# Service difficulty reports: N930SW

A list on [N930SW](https://openairdocs.org/aircraft/N930SW.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 · 233 reports

- [SDR SWIA2025112100017](https://openairdocs.org/sdr/SWIA2025112100017.md): Rib · damaged · Nov 17, 2025 · N930SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > DAMAGE ON THE RT WINGLET RIB LOCATED AT RIGHT SIDE WGLTS3.25 WAS FOUND TO BE OUT OF LIMITS PER SRM 57-31-14. DAMAGE IS OUT OF LIMITS AND THE REPLACEMENT OF THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR REPAIR. REPLACED RT WINGLET RIB P/N 600-1
- [SDR SWIA2025111800007](https://openairdocs.org/sdr/SWIA2025111800007.md): Rib · damaged · Nov 17, 2025 · N930SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > DAMAGE ON THE RH WING PLUG RIB LOCATED BETWEEN WS353.00 AND WS 389.00 WAS FOUND TO BE OUT OF LIMITS PER SRM 57-21-12. DAMAGE IS OUT OF LIMITS AND THE REPLACEMENT OF THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR REPAIR. OPEN
- [SDR SWIA2025102800020](https://openairdocs.org/sdr/SWIA2025102800020.md): Landing Gear · faulted · Oct 20, 2025 · N930SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. RAN QRH, MESSAGE CLEARED. MEL 32-30-1CAT: A DOWNGRADED, ODI EVENT REQUIRES SMOD APPROVAL TO CLEAR MEL. GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. RAN QRH, MESSAGE CLEARED (FLIGHT 5089) DEFERRED GEAR RETRACT
- [SDR SWI2025F01452](https://openairdocs.org/sdr/SWI2025F01452.md): Landing Gear · warning message · Oct 20, 2025 · N930SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > D: GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. RAN QRH, MESSAGE CLEAREDC: MEL 32-30-1CAT: A DUE DATE: 21 OCT 2025CAT 2 DOWNGRADED ODI EVENT REQUIRES SMOD APPROVAL TO CLEAR MEL. GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. RAN QRH, MESSAGE CLEARED (FLIGHT 5
- [SDR SWIA202506160010](https://openairdocs.org/sdr/SWIA202506160010.md): Landing Gear · warning message · Jun 10, 2025 · N930SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > LANDING GEAR DISAGREE WARNING DURING LANDING. NOSE GEAR DID NOT COME DOWN, BOTH MAINS CAME DOWN AND LOCKED. RAN QRH, NOSE GEAR CAME DOWN AND LOCKED AFTER PULLING MANUAL GEAR EXTENSION HANDLE AND LEAVING IT EXTENDED. TRYING TO STOW LANDING GEAR EXTENSION HANDLE
- [SDR SWI2025F00723](https://openairdocs.org/sdr/SWI2025F00723.md): Warning Message · illuminated · Jun 10, 2025 · N930SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > LANDING GEAR DISAGREE WARNING DURING LANDING. NOSE GEAR DID NOT COME DOWN, BOTH MAINS CAME DOWN AND LOCKED. RAN QRH, NOSE GEAR CAME DOWN AND LOCKED AFTER PULLING MANUAL GEAR EXTENSION HANDLE AND LEAVING IT EXTENDED. TRYING TO STOW LANDING GEAR EXTENSION HANDLE
- [SDR SWIA20250527425](https://openairdocs.org/sdr/SWIA20250527425.md): Intercostal · damaged · Apr 25, 2025 · N930SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR FWD DD5 INTERCOSTAL TO HAVE ELONGATED HOLE UPON REMOVAL OF INNER SKIN (C-CHECK RO 05/27/2025)REMOVED DAMAGED INTERCOSTAL, LOCATED NEW SERVICEABLE INTERCOSTAL. MODIFIED INTERCOSTAL IAW MHIRJ REO 601R-52-11-3055 AND INSTALLED INTERCOSTAL IAW CRJ 2
- [SDR SWIA20250527421](https://openairdocs.org/sdr/SWIA20250527421.md): Floor Support · corroded · Apr 21, 2025 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON R/H CABIN FLOOR SILL AT FS 451, FS 460, AND FS 508 (C-CHECK RO 05/27/2025)REPAIRED R/H CABIN FLOOR SILL AT FS451, FS460, AND FS508 IAW BOMBARDIER REO 601R-53-41-666 REV-C DATED 2012-11-06
- [SDR SWI2025F00662](https://openairdocs.org/sdr/SWI2025F00662.md): Support Beam · failed insp · Apr 16, 2025 · N930SW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > ENGINE SUPPORT BEAM RBL27.50 CLOSE OUT ANGLE AT FS625.30 & WL111.09 HAS AN INDICATION.75" LONG BY 100% FSH PROPERGATING FROM THE LOWER FASTENER HOLE. FAILED NDT INSPECTION. (C-CHECK RO 05/27/2025)REMOVED UNSERVICEABLE RH ENG SUPPORT BEAM CLOSE OUT ANGLE (P/
- [SDR SWIA20250527416](https://openairdocs.org/sdr/SWIA20250527416.md): Support Beam · failed insp · Apr 16, 2025 · N930SW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > ENGINE SUPPORT BEAM LBL27.50 CLOSE OUT ANGLE AT FS625.30 & WL119.12 HAS AN INDICATION.3" LONG BY 100% FSH PROPERGATING FROM THE UPPER FASTENER HOLE. FAILED NDT INSPECTION. (C-CHECK RO 05/27/2025)REMOVED UNSERVICEABLE LH ENG SUPPORT BEAM CLOSE OUT ANGLE (P/N:
- [SDR SWI2025F00661](https://openairdocs.org/sdr/SWI2025F00661.md): Angle · damaged · Apr 11, 2025 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FASTENER PULLED THROUGH STRUCTURE FS 310.00 AT THE INTERSECTION OF PAX DOOR SILL ANGLE AND FS 310.00 CROSSBEAM (C-CHECK RO 05/27/2025)REPLACED PAX SILL ANGLE AT F.S. 310.00 IAW CRJ 200 SRM 51-42-13, 51-42-06, AND 51-42-11. COMPLETED SKYCARD 51-900-1003-SKY A
- [SDR SWI2025F00660](https://openairdocs.org/sdr/SWI2025F00660.md): Floor Support · corroded · Apr 11, 2025 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9.0 FLOORBEAM INBOARD FLANGE CORRODED IN MULTIPLE AREAS FROM FS 409+4 TO FS 409+120 (C-CHECK RO 05/27/2025)REPLACED RBL9 FLOORBEAM WITH NEW FABRICATED FLOOR BEAM 601R31117-17 IAW DWG 601R31117, CRJ 200 SRM 51-42-21, 51-42-22, 51-42-36, SND 601R-53-31-1332
- [SDR SWI2025F00659](https://openairdocs.org/sdr/SWI2025F00659.md): Floor Support · corroded · Apr 11, 2025 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 FLOOR BEAM HAS CORROSION AT SEVERAL LOCATIONS BETWEEN F.S.559+112 TO F.S,621 (C-CHECK RO 05/27/2025)COMPLIED WITH REPAIR TO LBL 27 FLOORBEAM FS559+112 - FS621. COMPLETED SKYCARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337.NO WEIGHT CHANGE NOTED.
- [SDR SWI2025F00658](https://openairdocs.org/sdr/SWI2025F00658.md): Stringer · corroded · Apr 11, 2025 · N930SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR22R IS CORRODED BETWEEN FS574 AND FS587. (C-CHECK RO 05/27/2025)PERFORMED STRINGER SPLICE REPAIR IAW CRJ200 SRM 53-00-03 REV. 38, DATED 03/10/2021 AND MHIRJ REO 601R-53-61-8323 REV. - -, DATED 05/21/2025. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA20250527411](https://openairdocs.org/sdr/SWIA20250527411.md): Floor Support · damaged · Apr 11, 2025 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H CABIN FLOOR SILL UPPER SURFACE AT FS459, FS519 REQUIRES EG (C-CHECK RO 05/27/2025)REPAIRED LH CABIN FLOOR SILL UPPER SURFACE AT FS 459 & FS519 IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPL
- [SDR SWI2025F00657](https://openairdocs.org/sdr/SWI2025F00657.md): Door Sill · corroded · Apr 10, 2025 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H CABIN FLOOR SILL UPPER SURFACE CORRODED AT THE FOLLOWING FRAME STATIONS: FS 459.00, FS 486.00, FS 493.00, FS 519.00, FS 523.00, AND FS 554.00 (C-CHECK RO 05/27/2025)REPAIRED LH CABIN FLOOR SILL UPPER SURFACE AT FS 459, FS486, FS493, FS519, FS523, AND FS55
- [SDR SWI2025F00656](https://openairdocs.org/sdr/SWI2025F00656.md): Door Sill · corroded · Apr 10, 2025 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H CABIN FLOOR SILL UPPER SURFACE CORRODED AROUND NUTPLATE HOLE FS 446.00 (C-CHECK RO 05/27/2025)COMPLIED WITH R/H CABIN FLOOR SILL UPPER SURFACE REPAIR AROUND NUTPLATE HOLE AT FS446.00 IAW BOMBARDIER REO 601R-53-41-666 REV-C DATED 2012-11-06. MAJOR REPAIR,
- [SDR SWIA20250527410](https://openairdocs.org/sdr/SWIA20250527410.md): Angle · cracked · Apr 10, 2025 · N930SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP ANGLE BETWEEN FS621 AND FS625 AT STGR14R IS CRACKED. (C-CHECK RO 05/27/2025)INSTALLED NEW ANGLE (INTERCOSTAL) AT STR 14R, FS 625 IAW CRJ200 SRM 51-40-11, 51-42-21. REFERENCE CONTINUATION CARD FOR WORK PERFORMED. COMPLETED TASK CARD 51-900-1003-SKY AND ATT
- [SDR SWIA20250527409](https://openairdocs.org/sdr/SWIA20250527409.md): Skin · dented · Apr 9, 2025 · N930SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS 6EA. SMALL DENTS BETWEEN FS625 TO FS640 AND STRINGERS 27 TO 25L. (C-CHECK RO 05/27/2025)COMPLIED WITH FUSELAGE SKIN REPAIR BETWEEN FS625 TO FS640 STGR 27 TO 25L. REF CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2025042708](https://openairdocs.org/sdr/SWIA2025042708.md): Floorbeam · corroded · Apr 8, 2025 · N930SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP AT RBL 9.00 HAS CORROSION ON THE INBOARD FLANGE AT MULTIPLE LOCATIONS THAT EXTEND UNDER THE SEAT TRACK, BETWEEN F.S. 409.00+112 AND F.S. 559.00. (C-CHECK RO 05/27/2025)REMOVED CORROSION FROM RBL 9 FLOOR BEAM CAP AT FS 409+112 - FS 559 AND REPAIR
- [SDR SWIA2025052700401](https://openairdocs.org/sdr/SWIA2025052700401.md): Access Panel · corroded · Apr 1, 2025 · N930SW · Cndair CL6002B19 · Wing, Plate/Skin
  > L/H WING, LOWER WING PLANK FUEL ACCESS PANEL CUTOUT HAS MINOR CORROSION AT THE OUTBOARD AND INBOARD EDGES. (540BB) (C-CHECK RO 05/27/2025)COMPLIED WITH REPAIR TO 540BB HOLE#1 LOCATION LOWER WING PLANK CUTOUT IAW REO 601R-57-21-030 REV L DATED 2014-02-05. COMPL
- [SDR SWIA2025052700228](https://openairdocs.org/sdr/SWIA2025052700228.md): Skin · damaged · Feb 28, 2025 · N930SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA79453-601R-53-61-7855 REV N930SW MXCODEID62997-PR - MULTIPLE DAMAGE TO FUSELAGE SKIN BETWEEN FS589 €“ FS605 AND STR20R €“ STR26R. PERFORMED TEMPORARY REPAIR TO FUSELAGE SKIN BETWEEN FS589 - FS605 AND STR20R - STR26R
- [SDR SWI20241014001018](https://openairdocs.org/sdr/SWI20241014001018.md): Seal · failed · Oct 13, 2024 · N930SW · Cndair CL6002B19 · Service Doors
  > DURING CRUISE, LDG ELEVATION WAS SPIKING BETWEEN 3000 AND 8800. WE RECEIVED A CALL FROM THE FLIGHT ATTENDANT ABOUT A LOUD HISSING NOISE IN THE AREA OF THE SERVICE DOOR. C ALT STEADILY INCREASED FROM 3000 TO 9100. WE INITIATED AN EMERGENCY DESCENT TO DIVERT TO
- [SDR SWIA202265161](https://openairdocs.org/sdr/SWIA202265161.md): None · broken · Mar 23, 2022 · N930SW · Cndair CL6002B19 · Doors
  > DURING TROUBLESHOOTING FOR THE PAX DOOR TOO DIFFICULT TO CLOSE FROM THE OUTSIDE, FOUND MAIN CABIN DOOR UPPER FORWARD BRACKET STOP IS BROKEN. (FILED - CLOSED) REMOVED AND REPLACED PAX DOOR UPPER FORWARD BRACKET STOP PN-600-38087-31 REF CRJ200 SRM 51-42
- [SDR SWIA202264278](https://openairdocs.org/sdr/SWIA202264278.md): None · damaged · Feb 3, 2022 · N930SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > FOUND HARDWARE ON LH ELEVATOR TO BE MISSING AND DAMAGED. (C CHECK RO 2-11-2022) INSTALLED NEW SERVICABLE HARDWARE IN LOCATIONS WHERE MISSING AND DAMAGED IAW CRJ-200 AMM 27-34-05-400-801.
- [SDR SWIA202164275](https://openairdocs.org/sdr/SWIA202164275.md): None · broken · Dec 30, 2021 · N930SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > L/H FLOOR SILL HAS 2 EA BROKEN NUTPLATES AT FS 439.00 (C CHECK RO 2-11-2022) REMOVED AND REPLACED L/H FLOOR SILL 2 EA NUTPLATES AT FS 439.00 IAW CRJ200 SRM 51-45-00
- [SDR SWIA202164243](https://openairdocs.org/sdr/SWIA202164243.md): None · damaged · Dec 29, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > INDICATION NOTED DURING WING SPLICE JOINT INSPECTION RH LOWER PLANK WS65.00 FWD INBD. HOLE FROM WS65.75 RIB 100% FULL SCREEN HEIGHT INDICATIONS WITH SUBSURFACE, SURFACE SCAN AND BOLT HOLE INSP. INDICATION APPROX..250" FROM INSIDE OF TANK DOWN PERFORMING BOLT
- [SDR SWIA202164242](https://openairdocs.org/sdr/SWIA202164242.md): None · cracked · Dec 18, 2021 · N930SW · Cndair CL6002B19 · Fuselage Structure (General)
  > CENTER WINDSHIELD POST (LWR. LEFT ANGLE BRACKET) CRACKED THROUGH AT RADIUS (AS MARKED) (C CHECK RO 2-11-2022) REMOVED AND REPLACED CENTER WINDSHIELD POST LWR LEFT ANGLE BRACKET IAW CRJ 200 SRM 51-40-11 AND 51-42-21 AND SKY CARD 51-900-1003-SKY NO WEIGHT C
- [SDR SWIA202164266](https://openairdocs.org/sdr/SWIA202164266.md): None · corroded · Dec 16, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL 21L FROM FS 310 TO FS 333 IS CORRODED. (C CHECK RO 2-11-2022) REPLACED INTERCOSTAL 21L FROM FS 310 TO FS 333 IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. REFER TO CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202164241](https://openairdocs.org/sdr/SWIA202164241.md): None · cracked · Dec 15, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 276.00 BETWEEN STGR 2R AND STGR 2L IS CRACKED AT CREW ESCAPE HATCH HINGE CUTOUT. (C CHECK RO 2-11-2022) REMOVED AND REPLACED FRAME IAW CRJ-200-SRM-51-42-06. FORM 337 COMPLETED, SKYCARD 51-900-1003-SKY COMPLETED WEIGHT AND BALANCE NOT AFFECTED REFERENCE
- [SDR SWIA202164240](https://openairdocs.org/sdr/SWIA202164240.md): None · elongated · Dec 15, 2021 · N930SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > L/H PRESSURE FLOOR SIL HAS ELONGATED NUTPLATE HOLE AT FS 424. (C CHECK RO 2-11-2022) COMPLIED WITH REPAIR OF L/H PRESSURE FLOOR SIL IAW MHIRJ REO 601R-53-41-2995 REV.-- DATED 2022-01-10. ATTACHED COMPLETED TASK CARD 51-900-1003-SKY AND COMPLETED FORM 337.
- [SDR SWIA202164274](https://openairdocs.org/sdr/SWIA202164274.md): None · corroded · Dec 13, 2021 · N930SW · Cndair CL6002B19 · Ailerons
  > R/H OTBD FLAP HINGE ARM ASSY. MOUNTING HARDWARE AT WS178.00 AND WS264.00 WAS FOUND CORRODED AND REQUIRES REPLACEMENT. (C CHECK RO 2-11-2022) RH OTBD FLAP HINGE ARM ASSY MOUNTING HARDWARE AT WS178.00 AND WS264.00 REPLACED IAW CRJ 200 AMM 57-53-02-400-801
- [SDR SWIA202164273](https://openairdocs.org/sdr/SWIA202164273.md): None · corroded · Dec 13, 2021 · N930SW · Cndair CL6002B19 · Ailerons
  > L/H OTBD FLAP HINGE ARM ASSY. MOUNTING HARDWARE AT WS178.00 AND WS264.00 WAS FOUND CORRODED AND REQUIRES REPLACEMENT. (C CHECK RO 2-11-2022) LH OTBD FLAP HINGE ARM ASSY MOUNTING HARDWARE AT WS178.00 AND WS264.00 REPLACED IAW CRJ 200 AMM 57-53-02-400-801
- [SDR SWIA202164265](https://openairdocs.org/sdr/SWIA202164265.md): None · sheared · Dec 12, 2021 · N930SW · Cndair CL6002B19 · Fuselage Structure (General)
  > FS621-625 ATTACH ANGLE HAS SHEARED FASTENERS AT RBL 36 BETWEEN STGR 9R AND 10R (C CHECK RO 2-11-2022) REMOVED AND REPLACED FS621-FS 625 ANGLE AT RBL 36 BETWEEN STGR 9R AND 10R IAW MHIRJ REO 601R-53-61-7766 REV -- DATED 2021-12-16 REF ATTACHED CONTINUATION
- [SDR SWIA202164264](https://openairdocs.org/sdr/SWIA202164264.md): None · cracked · Dec 12, 2021 · N930SW · Cndair CL6002B19 · Fuselage Structure (General)
  > RH OBLIQUE ANGLE CRACKED FROM FS 621-625 (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH OBLIQUE ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-21 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
- [SDR SWIA202164239](https://openairdocs.org/sdr/SWIA202164239.md): None · damaged · Dec 10, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, Keel
  > FOUND LIGHTNING STRIKE DAMAGE BETWEEN F.S.409.00+80 - F.S.409.00+96 STRINGER 25R - 26R (C CHECK RO 2-11-2022) REPAIRED LIGHTNING STRIKE DAMAGE BETWEEN F.S.409.00+80 - F.S.409.00+96 STRINGER 25R - 26R IAW MHIRJ REO 601R-53-31-1217 REV -- DATED 2022-01-18 AN
- [SDR SWIA202164238](https://openairdocs.org/sdr/SWIA202164238.md): None · damaged · Dec 9, 2021 · N930SW · Cndair CL6002B19 · Aileron Tabs
  > WS 178 R/H FLAP HINGE BOX AFT O/B MOUNT FITTING I/B LUG I/B FACE AFT CORNER HAS TOOLING DAMAGE (C CHECK RO 2-11-2022) REPAIRED WS 178 R/H FLAP HINGE BOX AFT O/B MOUNT FITTING I/B LUG I/B FACE AFT CORNER TOOLING DAMAGE IAW MHIRJ REO 601R-57-21-3557 REV -- D
- [SDR SWIA202164237](https://openairdocs.org/sdr/SWIA202164237.md): None · corroded · Dec 8, 2021 · N930SW · Cndair CL6002B19 · Aileron Tabs
  > WS 264 O/B HINGE BOX ATF O/B FITTING I/B LUG I/B FACE AFT EDGE HAS TOOLING DAMAGE (C CHECK RO 2-11-2022) REPAIRED WS 264 O/B HINGE BOX ATF O/B FITTING I/B LUG I/B FACE AFT EDGE TOOLING DAMAGE IAW MHIRJ REO 601R-57-21-3557 REV -- DATED 2021-12-15 AND SKY C
- [SDR SWIA202164236](https://openairdocs.org/sdr/SWIA202164236.md): None · corroded · Dec 7, 2021 · N930SW · Cndair CL6002B19 · Fuselage Structure (General)
  > SEVERAL LOCATIONS ON SKIN SURROUNDING NUTPLATES UNDER FWD BELLY FAIRINGS 191BB AND 192BB ARE CORRODED (C CHECK RO 2-11-2022) COMPLIED WITH REO 601R-53-31-1214 REV-- DATED: 2022-01-05, 337 COMPLETE, SKYCARD 51-900-1003 -SKY ATTACHED. REFERENCE CONTINUE CAR
- [SDR SWIA202164272](https://openairdocs.org/sdr/SWIA202164272.md): None · corroded · Dec 2, 2021 · N930SW · Cndair CL6002B19 · Fuselage Structure (General)
  > ANGLE ATTACHING TO LEFT WING AFT SPAR HAS LIGHT SURFACE CORROSION AT APPROX. WS 176 (C CHECK RO 2-11-2022) FOUND CORROSION ON L/H WING T/E ATTACH ANGLE (P/N 601R10217-1) TO BE WITHIN ALLOWABLE LIMITS OF CRJ-200 SRM 57-51-14 AND 57-00-00. REMOVED MINOR CORR
- [SDR SWIA202164235](https://openairdocs.org/sdr/SWIA202164235.md): None · damaged · Dec 2, 2021 · N930SW · Cndair CL6002B19 · Wing Structure
  > INDICATIONS NOTED ON THE RH LOWER WING PLANK AROUND THE CIRCUMFERENCE OF THE LAND FOR ACCESS PANEL 650BB 100% FULL SCREEN HEIGHT FAILING NDT. (C CHECK RO 2-11-2022) REPAIRED CORROSION ON RH LOWER WING PLANK AROUND THE CIRCUMFERENCE TO INCLUDE IN THE CRITIC
- [SDR SWIA202164234](https://openairdocs.org/sdr/SWIA202164234.md): None · gouged · Dec 2, 2021 · N930SW · Cndair CL6002B19 · Doors
  > SERVICE DOOR LOWER SEAL STRIKER HAS 2EA. GOUGES APPROX..5 INCHES WIDE BY.025 INCHES DEEP) (C CHECK RO 2-11-2022) REMOVED AND REPLACED THE SERVICE DOOR LOWER SEAL STRIKER IAW CRJ 200 SRM 51-42-06, 51-40-11, 51-41-00, & SKYCARD 51-900-1003-SKY NO WEIGHT CH
- [SDR SWIA202164263](https://openairdocs.org/sdr/SWIA202164263.md): None · cracked · Dec 1, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, Keel
  > STRINGER REPAIR ANGLE AT F.S. 280 3L IS CRACKED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED STRINGER CLIP IAW CRJ-200-SRM-51-42-06 AND 51-42-21.
- [SDR SWIA202164271](https://openairdocs.org/sdr/SWIA202164271.md): None · corroded · Nov 30, 2021 · N930SW · Cndair CL6002B19 · Doors
  > PAX DOOR AFT ANCHOR FITTING IS CORRODED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING IAW CRJ 200 AMM 52-11-17-400-804 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
- [SDR SWIA202164270](https://openairdocs.org/sdr/SWIA202164270.md): None · corroded · Nov 30, 2021 · N930SW · Cndair CL6002B19 · Doors
  > PAX DOOR AFT ANCHOR FITTING PLATE IS CORRODED. (C CHECK RO 2-11-2022) REMOVED PAX DOOR AFT ANCHOR FITTING PLATE AND INSTALLED SERVICEABLE PLATE IAW CRJ200 AMM 52-11-17-400-804.
- [SDR SWIA202164262](https://openairdocs.org/sdr/SWIA202164262.md): None · gouged · Nov 30, 2021 · N930SW · Cndair CL6002B19 · Doors
  > PAX DOOR FWD ANCHOR FITTING IS GOUGED. (C CHECK RO 2-11-2022) REMOVED AND REPLACED PAX DOOR FWD ANCHOR FITTING IAW CRJ 200 AMM 52-11-17-400-804 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
- [SDR SWIA202164261](https://openairdocs.org/sdr/SWIA202164261.md): None · sheared · Nov 30, 2021 · N930SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FLIGHT COMPARTMENT FLOOR BEAM AT LBL 9 FWD SIDE OF FS 280.00 CROSSBEAM HAS A SHEARED RIVETS (C CHECK RO 2-11-2022) REMOVED AND REPLACED TWO RIVETS ONTHE FLIGHT COMPARTMENT FLOOR BEAM AT LBL 9 FWD SIDE OF FS 280.00 CROSSBEAM IAW CRJ 200 SRM 51-42-06
- [SDR SWIA202164260](https://openairdocs.org/sdr/SWIA202164260.md): None · sheared · Nov 30, 2021 · N930SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FLIGHT COMPARTMENT FLOOR BEAM AT RBL 9 FWD SIDE OF FS 280.00 CROSSBEAM HAS 2 SHEARED RIVETS. (C CHECK RO 2-11-2022) REMOVED AND REPLACED TWO RIVETS ON THE FLIGHT COMPARTMENT FLOOR BEAM AT RBL 9 FWD SIDE OF FS 280.00 CROSSBEAM IAW CRJ 200 SRM 51-42-06
- [SDR SWIA202164233](https://openairdocs.org/sdr/SWIA202164233.md): None · corroded · Nov 29, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333 LOWER L/H FRAME SEGMENT IS CORRODED BETWEEN STR 22L AND STR 23L. (C CHECK RO 2-11-2022) COMPLIED WITH REPLACEMENT OF F.S. 333 FRAME BETWEEN STR 17L AND STR 23L IAW CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND
- [SDR SWIA202164232](https://openairdocs.org/sdr/SWIA202164232.md): None · cracked · Nov 29, 2021 · N930SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL CRACKED AT FS 333.00 BETWEEN STGR 0 AND STRG 1. (C CHECK RO 2-11-2022) UPON FURTHER INVESTIGATION FOUND FS 333 FRAME SEGMENT CRACKED AT STR 0 AND STR 1. REPAIRED FRAME IAW REO 601R-53-21-3513 REV -- DATED 2021-12-21. COMPLETED SKYCARD 51-900-10

Next page: https://openairdocs.org/aircraft/N930SW/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 = 'N930SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N930SW/reports

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