N910SW

Service difficulty reports · 209

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 = 'N910SW' 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 SWIA2020090952416Seat Track · corrodedLT FLOOR SEAT TRACK CORRODED IN SEVERAL LOCATIONS BETWEEN FS 409.00+126.00 AND FS 559.00 ALONG LBL 9.00. C-CHECK RO 9/5/2020. REMOVED DAMAGED SEAT TRACKS AND INSTALLED NEW SERVICEABLE SEAT TRACKS, IAW CRJ 200 AMM. REFERENCE ATTACHED CHILD 21327708-1 FOR FABJul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020090952415Seat Track · corrodedRT FLOOR SEAT TRACK CORRODED IN SEVERAL LOCATIONS BETWEEN FS 409.00+126.00 AND FS 559.00 ALONG RBL 9.00. C-CHECK RO 9/5/2020. REMOVED UNSERVICEABLE RT FLOOR SEAT TRACK BETWEEN FS 409.00+126.00 AND FS 559.00 ALONG RBL 9.00 AND INSTALLED SERVICEABLE RT FLOOR SJul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020090952398Angle · crackedAFT EQUIPMENT BAY LEFT AND RIGHT FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. C-CHECK RO 9/5/2020. REMOVED AND REPLACED LEFT AND RIGHT FS 621 TO FS 625 OBLIQUE ANGLES, IAW CRJ 200 SRM.Jul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090952389Angle · corrodedFWD FACE OF FS 621 BULKHEAD ANGLE CORRODED BETWEEN LBL 27.0 AND RBL 27.00. C-CHECK RO 9/5/2020. REPAIRED FWD FACE OF FS 621 BULKHEAD, IAW REO AND CRJ 200 SRM. COMPLIED WITH FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.Jul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020090952374Stand Off · brokenAFT EQUIP BAY RT SIDE RIVETED STAND OFF CLIP HAS BROKEN FREE OF STRINGER. C-CHECK RO 9/5/2020. FOUND STRINGER TO BE DAMAGED AND IN NEED OF REPAIR. REPAIRED STRINGER 18R IAW CRJ 200 SRM. CUT OUT DAMAGE AND INSTALLED REPAIR PARTS AS DOCUMENTED ON ATTACHED COJul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090952372Strap · corrodedLT PRESSURE FLOOR STRAP CORRODED AT APPROX FS 559.00 AND BETWEEN LBL 36 AND LBL 45.00. C-CHECK RO 9/5/2020. REMOVED AND REPLACED LT PRESSURE FLOOR STRAP AT APPX FS559 BETWEEN LBL36 AND LBL 45, IAW CRJ200 SRM.Jul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090952368Seat Track · corrodedLT FLOOR SEAT TRACK CORRODED BETWEEN FS 559.00 TO FS 559.00+80 ALONG LBL 9.00. C-CHECK RO 9/5/2020. INSTALLED NEWLY FABRICATED SEAT TRACK (REFER TO CAMP 21326280), IAW CRJ 200 AMM.Jul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020090952366Fitting · crackedCOCKPIT WINDOW LT SIDE POST LOWER FITTING CRACKED AT WL 110.00. C-CHECK RO 9/5/2020. REMOVED LT SIDE POST LOWER FITTING AT WL 110.00. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE LT SIDE POST LOWER FITTING IAW SRM.Jul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020090952414Spring · corrodedRT OB FLAP HINGE BOXES SPRINGS AT WS 178.00, WS 220.00, AND WS 264.00 ARE CORRODED. C-CHECK RO 9/5/2020. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE HARDWARE ON HINGE BOX SPRINGS AT WS 178.00, 220.00, AND 264.00, IAW CRJ 200 AMM. PERFOMRED OPS TEST, OPSJul 18, 2020 · N910SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090952413Spring · corrodedLT OB FLAP HINGE BOXES SPRINGS AT WS 178.00, WS 220.00 AND 264.00 ARE CORRODED. C-CHECK RO 9/5/2020. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE HINGE BOX HARDWARE AT WS 178.00 AND 264.00, IAW CRJ 200 AMM. PERFORMED OPS TEST, OPS TEST GOOD. SEE ATTACHEJul 18, 2020 · N910SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090952412Frame · corrodedFRAME AT FS 409.00 CORRODED BETWEEN STGR 25L TO 26L. C-CHECK RO 9/5/2020. REMOVED CORROSION AT FRAME AT FS 409.00 BETWEEN STGR 25L TO 26L, IAW CRJ-200 SRM.Jul 15, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090952388Frame · corrodedFRAME AT FS 349.00 CORRODED BETWEEN STGR 26L TO 27L. C-CHECK RO 9/5/2020. REMOVED DAMAGED FRAME AT FS 349.00 AND INSTALLED A NEW FRAME, IAW CRJ 200 SRM AND DRAWING NUMBER FOR FASTENER CALL OUT AS DOCUMENTED ON ATTACHED CONTINUATION CARD. PRESSURIZATION AND Jul 15, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090952387Frame · corrodedFRAME AT FS 333.00 CORRODED BETWEEN STGR 25L TO 25R. C-CHECK RO 9/5/2020. INSTALLED NEW FRAME AT FS 333 BETWEEN STR 25L TO 25R, IAW CRJ 200 SRM AND DRAWING. COMPLIED WITH SKYWEST AND FORM M-337. PART FOR PART REPLACEMENT. WEIGHT AND BALANCE NOT AFFECTED.Jul 15, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090952386Frame Angle · corrodedFWD FRAME ANGLE AT FS 394.00 CORRODED BETWEEN STGR 25L TO 25R. C-CHECK RO 9/5/2020. INSTALLED NEW SERVICEABLE FWD FRAME ANGLE AT FS 394, IAW CRJ-200 SRM.Jul 15, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090952383Frame · corrodedFRAME AT FS 364.00 CORRODED BETWEEN STGR 25L TO 25R. C-CHECK RO 9/5/2020. REMOVED COMPONENTS AS REQUIRED FOR ACCESS, REMOVED DAMAGED LOWER FRAME SECTOR. INSTALLED A NEW LOWER FRAME SECTOR AND SAME SERVICEABLE SPLICE PLATES AT FS 364.00, IAW CRJ 200 SRM AND Jul 15, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090952382Frame · corrodedFRAME AT FS 319.70 CORRODED BETWEEN STGR 25L TO 25R. C-CHECK RO 9/5/2020. INSTALLED NEW FRAME AT FS 319.70 BETWEEN STR 25L TO 25R, IAW CRJ 200 SRM AND DRAWING. COMPLIED WITH SKYCARD AND FORM M-337. PART FOR PART REPLACEMENT. WEIGHT AND BALANCE NOT AFFECTEJul 15, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090952370Plate · corrodedDURING REMOVAL OF SERVICE DOOR PLATE ASSY FOUND CORROSION ON PLATE WHERE PLATE AND COIN MAT CONTRACTS THE PLATE. DOOR PLATE REQUIRES REPLACEMENT. C-CHECK RO 9/5/2020. REPLACED DOOR PLATE P/N 601R38957-31 AT SERVICE DOOR PLATE ASSY, IAW CRJ-200 SRM.Jul 13, 2020 · N910SW · Cndair CL6002B19 · Galley DoorsSDR SWIA2020090952411Nut · corrodedRT IB GROUND SPOILER MIDDLE AND OB HINGE NUTS ARE CORRODED. C-CHECK RO 9/5/2020. REPLACED NUTS ON IB GROUND SPOILER MIDDLE AND OUTBOARD HINGES WITH SERVICEABLE ONES, IAW CRJ 200 AMM. CALIBRATED TOOL USE TORQUE WRENCH ID WVACT1135, CAL DATE 16 MARCH 2020 DUEJul 12, 2020 · N910SW · Cndair CL6002B19 · SpoilersSDR SWIA2020090952410Nut · corrodedRT OB GROUND SPOILER 3 EA HINGE NUTS ARE CORRODED. C-CHECK RO 9/5/2020. RT OB GROUND SPOILER 3 EA HINGE NUTS REMOVED AND REPLACED, IAW CRJ 200 AMM.Jul 12, 2020 · N910SW · Cndair CL6002B19 · SpoilersSDR SWIA2020090952409Nut · corrodedRT FLIGHT SPOILER 4 EA HINGE NUTS AND 4 EA SAFETY BRACKET BOLTS ARE CORRODED. C-CHECK RO 9/5/2020. RT FLIGHT SPOILER 4 EA HINGE NUTS AND 4 EA SAFETY BRACKET BOLTS REPLACED, IAW CRJ 200 AMM.Jul 11, 2020 · N910SW · Cndair CL6002B19 · SpoilersSDR SWIA2020090952408Bolt · corrodedRT SPOILERON 4 EA HINGE NUTS AND 8 EA SAFETY BRACKET BOLTS ARE CORRODED. C-CHECK RO 9/5/2020. RT SPOILERON 4 EA HINGE NUTS AND 8 EA SAFETY BRACKET BOLTS REMOVED AND REPLACED, IAW CRJ 200 AMM.Jul 11, 2020 · N910SW · Cndair CL6002B19 · SpoilersSDR SWIA2020090952407Nut · corrodedLT IB GROUND SPOILER OB AND MIDDLE HINGE NUTS ARE CORRODED. C-CHECK RO 9/5/2020. LT IB GROUND SPOILER OB AND MIDDLE HINGE NUTS REMOVED AND REPLACED, IAW CRJ 200 AMM.Jul 11, 2020 · N910SW · Cndair CL6002B19 · SpoilersSDR SWIA2020090952406Nut · corrodedLT OB GROUND SPOILER ACTUATOR ROD END LOWER LINK NUT IS CORRODED. C-CHECK RO 9/5/2020. LT OB GROUND SPOILER ACTUATOR ROD END LOWER LINK NUT REMOVED AND REPLACED, IAW CRJ 200 AMM.Jul 11, 2020 · N910SW · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2020090952405Nut · corrodedLT OB GROUND SPOILER 3 EA HINGE NUTS ARE CORRODED. C-CHECK RO 9/5/2020. LT OB GROUND SPOILER 3 EA HINGE NUTS REMOVED AND REPLACED, IAW CRJ 200 AMM.Jul 11, 2020 · N910SW · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2020090952404Bolt · corrodedLT FLIGHT SPOILER IB AND OB HINGE NUTS AND 4 EA BRACKET BOLTS ARE CORRODED. C-CHECK RO 9/5/2020. LT FLIGHT SPOILER IB AND OB HINGE NUTS AND 4 EA SAFETY BRACKET BOLTS REMOVED AND REPLACED, IAW CRJ 200 AMM.Jul 11, 2020 · N910SW · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2020090952403Nut · corrodedLT SPOILERON 4 EA HINGE NUTS AND 4 EA SAFETY BRACKET BOLTS ARE CORRODED. C-CHECK RO 9/5/2020. LT SPOILERON 4 EA HINGE NUTS AND 4 EA SAFETY BRACKET BOLTS REMOVED AND REPLACED, IAW CRJ 200 AMM.Jul 11, 2020 · N910SW · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2020090952402Bolt · corrodedLT SPOILERON OB PCU LOWER MOUNTING HARDWARE IS CORRODED. C-CHECK RO 9/5/2020. REPLACED CORRODED HARDWARE WITH NEW ON THE LT OB PCU LOWER MOUNTING POINT, IAW CRJ200 AMM.Jul 11, 2020 · N910SW · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2020090952433Skin · corrodedRT INBOARD FLAP VANE LEADING EDGE INBOARD, MID, AND OUTBOARD DOUBLERS ARE CHAFED APPROX 1INL X .5INW X .015IND. C-CHECK RO 9/5/2020. REMOVED DAMAGED RT FLAP VANE LEADING EDGE SKINS, IAW CRJ 200 SRM, AS DOCUMENTED ON ATTACHED CONTINUATION CARD.Jul 10, 2020 · N910SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090952432Skin · chafedLT WING INBOARD FLAP VANE LEADING EDGE SKIN HAS CHAFES AT THREE LOCATIONS: FS 6.0 MEASURING L= 1.051"; W= .455"; D= .008". FS 54.5 MEASURING L= 1.136", W= .377", D= .013". FS 91.0 MEASURING L= 1.134", W= .360", D= .005". C-CHECK RO 9/5/2020. REPLACED 3 EACJul 9, 2020 · N910SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090952401Hinge Arm · corrodedLAV SERVICE DOOR (196AR) HINGES ARE CORRODED AND MISSING PAINT. C-CHECK RO 9/5/2020. REMOVED UNSERVICEABLE LAV SERVICE DOOR (196AR) HINGES AND INSTALLED SERVICABLE LAV SERVICE DOOR (196AR) HINGES, IAW CRJ-200 SRM.Jul 9, 2020 · N910SW · Cndair CL6002B19 · Fluid Service DoorsSDR SWIA2019111146739Connector · disconnectedGEAR DISAGREE WARNING MESSAGE ON TAKEOFF GEAR RETRACTION. HAD TO RUN QRH PROCEDURE AND PULL MANUAL GEAR EXTENSION HANDLE. RETURNED TO LAX. FLT# 5623 CLOSED FOUND ELEC CONNECTOR ON NLG DOOR SELECTOR VALVE DISCONNECTED. CONNECTED CONNECTOR AND INSURED LOCKINGNov 10, 2019 · N910SW · Cndair CL6002B19 · Landing Gear System WiringSDR SWIA2019103046631Flap System · malfunctionedFLAP FAIL CAUTION MESSAGE DURING APPROACH FLAPS DID NOT EXTEND BEYOND ZERO ON EICAS DISPLAY. FLAPS FAIL QRH PERFORMED AND COMPLIED WITH. FLAP FAIL CAUTION MESSAGE DURING APPROACH FLAPS DID NOT EXTEND BEYOND ZERO ON EICAS DISPLAY. FLAPS FAIL QRH PERFORMED AND COct 29, 2019 · N910SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA201744049Unknown · smokeSMOKE CARGO WARNING ANNUNCIATED 3 TIMES ON APPROACH. EMERGENCY DECLARED BOTH CARGO FIRE BOTTLES DISCHARGED. LANDED WITHOUT INCIDENT. SMOKE SMELL IN COCKPIT AFTER LANDING. ALL PASSENGER BAGS UNDAMAGED. NO DAMAGE TO AIRCRAFT NOTED AT THIS TIME. (FLT#5061) CLOSEDDec 8, 2017 · N910SW · Cndair CL6002B19 · Air Distribution SystemSDR SWIA201642525Structure · dentedDENT LOCATION NR 1 AT FS 680.5, STR 23L. REPAIRED DENT LOCATION NR 1 AT FS 680.50, STR 23L IAW SRM.Aug 9, 2016 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642524Skin · chafedRIGHT APRON CHAFED. R & R RT APRON SKIN IAW STS EA.Aug 3, 2016 · N910SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201642517Skin · gougedLEFT APRON SKIN HAS GOUGED DAMAGES CAUSED FROM P SEALS. REPAIRED THE LT APRON INSTALLING INTERNAL AND EXTERNAL DOUBLERS FROM FS530.0-FS559.0 IAW REO.Aug 3, 2016 · N910SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201642523Trunnion · crackedREPLACE THE LT TRUNNION DUE TO CRACKS. R & R THE LT MLG TRUNNION IAW RIL AND REO. FUEL LEAK CHECK PERFORMED WITH NO DEFECTS.Jul 31, 2016 · N910SW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR SWIA201642522Pressure Panel · crackedPRESSURE FLOOR CRACKED 2 PLACES, LOCATION IS APPROXIMATELY FS 461 BETWEEN BL 0 AND LBL 9. REPAIRED PRESSURE FLOOR AT CRACKED LOCATIONS BETWEEN FS 460.00 AND FS 461.00 AND BETWEEN BL 0.00 AND LBL 9.00 IAW REO. PRESSURE LEAK CHECK GOOD.Jul 30, 2016 · N910SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201642521Bulkhead · crackedFOUND CRACK AT AFT PRESSURE BULKHEAD FORWARD FACE RBL 27.50 APPROXIMATELY WL 108.64. PERFORMED REPAIR OF AFT PRESSURE BULKHEAD FORWARD FACE FS 621.00, RBL 27.50, APPROXIMATELY WL 108.64 IAW REO.Jul 30, 2016 · N910SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201642520Skin · crackedCRACK ON RT SIDE LOWER WING PLANK. COMPLIED WITH REPAIR OF RT LOWER WING PLANK IAW REO.Jul 29, 2016 · N910SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201642519Frame · corrodedRIGHT FS 605 FRAME JUST ABOVE THE FLOOR EDGE MEMBER, APPEARS TO BE CORRODED. REPAIRED IAW STS EA.Jul 29, 2016 · N910SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201642532Rib · crackedRIGHT MLG WHEEL WELL WS 53.60 HAS BATTERY ANGLE CRACK JUST ABOVE SOCKET CONTACTS OF MLG ELECTRICAL HARNESS. R & R RT BATTERY RIB ASSY AT WS 53.60 IAW SRM. LEAK CHECK GOOD.Jul 28, 2016 · N910SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA201642518Web · crackedAFT RT CORNER OTBD SIDE WEB ITS CRACK IN THE NOSE COMPARTMENT, TRU. COMPLIED WITH REPAIR OF AFT RT CORNER OTBD SIDE WEB, TRU FLOOR AT FS 193.00, IAW REO.Jul 28, 2016 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642531Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AFT CARGO DOOR. COMPLIED WITH REPAIR IAW STS EA AND SRM.Jul 27, 2016 · N910SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201642530Panel · chafedPANEL 699 AB ON RT WING IS CHAFED. REPLACED PANEL 699AB, PN 601R13031-156 IAW SRM.Jul 26, 2016 · N910SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201642529Panel · chafedRIGHT WING PANEL 692 BB IS CHAFED. R & R L/E GUIDE PLATE WITH NEW SERVICABLE PART IAW SRM.Jul 26, 2016 · N910SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201642528Structure · dentedDENT FORWARD OF FS 621 AND BELOW WL 79.50. PERFORMED PERMANENT REPAIR IAW STS EA.Jul 25, 2016 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642527Skin · dentedDENT ON LT OTBD FLAP UPPER SURFACE. COMPLIED WITH PERMANENT REPAIR IAW STS EA.Jul 25, 2016 · N910SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642526Spoiler · dentedDENT ON LT OTBD GROUND SPOILER. COMPLIED WITH PERMANENT REPAIR IAW STS EA.Jul 25, 2016 · N910SW · Cndair CL6002B19 · SpoilersSDR SWIA201438936Skin · chafedLT INBD FLAP VANE L/E SKIN CHAFED AT INBD END. C-CHECK, COMPLIED WITH REPAIR OF CHAFE ON LT INBD FLAP VANE SKIN L/E AT INBD END IAW REO.Jul 14, 2014 · N910SW · Cndair CL6002B19 · Trailing Edge Flaps
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