N959SW

Service difficulty reports · 196

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 = 'N959SW' 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 SWIA2025122075834Floor Support · corrodedCORROSION NOTED ON FLOOR SUPPORT CAP AT RBL 27 BETWEEN BS 609- 621. BLENDED OUT AND REPAIRED CORROSION ON FLOOR SUPPORT CAP AT RBL 27 BETWEEN FS609-FS621 REF SRM 51-21-06 AND REO 601R-53-61-8457 REV-.Dec 20, 2025 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025121975857Mount · crackedAPU DOOR LINEAR ACTUATOR MOUNTING STRUCTURE CRACKED. REMOVED AND REPLACED THE APU DOOR LINEAR ACTUATOR SUPPORT, REF SRM 51-42-06-00 AND DWG 601R35210 REV -M. COMPLIED WITH TASK CARD 51-900-1003-SKY,Dec 19, 2025 · N959SW · Cndair CL6002B19 · Auxiliary Power Unit (APU) DoorsSDR SWIA2025121175858Skin · dentedFWD FUSELAGE JUST FWD OF GPU RECEPTICLE DOOR FS 187.25 4 INCHES BELOW ADG CUTOUT SMALL CIRCULAR DENT 0.5 IN. IN DIAMETER 0.012 IN. DEEP. PERFORMED CUT-AWAY OF DAMAGED SECTION, FABRICATED FUSELAGE SKIN REPAIR DOUBLER -1 AND WET INSTALLED REPAIR DOUBLER AT FWDDec 11, 2025 · N959SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2025112575841Trunnion · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA26772-601R-57-21-2287 959SW-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 267723 EA. FASTENER HOLES WERE FOUND CRACKED ON R/H MLG TRUNNION. REPAIRED REF REO 601R-57-21-2287. TRUNNION FITTING LIFE LIMIT/DISCARD TIME DUE Nov 25, 2025 · N959SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWIA2025072300013Engine · warning messageENGINE WARNING MESSAGE ON CLIMB OUT. INTERMITTENT DURING DESCENT AND BACK ON DURING FINAL APPROACH. NOT ON DURING TAXI, (FLIGHT 5099) VERIFIED WITH PILOTS AND WAS LOW OIL PRESSURE ON RT ENG. REPLACED EDP CARBON SEAL. REF CP 30480407 FOR REPLACEMENT OF ATSJul 13, 2025 · N959SW · Cndair CL6002B19 · Engine Oil System (Airframe Furnished)SDR SWIA2025071400013Engine · warning messageENGINE WARNING MESSAGE ON CLIMB OUT. INTERMITTENT DURING DESCENT AND BACK ON DURING FINAL APPROACH. NOT ON DURING TAXI, (FLIGHT 5099 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSJul 13, 2025 · N959SW · Cndair CL6002B19 · Central WarningSDR SWIA20250613009Wire Harness · damagedNOSE DOOR AND GEAR DISAGREE WARNING ON TAKE OFF. (FLIGHT 5568 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30286107 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT NOSE DOOR AND GEAR DISAGREE WARNING ON TAKE OFF IN REFRENCE TO CRJ 200 FIM 3Jun 9, 2025 · N959SW · Cndair CL6002B19 · Landing Gear System WiringSDR SWIA202506050003Landing Gear · warning messageGEAR UP DISAGREE ON TAKEOFF, NOSE WHEEL INDICATED RED. MESSAGE WENT AWAY AT ABOUT 1300 FT AFTER TAKEOFF. (FLIGHT 5127 - FILED CLOSED)UPON ARRIVAL, TROUBLESHOT GEAR DISAGREE REF CRJ-200 FIM 32-60-09. INTERROGATED PSEU AND FOUND CODES S22 FAR, S31 FAR, S32 FAR,Jun 3, 2025 · N959SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA20250428004Skin · damagedFASTENER HOLE DAMAGED/ELONGATED (ORIGINAL FASTENER NAS1581F3R9) THROUGH STACK UP AT APPROX. RH WS 75.27 WING SKIN AND INBD T/E EDGE MEMBER 601R10225-14 MEMBER - SECOND SCREW HOLE INBOARD OF FLAP ACTUATOR. (FILED CLOSED)COMPLIED WITH REO 601R-57-51-1067 REV -- Apr 24, 2025 · N959SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA20250311028Skin · crackedLH LOWER WING PLANK HAS LONGITUDINAL CRACK WITH AN INDICATION OVER FULL SCREEN HEIGHT, APPROX. WS. 47.61 FROM TRAILING EDGE OF WING PLANK, APPROX. 2.4€? LONG. (FILED CLOSED) COMPLIED WITH TEMPORARY REPAIR OF LH LOWER WING PLANK APPROX WS 47.61 FROM TRAIMar 28, 2024 · N959SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA20250110328Skin · crackedLH LOWER WING PLANK HAS LONGITUDINAL CRACK WITH AN INDICATION OVER FULL SCREEN HEIGHT, APPROX. WS. 47.61 FROM TRAILING EDGE OF WING PLANK, APPROX. 2.4€? LONG. (FILED OPEN) COMPLIED WITH TEMPORARY REPAIR OF LH LOWER WING PLANK APPROX WS 47.61 FROM TRAILIMar 28, 2024 · N959SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWI2025F00314Skin · crackedRH LOWER WING PLANK HAS LONGITUDINAL CRACK WITH AN INDICATION OVER FULL SCREEN HEIGHT, APPROX. WS. 47.61 EMANATING FROM FIRST RIVET ROW CLOSEST TO TRAILING EDGE, APPROX. .75€? LONG, FROM THE TRAILING EDGE OF THE RIVET TO TRAILING EDGE OF WING PLANK. (FILEDMar 27, 2024 · N959SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202503110027Frame · chafedCHAFE DAMAGE ON INNER FRAME FLANGE AT FS 718.00 BETWEEN STR 16L - STR 17L. (FILED CLOSED) REPAIRED CHAFE DAMAGE ON INNER FRAME FLANGE AT FS 718.00 BETWEEN STR 16L - STR 17L IN REF TO REO 601R-53-61-8179, REV--, DATED 2024-03-30. COMPLETED TASK CARD 51-90Mar 27, 2024 · N959SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA20250110047Skin · crackedRH LOWER WING PLANK HAS LONGITUDINAL CRACK WITH AN INDICATION OVER FULL SCREEN HEIGHT, APPROX. WS. 47.61 EMANATING FROM FIRST RIVET ROW CLOSEST TO TRAILING EDGE, APPROX. .75€? LONG, FROM THE TRAILING EDGE OF THE RIVET TO TRAILING EDGE OF WING PLANK. (FILEDMar 27, 2024 · N959SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2025011040327Frame · chafedCHAFE DAMAGE ON INNER FRAME FLANGE AT FS 718.00 BETWEEN STR 16L - STR 17L. (FILED OPEN) REPAIRED CHAFE DAMAGE ON INNER FRAME FLANGE AT FS 718.00 BETWEEN STR 16L - STR 17L IN REF TO REO 601R-53-61-8179, REV--, DATED 2024-03-30. COMPLETED TASK CARD 51-900-Mar 27, 2024 · N959SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202503110021Intercostal · crackedAFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R, INTERCOSTAL CRACKED. (FILED CLOSED) REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R IN REF TO SRM 51-42-21. COMMar 21, 2024 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202501100046Intercostal · crackedAFT SIDE OF FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 15L, INTERCOSTAL CRACKED. (FILED OPEN) REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 15L IN REFE TO SRM 51-42-21. COMMar 21, 2024 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20250110321Intercostal · crackedAFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R, INTERCOSTAL CRACKED. (FILED OPEN) REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R IN REF TO SRM 51-42-21. COMPLMar 21, 2024 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20203110020Bracket · gougedAFT PRESSURE BULKHEAD FS.621.00 FWD FACE HAS SEVERAL GOUGES LOCATED APPROX. AT WL 93.00 AND LBL27.50, LBL 18.00, LBL 9.50, RBL 9.50, RBL 18.00, RBL 27.50, RBL 36.20 AND WL 87.00 AT LBL 9.50. (FILED CLOSED) BLENDED 8 GOUGES, REPLCAED 6 GOUGED RIVETS, REPLMar 20, 2024 · N959SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2025011040320Bracket · gougedAFT PRESSURE BULKHEAD FS.621.00 FWD FACE HAS SEVERAL GOUGES LOCATED APPROX. AT WL 93.00 AND LBL27.50, LBL 18.00, LBL 9.50, RBL 9.50, RBL 18.00, RBL 27.50, RBL 36.20 AND WL 87.00 AT LBL 9.50. (FILED OPEN) BLENDED 8 GOUGES, REPLCAED 6 GOUGED RIVETS, REPLACMar 20, 2024 · N959SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWI2025F00313Nut Plate · corrodedCORROSION AROUND NUTPLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 449.85 (FILED CLOSED) REMOVED CORROSION AROUND NUT PLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 449.85 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT Mar 18, 2024 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2025F00312Nut Plate · corrodedCORROSION AROUND NUTPLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 473.15 (FILED CLOSED) REMOVED CORROSION AROUND NUT PLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 473.15 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT Mar 18, 2024 · N959SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202503110018Nut Plate · corrodedCORROSION AROUND NUT PLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 559.00 (FILED CLOSED) REMOVED CORROSION AROUND NUT PLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 559.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENTMar 18, 2024 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202501100045Floor Support · corrodedCORROSION AROUND NUTPLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 449.85 (FILED OPEN) REMOVED CORROSION AROUND NUT PLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 449.85 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WIMar 18, 2024 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025011044Floor Support · corrodedCORROSION AROUND NUTPLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 473.15 (FILED OPEN) REMOVED CORROSION AROUND NUT PLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 473.15 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WIMar 18, 2024 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20250110318Floor Support · corrodedCORROSION AROUND NUT PLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 559.00 (FILED OPEN) REMOVED CORROSION AROUND NUT PLATE ON PRESSURE FLOOR SILL AT LBL 45.00 AND FS 559.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WMar 18, 2024 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202310276Unknown · warning messageR 10 DUCT. WARNING IN CLIMB. RAN QRH, MSG EXTINGUISHED WITHIN THE 40 SEC. RETURNED TO DEN. (FLIGHT 5346 FILED OPEN)Oct 26, 2023 · N959SW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR SWIA20231026004Unknown · warning messageR 10TH DUCT. MASTER WARNING AND EICAS, COMPLIED WITH QRH DID NOT RESOLVE WITH THRUST AT IDLE ON AFFECTED ENGINE IN APPROPRIATE TIME. WENT OUT APPROXIMATELY 2 MINUTES AFTER QRH TIME ELAPSED (FLIGHT 5817 FILED CLOSED)Oct 24, 2023 · N959SW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR SWIA202310250004Unknown · warning messageR 10TH DUCT. MASTER WARNING AND EICAS, COMPLIED WITH QRH DID NOT RESOLVE WITH THRUST AT IDLE ON AFFECTED ENGINE IN APPROPRIATE TIME. WENT OUT APPROXIMATELY 2 MINUTES AFTER QRH TIME ELAPSED (FLIGHT 5817 FILED OPEN)Oct 24, 2023 · N959SW · Cndair CL6002B19 · Air Conditioning SystemSDR SWIA20230627004Unknown · warning messageRECEIVED GEAR DISAGREE WARNING WHILE SELECTING GEAR DOWN. IT WAS THE RIGHT MAIN GEAR THAT WAS RED. RAN QRH AND FIRST STEP TURNING HYD 2 AND 3B ON CLEARED IT. (FLT 5637 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26805733 WITH THE FOLLOWING CORREJun 24, 2023 · N959SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA202266677None · damagedLT SIDE OF FUSELAGE, AFT OF MAIN CABIN DOOR, BELOW PAX WINDOW AT 1A, HAS DAMAGE THAT NEEDS TO BE EVALUATED (FILED CLOSED) COMPLIED WITH PERMANENT REPAIR ON LH FUSLAGE SKIN BETWEEN FS364.00 - FS374.00 AND STR13L -STR14L IN REFERENCE TO REO 601R-53-21-3576 ROct 29, 2022 · N959SW · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202266446None · crackedTRANSFER FROM EAML 987584 : L WINDOW HEAT CAUTION MESSAGE ON DESCENT. CRACK STARTED TO FORM ON LEFT WINDOW. (FLIGHT #5349 FILED CLOSED) REFERENCE CP 25458374 FOR REMOVAL OF L/H SIDE WINDOW. INSTALLED SERVICEABLE L/H SIDE WINDOW PER AMM 56-12-01. TASK CARDSep 7, 2022 · N959SW · Cndair CL6002B19 · Window/Windshield SystemSDR SWIA2019122747359Warning Message · illuminatedRECEIVED R REV UNLOCKED CAUTION MESSAGE AFTER TAKEOFF. RAN QRC/QRH, MESSAGE PERSISTED. FLIGHT 5997 - CLOSED DEFERRED R THRUST REVERSER PER MEL. COMPLIED WITH MAINT. ACTION AMM.Dec 27, 2019 · N959SW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA2019120246801Warning Message · illuminatedR REV UNLOCKED AND REV MESSAGE UNDER N1 GAUGE DURING DESCENT. FLIGHT 5706 CLOSEDDEFERRED RH THRUST REVERSER IAW MEL. ALL MAINTENANCE ACTION HAS BEEN COMPLIED WITH.Dec 2, 2019 · N959SW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA2019030545590Duct · failedR 14TH DUCT WARNING MESSAGE DURING CLIMB. RAN QRH, MESSAGE CLEARED. DECLARED AN EMERGENCY ON APPROACH. (FLT#5031) CLOSED REMOVED AND REPLACED RT 14TH STAGED PYLON DUCT IAW AMM. OPERATED RH 14TH STAGE SYSTEM FOR EXTENDED TIME WITH NO LEAKS OR ABNORMAL MESSAGES.Mar 4, 2019 · N959SW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR SWIA2018010345403Strap · corrodedLT PRESSURE FLOOR SILL STRAP AT FS559.00 HAS CORROSION. (C-CHECK) RO: 01/02/2019 REMOVED AND INSTALLED NEW FLOOR SILL STRAP PN 601R31025-29 AT FS559.00 IAW SRM.Dec 17, 2018 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018010345407Intercostal · corrodedPAX DOOR CENTER INTERCOSTAL DD6 HAS CORROSION. (C-CHECK) RO: 01/02/2019 REPLACED PAX DOOR CENTER INTERCOSTAL DD6 WITH NEW PN 601R318057-1S IAW SRM. PRESSURE CHECK GOOD IAW AMM.Dec 11, 2018 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018010345406Stringer · corrodedTHE AFT EQUIPMENT COMPARTMENT'S RT STRINGER 23, BETWEEN FS 736 AND FS 755, HAS SURFACE CORROSION NOTED ON ITS LOWER FLANGE NEAR THE AFT END. (C-CHECK) RO: 01/02/2019 BLENDED CORROSION THE AFT EQUIPMENT COMPARTMENT'S RT STRINGER 23, BETWEEN FS 736 AND FS 755 ATDec 11, 2018 · N959SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2018010345405Stringer · corrodedTHE AFT EQUIPMENT COMPARTMENT'S RT STRINGER 26, BETWEEN FS 736 AND FS 755, HAS SURFACE CORROSION NOTED ON ITS LOWER FLANGE NEAR THE AFT END. (C-CHECK) RO: 01/02/2019 BLENDED CORROSION THE AFT EQUIPMENT COMPARTMENT'S RT STRINGER 26, BETWEEN FS 736 AND FS 755 ATDec 11, 2018 · N959SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2018010345404Angle · chafedTHE FS 621 FLOOR ANGLE OUTBOARD OF LBL 27 IS CHAFED WITH MULTIPLE RIVET HEADS DAMAGED. (C-CHECK) RO: 01/02/2019 REMOVED AND REPLACED FS621.00 FLOOR ANGLE. LEAK CHECK GOOD IAW REO.Dec 11, 2018 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018010345402Intercostal · corrodedPAX DOOR AFT DD5 INTERCOSTAL HAS CORROSION. (C-CHECK) RO: 01/02/2019 REPLACED PAX DOOR AFT DD5 INTERCOSTAL WITH NEW PN 601R31602-317A IAW SRM. PRESSURE CHECK GOOD IAW AMM.Dec 11, 2018 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018010345401Intercostal · corrodedPAX DOOR FWD DD3 INTERCOSTAL HAS CORROSION. (C-CHECK) RO: 01/02/2019 REPLACED PAX DOOR FWD DD3 INTERCOSTAL WITH NEW PN 601R318054-1 IAW SRM. PRESSURE CHECK GOOD IAW AMM.Dec 11, 2018 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018010345400Intercostal · corrodedPAX DOOR AFT DD4 INTERCOSTAL HAS CORROSION. (C-CHECK) RO: 01/02/2019 REPLACED PAX DOOR AFT DD4 INTERCOSTAL WITH NEW PN 601R31902-317A IAW SRM. PRESSURE CHECK GOOD IAW AMM.Dec 11, 2018 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018010345399Hinge · groovedPASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE, NUMEROUS LUGS ON EXTERNAL SURFACE HAS GROOVES WORN INTO LUGS. (C-CHECK) RO: 01/02/2019 REPLACED PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE WITH NEW IAW SRM AND AMM.Dec 5, 2018 · N959SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2018110945158Landing Gear · malfunctionedNOSE GEAR DISAGREE UPON RETRACTION. WHEN RETRACTED FLAPS TO ZERO. NOSE GEAR THEN RETRACTED. (FLT#5211) FO: 10/18/2018 CLOSED PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTON SYSTEM IAW AMM WHILE OPERATING FLAPS IAW AMM. OPS CHECK GOOD AT THIS Oct 17, 2018 · N959SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2018101845158Warning System · activatedNOSE GEAR DISAGREE UPON RETRACTION. WHEN RETRACTED FLAPS TO ZERO. NOSE GEAR THEN RETRACTED. (FLT 5211) FO: 10/18/2018 WORK IN PROGRESS.Oct 17, 2018 · N959SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018052444715Warning System · false activationRECEIVED A GEAR DISAGREE WHEN SELECTING GEAR UP ON A GO AROUND. (FLT 5751) CLOSED PERFORMED OPS CHECK OF NOSE LANDING GEAR EXTENSION AND RETRACTION SYSTEM IAW FIM. COULD NOT DUPLICATE DISCREPANCY AFTER SEVERAL NOSE GEAR SWINGS.May 24, 2018 · N959SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201743410Bracket · damagedGEAR DISAGREE WITH NOSE GEAR OPEN WARNING. REPLACED THE NLG OLEO BRACKET AND AND PERFORMED EXTENSION AND RETRACTION. OPS CHECKED GOOD.Jun 26, 2017 · N959SW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR SWIA201642930Skin · dentedRIGHT UPPER TRANS COWL HAS MULITPLE DENTS. REPLACED RT NACELLE TRANS COWL IAW CMM.Nov 23, 2016 · N959SW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR SWIA201642348Landing Gear · malfunctionedNLG DISAGREE. HAD TO USE THE EMERGENCY EXTEND HANDLE. GEAR DID EXTEND WITH MANUAL HANDLE PULLED.Jul 25, 2016 · N959SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
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