# Service difficulty reports: N910SW

A list on [N910SW](https://openairdocs.org/aircraft/N910SW.md).

Newest first.

Page 1 of 5 · 209 reports

- [SDR SWIA2025100900005](https://openairdocs.org/sdr/SWIA2025100900005.md): Shutoff Valve · out of limits · Oct 5, 2025 · N910SW · Cndair CL6002B19 · Cabin Cooling System
  > LEFT PACK HIGH PRESSURE ON CLIMB OUT RESULTING IN CABIN ALT CAUTION/WARNING MESSAGE. RAN APPLICABLE QRH & RETURNED TO FIELD. MEL 21-51-1CCAT. RT PACK ALREADY DEFERRED. (FLIGHT 5514) DEFERRED LT PACK WITH RT PACK ALREADY DEFERRED PER MEL 21-51-1C. MX ACTIO
- [SDR SWIA2025100700005](https://openairdocs.org/sdr/SWIA2025100700005.md): A/C Pack · faulted · Oct 5, 2025 · N910SW · Cndair CL6002B19 · Cabin Cooling System
  > D: L PACK HI PRESS ON CLIMB OUT RESULTING IN CABIN ALT CAUTION/WARNING MESSAGE. RAN APPLICABLE QRH AND RETURNED TO FIELD. C: MEL 21-51-1CCAT: C. RT PACK ALREADY DEFERRED.L PACK HIGH PRESS ON CLIMB OUT RESULTING IN CABIN ALT CAUTION/WARNING MESSAGE. RAN APPLIC
- [SDR SWIA20250430116](https://openairdocs.org/sdr/SWIA20250430116.md): Pressure Web · cracked · Jan 16, 2025 · N910SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX-CAB, EVIDENCE OF CRACK ON PRESSURE WEB (CRACK LINE 3" LONG-APROX) FS 459, WL 64 APROX - BETWEEN LBL 9 - LBL 14 (C-CHECK RO 04/30/2025)PERFORMED PRESSURE WEB FLOOR REPAIR AS REQ'D PER REO 601R-53-41-3286 REV. -- DATED: 2025-03-11. SEE ATTACHED RS-01'S FOR
- [SDR SWIA20250430115](https://openairdocs.org/sdr/SWIA20250430115.md): Skin · dented · Jan 15, 2025 · N910SW · Cndair CL6002B19 · Rudder, Plate/Skin
  > DENT FOUND ON RUDDER AT UPPER R/H SIDE BELOW TOP MOST RIB (MARKED) (C-CHECK RO 04/30/2025)MEASURED AND EVALUATED DENT ON RUDDER AT RS-140 TO RS-148, DENT FOUND OUT OF LIMITS AND PERFROMED REPAIR IN REF TO MHIRJ REO 601R-55-41-299REV -- 2025-03-11
- [SDR SWI2025F00597](https://openairdocs.org/sdr/SWI2025F00597.md): Trunnion · gouged · Dec 4, 2024 · N910SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RH MLG TRUNNION FITTING HAS GOUGES ON THE FORWARD AND AFT BEARING LUGS. (C-CHECK RO 04/30/2025)BLENDED AREAS AT RH MLG TRUNNION FITTING FWD AND AFT BEARING,PERFORMED UT AND HFEC NDT INSPECTION, PERFORMED ROTO PEED AND RESTORED AREA TO SURFACE FINISH, REWORKED
- [SDR SWIA202504301204](https://openairdocs.org/sdr/SWIA202504301204.md): Seat Track · corroded · Dec 4, 2024 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH-PAX CAB, OVERWING SECTION, CORROSION ON SEAT TRACK FLANGES, MULTIPLE AREAS BETWEEN FS 409+128 TO 559, WL 73, RBL9 (C-CHECK RO 04/30/2025)PERFORMED REPAIR AT PRESSURE FLOOR BEAM RBL9 BTWN FS= 409+118 TO FS559 IN REF. TO REO 601R-53-41-3292 REV. --. REPLACED
- [SDR SWIA202504301126](https://openairdocs.org/sdr/SWIA202504301126.md): Floor Panel · corroded · Nov 26, 2024 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT MIDDLE LOWER FUSELAGE FLOOR FS. 529-FS.559 AROUND ANCHOR NUTS CORRODED AS MARKED. (C-CHECK RO 04/30/2025)COMPLIED WITH REO 601R-53-41-3288 REV-- DATE 2025-01-26 THRESHOLD 12 MONTH FROM ISSUE DATE 26 JANUARY 2025
- [SDR SWIA202504301119](https://openairdocs.org/sdr/SWIA202504301119.md): Vane · chafed · Nov 19, 2024 · N910SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH WING, OTBD FLAP VANE MOUNT FITTINGS SHOW CHAFFING AND WEAR ALONG THE LOWER EDGE, AT WS 171, 189, 235, 280, 296, (5EA FITTINGS) (C-CHECK RO 04/30/2025) COMPLIED WITH REO 601R-57-53-195 DISPOSITION FOR WEAR DAMAGE ON O/B FLAPS BUJTE DOOR CAMS AND RIB FITTING
- [SDR SWIA202404301118](https://openairdocs.org/sdr/SWIA202404301118.md): Fairing · corroded · Nov 18, 2024 · N910SW · Cndair CL6002B19 · Aerodynamic Fairings
  > CORROSION ON WING TO FUSELAGE FITTING OUTER SURFACE AT FS 473Â (C-CHECK RO 04/30/2025)CLEANED UP CORROSION, PERFORMED HFEC NDT INSPECTION, NO CRACKS NOTED, PERFORMED ROTO PEEN ON BLENDED AAREAS AND RESTORED AREAS TO SURFACE FINISH REF. TO MHIRJ CRJ200 SRM 51-
- [SDR SWIA202156370](https://openairdocs.org/sdr/SWIA202156370.md): Skin · gouged · Feb 19, 2021 · N910SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > 2 GOUGES ON UPPER CARGO DOOR OUTER SKIN. FILED CLOSED. COMPLIED WITH TEMPORARY REPAIR TO UPPER CARGO DOOR OUTER SKIN PER REO 601R-52-31-344 REV-- DATE 2021-02-19. COMPLIED WITH RII CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR AND WITH FORM M-337.
- [SDR SWIA202053685](https://openairdocs.org/sdr/SWIA202053685.md): Wire Harness · inoperative · Oct 26, 2020 · N910SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > STEERING INOPERABLE AND WOW INPUT CAUTION MESSAGES AFTER TAKEOFF. FLIGHT 5296-FILED CLOSED. REMOVED AND REPLACED THE NOSE WOW HARNESS ASSEMBLY IN REFERENCE TO CRJ 200 AMM. OPERATIONS AND RIG CHECK OF THE STEERING SYSTEM AND PROXIMITY SENSOR SYSTEM GOOD AT T
- [SDR SWIA2020090952378](https://openairdocs.org/sdr/SWIA2020090952378.md): Floor Support · corroded · Aug 17, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR BEAM CAP CORRODED AT FS 559-112 TO FS 621. C-CHECK RO 9/5/2020. INSTALLED A NEW SERVICEABLE FLOOR BEAM AT FS 559+112 TO FS 621.00, IAW CRJ 200 SRM AND BOMBARDIER REO. COMPLIED WITH FORM M337 AND NO CHANGE TO WEIGHT AND BALANCE.
- [SDR SWIA2020090952381](https://openairdocs.org/sdr/SWIA2020090952381.md): Seat Track · damaged · Aug 11, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > ON REMOVAL OF THE SEAT RAIL CAP BEAM AT LBL 27 AT FS 559+112-FS 621.00 FOUND THE WEBS AT FS 574.00-FS589.00, FS589.00-FS605.00 AND FS605.00-FS621.00 HOLES ARE ELONGATED AND BLOWN, NEED REPLACED. C-CHECK RO 9/5/2020. INSTALLED NEW WEBS, IAW CRJ 200 SRM AND DR
- [SDR SWIA2020090952377](https://openairdocs.org/sdr/SWIA2020090952377.md): Frame · cracked · Aug 11, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF FRAME FS 364.00 FOUND STR 24R TO BE CRACKED. C-CHECK RO 9/5/2020. REPAIRED FS 364.00 STR 24R, IAW CRJ 200 SRM PARAGRAPH 5 STEPS 1 THRU 17. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA2020090952375](https://openairdocs.org/sdr/SWIA2020090952375.md): Splice Angle · corroded · Aug 11, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SPLICE ANGLE AT FS 409 STRG 26L-STRG 26R REQUIRES REPLACEMENT. C-CHECK RO 9/5/2020. REMOVED AND REPLACED SPLICE ANGLE AT FS 409 STR 26L-STR 26R, IAW CRJ200 SRM AND DRAWING. COMPLIED WITH SKYCARD AND FORM M-337. PART FOR PART REPLACEMENT. WEIGHT AND BALANC
- [SDR SWIA2020090952397](https://openairdocs.org/sdr/SWIA2020090952397.md): Skin · chafed · Aug 5, 2020 · N910SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RT & LT LOWER WING PLANK SKIN AT REAR SPAR CHAFED AT BL45 APROX 2" LONG BY 1" WIDE BY.005" DEEP. C-CHECK RO 9/5/2020. RIGHT HAND AND LEFT HAND LOWER WING PLANK SKIN AT REAR SPAR BL 45 CHAFES WERE REPAIRED, IAW BOMBARDIER REO. MATERIAL REMOVED WAS.036' AT
- [SDR SWIA2020090952434](https://openairdocs.org/sdr/SWIA2020090952434.md): Seat Track · damaged · Aug 3, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT FLOOR SEAT TRACK BETWEEN FS 409+126 AND FS 559 AT LBL 9 REQUIRES REPLACEMENT IAW REO601R-53-00-485 REV D 2018-01-29. C-CHECK RO 9/5/2020. COMPLIED WITH ALL STEPS OF BOMBARDIER REO.
- [SDR SWIA2020090952400](https://openairdocs.org/sdr/SWIA2020090952400.md): Seat Track · cracked · Aug 2, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFTER REMOVING SEAT RAIL BEAM CAP AT LBL 27, FS 621-574, BEAM WEB FOUND TO BE CRACKED. C-CHECK RO 9/5/2020. REMOVED AND REPLACED LBL 27, FS 621-574, BEAM WEB IAW AMM SRM.
- [SDR SWIA2020090952384](https://openairdocs.org/sdr/SWIA2020090952384.md): Frame · damaged · Jul 31, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT SIDE OF FS 409 BETWEEN STINGERS 25R AND 26R WAS DAMAGED DURING PART REMOVALS. REQUIRES ENGINEERING. C-CHECK RO 9/5/2020. REPAIRED DAMAGE ON AFT SIDE OF FS 409 BETWEEN STRINGERS 25R AND 26R, IAW MHI RJ REO. TASK CARD COMPLIED WITH, M-337 COMPLETED. WEI
- [SDR SWIA2020090952396](https://openairdocs.org/sdr/SWIA2020090952396.md): Stiffener · cracked · Jul 27, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409+128 VERTICAL POSTS LBL 18 OUTBOARD SIDE HAS INDICATION NOTED.250 LONG 50% FSH AT WL 69.0 AFT FLANGE RADIUS, FAILED NDT INSPECTION. C-CHECK RO 9/5/2020. REMOVED AND INSTALLED NEW LBL 18 VERTICAL POST AT FS 409+128, IAW BOMBARDIER REO AND SRM. C
- [SDR SWIA2020090952395](https://openairdocs.org/sdr/SWIA2020090952395.md): Skin · corroded · Jul 27, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN A FS 559+16 BETWEEEN STR 26L AND STR 26R HAS MINOR CORROSION. C-CHECK RO 9/5/2020. REPAIRED FUSELAGE EXTERIOR SKIN AT FS 559+16 BETWEEEN STR 26L AND STR 26R BY REMOVING MINOR CORROSION, IAW REO. M-337 AND SKYCARD COMPLETED, NO CHANGE
- [SDR SWIA2020090952431](https://openairdocs.org/sdr/SWIA2020090952431.md): Seat Track · corroded · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK FS 399-FS 409+128 SEGMET IS CORRODED. C-CHECK RO 9/5/2020. NEW SEAT TRACK WAS FABRICATED ON CAMP 21331115 AND INSTALLED IAW CRJ 200 AMM, AS DOCUMENTED ON ATTACHED CONTINUATION CARD.
- [SDR SWIA2020090952430](https://openairdocs.org/sdr/SWIA2020090952430.md): Seat Track · corroded · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK FS 364-FS 399 SEGMENT IS CORRODED. C-CHECK RO 9/5/2020. REMOVED AND REPLACED LBL 9 FLOOR SEAT TRACK FS 364-FS 399, IAW CRJ-200 AMM PN NR 601R31032-15.
- [SDR SWIA2020090952399](https://openairdocs.org/sdr/SWIA2020090952399.md): Support Angle · cracked · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO BAY DOOR CAM TRACK SUPPORT ANGLE CRACKED ON LOWER SIDE OF BEAM AT FS 621.00.00. C-CHECK RO 9/5/2020. REMOVED AND REPLACED CARGO BAY DOOR CAM TRACK LOWER SUPPORT BRACKET, IAW CRJ200 SRM.
- [SDR SWIA2020090952394](https://openairdocs.org/sdr/SWIA2020090952394.md): Channel · corroded · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DRAIN MAST DOUBLER BETWEEN STRG 25R-24R AND FS333-349 IS CORRODED. C-CHECK RO 9/5/2020. REMOVED AND INSTALLED NEW DRAIN MAST DOUBLER, IAW CRJ 200 SRM AND DRAWING. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. P
- [SDR SWIA2020090952393](https://openairdocs.org/sdr/SWIA2020090952393.md): Floor Support · corroded · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR BEAM TOP CAP IS CORRODED FROM FS 409+5 TO FS 409+118. C-CHECK RO 9/5/2020. PERFORMED A MAJOR REPAIR BY REPLACING FLOOR BEAM CAP AT LBL 9 BETWEEN FS 409+5 AND FS 409 +118, IAW MHIRJ REO AND CRJ 200 SRM. SKYWEST TASK IS COMPLETE, FORM M-337 IS ATT
- [SDR SWIA2020090952385](https://openairdocs.org/sdr/SWIA2020090952385.md): Floor Support · corroded · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR BEAM TOP CAP IS CORRODED FROM FS 409+5 TO FS 409+118. C-CHECK RO 9/5/2020. REMOVED UNSERVICEABLE RBL 9 FLOOR BEAM TOP CAP AT FS 409+5 TO FS 409+118 AND INSTALLED SERVICEABLE RBL 9 FLOOR BEAM TOP CAP AT FS409+5 TO FS409+118, IAW CRJ-200 SRM AND MH
- [SDR SWIA2020090952380](https://openairdocs.org/sdr/SWIA2020090952380.md): Intercostal · corroded · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 4 EA INTERCOSTALS BETWEEN STGR 26L-26R AND FS 349-364 ARE CORRODED. C-CHECK RO 9/5/2020. INSTALLED NEW INTERCOSTALS AT FS 349-364 STR 26L - 26R, IAW CRJ 200 SRM. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. PA
- [SDR SWIA2020090952376](https://openairdocs.org/sdr/SWIA2020090952376.md): Seat Track · corroded · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK FS 399-FS 409+128 SEGMENT IS CORRODED. C-CHECK RO 9/5/2020. REMOVED DAMAGED SEAT TRACK ON FS 399 TO 499+128 AT RBL 9 AND INSTALLED WITH NEW SERVICEABLE SEAT TRACK, IAW CRJ200-AMM.
- [SDR SWIA2020090952373](https://openairdocs.org/sdr/SWIA2020090952373.md): Stringer · cracked · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR 3L IS CRACKED AT FS 378 AFT END OF PAX DOOR UPPER SILL. C-CHECK RO 9/5/2020. REPAIRED STR 3 AT FS 378 IAW CRJ 200 SRM. COMPLIED WITH SKYCARD AND FORM M-337. WEIGHT AND BALANCE NOT AFFECTED. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA2020090952369](https://openairdocs.org/sdr/SWIA2020090952369.md): Seat Track · corroded · Jul 25, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK FS 364-FS 399 SEGMENT IS CORRODED. C-CHECK RO 9/5/2020. REMOVED AND REPLACED RBL 9 FLOOR SEAT TRACK FS 364-FS 399, IAW CRJ-200 AMM.
- [SDR SWIA2020090952429](https://openairdocs.org/sdr/SWIA2020090952429.md): Floor Support · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 317 RBL 6 IS CORRODED. C-CHECK RO 9/5/2020. FLOOR SUPPORT DOUBLER WAS REMOVED, IAW CRJ 200 SRM. NEW PART WAS FABRICATED WITH DRAWING AND TEMPLATE AND INSTALLED IAW CRJ 200 SRM, AS DOCUMENTED ON ATTACHED CONTINUATION CAR
- [SDR SWIA2020090952428](https://openairdocs.org/sdr/SWIA2020090952428.md): Seat Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK CORRODED FROM FS 559+85 TO F 559.00+112 AT LBL 9.00. C-CHECK RO 9/5/2020. LOCATED AND DRILLED NEW SERVICEABLE CARGO FLOOR TRACK FROM FS 559+85 TO FS 559.00+112 AT LBL 9.00, IAW CRJ 200 SRM. REMOVED AND INSTALLED NEW SERVICEABLE CARGO FLOOR
- [SDR SWIA2020090952427](https://openairdocs.org/sdr/SWIA2020090952427.md): Cargo Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK CORRODED FROM FS 559+85 TO F 559.00+112 AT LBL 27.00. C-CHECK RO 9/5/2020. REMOVED AND INSTALLED NEW SERVICEABLE CARGO FLOOR TRACKS FROM FS 559+85 TO FS 559.00+112 AT LBL 27.00, IAW CRJ 200 AMM. REMOVED AND INSTALLED NEW CARGO FLOOR FITTIN
- [SDR SWIA2020090952426](https://openairdocs.org/sdr/SWIA2020090952426.md): Cargo Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK CORRODED FROM FS 559+85 TO F 559.00+112 AT RBL 27.00. C-CHECK RO 9/5/2020. LOCATED AND DRILLED NEW SERVICEABLE CARGO FLOOR TRACKS IAW CRJ 200 SRM. REMOVED AND INSTALLED NEW SERVICEABLE CARGO FLOOR TRACK AND NEW FITTING IAW CRJ 200 AMM.
- [SDR SWIA2020090952425](https://openairdocs.org/sdr/SWIA2020090952425.md): Cargo Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK CORRODED FROM FS 559+85 TO F 559.00+112 AT RBL 9.00. C-CHECK RO 9/5/2020. LOCATED AND DRILLED NEW SERVICEABLE CARGO FLOOR TRACK IAW CRJ 200 SRM. REMOVED AND INSTALLED NEW SERVICEABLE CARGO FLOOR TRACK IAW CRJ 200 AMM. REMOVED AND INSTALLE
- [SDR SWIA2020090952424](https://openairdocs.org/sdr/SWIA2020090952424.md): Cargo Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK CORRODED FROM FS 559+112 TO FS 621.00 AT LBL 9.00. C-CHECK RO 9/5/2020. REMOVED AND INSTALLED SERVICEABLE CARGO FLOOR TRACK AT FS 559- FS621 LBL 9 IAW CRJ 200 SRM.
- [SDR SWIA2020090952423](https://openairdocs.org/sdr/SWIA2020090952423.md): Floor Support · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL FLOOR SUPPORT CAP ANGLE HAS CORRODED FASTENERS. C-CHECK RO 9/5/2020. REMOVED AND REPLACED CORRODED FASTENERS IAW CRJ-200-SRM.
- [SDR SWIA2020090952422](https://openairdocs.org/sdr/SWIA2020090952422.md): Floor Support · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL FLOOR SUPPORT CUPS ARE CORRODED. C-CHECK RO 9/5/2020. PAX DOOR LOWER SILL FLOOR SUPPORT CUPS AND CLEATS WERE REMOVED AND NEW PARTS INSTALLED, IAW CRJ 200 SRM AS DOCUMENTED ON ATTACHED CONTINUATION CARD.
- [SDR SWIA2020090952421](https://openairdocs.org/sdr/SWIA2020090952421.md): Floor Support · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 310 LBL 37 IS CORRODED. C-CHECK RO 9/5/2020. FABRICATED NEW BOLT HOLE DOUBLER AND INSTALLED IAW CRJ 200 SRM.
- [SDR SWIA2020090952420](https://openairdocs.org/sdr/SWIA2020090952420.md): Seat Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK CORRODED FROM FS 559+112 TO FS 621.00 AT LBL 27.00. C-CHECK RO 9/5/2020. REMOVED UNSERVICEABLE CARGO FLOOR TRACK FROM FS 559+112 TO FS 621.00 AT LBL 27.00 AND INSTALLED NEW SERVICEABLE CARGO FLOOR TRACK FROM FS 559+112 TO FS 621.00 AT LBL 2
- [SDR SWIA2020090952392](https://openairdocs.org/sdr/SWIA2020090952392.md): Crossbeam · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 280 CROSSBEAM AND FWD J ANGLE ARE CORRODED LBL 19 TO RBL 27. C-CHECK RO 9/5/2020. REPAIRED FS 280 CROSSBEAM AND FWD J ANGLE, IAW REO CRJ-200 SRM. TASK CARD COMPLIED WITH, M-337 ATTACHED. WEIGHT AND BALANCE NOT AFFECTED.
- [SDR SWIA2020090952391](https://openairdocs.org/sdr/SWIA2020090952391.md): Seat Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL BEAM CAP CORRODED BETWEEN FS 605 AND FS 621 AND AT LBL 27. C-CHECK RO 9/5/2020. PERFORMED A MAJOR REPAIR BY REPLACING THE CARGO FLOOR BEAM AT LBL 27 BETWEEN FS 570 AND FS 621, IAW CRJ 200 SRM AND BOMBARDIER REO. COMPLETED SKYWEST TASK CARD. COMPL
- [SDR SWIA2020090952390](https://openairdocs.org/sdr/SWIA2020090952390.md): Frame · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CORRODED AT FS 605.00 BETWEEN STGR 26R AND STGR 23L. C-CHECK RO 9/5/2020. REMOVED AND REPLACED FS 605.00 BETWEEN STR 26R AND 23L, IAW CRJ 200 SRM AND DRAWING. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA2020090952379](https://openairdocs.org/sdr/SWIA2020090952379.md): Seat Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL BEAM CAP CORRODED BETWEEN FS 605 AND FS 621 AND AT RBL 27. C-CHECK RO 9/5/2020. PERFORMED A MAJOR REPAIR BY REPLACING THE SEAT RAIL CAP AT RBL 27 BETWEEN FS 605 AND FS 621, IAW BOMBARDIER REO AND CRJ-200 SRM. SKYWEST TASK IS COMPLETE. FORM M-337
- [SDR SWIA2020090952371](https://openairdocs.org/sdr/SWIA2020090952371.md): Seat Track · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK CORRODED FROM FS 559+112 TO FS 621.00 AT RBL 9.00. C-CHECK RO 9/5/2020. REMOVED AND INSTALLED NEW SERVICEABLE CARGO SEAT TRACK, IAW CRJ 200 AMM.
- [SDR SWIA2020090952367](https://openairdocs.org/sdr/SWIA2020090952367.md): Nut Plate · corroded · Jul 24, 2020 · N910SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT CAP STRIP CORRODED AT FS 574 AND BETWEEN RBL 27.00 AND RBL 47.00. C CHECK RO 9/5/2020. REMOVED AND REPLACED FLOOR SUPPORT CAP STRIP AT FS 589 BETWEEN RBL 27 AND 47, IAW CRJ-200.
- [SDR SWIA2020090952419](https://openairdocs.org/sdr/SWIA2020090952419.md): Strap · corroded · Jul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT PRESSURE FLOOR STRAP CORRODED AT APPROX FS 559.00 AND BETWEEN RBL 36 AND RBL 45.00. C-CHECK RO 9/5/2020. REMOVED AND REPLACED RT PRESSURE FLOOR STRAP AT APPROX FS 559 BETWEEN RBL 36 AND RBL 45 P/N 601R31025-29, IAW CRJ200 SRM.
- [SDR SWIA2020090952418](https://openairdocs.org/sdr/SWIA2020090952418.md): Floor Support · corroded · Jul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL CORRODED BETWEEN FS 559 TO FS 559+80 IN SEVERAL LOCATIONS ALONG RBL 42.90. C-CHECK RO 9/5/2020. COMPLIED WITH BOMBARDIER REO.
- [SDR SWIA2020090952417](https://openairdocs.org/sdr/SWIA2020090952417.md): Seat Track · corroded · Jul 23, 2020 · N910SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR SEAT TRACK CORRODED BETWEEN FS 559.00 TO FS 559.00+80 ALONG RBL 9.00. C-CHECK RO 9/5/2020. INSTALLED NEWLY FABRICATED SEAT TRACK (REFER TO 97566105$M51), IAW CRJ 200 AMM.

Next page: https://openairdocs.org/aircraft/N910SW/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 = 'N910SW'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N910SW/reports

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