND AURAL, THEN FIRE FAIL (APU). REMOVED AND REPLACED FIRE CONTROL UNIT IAW 26-00-00. OPERATIONAL CHECK GOOD.Oct 27, 2004 · N413SW · Cndair CL6002B19 · Fire DetectionSDR SWIA200414012Fire Warning · false activationON FINAL WHEN SWITCHING BLEEDS TO APU, APU FIRE WARNING FOLLOWED BY APU SHUTDOWN & APU FAULT CAUTION MESSAGE. ALSO NOTE DOOR INHIB - APU FIRE WARNING LASTED ONLY 2-3 SECONDS. COMPLIED WITH REINSPECT OF APU COMPARTMENT WITH NO DEFECTS NOTED. CLEARED FAULTS FOct 23, 2004 · N413SW · Cndair CL6002B19 · Fire DetectionSDR SWIA200413818Door · stuckMAIN CABIN DOOR WOULD NOT OPEN FROM BOTH INSIDE OR OUTSIDE. FREED DOOR UP, CYCLED OPEN & CLOSED, LOCKED & UNLOCKED. OPERATIONAL CHECK GOOD.Sep 19, 2004 · N413SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200413267Intercostal · wornRIGHT FIREWALL HYDRAULIC SHUTOFF VALVE SUPPORT INTERCOSTAL IS WORN AT AFT BULKHEAD FITTING FS 661 / ADJACENT STR 9.REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11 AND 51-42-06.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413266Floor Panel · corrodedRIGHT PRESSURE FLOOR HAS CORROSION AS MARKED AT FS 409+128 TO 559, RBL 36 TO RBL 48.REPAIRED IAW CRJ REO 601R-53-41-206 REV. NC.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA200413265Floor Panel · corrodedLEFT PRESSURE FLOOR HAS CORROSION AS MARKED AT FS 409+128 TO 559, LBL 36 TO LBL 48.REPAIRED IAW CRJ REO 601R-53-41-206 REV. NC.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA200413182Vertical Beam · crackedFUSELAGE LEFT VERTICAL BEAM LWR OUTBOARD FLANGE CRACKED AT FS 559 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-057 REV NC AND IAW RII53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413181Intercostal · crackedMAIN FUSELAGE PULLEY INTERCOSTAL CRACKED AT 2 LOCATIONS FS 484.00 RBL 27.0 AND RBL 36.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413180Fitting · crackedMAIN FUSELAGE FITTING CRACKED AT FS 460.00 RBL 9.0 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND RII 53 401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200413179Intercostal · crackedMAIN FUSELAGE PULLEY INTERCOSTAL CRACKED AT 2 LOCATIONS FS 484.00 LBL 27.0 AND LBL 36.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A REF RII 53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413178Structure · crackedMAIN FUSELAGE FITTING CRACKED AT FS 460.00 LB19 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND CONTINUATION SHEETS REF RII 53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413177Beam · crackedMAIN FUSELAGE; UPPER TRANSVERSE BEAM CRACKED AT FS 280.00 LBL 11.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-138 REV NC AND RII53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200413176Beam · crackedMAIN FUSELAGE; LOWER TRANSVERSE BEAM CRACKED AT FS 280.00 LBL 11.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV NC AND RII 53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200413175Receptacle · crackedSEVERAL CRACKS FOUND RADIATING FROM 115 VAC RECEPTACLE CUTOUT. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413174Stringer Clip · crackedNOSE HYDRAULIC COMPARTMENT AT FS 202.75 STR 21 CLIP IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CLIP (CLEAT) IAW CRJ SRM 53-11-19 FIG 1, SHEET 1.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200413173Floorbeam · crackedRIGHT ELECTRICAL BAY FLOOR AT FS 193, RBL 30 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-245 NC.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200413172Floorbeam · crackedLEFT ELECTRICAL BAY FLOOR AT FS 193, LBL 30 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-081 NC.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200413187Clip · crackedDISCOVERED DURING C-CHECK INSPECTION, CARGO PIT TRANSVERSE BEAM ATTACH CLIPS FOR CARGO DOOR STOP FITTINGS CRACKED AT FS 589.00 AND FS 605.00, LBL 42.0. ATTACH CLIPS REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-42-21, AMM 20-21-00 AND RII 53Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413186Beam · crackedDISCOVERED DURING C-CHECK INSPECTION, FUSELAGE LEFT VERTICAL BEAM LOWER INBOARD AND OUTBOARD FLANGE CRACKED AT 409 + 128 LBL 27. REPAIRED LT VERTICAL BEAM LWR IB FLANGE AT 409+120 LBL 27. REF. CRJ REO 601R-53-41-056 REV. NC, RII 53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413185Clip · crackedDISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE ATTACH CLIP CRACKED FS 280.00 RBL 9 OUTBOARD. REPLACED CLIP IAW CRJ REO 601R-53-11-171 REV. NC AND RII53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413184Beam · crackedDISCOVERED DURING C-CHECK INSPECTION, FUSELAGE LEFT VERTICAL BEAM LOWER OUTBOARD FLANGE CRACKED AT FS 409 + 128 LBL 18. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV. NC, RII53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413183Beam · crackedDISCOVERED DURING C-CHECK INSPECTION, FUSELAGE RIGHT VERTICAL BEAM LOWER INBOARD AND OUTBOARD FLANGE CRACKED AT FS 559 LBL 9. REPAIRED BEAMS IAW CRJ REO 601R-53-41-057 REV. NC AND IAW RII 53-401.Apr 13, 2004 · N413SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200412995Bushing · damagedELEVATOR SHUTTER DURING LEVEL FLIGHT AND INITIAL DESCENT AT APPROXIMATELY 290 KTS. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR OUTBOARD ACTUATOR TO CONTROL SURFACE BOLTS AND BUSHINGS IAW 27-33-01. INFLIGHT FUNCTIONAL CHECK OF ELEVATOR CONTROL SYSTEM GOOD.Mar 7, 2004 · N413SW · Cndair CL6002B19 · Elevator StructureSDR SWIA200412953Pcu · malfunctionedON TAXI-OUT, SPOILERON FAULT MESSAGE AND WHITE LT SPOILERON BOX. REPLACED LEFT INBOARD SPOILERON PCU WITH SERVICEABLE UNIT. LEAK, OPS CHECK GOOD. P/N: 27000-7, S/N OFF: 0590.Feb 25, 2004 · N413SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200312753Fire Bottle · dischargedAPU FIRE WARN IN FLIGHT. APU FIRE BOTTLE WAS FIRED. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE OR HEAT DAMAGE. REMOVED AND REPLACED THE APU FIRE BOTTLE ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. S/N OFF: 60810EL, P/N: 897776-01, S/N OFF: 01659.Dec 9, 2003 · N413SW · Cndair CL6002B19 · Fire Bottle, FixedSDR SWIA200312685Fire Warning · false indicationAPU FIRE WARN IN FLIGHT. COMPLIED WITH QRH. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE OR HEAT DAMAGE. REMOVED AND REPLACED THE APU FIRE BOTTLE ASSY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N: 897889, S/N OFF: 60810EL, P/N: 897776-01, S/N OFF: 01659Dec 8, 2003 · N413SW · Cndair CL6002B19 · Fire DetectionSDR SWIA200312197Seal · tornRIGHT AILERON IS UP INFLIGHT, REQUIRES 5 PERCENT LEFT RUDDER TRIM TO CENTER SLIP/SKID INDICATOR FOR STRAIGHT AND LEVEL FLIGHT. FOUND SEAL UNDER AILERON RT SIDE TO BE TORN. REPLACED TORN SEAL. OPS CHECKS GOOD.Jul 17, 2003 · N413SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA200311933Control Unit · malfunctionedEN ROUTE, STATUS MESSAGE OF FLT SPLRS FAULT AND IB GROUND SPLR FAULT UPON DEPLOYMENT. ON THE GROUND, RECEIVED A CAUTION MESSAGE OF GLD UNSAFE. ALL GLD'S DID DEPLOY ON LANDING. REMOVED AND REPLACED NR 2 SECU. OPS CHECK GOOD.May 2, 2003 · N413SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200311821Warning Light · illuminatedDURING DESCENT, APU WAS STARTED. AFTER APU SPOOL-UP DOOR-INHIBIT MESSAGE CAME ON. APU FIRE WAS DETECTED AND APU SHUT DOWN AUTOMATICALLY. APU BOTTLE LIGHT DID NOT ILLUMINATE AND WAS NOT DISCHARGED BY CREW. RESET APU ECU FAIL CODE. OPS CHECKED APU DOOR. OPFeb 28, 2003 · N413SW · Cndair CL6002B19 · APU ControlsSDR SWIA200311769Battery Pack · crackedFLOOR LEVEL EXIT ROW LIGHT AND FLOOR TRACK LIGHTS ARE INOP. FOUND BATTERY PACK #2 CRACKED. REMOVED AND REPLACED #2 ELBP AND #2 EMERGENCY LIGHTING INVERTER IAW MM 33-51-04 & 33-51-07. OPS CHECK GOOD.Feb 5, 2003 · N413SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200311763Connector · contaminatedLEFT EMERGENCY LIGHT (FORWARD LOWER) EXIT SIGN DOES NOT ILLUMINATE. CLEANED ELECTRICAL CONNECTOR ON LEFT EMERGENCY DOOR EXIT SIGN. OPS CHECK GOOD.Feb 4, 2003 · N413SW · Cndair CL6002B19 · Emergency Lighting
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