# Service difficulty reports: N825SK

A list on [N825SK](https://openairdocs.org/aircraft/N825SK.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 · 187 reports

- [SDR SWI2025F01051](https://openairdocs.org/sdr/SWI2025F01051.md): Drag Angle · cracked · Apr 22, 2025 · N825SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LEFT VERTICAL STABILIZER DRAG ANGLE AFT CRACKED. PERFORMED REPIAR DRAG ANGLE AFT ON LT VERTICAL STABILIZER IAW REO 670-55-31-018 REV-A, & SRM 51-26-01, NDT PERFORMED.
- [SDR SWIA2025072200422](https://openairdocs.org/sdr/SWIA2025072200422.md): Drag Angle · cracked · Apr 22, 2025 · N825SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > RIGHT VERTICAL STABILIZER DRAG ANGLE AFT CRACKED. PERFORMED REPAIR DRAG ANGLE AFT AT RH VERTICAL STABILIZER IAW REO 670-55-31-018 REV-A, SRM 51-26-01, NDT PERFORMED.
- [SDR SWI2025F01053](https://openairdocs.org/sdr/SWI2025F01053.md): Slat Track · corroded · Apr 13, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING NR 4 SLAT TRACK HAD CORROSION ON UPPER SIDE. PERFORMED REPAIR ON LT WING NR 4 SLAT TRACK ON UPPER SIDE IAW REO 690-57-42-1225, REV -, SRM 51-12-00. NDT PERFORMED.
- [SDR SWI2025F01052](https://openairdocs.org/sdr/SWI2025F01052.md): Slat Track · corroded · Apr 13, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING NR 1 SLAT TRACK HAS CORROSION ON UPPER SIDE. REPAIRED DAMAGE TO LT WING NR 1 SLAT TRACK IAW SRM 51-21-06 & REO 690-57-42-1226 REV-. NDT PERFORMED.
- [SDR SWIA2025072200413](https://openairdocs.org/sdr/SWIA2025072200413.md): Slat Track · corroded · Apr 13, 2025 · N825SK · Cndair CL6002D24 · Wing, Nacelle/Pylon Attach Fittings
  > LEFT WING NR 5 SLAT TRACK HAS CORROSION ON UPPER AND LWR SIDE REPAIRED DAMAGE TO LT WING NR 5 SLAT TRACK UPPER & LOWER SIDE IAW SRM 51-12-00 AND REO 690-57-42-1224 REV-. NDT PERFORMED, REPORT# S042425-8.
- [SDR SWIA2025072200411](https://openairdocs.org/sdr/SWIA2025072200411.md): Panel · cracked · Apr 11, 2025 · N825SK · Cndair CL6002D24 · Wing, Plate/Skin
  > LEFT WING UPPER SURFACE PANEL 522BL APPROX WS 199 APPROX 61 1/2 INCHES OTBD OF PANEL INBD EDGE CRACKED APPROX 4 INCHES LONG. REPAIRED DAMAGE TO LT WING LEADING EDGE PANEL 522BL IAW SRM 51-26-00, 57-41-01, 51-21-11 & REO 690-57-41-500 REV-P1 & REV-. NDT PER
- [SDR SWIA20250514310](https://openairdocs.org/sdr/SWIA20250514310.md): Lintel · cracked · Mar 10, 2025 · N825SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION LINTEL AND INCORPORATION OF SB670BA-53-040 FOUND STGR 3L LINTEL CRACKED. REQUIRES REO670-53-21-493 TO BE COMPLETED (FILED CLOSED)COMPLIED WITH DISPOSITION INSTRUCTIONS OUTLINED IN REO 670-53-21-493, REV -D, DATED 2015-07-10 AND SB670BA-53-040
- [SDR SWIA2025040400310](https://openairdocs.org/sdr/SWIA2025040400310.md): Lintel · cracked · Mar 10, 2025 · N825SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION LINTEL AND INCORPORATION OF SB670BA-53-040 FOUND STGR 3L LINTEL CRACKED. REQUIRES REO670-53-21-493 TO BE COMPLETED (FILED OPEN)COMPLIED WITH DISPOSITION INSTRUCTIONS OUTLINED IN REO 670-53-21-493, REV -D, DATED 2015-07-10 AND SB670BA-53-040 A
- [SDR SWI2025F01061](https://openairdocs.org/sdr/SWI2025F01061.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 2-2 900 RH - COMPLY WITH TASK CARD 27-630-809 RH TRACK ROLLER SEALED, TRACK 2-2, TOP FORWARD - SLAT 2 (PN CC670-12272-1). (MRB 27-81-43-725), COMPLIED WITH SKYWEST TASKCARD 27-630-809. NO DISCREPANCIES
- [SDR SWI2025F01060](https://openairdocs.org/sdr/SWI2025F01060.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 2-2 900 LH - COMPLY WITH TASK CARD 27-530-809 LH TRACK ROLLER SEALED, TRACK 2-2, TOP FORWARD - SLAT 2 (PN CC670-12272-1). (MRB 27-81-43-725), COMPLIED WITH SKYWEST TASKCARD 27-530-809.
- [SDR SWI2025F01059](https://openairdocs.org/sdr/SWI2025F01059.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-3 900 RH - COMPLY WITH TASK CARD 27-630-809 RH TRACK ROLLER SEALED, TRACK 1-3, TOP FORWARD - SLAT 1 (PN CC670-12272-1). (MRB 27-81-43-718), COMPLIED WITH SKYWEST TASKCARD 27-630-809.
- [SDR SWI2025F01058](https://openairdocs.org/sdr/SWI2025F01058.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-3 900 LH - COMPLY WITH TASK CARD 27-530-809 LH TRACK ROLLER SEALED, TRACK 1-3, TOP FORWARD - SLAT 1 (PN CC670-12272-1). (MRB 27-81-43-718), COMPLIED WITH SKYWEST TASKCARD 27-530-809.
- [SDR SWI2025F01057](https://openairdocs.org/sdr/SWI2025F01057.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 900 RH - COMPLY WITH TASK CARD 27-630-809 RH TRACK ROLLER SEALED, TRACK 1-2, TOP FORWARD - SLAT 1 (PN CC670-12272-1) (MRB 27-81-43-717), COMPLIED WITH SKYWEST TASKCARD 27-630-809.
- [SDR SWI2025F01056](https://openairdocs.org/sdr/SWI2025F01056.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 900 LH - COMPLY WITH TASK CARD 27-530-809 LH TRACK ROLLER SEALED, TRACK 1-2, TOP FORWARD - SLAT 1 (PN CC670-12272-1) (MRB 27-81-43-717), COMPLIED WITH SKYWEST TASKCARD 27-530-809.
- [SDR SWI2025F01055](https://openairdocs.org/sdr/SWI2025F01055.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 3-2 900 RH - RH SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK PN CC670-12459-4 DUE LIFE LIMIT. REMOVE AND DISCARD. REPLACE WITH SERVICEABLE PARTS IAW 27-630-816 (MRB 27-81-43-702), COMPLIED WITH SKYWEST
- [SDR SWI2025F01054](https://openairdocs.org/sdr/SWI2025F01054.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Wing, Nacelle/Pylon Attach Fittings
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 3-2 900 LH - LH SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK PN CC670-12459-3 DUE LIFE LIMIT. REMOVE AND DISCARD. REPLACE WITH SERVICEABLE PARTS IAW 27-530-816 (MRB 27-81-43-702), PART NUMBER: COMPLIE
- [SDR SWIA202507220103](https://openairdocs.org/sdr/SWIA202507220103.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Wing, Fuselage Attach Fittings
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 2-2 900 RH - RH SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK PN CC670-12027-3 (QTY 2) AND SIDE ROLLER ASSY 0.875 DIA. SLAT TRACK PN CC670-12048-3 (QTY 2) ARE DUE LIFE LIMIT. REMOVE AND DISCARD. REPLACE W
- [SDR SWIA202507220102](https://openairdocs.org/sdr/SWIA202507220102.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 2-2 900 LH - LH SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK PN CC670-12027-3 (QTY 2) AND SIDE ROLLER ASSY 0.875 DIA. SLAT TRACK PN CC670-12048-3 (QTY 2) ARE DUE LIFE LIMIT. REMOVE AND DISCARD. REPLACE W
- [SDR SWIA2025072200101](https://openairdocs.org/sdr/SWIA2025072200101.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 1-2 900 RT - RT SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK AND SIDE ROLLER ASSY 0.875 DIA. ARE DUE LIFE LIMIT. REMOVE AND DISCARD. REPLACE WITH SERVICEABLE PARTS IAW 27-620-804 (MRB 27-81-43-702, 27-
- [SDR SWIA2025072200102](https://openairdocs.org/sdr/SWIA2025072200102.md): Roller · out of limits · Jan 2, 2025 · N825SK · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 1-2 900 LH - LH SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK PN CC670-12027-3 (QTY 2) AND SIDE ROLLER ASSY 0.875 DIA. SLAT TRACK PN CC670-12048-3 (QTY 2) ARE DUE LIFE LIMIT. REMOVE AND DISCARD. REPLACE W
- [SDR SWIA20231208](https://openairdocs.org/sdr/SWIA20231208.md): Radome · damaged · Dec 8, 2023 · N825SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > TRANSFER FROM EAML 1259356: REF AML 1257667, THE RADOME BULKHEAD AND FUSELAGE SURFACE AREA AT 10 TO 12 O'CLOCK IS DAMAGED FROM A BIRD STRIKE. COMPLY WITH REO 670-51-00-085 REV "A" DATED 8/23/2017 (FILED CLOSED)COMPLIED WITH DRESS BACK OF DAMAGE TO FWD BULKHEA
- [SDR SWIA2024011131208](https://openairdocs.org/sdr/SWIA2024011131208.md): Unknown · damaged · Dec 8, 2023 · N825SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > TRANSFER FROM EAML 1259356: REF AML 1257667, THE RADOME BULKHEAD AND FUSELAGE SURFACE AREA AT 10 TO 12 O'CLOCK IS DAMAGED FROM A BIRD STRIKE. COMPLY WITH REO 670-51-00-085 REV "A" DATED 8/23/2017 (FILED OPEN)COMPLIED WITH DRESS BACK OF DAMAGE TO FWD BULKHEAD
- [SDR SWIA20240110208](https://openairdocs.org/sdr/SWIA20240110208.md): Unknown · damaged · Dec 8, 2023 · N825SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CLASSIFICATION OF THE DAMAGE REQUIRED IAW GMM 3-26, AIRCRAFT REPAIRS (MAJOR/MINOR), (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27533320 WITH THE FOLLOWING CORRECTIVE ACTION: "DETERMINED DAMAGE TO FWD BULKHEAD RADOME AREA AT FS169.00 TO BE CLAS
- [SDR SWIA2024011031204](https://openairdocs.org/sdr/SWIA2024011031204.md): Unknown · damaged · Dec 4, 2023 · N825SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > THE RADOME BULKHEAD AND FUSELAGE SURFACE AREA AT 10 TO 12 O'CLOCK IS DAMAGED FROM A BIRD STRIKE. CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1257093 (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27533316 WITH THE FOLLOWING CORRECTIVE A
- [SDR SWIA2024022200003](https://openairdocs.org/sdr/SWIA2024022200003.md): Radome · cracked · Dec 3, 2023 · N825SK · Cndair CL6002D24 · Aerodynamic Fairings
  > BIRD STRIKE. NOSE IS CRACKED AND DENTED. BIRD REMAINS FOUND NEAR ENGINE AND IN THE CRACKS ON THE NOSE (FLIGHT 3754 FILED CLOSED)COMPLIED WITH BIRD STRIKE INSP PER CRJ 900 AMM 05-51-25. REF AML1257481, 1257461, 1258140, 1257126, 1257667, 1257939 AND 1257572 FO
- [SDR SWIA202266905](https://openairdocs.org/sdr/SWIA202266905.md): Support Channel · cracked · Nov 16, 2022 · N825SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR AFT TRACK SUPPORT CHANNEL CRACKED THROUGH ABOUT 4 INCHES INBOARD OF DOOR SURROUND FRAME NEAREST TO THE FLOOR, EVALUATED AND FOUND TO BE OUT OF LIMITS IAW IAW SRM 53-61-58.
- [SDR SWIA202265372](https://openairdocs.org/sdr/SWIA202265372.md): None · failed · Apr 15, 2022 · N825SK · Cndair CL6002D24 · Window/Windshield System
  > L WINDOW HEAT CAUTION IN FLIGHT (FLIGHT 3844 - FILED CLOSED) REMOVED AND REPLACED LH SIDE WINDOW REF AMM 56-12-01 AND COMPLETED TC 56-220-1000-SKY / PLEASE REFERENCE AML 887914
- [SDR SWIA202162278](https://openairdocs.org/sdr/SWIA202162278.md): None · chafed · Nov 3, 2021 · N825SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > LH SLAT TRAILING EDGE AT SS199.66 CHAFED (C-CHECK RO 11/04/2021) BLENDED CHAFE ON LH SLAT NO.1 TRAILING EDGE AT SS199.66 AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO 690-57-42-854 REV -- 2021-11-02. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202162277](https://openairdocs.org/sdr/SWIA202162277.md): None · chafed · Nov 3, 2021 · N825SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > LH SLAT #3 TRAILING EDGE AT SS341.66 CHAFED (C-CHECK RO 11/04/2021) BLENDED CHAFE ON LH SLAT NO.3 TRAILING EDGE AT SS341.66 AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO 690-57-42-856 REV -- 2021-11-02. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202162276](https://openairdocs.org/sdr/SWIA202162276.md): None · chafed · Nov 3, 2021 · N825SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > LH SLAT #2 TRAILING EDGE AT SS199.66 AND SS341.66 CHAFED (C-CHECK RO 11/04/2021) BLENDED CHAFE ON LH SLAT NO.2 TRAILING EDGE AT SS199.66 AND SS341.66 AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO 690-57-42-855 REV -- 2021-11-02. COMPLIED WITH TAS
- [SDR SWIA202162275](https://openairdocs.org/sdr/SWIA202162275.md): None · mislocated · Oct 17, 2021 · N825SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > WHILE BACK DRILLIG NEW INTERCOSTALS ON PAX DOOR FOUND INTERCOSTAL AT DD2 FS320-338 TO BE MISSLOCATED (C-CHECK RO 11/04/2021) A NEW PART WAS REPLACED IAW CRJ900 SRM 51-42-06-00-A01 AND 51-42-21-001-001-A01 WITH REFERENCE TO DWG #601R31702 REV-N SEE CONTINU
- [SDR SWIA202162274](https://openairdocs.org/sdr/SWIA202162274.md): None · corroded · Oct 6, 2021 · N825SK · Cndair CL600* · Fuselage Main, Keel
  > STRINGER 23R PN: SH670-31380-1 @ FS333 TO FS379 IS CORRODED. (C-CHECK RO 11/04/2021) STRINGER 23R LOCATED BETWEEN FS333 & FS379 WAS FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ900 SRM 51-42-06-001-001-A01 & DWG SH670-31350 REV A, COMPLIED WITH T
- [SDR SWIA202162273](https://openairdocs.org/sdr/SWIA202162273.md): None · corroded · Oct 6, 2021 · N825SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > JOINT PIECE PN: SH670-32429-4 @ STGR 22R FS333 IS CORRODED. (C-CHECK RO 11/04/2021) REMOVED AND REPLACED JOINT PIECE PN: SH670-32429-4 AT STGR 22R ON FS333.0 REF CRJ900 SRM 51-42-06-001-001-A01 & DWG SH670-32420 REV E. SEE CONTINUE CARD FOR DETAILS. COMPLI
- [SDR SWIA202162272](https://openairdocs.org/sdr/SWIA202162272.md): None · corroded · Oct 4, 2021 · N825SK · Cndair CL600* · Fuselage Main, Keel
  > DURING ACCESS FOR REPLACEMENT OF LOWER FRAME SECTOR AT FS333 FOUND STRINGER AT 21R, FS333-FS379 TO BE EXFOLIATED (C-CHECK RO 11/04/2021) REMOVED EXFOLIATED STRINGER AT 21R, FS333-FS379 IAW CRJ900 SRM 51-42-06-001-001-A01, INSTALLED NEW STRINGER 21R LOCATED
- [SDR SWIA202162271](https://openairdocs.org/sdr/SWIA202162271.md): None · corroded · Oct 4, 2021 · N825SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > DURING ACCESS FOR REPLACEMENT OF LOWER FRAME SECTOR AT FS333 FOUND INTERCOSTAL AT 21L, FS333-FS349 TO BE EXFOLIATED (C-CHECK RO 11/04/2021) REPLACED INTERCOSTAL 21L BETWEEN FS333.00 - FS349.00 IAW DWG SH670-31823 REV NC AND REF CRJ900 SRM 51-42-06-001-001-
- [SDR SWIA202162270](https://openairdocs.org/sdr/SWIA202162270.md): None · corroded · Oct 4, 2021 · N825SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > DURING ACCESS OF PAX DOOR INTERCOSTAL AT DD1A FS320-338. FOUND CHANNEL PN: 601R318274-1 TO BE CORRODED (C-CHECK RO 11/04/2021) CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED CHANNEL WITH NEW P/N601R318274-1 IAW CRJ900 SRM 51-42-21-001-001-A01 AN
- [SDR SWIA202162269](https://openairdocs.org/sdr/SWIA202162269.md): None · corroded · Oct 4, 2021 · N825SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > STRG21R JOINT PIECE AT FS333 IS CORRODED (C-CHECK RO 11/04/2021) REMOVED AND REPLACED JOINT PIECE AT STGR 21R ON FS333.0 REF CRJ900 SRM 51-42-06-001-001-A01 & DWG SH670-32420 REV E. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-
- [SDR SWIA202162268](https://openairdocs.org/sdr/SWIA202162268.md): None · corroded · Oct 3, 2021 · N825SK · Cndair CL600* · Fuselage Main, Keel
  > STRG23R BETWEEN FS319.70 AND FS333 IS CORRODED (C-CHECK RO 11/04/2021) STGR 23R BETWEEN FS280.00 - FS333.00 WAS FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED INSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, DWG SH670-31630 R
- [SDR SWIA202162267](https://openairdocs.org/sdr/SWIA202162267.md): None · corroded · Oct 3, 2021 · N825SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > STRG23R 333 JOINT PIECE IS CORRODED (C-CHECK RO 11/04/2021) REMOVED AND REPLACED JOINT PIECE AT STGR 23R ON FS333.0 REF CRJ900 SRM 51-42-06-001-001-A01 & DWG SH670-32420 REV E. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA202162266](https://openairdocs.org/sdr/SWIA202162266.md): None · corroded · Oct 3, 2021 · N825SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > STRG24R 333 JOINT PIECE IS CORRODED (C-CHECK RO 11/04/2021) REMOVED AND REPLACED JOINT PIECE AT STGR 24R ON FS333.0 REF CRJ900 SRM 51-42-06-001-001-A01 & DWG SH670-32420 REV E. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA202162265](https://openairdocs.org/sdr/SWIA202162265.md): None · damaged · Oct 2, 2021 · N825SK · Cndair CL600* · Fuselage Structure (General)
  > WHILE PERFORMING REPAIR FOR REO 690-53-61-1034 REV--, DATED 2021-09-29 FOR DOME NUTPLATE HOLE #2 ON FUSELAGE SKIN AT AFT BAG BAY SCUFF PLATE, APPROX. FS 1010, STGR 17L, THE FASTENER HOLE WAS INADVERTENTY REAMED TO 0.4688". (C-CHECK RO 11/04/2021) COMPLIED
- [SDR SWIA202162264](https://openairdocs.org/sdr/SWIA202162264.md): None · corroded · Sep 27, 2021 · N825SK · Cndair CL600* · Fuselage Internal Stairs
  > AFTER REMOVED SERVICE DOOR LOWER SILL BETWEEN FS319 AND FS349 IS FOUND CORROSION 80% SURFACE ON LOWER FLOOR SUPPORT TOP ANGLE (C-CHECK RO 11/04/2021) REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT SERVICE DOOR LWR SILL PER CRJ900 SRM 51-42-06-001-001-A01, CR
- [SDR SWIA202162263](https://openairdocs.org/sdr/SWIA202162263.md): None · corroded · Sep 26, 2021 · N825SK · Cndair CL600* · Fuselage Main, Frame
  > AFTER REMOVAL OF THE RH FS280 CROSSBEAM FOUND THE RH LOWER BULKHEAD WEB TO BE EXFOLIATED (C-CHECK RO 11/04/2021) REMOVED AND REPLACED RH FS280 CROSSBEAM AT RH LOWER BULKHEAD WEB REF CRJ900 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202162262](https://openairdocs.org/sdr/SWIA202162262.md): None · corroded · Sep 26, 2021 · N825SK · Cndair CL600* · Fuselage Main, Keel
  > STRG25R JOINT PIECE AT FS333 IS CORRODED (C-CHECK RO 11/04/2021) STRG25R JOINT PIECE AT FS333 WAS FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ-900 SRM 51-42-06-001-001-A01 & DWG: SH670-32420 REV E, COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK
- [SDR SWIA202162261](https://openairdocs.org/sdr/SWIA202162261.md): None · corroded · Sep 24, 2021 · N825SK · Cndair CL600* · Doors
  > RH FLOOR SILL SPLICE ANGLE AT FS307.00 CORRODED (C-CHECK RO 11/04/2021) REMOVED AND INSTALLED NEW RH FLOOR SILL SPLICE ANGLE AT FS307.00. REF CRJ-900 SRM 51-42-10-001-001-A01 AND DWG: SH690-32170 REV AD. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202162260](https://openairdocs.org/sdr/SWIA202162260.md): None · corroded · Sep 23, 2021 · N825SK · Cndair CL600* · Fuselage Main, Keel
  > STRG27 BETWEEN FS319.70 AND FS310.00 IS CORRODED (C-CHECK RO 11/04/2021) COMPLIED WITH REO 690-53-21-1432 REV -- DATED 2021-09-28 FOR THE REPAIR OF STRG27 BETWEEN FS319.70 AND FS310.00, COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK CHECK GOOD
- [SDR SWIA202162258](https://openairdocs.org/sdr/SWIA202162258.md): None · cracked · Sep 21, 2021 · N825SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > DURING INSPECTION OF TC 57-540-140 DISCOVERED THAT THE LEFT #1-3 SLAT TRACK CANISTER BRACKET IS CRACKED. (MARKED) (C-CHECK RO 11/04/2021) COMPLIED WITH THE REPAIR AT LH WING SLAT TRACK 1-3 CANNISTER REF-CRJ-900 REO 670-57-42-577 REV -- DATE 2016-12-02. /
- [SDR SWIA202162257](https://openairdocs.org/sdr/SWIA202162257.md): None · corroded · Sep 21, 2021 · N825SK · Cndair CL600* · Fuselage Main, Frame
  > PAX DOOR FRAME AT FS313.5 BTWN DD4 AND DD5 HAS CORROSION (C-CHECK RO 11/04/2021) REMOVED AND REPLACED PAX DOOR FRAMEL AT FS313.5 BTWN DD4 AND DD5 IAW CRJ900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV-N, SEE CONTINUATION FOR WORK ACCOMPLISHED, COMPLIED
- [SDR SWIA202162256](https://openairdocs.org/sdr/SWIA202162256.md): None · corroded · Sep 20, 2021 · N825SK · Cndair CL600* · Fuselage Main, Frame
  > AFTER REMOVAL OF THE LH FS280 CROSSBEAM FOUND LH LOWER BULKHEAD WEB TO BE EXFOLIATED (C-CHECK RO 11/04/2021) REMOVED AND REPLACED LH FS280 CROSSBEAM AT LH LOWER BULKHEAD WEB REF CRJ900 SRM 53-11-10-201-004-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002
- [SDR SWIA202162255](https://openairdocs.org/sdr/SWIA202162255.md): None · corroded · Sep 20, 2021 · N825SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL ATTACH CLIP AT DD4 FS320 HAS CORROSION (C-CHECK RO 11/04/2021) THE ATTATCH CLIP AT DD4 F/S320 WAS REMOVED AND REPLACED WITH A NEW PART IAW CRJ900 SRM 51-42-06-001-001-A01 SEE CONTINUE CARD FOR PERTINENT DETAILS C/W TASK CARD 51-900-100

Next page: https://openairdocs.org/aircraft/N825SK/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 = 'N825SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N825SK/reports

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