# Service difficulty reports: N963SW

A list on [N963SW](https://openairdocs.org/aircraft/N963SW.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 · 182 reports

- [SDR SWIA2026041375687](https://openairdocs.org/sdr/SWIA2026041375687.md): Door Seal · torn · Apr 13, 2026 · N963SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AT CRUISE FELT MODERATE VIBRATION IN AIRFRAME FOLLOWED BY UNCOMMANED DEPRESSUIZATION. FOLLOWED QRC & QRH, NEITHER HAD ANY EFFECT. AT APPROX FL240-200 GOT CABIN ALT CAUTION FOLLOWED BY WARNING. DECLARED EMERGENCY AND DEVIRTED. UPON ARRIVAL AT GATE FOUND MCD DOO
- [SDR SWIA20251212008](https://openairdocs.org/sdr/SWIA20251212008.md): Trim System · warning message · Dec 8, 2025 · N963SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > ROUGHLY 2000 FT AFTER TAKEOFF. STAB TRIM & MACH TRIM CAUTION APPEARED. REENGAGED BRIEFLY & BEGAN HAVING STAB TRIM RUNAWAY. DISCONNECTED TRIM & USING MEMORY ITEMS. SHORTLY AFTER, AILERON TRIM KICKED OFF & GOT AILERON LWD & RWD. ACFT BECAME EXTREMELY DIFFICULT T
- [SDR SWIA202512090008](https://openairdocs.org/sdr/SWIA202512090008.md): Trim System · runaway · Dec 8, 2025 · N963SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > ROUGHLY 2000FT AFTER TAKEOFF. STAB TRIM & MACH TRIM CAUTION APPEARED. REENGAGED BRIEFLY & BEGAN HAVING STAB TRIM RUNAWAY. DISCONNECTED TRIM & USING MEMORY ITEMS. SHORTLY AFTER, AILERON TRIM KICKED OFF AND RECEIVED AILERON LWD AND RWD. AIRCRAFT BECAME EXTREME
- [SDR SWIA2025090200703](https://openairdocs.org/sdr/SWIA2025090200703.md): Tie Down · damaged · Jul 3, 2025 · N963SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CENTER CARGO NET TIE DOWN RING ASSY WITH TWO ANGLES (REF SRM 53-61-43 ITEMS 6 & 8) REMOVED TO F.O.M. WITH REFERENCE TO SRM 51-42-21. (C-CHECK RO 08/29/2025)INSTALLED CENTER CARGO NET TIE DOWN RING ASSY WITH TWO ANGLES (REF SRM 53-61-43 ITEMS 6 & 8) WITH REFER
- [SDR SWIA202507070003](https://openairdocs.org/sdr/SWIA202507070003.md): Tie Down · damaged · Jul 3, 2025 · N963SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CENTER CARGO NET TIE DOWN RING ASSY WITH TWO ANGLES (REF SRM 53-61-43 ITEMS 6 & 8) REMOVED TO F.O.M. WITH REFERENCE TO SRM 51-42-21. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025090200702](https://openairdocs.org/sdr/SWIA2025090200702.md): Floor Panel · cracked · Jul 2, 2025 · N963SW · Cndair CL6002B19 · Fuselage Floor Panel
  > CRACK FOUND IN ELECTRICAL BAY FLOOR PANEL (REF DWG 601R33101) AT FS 193.00 JUST BELOW AND OUTBOARD OF BRAKE ACCUMULATOR GUAGES. (C-CHECK RO 08/29/2025) REPAIRED CRACK IN ELECTRICAL BAY FLOOR PANEL AT FS 193.00 JUST BELOW AND OUTBOARD OF BRAKE ACCUMULATOR GUAG
- [SDR SWIA2025090200629](https://openairdocs.org/sdr/SWIA2025090200629.md): Frame · cracked · Jun 29, 2025 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING CLEANING FOUND FS 605.00 FRAME CRACKED AT APPROX STRINGER 18L. REMOVED AND REPLACED FRAME SECTOR ON FS605 FROM WL73 (LEFT HAND) - STR21L WITH REFERENCE TO SRM 53-61-15, SRM 51-42-06 AND REO 601R-53-61-8354 REV-- DATED 2025-07-04. COMPLETED TASK CAR
- [SDR SWIA2025090200628](https://openairdocs.org/sdr/SWIA2025090200628.md): Skin · gouged · Jun 28, 2025 · N963SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 3 GOUGES TO FUSELAGE SKIN BETWEEN FS589.00 - FS605.00 AND STR 23R-24R (C-CHECK RO 08/29/2025)BLENDED 3 GOUGES TO FUSELAGE SKIN BETWEEN FS589.00 - FS605.00 AND STR 23R-24R WITH REFERENCE TO REO 601R-53-61-8350 REV-- DATED 2025-06-28. REFERENCE CP 30398090 FOR
- [SDR SWIA202506300028](https://openairdocs.org/sdr/SWIA202506300028.md): Skin · gouged · Jun 28, 2025 · N963SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 3 GOUGES TO FUSELAGE SKIN BETWEEN FS589.00 - FS605.00 AND STR 23R-24R (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025090201131](https://openairdocs.org/sdr/SWIA2025090201131.md): Support · corroded · Jun 19, 2025 · N963SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RH PRESSURE SILL HAS NUMEROUS AREAS OF CORROSION FROM FS409.00 +128 - FS559.00, RBL45.00 (C-CHECK RO 08/29/2025)BLENDED CORROSION ON RH PRESSURE SILL FROM FS409.00 +128 - FS559.00, RBL45.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEA
- [SDR SWIA2025090201130](https://openairdocs.org/sdr/SWIA2025090201130.md): Support · corroded · Jun 19, 2025 · N963SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE SILL HAS NUMEROUS AREAS OF CORROSION FROM FS409.00 +128 - FS559.00, LBL45.00 (C-CHECK RO 08/29/2025)BLENDED CORROSION ON LH PRESSURE SILL FROM FS409.00 +128 - FS559.00, RBL45.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEA
- [SDR SWIA2025090201128](https://openairdocs.org/sdr/SWIA2025090201128.md): Channel · cracked · Jun 19, 2025 · N963SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. (C-CHECK RO 08/29/2025)REMOVED AND REPLACED CARGO DOOR FWD TRACK LOWER CHANNEL WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.
- [SDR SWIA202503021129](https://openairdocs.org/sdr/SWIA202503021129.md): Floorbeam · cracked · Jun 19, 2025 · N963SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280, LBL 9.50, INBOARD CLIP/ANGLE CRACKED AT TOP. REMOVED AND REPLACED FS280, LBL 9.50, INBOARD CLIP/ANGLE WITH REFERENCE TO SRM 51-42-21 AND REO 601R-53-11-136, REV A. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2025F01128](https://openairdocs.org/sdr/SWI2025F01128.md): Track · cracked · Jun 19, 2025 · N963SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. (C-CHECK RO 08/29/2025)REMOVED AND REPLACED CARGO DOOR FWD TRACK LOWER CHANNEL WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.
- [SDR SWIA2025062300619](https://openairdocs.org/sdr/SWIA2025062300619.md): Track · cracked · Jun 19, 2025 · N963SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2025F00748](https://openairdocs.org/sdr/SWI2025F00748.md): Floorbeam · cracked · Jun 19, 2025 · N963SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280, LBL 9.50, INBOARD CLIP/ANGLE CRACKED AT TOP. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025090200015](https://openairdocs.org/sdr/SWIA2025090200015.md): Access Panel · corroded · Jun 10, 2025 · N963SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING FUEL CELL ACCESS PANEL LANDING HAS MULTIPLE AREAS OF MINOR SURFACE CORROSION. BLENDED CORRODED AREA OF LT WING FUEL ACCESS PANEL LANDING 510AB IAW REO 601R-57-21-030 REV. -L,. PERFORMED UT REMAINING THICKNESS INSPECTION WITH REFERENCE TO NDTM PART 4
- [SDR SWI2025F00722](https://openairdocs.org/sdr/SWI2025F00722.md): Access Panel · corroded · Jun 10, 2025 · N963SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING FUEL CELL ACCESS PANEL LANDING (510AB) HAS MULTIPLE AREAS OF MINOR SURFACE CORROSION (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20230200009](https://openairdocs.org/sdr/SWIA20230200009.md): Unknown · damaged · Feb 9, 2023 · N963SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > NOSE LANDING GEAR BAY LH WEB TOOLING DAMAGE BETWEEN FS177.00 - FS185.00, AND WL74.30 - WL59.40 HAS BEEN EVALUATED AND FOUND TO BE OUT OF LIMITS PER SRM 53-11-67. REFERENCE CP 26188343 FOR INITIAL DISCREPANCY. THIS IS A "MAJOR REPAIR". FORM M-337 INITIATED. (FI
- [SDR SWIA2023010567072](https://openairdocs.org/sdr/SWIA2023010567072.md): Proximity Sensor · out of adjust · Dec 31, 2022 · N963SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON GEAR UP SELECTION, MLG DISAGREE WARNING MESSAGE WITHIN 10 SECS. NLG WAS RED AND HAD SLASHES THROUGH THE BOX. ABNORMAL NOISE LIKE SOMETHING HANGING INTO THE WIND AT NLG AREA. RAN QRH & ALL GEAR CAME DOWN & LOCKED UPON MANUAL GEAR EXTENSION HANDLE BEING PULLE
- [SDR SWIA202265968](https://openairdocs.org/sdr/SWIA202265968.md): None · failed · Jun 24, 2022 · N963SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > D:GEAR DISAGREE LEVER DOWN ON APPROACH. LEFT MAIN. RAN QRH, MESSAGE EXTINGUISHED. MESSAGE REAPPEARED ON SECOND ATTEMPT, GEAR LOCKED INTO PLACE PRIOR TO QRH ON SECOND ATTEMPT. / C: MEL 32-30-1 / CAT A DUE WITHIN ONE FLIGHT DAY FROM 06/25/2022 / NOTES:FOUND CODE
- [SDR SWIA202265613](https://openairdocs.org/sdr/SWIA202265613.md): None · cracked · Apr 27, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Keel
  > CRACK NOTED AT SPLICE ANGLE AT STRG3L JUST AFT OF FS.280. (C-CHECK RO 5/16/2022) REPLACED SPLICE ANGLE P/N 600-31057-19 AT STGR 3L AFT OF FS280.00. REF DWG# 600-31057 REV P, CRJ-200 SRM 51-42-06, AND CRJ-200 SRM 51-42-21. PRESSURE LEAK CHECK IS SATISFAC
- [SDR SWIA202265612](https://openairdocs.org/sdr/SWIA202265612.md): None · cracked · Apr 19, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *AFT BAGGAGE BAY AFT INTER-COSTAL "BAGGAGE BAY CURTAIN" LOWER CLIP IS CRACKED. FLAGGED (C-CHECK RO 5/16/2022) REPLACED AFT BAGGAGE BAY CROSS-MEMBER LWR CLIP. REF DWG# 601R35050 REV AC AND CRJ-200 SRM 51-42-21. PRESSURE LEAK CHECK GOOD. COMPLIED WITH TAS
- [SDR SWIA202265611](https://openairdocs.org/sdr/SWIA202265611.md): None · damaged · Apr 19, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *AFT BAGGAGE BAY OUTBOARD/AFT INTER-COSTAL "BAGGAGE BAY DOOR CURTAIN" CUT INTO FROM DOOR CABLE. FLAGGED (C-CHECK RO 5/16/2022) REPLACED AFT BAGGAGE BAY DOOR CUTOUT CROSSMEMBER BETWEEN APPROX. FS574.00 AND FS621.00. REF DWG# 601R35050 REV AC AND CRJ-200
- [SDR SWIA202265610](https://openairdocs.org/sdr/SWIA202265610.md): None · cracked · Apr 5, 2022 · N963SW · Cndair CL6002B19 · Fuselage Floor Panel
  > COCKPIT FLOOR SUPPORT ANGLE CRACKED AT FS 280.0 LBL 9.0 (C-CHECK RO 5/16/2022) NEW COCKPIT FLOOR SUPPORT ANGLE P/N 600-34017-351S INSTALLED TO REWORK AREA REF BOMBARDIER DWG 600-33100 REV AE / CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202265609](https://openairdocs.org/sdr/SWIA202265609.md): None · scratched · Apr 5, 2022 · N963SW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > *PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE, MULTIPLE LUGS SCRATCHED AND SOME WITH PIN HOLES. MARKED WITH GREASE PENCIL (C-CHECK RO 5/16/2022) REPLACED PAX DOOR FUSELAGE SIDEPIANO HINGE HALF. REF CRJ-200 SRM 53-21-23, CRJ-200 SRM 51-42-06, CRJ-20
- [SDR SWIA202265608](https://openairdocs.org/sdr/SWIA202265608.md): None · cracked · Apr 2, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CRACK NOTED ON FRAME FLANGE AT FS605.00 AND STRG9L (MARKED) (C-CHECK RO 5/16/2022) CUT OUT CRACK ON FS605.00 FRAME AT STGR 9L AND PERFORMED REO REPAIR. REF REO 601R53-61-5214 REV -A DATED 2016-11-04. SEE CONTINUE CARD FOR DETAILS COMPLIED WITH TASK CA
- [SDR SWIA202265606](https://openairdocs.org/sdr/SWIA202265606.md): None · corroded · Apr 1, 2022 · N963SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION NOTED ON R/H PRESSURE FLOOR SILL PANEL AT APPROX. FS439.00 AND FS559.00 (MARKED) (C-CHECK RO 5/16/2022) BLENDED CORROSION ON R/H PRESSURE FLOOR FLOOR SILL BETWEEN FS439.00 AND FS559.00 @ 2 LOCATIONS TO A SMOOTH CONTOUR AND RESTORED FINISH. R
- [SDR SWIA202265605](https://openairdocs.org/sdr/SWIA202265605.md): None · corroded · Apr 1, 2022 · N963SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION NOTED IN MULTIPLE AREAS ON L/H PRESSURE FLOOR SILL PANEL BETWEEN FS409.00+128-FS559.00 (MARKED) (C-CHECK RO 5/16/2022) BLENDED CORROSION DAMAGE ON L/H PRESSURE FLOOR SILL PANEL BETWEEN FS409.00+128 TO FS559.00 AND RESTORED FINISH. REMAINING
- [SDR SWIA202265604](https://openairdocs.org/sdr/SWIA202265604.md): None · cracked · Mar 31, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > INTERNAL FUSELAGE AT RBL 9.0 AT FS 460 CASTING HAS CRACK AT UPPER RADIUS. (C-CHECK RO 5/16/2022) REPLACED INTERNAL FUSELAGE CASTING (FITTING) AT FS460.00 RBL 9. REF CRJ200 SRM 51-42-21 AND DWG 601R31146 REV. J. COMPLIED WITH 51-900-1003-SKY. LEAK CHECK
- [SDR SWIA202265603](https://openairdocs.org/sdr/SWIA202265603.md): None · cracked · Mar 31, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 484.0 RBL 27 INBOARD CLIP IS CRACKED. (C-CHECK RO 5/16/2022) REMOVED AND REPLACED NEW INBOARD CLIP AT FS 484.00 LBL 27 THAT WAS PREVIOUSLY REPAIR PER REO 601R-53-41-059 REV C, DATED 2020-03-11.COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202265602](https://openairdocs.org/sdr/SWIA202265602.md): None · cracked · Mar 31, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > LBL 27L AT FS 484 INB CLIP IS CRACKED. (C-CHECK RO 5/16/2022) REMOVED AND REPLACED NEW INBOARD CLIP AT FS 484.00 RBL 27 THAT WAS PREVIOUSLY REPAIR PER REO 601R-53-41-059 REV C, DATED 2020-03-11.COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202265601](https://openairdocs.org/sdr/SWIA202265601.md): None · corroded · Mar 30, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333.0 AT APPROX STR 27 FRAME FLANGE HAS CORROSION. (C-CHECK RO 5/16/2022) REPLACED THE FS333.00 LWR FRAME SECTOR. REF CRJ200 SRM 51-42-06, CRJ 200 SRM 51-42-21, DWG 601R32004 REV L AND DWG 601R31022 REV B. LEAK CHECKS ARE GOOD. COMPLIED WITH TASK CA
- [SDR SWIA202265600](https://openairdocs.org/sdr/SWIA202265600.md): None · cracked · Mar 30, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 280.0 RBL 9.0 OUTBOARD CLIP IS CRACKED (C-CHECK RO 5/16/2022) REMOVED AND INSTALLED OUTBOARD CLIP P/N 601R31113-58 AT FS 280.0 RBL 9.0 REF BOMBARDIER REO 601R-53-11-137 REV A DATED 12-FEB-07. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR D
- [SDR SWIA202265599](https://openairdocs.org/sdr/SWIA202265599.md): None · cracked · Mar 30, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 280 RBL 9.0 INBOARD CLIP IS CRACKED. (C-CHECK RO 5/16/2022) REMOVED AND INSTALLED INBOARD CLIP P/N 601R31113-58 AT FS 280.0 RBL 9.0 REF BOMBARDIER REO 601R-53-11-137 REV A DATED 12-FEB-07. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETA
- [SDR SWIA202265598](https://openairdocs.org/sdr/SWIA202265598.md): None · cracked · Mar 30, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 280.0 LBL 9.0 MOST OUTBOARD CLIP IS CRACKED. (C-CHECK RO 5/16/2022) REMOVED AND INSTALLED OUTBOARD CLIP P/N 601R31113-58 AT FS 280.0 LBL 9.0 REF BOMBARDIER REO 601R-53-11-136 REV -A DATED 2007/11/01. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CA
- [SDR SWIA202265597](https://openairdocs.org/sdr/SWIA202265597.md): None · cracked · Mar 30, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Keel
  > R/H SIDE STR 14 FS 625 CLIP IS CRACKED. (C-CHECK RO 5/16/2022) REMOVED AND REPLACED FS625 CLIP AT STGR 14R REF. CRJ 200 SRM 51-42-06 AND DWG 601-35012 REV. D. / COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202265596](https://openairdocs.org/sdr/SWIA202265596.md): None · cracked · Mar 30, 2022 · N963SW · Cndair CL6002B19 · Fuselage Main, Keel
  > L/H SIDE STR 14 FS 625 CLIP IS CRACKED. (C-CHECK RO 5/16/2022) REMOVED AND REPLACED FS625 CLIP AT STGR 14L REF. CRJ 200 SRM 51-42-06 AND DWG 601-35012 REV D. / COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202265595](https://openairdocs.org/sdr/SWIA202265595.md): None · cracked · Mar 27, 2022 · N963SW · Cndair CL6002B19 · Hydraulic Accumulator, Auxiliary
  > *HYD. PRESSURE SWITCH BRACKET IN RIGHT WHEEL WELL CRACKED. (MARKED) (C-CHECK RO 5/16/2022) REPLACED WITH NEW HYD. PRESSURE SWITCH BRACKET AT RH WHEEL WELL REF CRJ200 SRM 51-42-06 AND DWG:601R75262, REV -K. COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202265594](https://openairdocs.org/sdr/SWIA202265594.md): None · chafed · Mar 25, 2022 · N963SW · Cndair CL6002B19 · Ailerons
  > *CHAFFING NOTED AT L/H AILERON LOWER L/E SKIN (MARKED) (C-CHECK RO 5/16/2022) BLENDED CHAFE TO A SMOOTH CONTOUR. BLEND IS OUT OF LIMITS OF REO670-57-61-194 REV -C DATED 2019-01-07, REPLACED LH AILERON LE SKIN REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-2
- [SDR SWIA202265593](https://openairdocs.org/sdr/SWIA202265593.md): None · worn · Mar 24, 2022 · N963SW · Cndair CL6002B19 · Wing Structure
  > L/H SIDE AILERON LOWER L/E EDGE HAS AREAS OF WEAR ON OUTBOARD AND MOST INBOARD AREAS OF AILERON. (C-CHECK RO 5/16/2022) BLENDED CHAFE TO A SMOOTH CONTOUR. BLEND IS OUT OF LIMITS OF REO 670-57-61-194 REV -C DATED 2019-01-07, REPLACED LH AILERON LE SKI
- [SDR SWIA202265592](https://openairdocs.org/sdr/SWIA202265592.md): None · chafed · Mar 24, 2022 · N963SW · Cndair CL6002B19 · Wing Structure
  > L/H AILERON UPPER L/E SHROUD HAS AREAS OF CHAFFING WEAR.COMPLETELY ACCROSS THE ENTIRE AILERON. (C-CHECK RO 5/16/2022) REMOVED AND INSTALLED NEW L/H AILERON UPPER L/E SHROUD SKIN AND RESTORED FINISH. REF: CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, CRJ200
- [SDR SWIA202265591](https://openairdocs.org/sdr/SWIA202265591.md): None · dented · Mar 23, 2022 · N963SW · Cndair CL6002B19 · Doors
  > * FOUND A DENT ON THE LOWER LIP SIDE OF THE RH BOTTOM AREA OF THE CARGO COMPARTMENT DOOR.(AREA MARKED) (C-CHECK RO 5/16/2022) REWORKED DENT PER REO 601R-52-31-367 REV-A DATED 2022-05-01 AND REO 601R-51-00-309 REV-A DATED 2017-08-23. COMPLIED WTIH TASK
- [SDR SWIA202265590](https://openairdocs.org/sdr/SWIA202265590.md): None · dented · Mar 22, 2022 · N963SW · Cndair CL6002B19 · Fuselage Structure (General)
  > MULTIPLE DENTS (7) FOUND ON RHS OF FUSELAGE, AT APPROXIMATELY BETWEEN FS589 TO FS574, AFT & I/B OF GROUND AIR DOOR. (MARKED) / PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-C
- [SDR SWIA202265589](https://openairdocs.org/sdr/SWIA202265589.md): None · dented · Mar 22, 2022 · N963SW · Cndair CL6002B19 · Air Conditioning Doors
  > DENT FOUND ON RHS OF FUSELAGE, AT APPROXIMATELY BETWEEN FS589 TO FS574, AFT UPPER CORNER OF GROUND AIR CONNECTION DOOR. (MARKED) PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-
- [SDR SWIA202163106](https://openairdocs.org/sdr/SWIA202163106.md): None · dented · Dec 2, 2021 · N963SW · Cndair CL6002B19 · Fuselage Structure (General)
  > 3 SMALL DENTS NEAR GPU PLUG ACCESS DOOR ON FORWARD #2 SIDE OF AC BETWEEN FS 177.00 €“ FS 193.00 AND STGR 22R €“ STGR 24R EVALUATED AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-31. DENT #1 IS L= 2.5€? X W= 3.5€? X D=.045, DENT #2 IS L=2.0€? X W= 3.0€? X D
- [SDR SWIA202161799](https://openairdocs.org/sdr/SWIA202161799.md): None · malfunctioned · Oct 23, 2021 · N963SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > ON APPROACH AIRSPEED AT 170. GEAR WAS SELECTED DOWN. BOTH MAIN GEAR INDICATED DOWN AND LOCKED. NOSE GEAR INDICATED UP. GOT GEAR DISAGREE WARNING MESSAGE. RAN THE FULL QRH PROCEDURE INCLUDING PULLING THE LANDING GEAR MANUAL RELEASE HANDLE TO GET THE NOSE GEAR D
- [SDR SWIA202156586](https://openairdocs.org/sdr/SWIA202156586.md): Shear Tie · cracked · Feb 12, 2021 · N963SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FS605 FRAME LOWER FLANGE AT STGR19R IS CRACKED (MARKED) (C-CHECK) RO 3/2/2021 COMPLIED WITH MHIRJ REO 601R-53-61-7574 REV -- DATED 2021-02-23. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO LEAKS NOTED
- [SDR SWIA202156589](https://openairdocs.org/sdr/SWIA202156589.md): Seat Track · corroded · Feb 11, 2021 · N963SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL 399 TO 409+128 RBL 9 APPROX. HAS CORROSION AS MARKED (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED WITH NEW SERVICEABLE PN 601R31032-21 FROM FS399-FS409+126 RBL9 REF CRJ200 AMM 53-01-11-000-802. TUC8607 CAL DUE:28-FEB-22
- [SDR SWIA202156588](https://openairdocs.org/sdr/SWIA202156588.md): Seat Track · corroded · Feb 11, 2021 · N963SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL 399 TO 409+128 LBL 9 APPROX. HAS CORROSION AS MARKED (C-CHECK) RO 3/2/2021 FABRICATED NEW LBL9 SEAT RAIL P/N 601R31032-21, FROM FS399 TO FS409+126, USING EXTRUSION 20276-288-0-0A, PO# T58082, REF. BOMBARDIER REO 601R-53-00-485, REV. D, DATED 2018

Next page: https://openairdocs.org/aircraft/N963SW/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 = 'N963SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N963SW/reports

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