# Service difficulty reports: N959SW A list on [N959SW](https://openairdocs.org/aircraft/N959SW.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 4 · 196 reports - [SDR SWIA2026070276443](https://openairdocs.org/sdr/SWIA2026070276443.md): Window · cracked · Jul 2, 2026 · N959SW · Cndair CL6002B19 · Flight Compartment Windows > LEFT WINDOW INBOARD PLY COMPLETELY CRACKED ON DOWNWIND GOING 170KTS AND AT 2400MSL. DID NOT IMPACT ANYTHING. PERFORMED QRH AND LANDED NORMALLY. (FLIGHT 5566) REMOVED AND REPLACED LT COCKPIT WINDOW IAW AMM 56-12-01 AND COMPLIED WITH SKYWEST TASK CARD 56-220-1 - [SDR SWIA2026040275872](https://openairdocs.org/sdr/SWIA2026040275872.md): Access Panel · damaged · Apr 2, 2026 · N959SW · Cndair CL6002B19 · Fuselage Main, Structure > FASTENER HOLE OF ACCESS PANEL 132AL DAMAGE. REPAIRED FASTENER HOLE OF ACCESS PANEL 132AL. COMPLIED WITH REO 601R-53-11-162 REV D DATE 2019-02-05. STEPS 1-8 AND REF SRM 51-21-16. LEAK CHECK GOOD. COMPLIED WITH 51-900-1003-SKY - [SDR SWIA2026030575873](https://openairdocs.org/sdr/SWIA2026030575873.md): Stop Fitting · wrong part · Mar 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > DURING THE REPLACEMENT OF THE PAX DOOR FS310.00 STOP DROP DOWN DOOR FITTING, IT WAS FOUND THAT INCORRECT HARDWARE WAS INSTALLED IN THE FWD SUPPORT BRACKET STOP DURING A PREVIOUS REPAIR. REMOVED AND INSTALLED NEW PAX DOOR FS 310 FWD SUPPORT BRACKET STOP. IAW S - [SDR SWIA2026030575871](https://openairdocs.org/sdr/SWIA2026030575871.md): Door Frame · damaged · Mar 5, 2026 · N959SW · Cndair CL6002B19 · Fuselage Main, Structure > UPON REMOVAL OF PAX DOOR FWD UPPER STOP BRACKET, FOUND 4EA ELONGATED HOLES AND GOUGES AROUND HOLES ON F.S 310.00 PAX DOOR SURROUND FRAME STRUCTURE BETWEEN STR 3L AND 4L, COMMON TO UPPER STOP BRACKET. PERFORMED EVAL. TO DAMAGE HOLES #1 DAMAGE AROUND THE HOLE E - [SDR SWIA2026030575866](https://openairdocs.org/sdr/SWIA2026030575866.md): Door Frame · chafed · Mar 5, 2026 · N959SW · Cndair CL6002B19 · Fuselage Main, Structure > PAX DOOR CUTOUT FRAME FS310 FITTING CAM CHAFED AFTER CLEANED AREA FOUND CORROSION ON CHAFFED AREA, NO ALLOW. LIMIT FOUND ON SRM. REQ. REPLACEMENT. ORDER NEW FITTING CAM FS310.00 P/N 600-31688-17. PERFORMED LOCATE AND DRILL NEW PAX DOOR FS310 FITTING CAM. I - [SDR SWIA2026021875877](https://openairdocs.org/sdr/SWIA2026021875877.md): Cleat · corroded · Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FS338.963 FRAME AND INTERCOSTAL DD6 CLEAT INBD SIDE CORRODE. PAX DOOR FS338.963. FRAME AND INTERCOSTAL DD6 CLEAT. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00. CORROSION EXIST ON 2 ELEMENT, OUT OF LIMITS, REPLACE CLEAT IAW SRM 52-0 - [SDR SWIA2026021875876](https://openairdocs.org/sdr/SWIA2026021875876.md): Former · corroded · Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FS338.963 FORMER CORRODE. INSTALLED NEW PASSENGER DOOR FS338.963 FORMER. IAW. SRM 51-42-06-00 AND SRM 51-42-21-00. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY - [SDR SWIA2026021875869](https://openairdocs.org/sdr/SWIA2026021875869.md): Cleat · corroded · Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FS338.963 FRAME AND INTERCOSTAL DD1 CLEAT INBD SIDE CORRODE. PAX DOOR FS338.963. FRAME AND INTERCOSTAL DD1 CLEAT. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00. CORROSION EXIST ON 2 ELEMENT, OUT OF LIMITS, REPLACE CLEAT IAW SRM 52- - [SDR SWIA2026021875863](https://openairdocs.org/sdr/SWIA2026021875863.md): Cleat · corroded · Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FS338.963 FRAME AND INTERCOSTAL DD5 CLEAT CORRODE. INSTALLED NEW PAX DOOR FS338.963 FRAME AND INTERCOSTAL DD5 CLEAT. IAW. SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026021875848](https://openairdocs.org/sdr/SWIA2026021875848.md): Cleat · corroded · Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FS338.963 FRAME AND LOWER CHANNEL CLEAT INBD SIDE CORRODE. PASSENGER DOOR FS338.963 FRAME AND LOWER CHANNEL CLEAT INBD SIDE. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00. CORROSION EXIST ON 2 ELEMENT, OUT OF LIMITS, REPLACE CLEAT I - [SDR SWIA2026021875835](https://openairdocs.org/sdr/SWIA2026021875835.md): Intercostal · corroded · Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FS338.963 FRAME AND INTERCOSTAL DD5 CLEAT INBD SIDE CORRODE. PAX DOOR FS338.963. FRAME AND INTERCOSTAL DD5 CLEAT. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00. CORROSION EXIST ON 2 ELEMENT, OUT OF LIMITS, REPLACE CLEAT IAW SRM 52-0 - [SDR SWIA2026021675846](https://openairdocs.org/sdr/SWIA2026021675846.md): Cleat · corroded · Feb 16, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > FOUND CORROSION ON PASSENGER DOOR DD4 MID INTERCOSTAL AND FS335.163 CLEAT. PAX DOOR DD4 FS335.163 CLEAT, ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00 CORROSION ON MORE THAN ONE ELEMENT AT A GIVEN CROSS-SECTION, PAX DOOR DD4 FS335.163 INBD CLEAT - [SDR SWIA2026021675842](https://openairdocs.org/sdr/SWIA2026021675842.md): Skin · gouged · Feb 16, 2026 · N959SW · Cndair CL6002B19 · Wing, Plate/Skin > RH WING INBOARD FLAP UPPER INTERNAL SKIN HAS MULTIPLE GOUGES UNDER PANEL 684AB. REMOVED MULTIPLE GOUGES AND RESTORED AREA AT RH WING INBOARD FLAP UPPER INTERNAL SKIN UNDER PANEL 684AB REF SRM 51-12-00, COMPLIED WITH ALL THE STEPS OF THE REO 601R-57-52-2543 RE - [SDR SWIA2026021275865](https://openairdocs.org/sdr/SWIA2026021275865.md): Landing · corroded · Feb 12, 2026 · N959SW · Cndair CL6002B19 · Fuselage Main, Structure > DURING REMOVAL OF FWD DRAIN MAST. TO FOM FOUND CORROSION ON FWD DRAIN MAST LANDING. PERFORMED REPAIR OF FUSELAGE SKIND UNDER FWD DRAIN MAST BETWEEN FS333.00-FS349.00 AND STR24R-STR25R ON FWD DRAIN MAST LANDING PER REO 601R-53-21-3794 REV -- DATE 2026-03-06. F - [SDR SWIA2026020975826](https://openairdocs.org/sdr/SWIA2026020975826.md): Cleat · corroded · Feb 9, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > FOUND CORROSION ON PAX DOOR FS320.163 LOWER CHANNEL CLEAT. INSTALLED NEW PAX DOOR FS320.163 LOWER CHANNEL CLEAT. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020875878](https://openairdocs.org/sdr/SWIA2026020875878.md): Cleat · corroded · Feb 8, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > FOUND CORROSION ON PAX DOOR FS311.75 INTERCOSTAL DD7 CLEAT. INSTALLED NEW PAX DOOR FS311.75 INTERCOSTAL DD7 CLEAT. IAW. SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020875868](https://openairdocs.org/sdr/SWIA2026020875868.md): Support Angle · gouged · Feb 8, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > FOUND GOUGE ON PAX DOOR FWD ANGLE SUPPORT. UNDER PULL-IN LEVER. REMOVED AND INSTALLED NEW PAX DOOR FWD ANGLE SUPPORT. IAW SRM 51-42-06-00. SRM 51-42-21-00, SRM 51-41-02. AND DWG 601R31702 REV. N. COMPLIED WITH 51-900-1003-SKY, PRESSURE LEAK CHECK WAS GOOD - [SDR SWIA2026020875845](https://openairdocs.org/sdr/SWIA2026020875845.md): Intercostal · corroded · Feb 8, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > FOUND CORROSION ON FWD INTERCOSTAL DD5. INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD5. IAW. SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020875844](https://openairdocs.org/sdr/SWIA2026020875844.md): Bracket · damaged · Feb 8, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR FS311.75 INTERCOSTAL DD2 BRACKET HOLES PREVIUSLY OVERSIZE. REMOVED AND INSTALLED NEW PAX DOOR FS311.75 INTERCOSTAL DD2 BRACKET. IAW. SRM 51-42-06-00 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY - [SDR SWIA2026020875837](https://openairdocs.org/sdr/SWIA2026020875837.md): Cleat · corroded · Feb 8, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > FOUND CORROSION ON PAX DOOR FS320.163 INTERCOSTAL DD6 CLEAT. PAX DOOR FS320.163 INTERCOSTAL DD6 CLEAT, ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00 CORROSION EXIST ON 2 ELEMENT OUT OF LIMITS REPLACE CLEAT. IAW SRM 52-00-00 PERFORMED LOCATE AND D - [SDR SWIA2026020875828](https://openairdocs.org/sdr/SWIA2026020875828.md): Bracket · corroded · Feb 8, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > FOUND CORROSION ON PAX DOOR FS311.75. DD5 BRACKET. INSTALLED NEW PAX DOOR FS311.75 INTERCOSTAL DD5 BRACKET. IAW SRM 51-42-06-00 AND DWG 601R31702 REV. N.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY - [SDR SWIA2026020575870](https://openairdocs.org/sdr/SWIA2026020575870.md): Intercostal · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD4 MID INTERCOSTAL IS CORRODED. REMOVED AND INSTALLED NEW PASSENGER DOOR DD4 MID INTERCOSTAL. IAW SRM 51-42-06-00 AND SRM 51-42-21. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020575867](https://openairdocs.org/sdr/SWIA2026020575867.md): Frame · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR FS320.163 FRAME BETWEEN DD5 INTERCOSTAL AND LOWER CHANNEL IS CORRODED. INSTALLED NEW PAX DOOR FS320.163 FRAME. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY - [SDR SWIA2026020575860](https://openairdocs.org/sdr/SWIA2026020575860.md): Intercostal · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD1A MID INTERCOSTAL IS CORRODED. INSTALLED NEW PAX DOOR DD1A MID INTERCOSTAL. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020575856](https://openairdocs.org/sdr/SWIA2026020575856.md): Cleat · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD5 FS347.25 CLEAT IS CORRODED. INSTALLED NEW PAX FS347.25 DD5 CLEAT. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020575853](https://openairdocs.org/sdr/SWIA2026020575853.md): Intercostal · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD3 MID INTERCOSTAL IS CORRODED. INSTALLED NEW PASSENGER DOOR DD3 MID INTERCOSTAL IAW SRM 51-42-06-00 AND SRM 51-42-21-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020575850](https://openairdocs.org/sdr/SWIA2026020575850.md): Intercostal · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD1A AFT INTERCOSTAL IS CORRODED. INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD1A. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY - [SDR SWIA2026020575847](https://openairdocs.org/sdr/SWIA2026020575847.md): Cleat · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD7 FS347.25 CLEAT IS CORRODED. INSTALLED NEW PAX FS347.25 DD7 CLEAT. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020575839](https://openairdocs.org/sdr/SWIA2026020575839.md): Intercostal · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD2 MID INTERCOSTAL IS CORRODED. INSTALLED NEW PASSENGER DOOR DD2 MID INTERCOSTAL. IAW SRM 51-42-06-00 AND CRJ200 SRM 51-42-21-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020575838](https://openairdocs.org/sdr/SWIA2026020575838.md): Cleat · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD7A FS327.763 CLEAT IS CORRODED. PAX DOOR FS327.763 DD7A CLEAT. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00 CORROSION EXIST ON 2 ELEMENT OUT OF LIMITS REPLACE CLEAT IAW SRM 52-00-00 PERFORMED LOCATE AND DRILL NEW PASSENGER DOOR FS327.7 - [SDR SWIA2026020575836](https://openairdocs.org/sdr/SWIA2026020575836.md): Retainer · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR FWD LOWER CORNER SEAL RETAINER IS CORRODED. INSTALLED NEW PASSENGER DOOR LOWER FWD CORNER SEAL RETAINER. IAW SRM 51-42-06-00 AND DWG 601R31871 REV D. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020575833](https://openairdocs.org/sdr/SWIA2026020575833.md): Intercostal · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD1 MID INTERCOSTAL IS CORRODED. INSTALLED NEW PAX DOOR DD1 MID INTERCOSTAL. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026020575830](https://openairdocs.org/sdr/SWIA2026020575830.md): Cleat · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR DD1A FS338.963 INBD CLEAT IS CORRODED. PAX DOOR DD1A FS338.963 INBD CLEAT, ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00 CORROSION ON MORE THAN ONE ELEMENT AT A GIVEN CROSS-SECTION, PAX DOOR DD1A FS338.963 INBD CLEAT IS OUT OF LIMITS, IAW - [SDR SWIA2026020575829](https://openairdocs.org/sdr/SWIA2026020575829.md): Channel · corroded · Feb 5, 2026 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > (MX 31663791) PAX DOOR FS327.763 FRAME BETWEEN DD6 INTERCOSTAL AND LOWER CHANNEL IS CORRODED. (C-CHECK RO 04/19/2026)INSTALLED NEW PAX DOOR FS327.763 FRAME. IAW. CRJ200 SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026011575874](https://openairdocs.org/sdr/SWIA2026011575874.md): Former · gouged · Jan 15, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FS311.75 FORMER GOUGED FROM PULL-IN LEVER. INSTALLED NEW PASSENGER DOOR FORMER FS311.75. IAW SRM 51-42-06-00, CRJ2500 SRM 51-42-21-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026011575852](https://openairdocs.org/sdr/SWIA2026011575852.md): Retainer · bent · Jan 15, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR LOWER AFT CORNER SEAL RETAINER BENT. INSTALLED NEW PASSENGER DOOR LOWER AFT CORNER SEAL RETAINER IAW SRM 51-42-06-00 AND DWG 601R31871 REV D. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY - [SDR SWIA2026011575851](https://openairdocs.org/sdr/SWIA2026011575851.md): Intercostal · corroded · Jan 15, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FS338.963 FRAME HAS CORROSION AT INTERCOSTAL DD2. REPAIRED PASSENGER DOOR FS338.963 FRAME HAS CORROSION AT INTERCOSTAL DD2 REF SRM 51-23-00, SRM 51-42-14, SRM 51-42-06-00, SRM 51-42-21-00 REV. 39 AND DWG 601R31702 REV. N. REO 601R-52-11-3085. - [SDR SWIA2026011575827](https://openairdocs.org/sdr/SWIA2026011575827.md): Intercostal · corroded · Jan 15, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR INTERCOSTAL DD7A HAS CORROSION. INSTALLED NEW PAX DOOR INTERCOSTAL DD7A. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA2026011475864](https://openairdocs.org/sdr/SWIA2026011475864.md): Skin · chafed · Jan 14, 2026 · N959SW · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP VANE LEADING EDGE CHAFED IN MULTIPLE SPOTS. REPAIRED LT INBD FLAP VANE LEADING EDGE INBD PANEL AT BLENDED AREA 1 THAT WAS FOUND TO BE IN LIMITS REF REO 601R-57-52-004 REV.D DATE:2012-12-19. STEPS 1 TO 3. BLENDED AREAS #2 AND #3 ON (MID PANEL & - [SDR SWIA2026011175832](https://openairdocs.org/sdr/SWIA2026011175832.md): Shroud · chafed · Jan 11, 2026 · N959SW · Cndair CL6002B19 · Wing Miscellaneous Structure > RIGHT AILERON UPPER FIXED SHROUD IS CHAFED ALONG LEADING EDGE. REMOVED RIGHT AILERON UPPER LEADING EDGE SKIN IAW SRM 51-42-06 AND INSTALLED NEW RIGHT AILERON UPPER LEADING EDGE SKIN IAW SRM 51-42-06 & DWG PL601R13031 REV K AND REO 601R-57-61-894 REV -. - [SDR SWIA2026010875861](https://openairdocs.org/sdr/SWIA2026010875861.md): Skin · dented · Jan 8, 2026 · N959SW · Cndair CL6002B19 · Cargo/Baggage Doors > CARGO DOOR EXTERIOR SKIN SKIN CUTOUT 2 DENTS ON LOWER AFT CORNER (C-CHECK RO 04/19/2026)REPAIRED 2 EA. DENTS ON THE EXTERIOR FUSELAGE SKIN AT THE CARGO DOOR CUTOUT LOWER AFT CORNER AT FS 621.00 REF REO 601R-51-00-309 REV-A DATE 2017-08-23 AND REO 601R-53-61-8 - [SDR SWIA2026010875854](https://openairdocs.org/sdr/SWIA2026010875854.md): Lug · gouged · Jan 8, 2026 · N959SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings > LEFT INBD FLAP INBD HINGE ARM LUG GOUGED. REPAIRED FLAP HINGE ARM LUG IAW REO 601R-57-54-389, REV-. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. - [SDR SWIA2026010875840](https://openairdocs.org/sdr/SWIA2026010875840.md): Floor Support · corroded · Jan 8, 2026 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > MULTIPLE SPOTS OF CORROSION ON L/H PRESSURE FLOOR SILL PANEL BETWEEN FS-409+128 €“ FS-559. REMOVED MULTIPLE SPOTS OF CORROSION AND RESTORED AT L/H PRESSURE FLOOR SILL PANEL FS-409+128 - FS-559.00 IN COMPLIANCE WITH GREO 601R-53-41-666 REV. C- DATED 2012-11-0 - [SDR SWIA2026010875831](https://openairdocs.org/sdr/SWIA2026010875831.md): Floor Support · corroded · Jan 8, 2026 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > MULTIPLE SPOTS OF CORROSION ON RT PRESSURE FLOOR SILL PANEL BETWEEN FS-409+128 €“ FS-559.00. REMOVED DAMAGES ON R/H PRESSURE FLOOR SILL PANEL BETWEEN FS-409+128 - FS-559.00. IAW SRM 51-21-06-00. AND COMPLIED WITH THE STEPS OF THE GREO 601R-53-41-666 REV. C- - [SDR SWIA2026010775862](https://openairdocs.org/sdr/SWIA2026010775862.md): Channel · corroded · Jan 7, 2026 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CORROSION IN CHANNEL BETWEEN FS333-349 FOR FORWARD WATER DRAIN HOSES. INSTALLED NEW FWD DRAIN MAST CHANNEL AT FS333-FS349 REF. SRM 51-42-06, SRM 51-42-13 AND DWG 601R43200 REV DCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY - [SDR SWIA2026010775859](https://openairdocs.org/sdr/SWIA2026010775859.md): Lug · gouged · Jan 7, 2026 · N959SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings > LH OTBD FLAP CENTER HINGE FWD INBD LUG GOUGED. COMPLIED WITH ALL STEPS OF REO 601R-57-53-1329 REV-. COMPLIED WITH 51-900-1003-SKY - [SDR SWIA2026010775855](https://openairdocs.org/sdr/SWIA2026010775855.md): Frame · corroded · Jan 7, 2026 · N959SW · Cndair CL6002B19 · Fuselage Main, Frame > CORROSION ON FS364.00 FRAME AT STGR 23L REPAIRED CORROSION ON FRAME AT FS 364.00 AT STGR. 23L REF 601R-53-21-3793 REV--, COMPLIED WITH 51-900-1003-SKY. - [SDR SWIA2025123075875](https://openairdocs.org/sdr/SWIA2025123075875.md): Angle · cracked · Dec 30, 2025 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > BS 484 LBL 27 CLIP HAS CRACK AT UPPER RADIUS. REMOVED AND INSTALLED NEW CLIP AT BS 484 LBL27 REF SRM 51-42-21 AND REO 601R-53-41-059 REV. -C DATE: 2020-03-11. COMPLIED WITH ALL STEPS OF REO 601R-53-41-059 REV. -C DATE: 2020-03-11. COMPLIED WITH TASK CARD 51-9 - [SDR SWIA2025123075849](https://openairdocs.org/sdr/SWIA2025123075849.md): Door Frame · cracked · Dec 30, 2025 · N959SW · Cndair CL6002B19 · Fuselage Main, Structure > FS 605 ( FRAME) AFT CARGO JUST ABOVE DOOR OPENING FRAME FLANGE JUST ABOVE STR 9.0 AND BELOW FLANGE IS CRACKED AT RIVET LOCATIONS. MARKED. REPAIRED FS 605 ( FRAME) AFT CARGO JUST ABOVE DOOR OPENING FRAME FLANGE JUST ABOVE STR 9.0 AND BELOW, FLANGE IS CRACKED - [SDR SWIA2025123075843](https://openairdocs.org/sdr/SWIA2025123075843.md): Casting · cracked · Dec 30, 2025 · N959SW · Cndair CL6002B19 · Fuselage Main, Structure > FS 460 AT RBL 9.0 CASTING HAS CRACK AT CASTING UPPER RADIUS. INSTALLED NEW CASTING FITTING AT FS460, RBL9 REF. SRM 51-42-06. SRM 51-42-21, DWG 601R31118 REV. -L AND DWG 601R31146 REV. -J.COMPLIED WITH SKYWEST TASK CARD 51-900-1003. Next page: https://openairdocs.org/aircraft/N959SW/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N959SW/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.