# Service difficulty reports: N952SW

A list on [N952SW](https://openairdocs.org/aircraft/N952SW.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 · 195 reports

- [SDR SWIA2026030575737](https://openairdocs.org/sdr/SWIA2026030575737.md): Rib · corroded · Mar 5, 2026 · N952SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > CAPTURE MAJOR REPAIR/RII REQUIREMENTS FOR CORROSION DISCOVERED ON LT WING BATTERY RIB AT WS 48.3 DURING REPLACEMENT OF UPPER ANGLE ON HN00281977 CAMP 31329618. 5720COMPLIED WITH ALL THE STEPS OF REO 601R-57-21-4030 REV-- DATED 2026-03-06, INSTALLED -1 REPAIR
- [SDR SWIA2026022175743](https://openairdocs.org/sdr/SWIA2026022175743.md): Skin · gouged · Feb 21, 2026 · N952SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP AT WS 97.009 INNER SKIN AND DOUBLER HAS GAUGES. REPAIRED LT INBD FLAP AT WS 97.009 INNER SKIN AND DOUBLE IAW REO 601R-57-52-2545, REV-. CHECKS GOOD.
- [SDR SWIA2026021175746](https://openairdocs.org/sdr/SWIA2026021175746.md): Rib · corroded · Feb 11, 2026 · N952SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LEFT WHEEL WELL BATTERY RIB AT WS58.8 HAS FWD CHANNEL CORRODED. REMOVED AND REPLACED FWD CHANNEL IAW SRM 51-42-21 AND DWG. 601R10205 REV. -F. LEAK CHECKED GOOD.
- [SDR SWIA202604175770](https://openairdocs.org/sdr/SWIA202604175770.md): Intercostal · corroded · Jan 31, 2026 · N952SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD6 MIDDLE HAS CORROSION. REMOVED, REPLACED AND INSTALLED NEW PASSENGER DOOR INTERCOSTAL DD6 MIDDLE IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R31702, REV-N. COMPLIED WITH SKY WEST TASK CARD 51-900-1003-SKY. MAJOR REPAIR.
- [SDR SWIA2026013075742](https://openairdocs.org/sdr/SWIA2026013075742.md): Rib · corroded · Jan 30, 2026 · N952SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING BATTERY RIB AT WS58.88, FWD LOWER ANGLE IS CORRODED THROUGH (601R10205-7). REMOVED AND REPLACED FWD LOWER ANGLE ON WS 58.8 LT BATTERY RIB REF. SRM 51-42-21 AND DWG. 601R10205 REV. -F.
- [SDR SWIA2026012975758](https://openairdocs.org/sdr/SWIA2026012975758.md): Skin Panel · damaged · Jan 29, 2026 · N952SW · Cndair CL6002B19 · Wing, Plate/Skin
  > PERFORM REPAIR TO LOWER WING PLANK, LOWER SKIN PANEL, AND BATT RIB AT WS53.6 REF. REO 601R-57-21-4021. COMPLIED WITH ALL STEPS OF REO601R-57-4021 REV -- DATED 2026-02-16, DWG 601R10203 REV. G. NO FUEL LEAKS NOTED AT THIS TIMECOMPLIED WITH SKYWEST TASK CARD
- [SDR SWIA2026012875745](https://openairdocs.org/sdr/SWIA2026012875745.md): Frame · corroded · Jan 28, 2026 · N952SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FWD FACE FRAME AT BS 280 APPROXIMATELY BETWEEN STGR 25L TO 24L HAS CORROSION. REPAIRED FWD FACE FRAME AT FS280 APPROXIMATELY BETWEEN STGR 25L TO 24L PER REO 601R-53-21-3787 REV.-. COMPLIED WITH SKYWEST TASK CARD 51-900-1003.
- [SDR SWIA2026012875732](https://openairdocs.org/sdr/SWIA2026012875732.md): Yoke · gouged · Jan 28, 2026 · N952SW · Cndair CL6002B19 · Engine Mount Section
  > ORDERED AND RECEIVED RT ENGINE FWD MOUNT YOKE 601370158, S/N) WITH GOUGES. RECEIVED REO 601R-71-21-082 REV -- DATE 2026-02-23. COMPLIED WITH REO 601R-71-21-082 REV -- DATE 2026-02-23 STEP 1-5. ENSURED BLEND-OUT WAS PERFORMED IAW GENERIC REO 601R-71-21-005 REV
- [SDR SWIA2026012475759](https://openairdocs.org/sdr/SWIA2026012475759.md): Angle · corroded · Jan 24, 2026 · N952SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION AFT ANGLE OF INNER PLATE OF LOW PRESSURE GROUND CONNECTION BETWEEN FS559.00+112-FS574. REMOVED AND INSTALLED NEW AFT ANGLE ON INNER PLATE OF LOW PRESSURE GROUND CONNECTION BETWEEN FS559.00+112-FS574.00 REF. SRM 51-42-06, CRJ-200 SRM 51-42-21 AND DW
- [SDR SWIA2026011875735](https://openairdocs.org/sdr/SWIA2026011875735.md): Skin · corroded · Jan 18, 2026 · N952SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DEEP CORROSION PIT FOUND BEHIND RH FUSELAGE HINGE FITTING OF REAR NOSE LANDING GEAR DOOR. WET INSTALLED ALL REPAIR PARTS AT STR 26R & NLG BAY WEB FWD OF FS.235 & RBL 6 WITH NEW FASTENERS PER REO 601R-53-11-4054 REV --. LEAK CHECK GOOD. COMPLIED WITH TASK CARD
- [SDR SWIA2025122375769](https://openairdocs.org/sdr/SWIA2025122375769.md): Plate · damaged · Dec 23, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Structure
  > DURING ACCESS FOR DAMAGED NUTPLATES. FOUND DAMAGED FASTENER HOLES ON INNER PLATE OF LOW PRESSURE GROUND CONNECTION BETWEEN BS 559+112 - 574. INSTALLED NEW INNER PLATE OF LOW PRESSURE GROUND CONNECTION BETWEEN BS 559+112 - 574 IAW SRM 51-42-06, SRM 51-42-13,
- [SDR SWIA2025121975736](https://openairdocs.org/sdr/SWIA2025121975736.md): Fastener · misinstalled · Dec 19, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING AUDIT OF RA48003 REPAIR TO THE AFT FUSE SKIN BTWN FS682-FS718 & STR20R- 22R IN REF TO REO 601R-53-61-6966, REV--, WAS FOUND THAT THERE ARE TWO EXTRA FASTENERS INSTALLED FORWARD OF FS 700 AT STRINGER 20R. EVALUATED REPAIR AT AFT FUSELAGE SKIN BETWEEN
- [SDR SWIA2025121875730](https://openairdocs.org/sdr/SWIA2025121875730.md): Frame · cracked · Dec 18, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING AUDIT OF RA 44367, BS 333 UPPER FRAME IS CRACKED BTWN STR 0 - 2L. REPAIRED IAW REO 601R-53-21-3018, REV--, IT WAS FOUND THAT THE SHIMS FOR THE REPAIR ARE THE WRONG DIMENSIONS AND ARE INSTALLED INCORRECTLY. INSTALLED NEW SHIM FABRICATED (ITEM -2) PER
- [SDR SWIA2025121675749](https://openairdocs.org/sdr/SWIA2025121675749.md): Hinge · gouged · Dec 16, 2025 · N952SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > DURING PAX DOOR REMOVAL FOUND PIANO HINGE WITH MULTIPLE LUG LANDS GOUGED ON FUSELAGE SIDE. WET INSTALLED NEW PAX DOOR PIANO HINGE ON FUSELAGE SIDE REF SRM 53-21-23 REPAIR 01, REO 601R-53-21-656 REV - ALL STEPS COMPLIED WITH, DWG 601R31527 REV AM, AND DWG 60
- [SDR SWIA2025121575754](https://openairdocs.org/sdr/SWIA2025121575754.md): Support · cracked · Dec 15, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOT SIDE WINDOW POST, THE LOWER SUPPORT ASSY THAT IS BELOW THE SILL, IS CRACKED. REMOVED AND REPLACED CO-PILOT SIDE WINDOW POST, THE LOWER SUPPORT ASSY THAT IS BELOW THE SILL REF. SRM 51-42-06 AND DWG 601R34032 REV. -V. COMPLIED WITH SKYWEST TASK CARD 51
- [SDR SWIA2025121575753](https://openairdocs.org/sdr/SWIA2025121575753.md): Window Post · cracked · Dec 15, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOT SIDE WINDOW POST, THE LOWER SUPPORT ASSY THAT IS BELOW THE SILL, IS CRACKED. REMOVED AND REPLACED PILOT SIDE WINDOW POST, THE LOWER SUPPORT ASSY THAT IS BELOW THE SILL REF. SRM 51-42-06 AND DWG 601R34032 REV. -V. COMPLIED WITH SKYWEST TASK CARD 51-900-
- [SDR SWIA2025121175768](https://openairdocs.org/sdr/SWIA2025121175768.md): Stop Fitting · corroded · Dec 11, 2025 · N952SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR LOWER AFT STOP FITTING CORRODED. REMOVED CORROSION ON CARGO DOOR, LOWER AFT STOP FITTING, PER REF.CRJ/200 SRM.51-21-06-00. COMPLIED WITH REO 601R-53-61-8451 REV -. OPS AND FITS AND CLEARANCES CHECKS OK AT THIS TIME. LEAK CHECK GOOD. COMPLIED WITH T
- [SDR SWIA2025121175763](https://openairdocs.org/sdr/SWIA2025121175763.md): Stop Fitting · corroded · Dec 11, 2025 · N952SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER AFT STOP FITTING CORRODED. REMOVED CORROSION ON CARGO DOOR, UPPER AFT STOP FITTING, PER SRM.51-21-06-00. COMPLIED WITH REO 601R-53-61-8451 REV-. OPS AND FITS AND CLEARANCES CHECKS OK AT THIS TIME. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-
- [SDR SWIA2025121175747](https://openairdocs.org/sdr/SWIA2025121175747.md): Stop Fitting · corroded · Dec 11, 2025 · N952SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT LOWER CENTER STOP FITTING CORRODED. REMOVED CORROSION ON CARGO DOOR, AFT LOWER CENTER STOP FITTING, IAW SRM.51-21-06-00. COMPLIED WITH REO 601R-53-61-8451 REV--.
- [SDR SWIA2025121175740](https://openairdocs.org/sdr/SWIA2025121175740.md): Stop Fitting · corroded · Dec 11, 2025 · N952SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR LOWER FWD STOP FITTING CORRODED. REPAIRED CARGO DOOR LOWER FWD STOP FITTING REF ALL STEPS OF REO 601R-53-61-8451 REV. --. FITS AND CLEARANCES GOOD. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025121175739](https://openairdocs.org/sdr/SWIA2025121175739.md): Stop Fitting · corroded · Dec 11, 2025 · N952SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD LOWER CENTER STOP FITTING CORRODED. REMOVED CORROSION ON CARGO DOOR, FWD LOWER CENTER STOP FITTING, PER SRM.51-21-06-00. COMPLIED WITH ALL STEPS OF REO 601R-53-61-8451 REV--, OPS AND FITS AND CLEARANCES CHECKS OK AT THIS TIME. LEAK CHECK GOOD
- [SDR SWIA2025121075728](https://openairdocs.org/sdr/SWIA2025121075728.md): Stringer · cracked · Dec 10, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED AT THE AFT END OF THE PASSENGER DOOR UPPER LINTEL BS 379. REPLACED STRINGER 3L IAW SRM 51-42-06, AND DWG 601R31016, REV C.
- [SDR SWIA2025120975761](https://openairdocs.org/sdr/SWIA2025120975761.md): Intercostal · cracked · Dec 9, 2025 · N952SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 - 625, STRG 14RH, ANGLE FROM PRESSURE BULKHEAD INTERCOSTAL TO THE 625 FRAME IS CRACKED (MARKED) (C-CHECK RO 04/16/2026)PERFORMED A VISUAL INSPECTION IAW NDTM.51-20-09, THE ANGLE (IN THE AEB) FROM PRESSURE BULKHEAD INTERCOSTAL TO THE FS625.00 AND STRG
- [SDR SWIA2025120975757](https://openairdocs.org/sdr/SWIA2025120975757.md): Angle · cracked · Dec 9, 2025 · N952SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 - 625, STRINGER 14L, ANGLE IN THE AEB, FROM PRESSURE BULKHEAD INTERCOSTAL TO THE 625 FRAME IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-42-21, SRM 51-40-11, SRM 51-21-16, AND REO 601R-53-61-422 REV NC. COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA2025120875767](https://openairdocs.org/sdr/SWIA2025120875767.md): Pressure Blkhd · cracked · Dec 8, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 409+128, RBL 27 PRESSURE BULKHEAD POST, POSSIBLE CRACK AT BOTTOM INBD AFT RADIUS. REPAIRED THE CRACK AS PER REO 601R-53-41-056 REV -F. LEAK CHECKED GOOD
- [SDR SWIA2025120875751](https://openairdocs.org/sdr/SWIA2025120875751.md): Rib · cracked · Dec 8, 2025 · N952SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RIGHT MLG WHEEL WELL BATTERY RIB AT WS.48.3 HAS POSSIBLE CRACK ON FWD AND AFT END. REMOVED AND REPLACED CRACKED BATTERY RIB IN THE RT MLG WHEEL WELL IAW DWG 600-10204 REV M AND SRM 51-42-21. COMPLIED WITH 51-900-1003 SKY.
- [SDR SWIA2025120875733](https://openairdocs.org/sdr/SWIA2025120875733.md): Rib · cracked · Dec 8, 2025 · N952SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LEFT MLG WHEEL WELL BATTERY RIB AT WS.48.3 HAS POSSIBLE CRACK ON FWD OB END. REPAIRED THE LT BATTERY RIB WEB AT WS48.3. REO 601R-57-21-4030 REV --, COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025120875731](https://openairdocs.org/sdr/SWIA2025120875731.md): Pressure Blkhd · cracked · Dec 8, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS409.00+128 LBL 18 PRESSURE BULKHEAD POST, POSSIBLE CRACK AT BOTTOM OUTBD AFT RADIUS. REPLACED FS409.00+128 LBL 18 PRESSURE BULKHEAD POST IAW SRM 51-42-06 & REO 601R-53-41-889 REV -D. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025120775765](https://openairdocs.org/sdr/SWIA2025120775765.md): Strap · corroded · Dec 7, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS559.00 RBL 27 - RBL 42, THE STRAP THAT CROSSES THE FLOOR BEAMS IS CORRODED. REPLACED BS 559, RBL 27 - RBL 42, THE STRAP THAT CROSSES THE FLOORBEAMS PER REO 601R-53-41-3393 REV-. AND SRM 51-42-06.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025120775764](https://openairdocs.org/sdr/SWIA2025120775764.md): Pressure Deck · corroded · Dec 7, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS449.00 - 559.00 LH PRESSURE FLOOR SILL PANEL HAS NUMEROUS AREAS OF CORROSION. REPAIRED CORROSION DAMAGE TO LT PRESSURE FLOOR SILL PANEL FS449-FS559 REF. REO 601R-53-41-3379 REV -, STEPS 1-6, ALL STEPS COMPLIED WITH. COMPLETED ATTACHED TASK CARD 51-900-1003-
- [SDR SWIA2025120775760](https://openairdocs.org/sdr/SWIA2025120775760.md): Attach Angle · cracked · Dec 7, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS484.00 RBL 27-36, THE FLT CONTROL CABLE GUIDE ROLLER ASSY, THE AFT OUTBD VERTICAL ATTACH ANGLE IS CRACKED IN THE UPPER RADIUS. PERFORMED REPAIR FOR CRACKED ANGLE AND DAMAGED INTERCOSTAL AT FS484.00 AND RBL36.00 IAW ALL STEPS OF MHIRJ REO 601R-53-41-3391 REV
- [SDR SWIA2025120775750](https://openairdocs.org/sdr/SWIA2025120775750.md): Attach Angle · cracked · Dec 7, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BS 484, LBL 27-36, THE FLT CONTROL CABLE GUIDE ROLLER ASSY, THE AFT INBD VERTICAL ATTACH ANGLE IS CRACKED IN THE UPPER RADIUS. REMOVED AND REPLACED WITH NEW ATTACH ANGLE, THE CONTROL CABLE GUIDE ROLLER ASSY. IAW SRM 51-42-21, AND DWG 601R31171, REV. B, AND L
- [SDR SWIA2025120775744](https://openairdocs.org/sdr/SWIA2025120775744.md): Floor Support · corroded · Dec 7, 2025 · N952SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 424 - 559 RT PRESSURE FLOOR SILL PANEL HAS NUMEROUS AREAS OF CORROSION. REMOVED CORROSION ON RT PRESSURED FLOOR SUPPORT PANEL BETWEEN BS 424 - 559 AND REPAIRED PER REO 601R-53-41-666, REV-C, ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD 51-9
- [SDR SWIA2025120775738](https://openairdocs.org/sdr/SWIA2025120775738.md): Strap · corroded · Dec 7, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 559, LBL 27 - LBL 42, THE STRAP THAT CROSSES THE FLOOR BEAMS IS CORRODED. REMOVED AND INSTALLED NEW STRAP WITH SRM 51-42-06-00. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025120675741](https://openairdocs.org/sdr/SWIA2025120675741.md): Striker · gouged · Dec 6, 2025 · N952SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR SURROUND, LOWER SEAL STRIKER GOUGED IN TWO AREAS, INSTALLED NEW LOWER SEAL STRIKER WITH IAW DWG.601R38340 REV B, REF. SRM.51-41-02 AND REF. AMM.20-21-00-910-801. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY.
- [SDR SWIA2025120375762](https://openairdocs.org/sdr/SWIA2025120375762.md): Skin · chafed · Dec 3, 2025 · N952SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED ON MID WEAR CAP OF LEADING EDGE AT APPROX. WS. 104. INSTALLED NEW LT INBD FLAP - SKIN, L/E MID REF. SRM 51-42-13 & NEW CAP AT INBOARD FLAP VANE WS105.67 PER SERVICE BULLETIN 601R-57-022 REV. B. COMPLIED WITH SKYWEST TASK CARD 51
- [SDR SWIA2025120375748](https://openairdocs.org/sdr/SWIA2025120375748.md): Former · corroded · Dec 3, 2025 · N952SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT FORMER CORROSION UNDER PNL 832GR. REMOVED PASSENGER DOOR AFT FORMER IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW PAX DOOR AFT FORMER IAW SRM 51-42-06, SRM 51-42-21 AND DWG 601R31702 REV-N. PRESSURE LEAK CHECKED GOOD. COMPLIED WITH SKYWE
- [SDR SWIA2025120375734](https://openairdocs.org/sdr/SWIA2025120375734.md): Intercostal · corroded · Dec 3, 2025 · N952SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL AFT DD5 HAS CORROSION. INSTALLED NEW PAX DOOR INTERCOSTAL AFT DD5 REF SRM 51-42-06 AND DWG. 601R31702, REV -N. LEAK CHECKED GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025120175727](https://openairdocs.org/sdr/SWIA2025120175727.md): Skin · chafed · Dec 1, 2025 · N952SW · Cndair CL6002B19 · Aerodynamic Fairings
  > LEFT APRON SKIN CHAFED WHERE IT MEETS THE WING. REMOVED DAMAGE ON LT APRON SKIN WHERE IT MEETS THE WING. CUT AWAY DAMAGED PORTION OF LT APRON SKIN PANEL. FABRICATED REPLACEMENT AND WET INSTALLED. APPLIED CIC AND PRIMER. PER REO 601R-53-41-115 REV -A, COMPLETE
- [SDR SWIA2025113075752](https://openairdocs.org/sdr/SWIA2025113075752.md): Skin · cracked · Nov 30, 2025 · N952SW · Cndair CL6002B19 · Landing Gear Doors
  > AFT NLG DOOR SKIN CUT-OUT, THE AFT RH CORNER OF THE FUSELAGE SKIN HAS POSSIBLE CRACK IN THE RADIUS. REPAIRED AFT NLG DOOR SKIN CUT-OUT ON THE AFT RH CORNER OF THE FUSELAGE SKIN REF R.E.O. 601R-53-11-048 REV. -D DATED 2015-06-10 ALSO INCORPORATED WITH REO 601R
- [SDR SWIA2025113075729](https://openairdocs.org/sdr/SWIA2025113075729.md): Floorbeam · damaged · Nov 30, 2025 · N952SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DURING PRESSURE BOX ASSY REMOVAL, FOUND ELONGATED HOLES ON FLOORBEAM LBL 9 AT BS 559. REPAIRED ELONGATED HOLES ON FLOORBEAM IAW REO 601R-53-41-3378 REV -A.
- [SDR SWIA2025112575756](https://openairdocs.org/sdr/SWIA2025112575756.md): Web · cracked · Nov 25, 2025 · N952SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FORWARD EQUIPMENT COMPARTMENT FLOOR WEBBING IS CRACKED AT THE BRAKE ACCUMULATOR GAGE FITTING AREA. REPAIRED LT FORWARD EQUIPMENT COMPARTMENT FLOOR WEBBING AT THE BRAKE ACCUMULATOR GAGE FITTING AREA PER REO 601R-53-11-4045 REV.--. COMPLIED WITH SKYWEST
- [SDR SWIA2025112475755](https://openairdocs.org/sdr/SWIA2025112475755.md): Structure · damaged · Nov 24, 2025 · N952SW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > T/E OF THE RT PYLON IS DELAMINATED AND MISSING COMPOSITE MATERIAL REPLACED AND INSTALLED NEW TRAILING EDGE ASSY, PYLON RT, PER DWG.601-37012 REV B AND REF.CRJ/200 SRM.51-42-10-00, 51-74-00-00. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY.
- [SDR SWIA2025092475766](https://openairdocs.org/sdr/SWIA2025092475766.md): Strap · cracked · Sep 24, 2025 · N952SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA25822-601R-57-21-2228 952SW OP94-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 25822WHILE C/W SB 601R-57-046, PART B (R/H WING) STEP 4 (B), NDT NOTED 3 FASTENER HOLES WITH CRACKING INDICATIONS AND ONE FASTENER HOLE (AFT
- [SDR SWIA2020090852315](https://openairdocs.org/sdr/SWIA2020090852315.md): Windshield · delaminated · Sep 4, 2020 · N952SW · Cndair CL6002B19 · Flight Compartment Windows
  > TRANSFER FROM EAML 485283, CAPTAIN SIDE WINDSHIELD LOOKS LIKE IT IS DELAMINATING BEYOND LIMITS. FLIGHT 5307 - FILED CLOSED. REMOVED AND REPLACED THE CAPTAINS SIDE WINDOW IAW AMM AND TASK CARD. OPERATIONS CHECK GOOD AT THIS TIME, NO LEAKS NOTED AT THIS TIME.
- [SDR SWIA202005050482](https://openairdocs.org/sdr/SWIA202005050482.md): Sensor · malfunctioned · May 5, 2020 · N952SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > WOW OUTBOARD CAUTION MESSAGE ON TAKEOFF, PERFORMED QRH, MESSAGE PERSISTED. FLIGHT 5552 - FILED CLOSED INTERROGATED PSEU AND HAVE FOLLOWING CODES SET FOR CURRENT LEG: S36, S38, S25, S40, S26, S41, S27, S46, DI13, S47, DI16, DI17, S48, S04, S12 (ALL INVALID
- [SDR SWIA2019120646822](https://openairdocs.org/sdr/SWIA2019120646822.md): Warning Message · illuminated · Dec 6, 2019 · N952SW · Cndair CL6002B19 · Landing Gear Steering System
  > ON LANDING IN SFO HAD A STEERING INOP CAUTION MESSAGE ON THE GO AROUND WE GOT GEAR DISAGREE WITH THE NOSE GEAR NOT SHOWING RAN QRH AND HAD TO PULL MANUAL GEAR GOT THREE GREEN AND CAME IN FOR NORMAL LANDING FLIGHT 5349 CLOSED INTERROGATED PSEU IN REF TO CRJ
- [SDR SWIA2019111246754](https://openairdocs.org/sdr/SWIA2019111246754.md): Sensor · damaged · Nov 11, 2019 · N952SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > WOW INPUT CAUTION AFTER TAKEOFF FLIGHT # 5368 CLOSEDLARGE BIRD REMAINS FOUND IN WOW SENSORS. REMOVED BIRD REMAINS JACKED AIRCRAFT AND COMPLIED WITH GEAR SWING AND PERFORMED OPS CHECKS OF WOW SENSORS WITH NO FURTHER FAULTS AT THIS TIME IAW AMM.
- [SDR SWIA2018091245066](https://openairdocs.org/sdr/SWIA2018091245066.md): Intercostal · cracked · Aug 24, 2018 · N952SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BELOW FLOOR BETWEEN FS280 AND FS295 AT APPROX LBL35 IS CRACKED. (C-CHECK) RO: 09/12/2018. REMOVED AND REPLACED INTERCOSTAL BELOW FLOOR BETWEEN FS280 AND FS295 AT APPROX LBL35 IAW SRM.
- [SDR SWIA2018091245065](https://openairdocs.org/sdr/SWIA2018091245065.md): Floorbeam · corroded · Aug 20, 2018 · N952SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO, FLOORBEAM CORRODED FS568 - FS611 LBL27. (C-CHECK) RO: 09/12/2018. REPAIRED OTBD FLANGE IAW SRM AND REO.

Next page: https://openairdocs.org/aircraft/N952SW/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 = 'N952SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N952SW/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.