# Service difficulty reports: N951SW

A list on [N951SW](https://openairdocs.org/aircraft/N951SW.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 · 183 reports

- [SDR SWIA2026070776607](https://openairdocs.org/sdr/SWIA2026070776607.md): Windshield · cracked · Jul 7, 2026 · N951SW · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT WINDSHIELD CRACK AND R WSHLD HEAT CAUTION MESSAGE CLIMBING THROUGH 18,000 FEET. (FLIGHT 6097) OPEN
- [SDR SWIA2026041776314](https://openairdocs.org/sdr/SWIA2026041776314.md): Frame · chafed · Apr 17, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING AUDIT OF TASK CARD 53-350-500 IT WAS FOUND THAT THERE IS A CHAFED FRAME AREA AFT OF APU EXHAUST BS 654.50. REPAIRED FRAME AFT OF APU EXHAUST BS 654.5 IAW SRM 51-42-06, 51-42-21, DWG 601R35004, REV BJ, AND REO 601R-53-61-8529, REV.--. COMPLIED WITH TAS
- [SDR SWIA2026041576339](https://openairdocs.org/sdr/SWIA2026041576339.md): Angle · cracked · Apr 15, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOT SIDE POST OTBD LWR ANGLE CRACKED. REPLACED CO-PILOT SIDE POST OTBD LOWER ANGLE IAW DWG 601R33007, REV -U, SRM 51-42-21, AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026041576316](https://openairdocs.org/sdr/SWIA2026041576316.md): Seat Track · out of limits · Apr 15, 2026 · N951SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > REMOVE AND REPLACE DAMAGED OUT OF LIMITS SEAT RAIL BEAM P/N 601R35031-263. SEE JOB HN00303609, CAMP# 31969028. (32083421). (C-CHECK RO 06/25/2026)REMOVED AND REPLACED SEAT RAIL BEAM AT LBL27 BETWEEN APPROX. FS574 AND FS621. IAW SRM 51-42-06, SRM 51-42-21, RE
- [SDR SWIA2026062676318](https://openairdocs.org/sdr/SWIA2026062676318.md): Floorbeam · damaged · Apr 13, 2026 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AT BS 574, RBL 36 FLOOR SUPPORT HAS A SCRIBE LINE ACROSS THE TOP. INSTALLED NEW TOP CAP STRIP AT BS 574 AT APPOX RBL36 IAW SRM 51-42-06, SRM 51-42-15, AND DWG 601R35031, REV AG. FOR FASTENER CALL OUTCOMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026041076337](https://openairdocs.org/sdr/SWIA2026041076337.md): Hinge Fitting · corroded · Apr 10, 2026 · N951SW · Cndair CL6002B19 · Elevator, Tab Structure
  > UPON REMOVAL ON JOB HN00303104 CAMP 31954799, FOUND LT ELEVATOR L/E HINGE FITTING ASSY, ES 16.52 TO HAVE PITTING CORROSION IN BEARING BORES ON BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. INSTALLED 1 EA NEW L/E HINGE FITTING ASSY ON L/H ELEVATOR AT ES16.52
- [SDR SWIA2026040976344](https://openairdocs.org/sdr/SWIA2026040976344.md): Bulkhead Web · cracked · Apr 9, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > UPON REMOVAL FWD FLOORBEAM ANGLE AT BS 280 BETWEEN RBL 9 AND LBL 9, FOUND CRACKED. REPAIRED BULKHEAD WEB IAW REO 601R-53-11-926, REV -B, & REO 601R-53-21-3811, REV -, COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026062676341](https://openairdocs.org/sdr/SWIA2026062676341.md): Hinge Arm · gouged · Apr 8, 2026 · N951SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP HINGE ARM WS 80.50 ATTACH LUG GOUGED. REPAIRED GOUGED DAMAGE ON LT INBD FLAP HINGE ARM WS 80.50 ATTACH LUG IAW REO 601R-57-54-392 REV -. COMPLIED WITH SKYCARD 51-900-1003-SKY. MAJOR REPAIR.
- [SDR SWIA2026040776334](https://openairdocs.org/sdr/SWIA2026040776334.md): Floorbeam · cracked · Apr 7, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CRACKED ON ANGLE AT FLOORBEAM ON BS 621 BETWEEN LBL 27 & LBL 35. COMPLIED WITH GREO 601R-53-61-117, REV -E. FABRICATED AND INSTALLED NEW ANGLE IAW REO 601R-53-61-8533, REV. --, AND RESTORED FINISH AND APPLIED CIC, PRESSURE LEAK CHECK GOOD AT THIS TIME. COMP
- [SDR SWIA2026040476351](https://openairdocs.org/sdr/SWIA2026040476351.md): Windshield · cracked · Apr 4, 2026 · N951SW · Cndair CL6002B19 · Flight Compartment Windows
  > PILOT SIDE WINDOW CRACKED ALL AROUND THE EDGES OF THE WINDOW. INSTALLED NEW/SERVICEABLE PILOT SIDE WINDOW IAW AMM 56-12-01-400-801. COMPLIED WITH 56-220-1000-SKY.
- [SDR SWIA2026040376326](https://openairdocs.org/sdr/SWIA2026040376326.md): Intercostal · corroded · Apr 3, 2026 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE STR 21L INTERCOSTAL (BACKUP SILL) BS 310 - 319.70 IS CORRODED THROUGH AND CRACKED. REMOVED AND REPLACED INTERCOSTAL AT STR 21L BETWEEN BS 310 & 333. IAW SRM 51-42-06, SRM 51-42-21, AND DRAWING 601R31527, REV AM, SHEET 2. COM
- [SDR SWIA2026040276328](https://openairdocs.org/sdr/SWIA2026040276328.md): Skin · scratched · Apr 2, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CIRCUMFERENTIAL FUSELAGE SPLICE AT BS 280, BETWEEN STR 23-22 LT, HAS SCRATCHES, COMPLIED WITH REO 601R-53-00-936 REV-, ALL STEPS, STEP 1 ENSURED BLEND-OUTS WERE PERFORMED TO A SMOOTH CONTOUR, STEP 2 PERFORMED NDT (SEE STEP 2A OF THIS CONTINUE CARD), STEP 3 R
- [SDR SWIA2026040176335](https://openairdocs.org/sdr/SWIA2026040176335.md): Rib · cracked · Apr 1, 2026 · N951SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > CRACK NOTED ON RT WING BATT RIB AT WS48.3. REMOVED AND REPLACED RT WING BATT RIB AT WS48.3 REF. SRM 51-42-21 REV. AND DWG 600-10204, REV-M. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026040176327](https://openairdocs.org/sdr/SWIA2026040176327.md): Doubler · corroded · Apr 1, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION NOTED ON DOUBLER COMMON TO ELECTRICAL CONNECTORS J410 AND J412 AT RT RIB REAR SPAR ASSY. AT WS53.60. REMOVED AND INSTALLED NEW DOUBLER ANGLE ON BATT RIB, WS53.6 PER CRJ200 SRM 51-42-06 AND DWG NO. 601R10203 REV -G. OPS CHECK GOOD. COMPLIED TASK CARD
- [SDR SWIA2026062676343](https://openairdocs.org/sdr/SWIA2026062676343.md): Retainer · corroded · Mar 30, 2026 · N951SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR FORWARD LEFT SEAL RETAINER CORRODED. REMOVED AND INSTALLED NEW AVIONICS BAY DOOR FORWARD LEFT SEAL RETAINER IAW SRM 51-42-06 AND DWG CC670-38651 REV -E. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026062676321](https://openairdocs.org/sdr/SWIA2026062676321.md): Angle · corroded · Mar 30, 2026 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UNDERFLOOR BS 605, ANGLE BETWEEN STR 20 - 21 LT, WAS CORRODED, REMOVED AND INSTALLED NEW ANGLE AT BS 605 BETWEEN STR 20L- STR 21L IAW SRM 51-42-06, SRM 51-42-21, & DWG 601R36026, REV AF, RESTORED FINISH TO OUTER SKIN RIVETS AND INSIDE ANGLE AREA IAW SRM 51-2
- [SDR SWIA2026032976346](https://openairdocs.org/sdr/SWIA2026032976346.md): Skin · dented · Mar 29, 2026 · N951SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INNER SKIN UNDERNEATH FWD STAIR WEB DRAG ANGLE DENTED NEXT TO A HOLE. COMPLIED REPAIR STEPS 1 TO 15 ON PASSENGER DOOR INNER SKIN BETWEEN DOOR DATUM 6 AND DOOR DATUM 7 OF REO 601R-52-11-3096, REV. --. COMPLIED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026032976324](https://openairdocs.org/sdr/SWIA2026032976324.md): Floorbeam · corroded · Mar 29, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > UNDERFLOOR BS 589, LBL 9 - 27, FLOORBEAM WAS CORRODED, INSTALLED A NEW TOP CAP STRIP IAW SRM 51-42-21, REV 39, 51-42-06, REV 39, SRM 51-42-15, REV 39, AND DWG. 601R35031 REV. AG COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026032976312](https://openairdocs.org/sdr/SWIA2026032976312.md): Floorbeam · corroded · Mar 29, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > UNDERFLOOR BS 559+48, RBL 9-27, FLOORBEAM HAS CORROSION, REMOVED AND REPLACED THE PLATE AT FS 559+48 BETWEEN LBL9 AND LBL27. IAW SRM 51-42-06, SRM 51-42-15, AND DWG 601R32215, REV. M, SHEET 8. COMPLIED WITH TASK CARD 51-900-1003-SKY. MAJOR REPAIR.
- [SDR SWIA2026032876350](https://openairdocs.org/sdr/SWIA2026032876350.md): Windshield · cracked · Mar 28, 2026 · N951SW · Cndair CL6002B19 · Flight Compartment Windows
  > PILOT WINDSHIELD HAS POSSIBLE CRACK LT LOWER SIDE. INSTALLED NEW SERVICEABLE PILOT WINDSHIELD IAW AMM 56-11-01-400-801.
- [SDR SWIA2026062676317](https://openairdocs.org/sdr/SWIA2026062676317.md): Floor Support · corroded · Mar 27, 2026 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAD MULTIPLE SPOTS OF CORROSION AT LBL 27 BETWEEN BS 574 - 621. REPLACEMENT OF FLOOR SUPPORT AT LBL 27 BETWEEN BS 574 AND BS 606.5 PERFORMED ON JOB HN00307254, CAMP 32083421. REPAIRED END FITTING AT LBL 27 BETWEEN BS 606.5 AND BS 621 IAW REO 60
- [SDR SWIA2026032576330](https://openairdocs.org/sdr/SWIA2026032576330.md): Lug · damaged · Mar 25, 2026 · N951SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE LUGS ELONGATED ON FUSELGE SIDE. INSTALLED NEW PASSENGER DOOR HINGE ON FUSELAGE SIDE. IAW SRM 53-21-23 REPAIR NR -01 AND REO 601R-53-21-656, REV. B. COMPLIED WITH 51-900-1003-SKY. LEAK CHECKED GOOD.
- [SDR SWIA2026032476345](https://openairdocs.org/sdr/SWIA2026032476345.md): Skin · gouged · Mar 24, 2026 · N951SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON LEADING EDGE GOUGED AND CHAFED IN MULTIPLE LOCATIONS. REPLACED THE LH AILERON LEADING EDGE SKIN IAW DWG CC670-13000, REV-D, SRM 51-42-06, SRM 51-42-21, AND SRM 51-42-22. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026032476342](https://openairdocs.org/sdr/SWIA2026032476342.md): Skin · gouged · Mar 24, 2026 · N951SW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON LEADING EDGE GOUGED AND CHAFED IN MULTIPLE LOCATIONS. REPLACED RT AILERON LEADING EDGE SKIN IAW DWG 601R13031, REV-K, SRM 51-42-06 AND SRM 51-42-13. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026032376338](https://openairdocs.org/sdr/SWIA2026032376338.md): Retainer · corroded · Mar 23, 2026 · N951SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONIC BAY DOOR FORWARD RIGHT ANGLE UNDER SEAL RETAINER HAS CORROSION AROUND FASTENER HOLES. REMOVED AND INSTALLED NEW FORWARD RIGHT ANGLE ON AVIONICS BAY DOOR IAW SRM 51-42-06, SRM 51-42-21, SRM 51-41-02, AND DWG CC670-38651 REV -E. OPS & LEAK CHKD GOOD.
- [SDR SWIA2026032376332](https://openairdocs.org/sdr/SWIA2026032376332.md): Retainer · corroded · Mar 23, 2026 · N951SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONIC BAY DOOR AFT RIGHT ANGLE UNDER SEAL RETAINER HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED AFT RIGHT ANGLE ON AVIONICS BAY DOOR IAW SRM 51-42-06, SRM 51-42-21, SRM 51-41-02, AND DWG CC670-38651 REV -E SHEET 1. COMPLIED WITH SKYWEST TASK C
- [SDR SWIA2026032376325](https://openairdocs.org/sdr/SWIA2026032376325.md): Housing · gouged · Mar 23, 2026 · N951SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR EXTERIOR HANDLE HOUSING GOUGED. FOUND DAMAGE TO BE OUT OF LIMITS IAW REO 601R-52-31-086, REV -. REMOVED AND REPLACED CARGO DOOR EXTERIOR HANDLE HOUSING ASSY. IAW SRM 51-40-11, SRM 51-42-21, SRM 51-23-00 AND DWG CC670-38702, REV -F. RESTORED FINISH
- [SDR SWIA2026032376320](https://openairdocs.org/sdr/SWIA2026032376320.md): Vane · dented · Mar 23, 2026 · N951SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT OTBD FLAP VANE LEADING EDGE DENTED ON INBD END. REPAIRED DENTED AREA ON THE RH OTBD FLAP VANE LEADING EDGE AT INBD END IAW SRM 51-42-13, REV 39, AND DWG 601R14502, REV D. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026032376313](https://openairdocs.org/sdr/SWIA2026032376313.md): Rib · corroded · Mar 23, 2026 · N951SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING BATT RIB WS53.60 FORWARD END, ANGLE IS CORRODED ON THE FLANGE AND WEB. REMOVED AND INSTALLED NEW ANGLE ON LEFT WING BATT RIB WS53.60 FWD. IAW DWG 601R10203, REV G. AND SRM 51-42-21, SRM 51-42-06 AND SRM 51-42-15. OPS TESTED GOOD. COMPLIED WITH TASK
- [SDR SWIA2026032176336](https://openairdocs.org/sdr/SWIA2026032176336.md): Floor Support · corroded · Mar 21, 2026 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN APPROX. BS 409+128 - BS 559. REMOVED MULTIPLE AREAS OF CORROSION ON LT PRESSURE FLOOR SILL BETWEEN APPROX. BS 409+128 - 559 IAW SRM 51-21-06. REV. 39. COMPLIED W/ ALL STEPS OF REO 601R-53-41-3
- [SDR SWIA2026032176333](https://openairdocs.org/sdr/SWIA2026032176333.md): Floor Support · corroded · Mar 21, 2026 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT PRESSURE FLOOR SUPPPORT HAS MULTIPLE AREAS OF CORROSION. REPAIRED MULTIPLE AREAS OF CORROSION IAW SRM 51-26-00, GREO 601R-53-41-666, REV-C, & REO 601R-53-41-3421 REV-. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2026032176331](https://openairdocs.org/sdr/SWIA2026032176331.md): Floorbeam · damaged · Mar 21, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > AT BS 574, RBL 36 FLOORBEAM HAS A SCRIBE LINE ACROSS THE TOP. REMOVED AND REPLACED FLOORBEAM CAP STRIP AT BS 574 BETWEEN RBL 9 AND RBL 27 IAW SRM 51-42-06, REV-. COMPLIED WITH TASK CARD 51-900-1003-SKY AND DWG. 601R35031 REV. AG.
- [SDR SWIA2026032176322](https://openairdocs.org/sdr/SWIA2026032176322.md): Floor Support · corroded · Mar 21, 2026 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT LBL 9 JUST FORWARD OF BS 621 CORRODED AROUND NUTPLATES. REMOVED CORROSION FROM FLOOR SUPPORT LBL 9 JUST FORWARD OF BS 621 IAW REO 601R-53-61-8497. REV. -, ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026032076329](https://openairdocs.org/sdr/SWIA2026032076329.md): Skin · corroded · Mar 20, 2026 · N951SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RBL45 RT WING LOWER PLANK TRAILING EDGE AREA, CORRODED & CHAFFED FROM THE WING TO BODY FAIRING. REPAIRED RBL45 RT WING LOWER PLANK TRAILING EDGE IAW REO 601R-57-21-4071 REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026062676323](https://openairdocs.org/sdr/SWIA2026062676323.md): Skin · corroded · Mar 19, 2026 · N951SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LBL 45 LT WING LOWER PLANK TRAILING EDGE AREA, CORRODED & CHAFED FROM THE WING TO BODY FAIRING. REPAIRED LBL 45 LT WING LOWER PLANK TRAILING EDGE AREA IAW GREO 601R-57-21-880, REV-D. NOTES/STEPS 1, 2, 3,5,6,7,9 AND10.,COMPLIED WITH 51-900-1003-SKY, FUEL LEAK C
- [SDR SWIA2026062676315](https://openairdocs.org/sdr/SWIA2026062676315.md): Skin · damaged · Mar 19, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TWO SCREW HOLES ELONGATED ON LT SIDE EXTERNAL SKIN BETWEEN BS 409+80 - 409+96, STR 18L- STR 20L. RECEIVED AND COMPLIED WITH REO 601R-53-31-1369 REV.--, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK GOOD.
- [SDR SWIA2026031876340](https://openairdocs.org/sdr/SWIA2026031876340.md): Skin · corroded · Mar 18, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN IS CORRODED AT SEVERAL LOCATIONS SURROUND SCREW HOLES COMMON TO PANEL 195BB. REPAIRED EXTERNAL SKIN COMMON TO PANEL 195BB IAW REO 601R-53-00-937 REV --. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026031876319](https://openairdocs.org/sdr/SWIA2026031876319.md): Skin · gouged · Mar 18, 2026 · N951SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT EXTERNAL SKIN IS GOUGED BETWEEN BS 559+96 - 574, STR 19L - 21L. REPAIRED LT EXTERNAL SKIN IAW REO 601R-53-00-937, REV--. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR ICRR20200810001](https://openairdocs.org/sdr/ICRR20200810001.md): Link · out of limits · Dec 8, 2020 · N951SW · Cndair CL6002B19 · Engine Mount Section
  > OUT OF LIMIT INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-23-103 PART 4. TSN & CSN UNKNOWN PER OPERATOR.
- [SDR SWIA202054506](https://openairdocs.org/sdr/SWIA202054506.md): Angle · cracked · Nov 17, 2020 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT UPPER OBLIQUE ANGLE BETWEEN FS 621.00 AND FS 625.00 IS CRACKED. C-CHECK RO 12/04/2020. REPLACED RT UPPER OBLIQUE ANGLE BETWEEN FS 621.00 AND FS 625.00, IAW CRJ-200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202054502](https://openairdocs.org/sdr/SWIA202054502.md): Skin · chafed · Nov 17, 2020 · N951SW · Cndair CL6002B19 · Leading Edge Devices
  > RIGHT INBOARD FLAP VANE LEADING EDGE CHAFED AT OUTBOARD STOP.010" DEEP REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED DAMAGED LEADING EDGE CAP AND INSTALLED A NEW PART, IAW CRJ 200 SRM.
- [SDR SWIA202054501](https://openairdocs.org/sdr/SWIA202054501.md): Skin · chafed · Nov 17, 2020 · N951SW · Cndair CL6002B19 · Leading Edge Devices
  > RIGHT INBOARD FLAP VANE LEADING EDGE CHAFED AT MIDDLE-OUTBOARD STOP.010" DEEP REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED AND INSTALLED NEW RT INBOARD FLAP VANE LEADING EDGE, IAW CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED.
- [SDR SWIA202054500](https://openairdocs.org/sdr/SWIA202054500.md): Skin · chafed · Nov 17, 2020 · N951SW · Cndair CL6002B19 · Leading Edge Devices
  > RIGHT INBOARD FLAP VANE LEADING EDGE CHAFED AT INBOARD STOP.020" DEEP REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED DAMAGED RT INBOARD FLAP VANE LEADING EDGE INBOARD CAP AND INSTALLED A NEW INBOARD CAP, IAW CRJ 200 SRM.
- [SDR SWIA202054507](https://openairdocs.org/sdr/SWIA202054507.md): Strap · corroded · Nov 16, 2020 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT OUTBOARD STRAP AT FS 559.00 CORRODED IN SEVERAL AREAS 601 R31025-29. C-CHECK RO 12/04/2020. REMOVED DAMAGED RT OUTBOARD STRAP AT FS 559 AND INSTALLED NEW SERVICEABLE STRAP, IAW CRJ200-SRM.
- [SDR SWIA202054499](https://openairdocs.org/sdr/SWIA202054499.md): Skin · chafed · Nov 16, 2020 · N951SW · Cndair CL6002B19 · Leading Edge Devices
  > LEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT OUTBOARD.010" OUT OF LIMIT REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. LT INBOARD FLAP LEADING EDGE OUTBOARD PANEL WAS REMOVED AND NEW PART INSTALLED, IAW CRJ 200 SRM.
- [SDR SWIA202054498](https://openairdocs.org/sdr/SWIA202054498.md): Skin · chafed · Nov 16, 2020 · N951SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT INBOARD.018" OUT OF LIMIT REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED LT INBOARD FLAP LEADING EDGE INBOARD PANEL AND INSTALLED A NEW PANEL, IAW CRJ 200 SRM.
- [SDR SWIA202054497](https://openairdocs.org/sdr/SWIA202054497.md): Seat Track · corroded · Nov 16, 2020 · N951SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK BETWEEN FS 409.0 AND 409+126 HAS SEVERAL AREAS OF CORROSION. C-CHECK RO 12/04/2020. REMOVED DAMAGED SEAT TRACK, LOCATED AND DRILLED NEW SEAT TRACK AND INSTALLED, IAW CRJ 200 SRM AND AMM.
- [SDR SWIA202054496](https://openairdocs.org/sdr/SWIA202054496.md): Floor Support · corroded · Nov 16, 2020 · N951SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SUPPORT ANGLE IS CORRODED. C-CHECK RO 12/04/2020. REPLACED PAX DOOR FLOOR SUPPORT ANGLES. REFERENCE CONTINUATION CARD FOR WORK PREFORMED.
- [SDR SWIA202054495](https://openairdocs.org/sdr/SWIA202054495.md): Seat Track · corroded · Nov 16, 2020 · N951SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK FROM FS 409 TO 409+126 HAS SEVERAL AREAS OF CORROSION. C-CHECK RO 12/04/2020. REMOVED AND REPLACED SEAT TRACK, IAW CRJ 200 AMM.
- [SDR SWIA202054494](https://openairdocs.org/sdr/SWIA202054494.md): Floorbeam · cracked · Nov 16, 2020 · N951SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 FLOORBEAM INBOARD CLIP AT FS 280 IS CRACKED. C-CHECK RO 12/04/2020. REMOVED DAMAGED INBOARD CLIP ON RBL 9 ATTACHED AT FS 280 AND INSTALLED NEW SERVICEABLE CLIP, IAW CRJ200-SRM AND RE0.

Next page: https://openairdocs.org/aircraft/N951SW/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 = 'N951SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N951SW/reports

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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.