# Service difficulty reports: N924SW

A list on [N924SW](https://openairdocs.org/aircraft/N924SW.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 5 · 223 reports

- [SDR SWIA2025102700022](https://openairdocs.org/sdr/SWIA2025102700022.md): Track · damaged · Oct 22, 2025 · N924SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER FWD TRACK IS DAMAGED CAUSING CARGO DOOR ROLLER TO COME OUT OF TRACK. REMOVED AND REPLACED CARGO DOOR FWD TRACK ASSY IN REFERENCE TO AMM 52-31-00-400-801, SRM 51-40-11, SRM 51-42-06 & SRM 51-77-00 AND COMPLIED WITH RII TASK CARD 51-900-1003-SK
- [SDR SWIA2025102300002](https://openairdocs.org/sdr/SWIA2025102300002.md): Track · damaged · Oct 22, 2025 · N924SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER FWD TRACK IS DAMAGED CAUSING CARGO DOOR ROLLER TO COME OUT OF TRACK. (OPEN)
- [SDR SWI2025F00702](https://openairdocs.org/sdr/SWI2025F00702.md): Stringer · corroded · Apr 23, 2025 · N924SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 24L APPROX. 8.4" AFT OF FS574.00 (C-CHECK RO 05/28/2025)COMPLIED WITH REO 601R-53-61-8314 REV "--" DATED 2025-05-22 REPAIR FOR DENT TO LOWER FUSELAGE SKIN AND FOR CORROSION TO STRINGER BETWEEN FS574.00 - FS589.00 AND STR24L - STR25L. PERFORM
- [SDR SWIA20250530423](https://openairdocs.org/sdr/SWIA20250530423.md): Skin · dented · Apr 23, 2025 · N924SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING THE ADM INSPECTION, 1 DENT WAS FOUND ON THE LH NOSE EXTERNAL FUSELAGE SKIN IN BETWEEN FS 220.00 - FS 235.00 AND IN BETWEEN STR 24L & STR 25L. (C-CHECK RO 05/28/2025)PERFORMED REPAIR OF DENT ON LH NOSE EXTERNAL FUSELAGE SKIN LOCATED BTWN FS220.00 - FS2
- [SDR SWI2025F00694](https://openairdocs.org/sdr/SWI2025F00694.md): Skin · dented · Apr 14, 2025 · N924SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REPAIR FOR DENTS TO LOWER FUSELAGE SKIN BETWEEN FS625.30 - FS640.00 AND STR24L - STR27. (C-CHECK RO 05/28/2025)COMPLIED WITH REO 601R-53-61-8315 DATED: 2025-04-18 REPAIR FOR DENTS TO LOWER FUSELAGE SKIN BETWEEN FS625.30 - FS640.00 AND STR24L - STR27. COMPLET
- [SDR SWIA20250530414](https://openairdocs.org/sdr/SWIA20250530414.md): Skin · dented · Apr 14, 2025 · N924SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT TO LOWER FUSELAGE SKIN BETWEEN FS574.00 - FS589.00 AND STR24L - STR25L. (C-CHECK RO 05/28/2025)COMPLIED WITH REO 601R-53-61-8314 REV "--" DATED 2025-05-22 REPAIR FOR DENT TO LOWER FUSELAGE SKIN AND FOR CORROSION TO STRINGER BETWEEN FS574.00 - FS589.00
- [SDR SWI2025F00448](https://openairdocs.org/sdr/SWI2025F00448.md): Skin · dented · Apr 14, 2025 · N924SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REPAIR FOR DENTS TO LOWER FUSELAGE SKIN BETWEEN FS625.30 - FS640.00 AND STR24L - STR27. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2025F00698](https://openairdocs.org/sdr/SWI2025F00698.md): Skin · dented · Mar 29, 2025 · N924SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING THE ADM INSPECTION, 14 INWARD/OUTWARD DENTS WERE FOUND ON THE EXTERIOR LOWER FUSELAGE SKIN PANELS BETWEEN FS574.00-FS682.00 & STR 24L - 21R. (C-CHECK RO 05/28/2025)UPON INSPECTION, FOUND ALL 14 INWARD/OUTWARD DENTS ON THE EXTERIOR LOWER FUSELAGE SKIN
- [SDR SWI2025F00697](https://openairdocs.org/sdr/SWI2025F00697.md): Skin · dented · Mar 29, 2025 · N924SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING THE ADM INSPECTION, 2 DENTS WERE FOUND BETWEEN FS654 - FS762 AND BETWEEN STR 0-1R (C-CHECK RO 05/28/2025)COMPLIED WITH REWORK OF DENTS TO FUSELAGE SKIN BETWEEN FS654.50 - FS672.00 AND STR 0 - STR 1L WITH REFERENCE TO REO 601R-53-61-8311 REV "--" DATED 2
- [SDR SWI2025F00696](https://openairdocs.org/sdr/SWI2025F00696.md): Skin · dented · Mar 29, 2025 · N924SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING THE ADM INSPECTION, 3 DENTS WERE FOUND FROM FS 654- FS 672 BETWEEN STR 7R-8R (C-CHECK RO 05/28/2025)COMPLIED WITH REWORK OF DENTS TO FUSELAGE SKIN BETWEEN FS654.50 - FS672.00 AND STR 7R - STR 8R WITH REFERENCE TO REO 601R-53-61-8311 REV "--" DATED 2025-
- [SDR SWIA20250530329](https://openairdocs.org/sdr/SWIA20250530329.md): Skin · dented · Mar 29, 2025 · N924SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > DURING THE ADM INSPECTION, 1 DENT WAS FOUND ON THE LH HORIZONTAL STAB LOWER LEADING EDGE AT APPROX. INBETWEEN (HORIZONTAL STABILIZER FRONT SPAR STATION) 10.91 AND 21.91. (C-CHECK RO 05/28/2025)COMPLIED WITH REO 601R-55-11-788 REV -- DATED: 2025-04-22 REPAIR TO
- [SDR SWIA202505300218](https://openairdocs.org/sdr/SWIA202505300218.md): Floor Support · corroded · Feb 18, 2025 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS559.00 TO 559.00 +32 RH CABIN FLOOR SILL HAS SURFACE CORROSION. (C-CHECK RO 05/28/2025)COMPLIED WITH REO 601R-53-51-704 DATED: 2025-02-24 REV: "--" REPAIR FOR CORROSION DAMAGE TO INTERCOSTAL, FLOOR SILL INSTALLATION BETWEEN FS559.00- FS559.00+16 AT WL73.00
- [SDR SWIA202505300214](https://openairdocs.org/sdr/SWIA202505300214.md): Skin · dented · Feb 14, 2025 · N924SW · Cndair CL6002B19 · Rudder, Plate/Skin
  > DENT ON RH SIDE OF THE RUDDER, LOCATED ROUGHLY 6" FROM THE TOP AND 18" AFT OF THE LEADING EDGE OF THE RUDDER. (C-CHECK RO 05/28/2025)COMPLIED WITH REO 601R-55-41-300 DATED: 2025-02-21 AND REV -- FOR THE PERMANENT DISPOSITION FOR THE DENT TO THE RUDDER SKIN BE
- [SDR SWI2025F00701](https://openairdocs.org/sdr/SWI2025F00701.md): Floor Support · corroded · Feb 5, 2025 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409.00 TO 409.00 +80 LBL 9.50 FLOORBOARD LANDING HAS NUMEROUS AREAS OF SURFACE CORROSION (C-CHECK RO 05/28/2025)UPON INSPECTION FOUND AREAS OF SURFACE CORROSION TO EXTEND FROM FS 409.00 TO FS 499.00. COMPLIED WITH REO 601R-53-00-903 DATED: 2025-03-14 REV
- [SDR SWI2025F00700](https://openairdocs.org/sdr/SWI2025F00700.md): Floor Support · corroded · Feb 5, 2025 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS484.00 TO 513.00 RH PRESSURE FLOOR SILL HAS NUMEROUS AREAS OF CORROSION. (C-CHECK RO 05/28/2025)BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL FS484.00 TO FS513.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE
- [SDR SWI2025F00699](https://openairdocs.org/sdr/SWI2025F00699.md): Floor Support · corroded · Feb 5, 2025 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS499.00 TO 544.00 LH PRESSURE FLOOR SILL HAS NUMEROUS AREAS OF CORROSION. (C-CHECK RO 05/28/2025)BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL FS499.00 TO FS544.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE
- [SDR SWIA20250530205](https://openairdocs.org/sdr/SWIA20250530205.md): Floor Support · corroded · Feb 5, 2025 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409.00 TO 409.00 +112 RBL 9.50 FLOORBOARD LANDING HAS NUMEROUS AREAS OF SURFACE CORROSION. (C-CHECK RO 05/28/2025)UPON INSPECTION FOUND AREAS OF SURFACE CORROSION TO EXTEND FROM FS 409.00 TO FS 424.00.COMPLIED WITH REO 601R-53-00-902 DATED: 2025-03-14 REV
- [SDR SWIA2023031600001](https://openairdocs.org/sdr/SWIA2023031600001.md): Proximity Sensor · malfunctioned · Mar 14, 2023 · N924SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > PROX SYS CHAN CAUTION MESSAGE APPEARED IN CRUISE. RAN QRH AND LANDED NORMALLY BUT DID NOT HAVE NOSE WHEEL STEERING UPON TOUCHDOWN THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26346989 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT PROX SYS CHAN CAUTION MS
- [SDR SWIA202054980](https://openairdocs.org/sdr/SWIA202054980.md): Skin · dented · Dec 7, 2020 · N924SW · Cndair CL6002B19 · Ailerons
  > RT AILERON UPPER SKIN DENTED BEYOND LIMITS AT SEVERAL LOCATIONS OPPOSITE OF ACCESS PANEL 699DB AND FOD REMAINS INTERNALLY. C-CHECK RO 12/30/2020. REPAIRED SKIN DENTS, IAW CRJ 200 SRM. REMOVED FOD DURING REPAIR. MAJOR REPAIR TASK & FORM M337 COMPLETED AND A
- [SDR SWIA202054982](https://openairdocs.org/sdr/SWIA202054982.md): Door Frame · corroded · Nov 30, 2020 · N924SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND PAX DOOR FRAME 313.56 TO BE CORRODED. C-CHECK RO 12/30/2020. REMOVED AND REPLACED PAX DOOR FRAME FS 313.56, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWIA202054988](https://openairdocs.org/sdr/SWIA202054988.md): Intercostal · corroded · Nov 28, 2020 · N924SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND CORROSION ON PAX DOOR INTERCOSTAL DD3. C-CHECK RO 12/30/2020. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWIA202054976](https://openairdocs.org/sdr/SWIA202054976.md): Intercostal · corroded · Nov 28, 2020 · N924SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND CORROSION ON PAX DOOR INTERCOSTAL DD4. C-CHECK RO 12/30/2020. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWIA202054965](https://openairdocs.org/sdr/SWIA202054965.md): Floor Support · corroded · Nov 28, 2020 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SILL HAS CORROSION DAMAGE BETWEEN FS 473 TO FS 484 THAT IS OUT OF LIMITS OF REO. C-CHECK RO 12/30/2020. REPAIRED LT PRESSURE SILL, IAW REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. WEIGHT CHANGE FOUND TO BE NEGLIGIBLE.
- [SDR SWIA202054985](https://openairdocs.org/sdr/SWIA202054985.md): Rib · cracked · Nov 22, 2020 · N924SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RIGHT BATT RIB AT WS 53.6 IS CRACKED AT THE UPPER AFT FLANGE THROUGH RADIUS APPROXIMATELY 2 INCHES IN LENGTH ALSO DOUBLER ATTACHED TO BATT RIB IS CORRODED AROUND J410 AND J412. C-CHECK RO 12/30/2020. REPAIRD RT BATT RIB AT WS 53.6 WITH REO. COMPLETED TASK C
- [SDR SWIA202055046](https://openairdocs.org/sdr/SWIA202055046.md): Nut · corroded · Nov 19, 2020 · N924SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT SIDE FLAP BPSU MOUNTING BOLT NUT IS CORRODED. C-CHECK RO 12/30/2020. REMOVED AND REPLACED RIGHT SIDE FLAP BPSU MOUNTING BOLT NUT, IAW AMM.
- [SDR SWIA202055045](https://openairdocs.org/sdr/SWIA202055045.md): Nut Plate · corroded · Nov 19, 2020 · N924SW · Cndair CL6002B19 · Wing, Attach Fittings
  > MULTIPLE NUT PLATES ARE CORRODED ON RIGHT WING OUTBOARD TRAILING EDGE BETWEEN WS 317 TO WS 353. C-CHECK RO 12/30/2020. REPLACED MULTIPLE NUT PLATES ON RIGHT WING OUTBOARD TRAILING EDGE BETWEEN WS 317 TO WS 35, IAW CRJ 200 SRM.
- [SDR SWIA202055005](https://openairdocs.org/sdr/SWIA202055005.md): Bracket · cracked · Nov 19, 2020 · N924SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > BRACKET AT APPROXIMATELY WS 50 ON RIGHT WING TRAILING EDGE IS CRACKED. C-CHECK RO 12/30/2020. REMOVED AND REPLACED DAMAGED BRACKET RT WING APPROXIMATELY WS-50, IAW CRJ200 SRM INSTALL HI-LITE IAW CRJ SRM.
- [SDR SWIA202054998](https://openairdocs.org/sdr/SWIA202054998.md): Hinge Fitting · chafed · Nov 19, 2020 · N924SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING FLAP HINGE BOX HAS CHAFING DAMAGE ON CENTER MOUNT FITTING. C-CHECK RO 12/30/2020. REPAIRED RT WING FLAP HINGE BOX CENTER MOUNT FITTING, IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASURABLE WEIGHT CHANGE. REFER TO CONTINU
- [SDR SWIA202054997](https://openairdocs.org/sdr/SWIA202054997.md): Hinge Fitting · gouged · Nov 19, 2020 · N924SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBOARD FLAP, OUTBOARD/AFT HINGE BOX ATTACH FITTING GOUGED APPROXIMATELY.5" LONG. C-CHECK RO 12/30/2020. REPAIRED IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASUREABLE WEIGHT CHANGE. REFER TO CONTINUE CARD FOR WORK. PERFORMED
- [SDR SWIA202054964](https://openairdocs.org/sdr/SWIA202054964.md): Skin · chafed · Nov 19, 2020 · N924SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK IS CHAFED AT APPROXIMATELY RBL 45. C-CHECK RO 12/30/2020. REPAIRED IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASREUABLE WEIGHT CHANGES MADE.
- [SDR SWIA202054991](https://openairdocs.org/sdr/SWIA202054991.md): Door Frame · corroded · Nov 18, 2020 · N924SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FRAME IS CORRODED INSIDE OF THE VENT FLAP STRUCTURE ON THE AFT SIDE OF CUT OUT. C-CHECK RO 12/30/2020. REMOVED AND REPLACED PAX DOOR FRAME AT FS 349, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWIA202054979](https://openairdocs.org/sdr/SWIA202054979.md): Skin · corroded · Nov 18, 2020 · N924SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN, ALL ACCESS PANEL CUT OUTS HAVE CORROSION AREAS AROUND NUMEROUS NUTPLATES. C-CHECK RO 12/30/2020. REMOVED AND REPLACED PAX DOOR INNER SKIN, IAW CRJ 200 SRM.
- [SDR SWIA202054975](https://openairdocs.org/sdr/SWIA202054975.md): Striker · corroded · Nov 18, 2020 · N924SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR LOWER SEAL STRIKER FOUND CORRODED AT FWD DOOR FITTINGS. C-CHECK RO 12/30/2020. REPLACED THE SERVICE DOOR LOWER SEAL STRIKER, IAW CRJ 200 SRM. REFERENCE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202054996](https://openairdocs.org/sdr/SWIA202054996.md): Mount · gouged · Nov 17, 2020 · N924SW · Cndair CL6002B19 · Engine Mount Section
  > LT ENGINE MOUNT FORWARD SPAR HAS A GOUGE ON THE UPPER FORWARD SIDE WITH HIGH METAL. C-CHECK RO 12/30/2020. REPAIRED IAW REO. NO MEASURABLE WEIGHT CHANGE. FORM M337 & MAJOR REPAIR TASK COMLETED AND ATTACHED. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202054978](https://openairdocs.org/sdr/SWIA202054978.md): Door Sill · corroded · Nov 17, 2020 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE IS CORRODED BETWEEN FS 319.70 AND FS 349.00. C-CHECK RO 12/30/2020. REMOVED AND REPLACED SERVICE DOOR LOWER SILL, IAW CRJ 200 SRM.
- [SDR SWIA202054963](https://openairdocs.org/sdr/SWIA202054963.md): Floorbeam · corroded · Nov 17, 2020 · N924SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CABIN FLOOR CROSSBEAM AT FS 349.00 RBL 36 IS CORRODED ON THE END. C-CHECK RO 12/30/2020. REPAIRED CABIN FLOOR CROSSBEAM AT FS 349.00 RBL 36, IAW REO. MAJOR REPAIR & FORM 337 ATTACHED. WEIGHT CHANGE IS NEGLIGIBLE.
- [SDR SWIA202055050](https://openairdocs.org/sdr/SWIA202055050.md): Seat Track · damaged · Nov 16, 2020 · N924SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL BETWEEN FS 535 AND FS 559+79 P/N 601R38312-137 REQUIRES FABRICATION DUE TO LACK OF PART AVAILIBILITY. C-CHECK RO 12/30/2020. FABRICATED LT SIDE SEAT RAIL BETWEEN FS 535 AND FS 559+79 P/N 601R38312-137, IAW BOMBARDIER REO. SEE CONTINUATION
- [SDR SWIA202055049](https://openairdocs.org/sdr/SWIA202055049.md): Skin · chafed · Nov 16, 2020 · N924SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON LEADING EDGE SKIN IS CHAFED. C-CHECK RO 12/30/2020. REMOVED AND REPLACED LT AILERON LEADING EDGE SKIN, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202055048](https://openairdocs.org/sdr/SWIA202055048.md): Hinge Fitting · chafed · Nov 16, 2020 · N924SW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON INBOARD HINGE FITTING HAS CHAFING DAMAGE. C-CHECK RO 12/30/2020. REMOVED AND REPLACED HINGE FITTING PLATE (FAILSAFE), IAW CRJ 200 SRM.
- [SDR SWIA202055044](https://openairdocs.org/sdr/SWIA202055044.md): Hinge Fitting · corroded · Nov 16, 2020 · N924SW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON OUTBOARD WING HINGE FITTING IS CORRODED. C-CHECK RO 12/30/2020. REMOVED AND REPLACED RT OUTBOARD HINGE FITTING, IAW CRJ 200 AMM.
- [SDR SWIA202055043](https://openairdocs.org/sdr/SWIA202055043.md): Angle · corroded · Nov 15, 2020 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL ANGLE FLANGE IS CORRODED AT FORWARD EDGE APPROXIMATELY FS 347. C-CHECK RO 12/30/2020. PASSENGER DOOR LOWER SILL ANGLE FLANGE FOUND TO BE OUT OF LIMITS, IAW CRJ 200 SRM. REVIEW WORK PERFORMED ON CAMP 21840703.
- [SDR SWIA202055004](https://openairdocs.org/sdr/SWIA202055004.md): Bracket · cracked · Nov 15, 2020 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE IS CRACKED IN RADIUS AT RIGHT SIDE STRINGER 14 BETWEEN FS 621 TO FS 625. C-CHECK RO 12/30/2020. REMOVED AND REPLACED WITH SERVICEABLE ANGLE PN 601-35012-52, IAW CRJ 200 SRM.
- [SDR SWIA202055003](https://openairdocs.org/sdr/SWIA202055003.md): Bracket · cracked · Nov 15, 2020 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE IS CRACKED IN RADIUS AT LEFT SIDE STRINGER 14 BETWEEN FS 621 TO FS 625. C-CHECK RO 12/30/2020. REMOVED AND REPLACED WITH SERVICEABLE ANGLE PN 601-35012-51, IAW CRJ200 SRM.
- [SDR SWIA202054989](https://openairdocs.org/sdr/SWIA202054989.md): Skin · chafed · Nov 15, 2020 · N924SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER WING PLANK IS CHAFED AT APPROXIMATELY LBL 45 FROM CONTACT WITH FAIRING 193AB. C-CHECK RO 12/30/2020. REPAIRED LEFT WING LOWER WING PLANK AT LBL 45, IAW REO. NO MEASUREABLE WEIGHT CHANGE. MAJOR REPAIR TASK & M337 COMPLETED AND ATTACHED.
- [SDR SWIA202055042](https://openairdocs.org/sdr/SWIA202055042.md): Support Bracket · corroded · Nov 14, 2020 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409 AVIONICS BAY FLOORBOARD SUPPORT ANGLE IS CORRODED. C-CHECK RO 12/30/2020. REMOVED FRAME INTERCOSTAL ANGLE AFT OF FS 409 LOCATED AND DRILLED NEW ANGLE AND INSTALLED, IAW CRJ 200 SRM.
- [SDR SWIA202055002](https://openairdocs.org/sdr/SWIA202055002.md): Angle · cracked · Nov 14, 2020 · N924SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE WORKING 621 BULKHEAD REPAIR. FOUND LOWER ANGLE FOR CARGO BAY DOOR BEAM TO BE CRACKED. C-CHECK RO 12/30/2020. REMOVED AND REPLACED THE CARGO BAY DOOR BEAM LOWER BRACKET, IAW CRJ 200 SRM.
- [SDR SWIA202054971](https://openairdocs.org/sdr/SWIA202054971.md): Frame · corroded · Nov 14, 2020 · N924SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 364 FRAME SEGMENT AND DOUBLER ARE CORRODED BETWEEN STGR 26L AND STGR 26R. C-CHECK RO 12/30/2020. REMOVED AND REPLACED LOWER FRAME SEGMENT AND DOUBLER BETWEEN STGR 26L AND STGR 26R FS 364.00, IAW CRJ 200 SRM. COMPLETED TASK CARD CARD AND ATTACHED COMPLETE
- [SDR SWIA202054983](https://openairdocs.org/sdr/SWIA202054983.md): Bulkhead · corroded · Nov 13, 2020 · N924SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 67.5% REAR SPAR BULKHEAD AND SUPPORT ANGLE CORRODED AT BL 0 LOWER POSITION. C-CHECK RO 12/30/2020. REPAIRED IAW REO. MAJOR REPAIR TASK CARD & FORM M337 COMLETED AND ATTACHED. WEIGHT CHANGE AS NOTED ON CONTINUE CARD.
- [SDR SWIA202054977](https://openairdocs.org/sdr/SWIA202054977.md): Bushing · dented · Nov 13, 2020 · N924SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP HAS 2 DENTS/GOUGES. ONE MEASURES.5" X.5" AND IS LOCATED BETWEEN WS 68.138 & WS 79.062 BELOW LOWER INTERCOSTAL. THE SECOND MEASURES 1" X 1" BETWEEN WS 68.138 & WS 79.062 ABOVE TOP INTERCOSTAL. BOTH DENTS HAVE BEEN DETERMINED TO BE OUT OF LI
- [SDR SWIA202055041](https://openairdocs.org/sdr/SWIA202055041.md): Bulkhead Web · corroded · Nov 12, 2020 · N924SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AT 280 BULKHEAD ON LEFT HAND SIDE OF ENTRANCE TO FLIGHT DECK AT STR 2L (TOP), FOUND BRACKET TO BE HEAVILY CORRODED, MARKED WITH ORANGE TAPE. C-CHECK RO 12/30/2020. REMOVED AND REPLACED NEW ANGLE PN NR 600-34017-569 & ANLGE DOUBLER PLATE 600-34017-567, IAW CR

Next page: https://openairdocs.org/aircraft/N924SW/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 = 'N924SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N924SW/reports

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