# Service difficulty reports: N606SK

A list on [N606SK](https://openairdocs.org/aircraft/N606SK.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 · 232 reports

- [SDR SWIA2026071176617](https://openairdocs.org/sdr/SWIA2026071176617.md): Gcu · failed · Jul 11, 2026 · N606SK · Cndair CL6002C10 · Electrical Power System
  > AFTER RECEIVING GEN 1 OFF, RECEIVED A FWD SMOKE CARGO. SMOKE WARNING WENT AWAY AFTER ABOUT 2 MINS. CHKD W FLT ATTS & NO SMOKE OR ODOR IN CABIN. RETURNED TO SHV. AFTER LANDING, COULD SMELL AN ELECT BURNING ODOR & BLEW FWD CARGO HALON BOTTLES. SMOKE WARNING CAME
- [SDR SWIA2025120124](https://openairdocs.org/sdr/SWIA2025120124.md): Skin · dented · Nov 24, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EVALUATE DENT MARKED WITH YELLOW DOT ON LH FUSELAGE SKIN ABOVE FWD CARGO DOOR. (C-CHECK RO 11/30/2025)AFTER REMOVAL OF PAINT 3EA DENTS WERE IDENTIFIED WHERE YELLOW DOT WAS LOCATED. 2EA DENTS WERE WITHIN LIMITS OF CRJ 700 SRM 53-00-01-101-001-A01. THE THIRD D
- [SDR SWIA2025120101102](https://openairdocs.org/sdr/SWIA2025120101102.md): Attach Angle · corroded · Nov 2, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON ATTACH FLANGE OF STR22L FS280-FS333 (C-CHECK RO 11/30/2025)REPLACED STRINGER FROM STR22L FS280-FS333 REF. DWG#SH670-31630 REV K, CRJ700 SRM 51-42-06-001-001-A01; 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOO
- [SDR SWIA20251201016](https://openairdocs.org/sdr/SWIA20251201016.md): Plate · damaged · Oct 16, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Structure
  > COMPLY WITH REO 670-53-22-099, SPLICE REPAIR TO MTG PLATE BETWEEN BS 319 - 333, RT. COMPLIED WITH SPLICE REPAIR TO MTG PLATE BETWEEN IAW REO 670-53-22-099 REV-. ALL CHECKED GOOD.
- [SDR SWI2025F01677](https://openairdocs.org/sdr/SWI2025F01677.md): Crossbeam · damaged · Oct 13, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CROSSBEAM UPPER FLANGE EXFOLIATED AROUND FLOORBOARD ANCHOR NUT. FS333 APPROX. RBL 18 (C-CHECK RO 11/30/2025)REPAIRED CROSSBEAM UPPER FLANGE FS333.00 APPROX RBL18 REF. REO 670-53-21-2729, REV: --, DATED 2025-11-07. COMPLIED WITH ALL THE STEPS OF TASK CARD 51
- [SDR SWIA202512010013](https://openairdocs.org/sdr/SWIA202512010013.md): Bulkhead · corroded · Oct 13, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > EXFOLIATED CORROSION FOUND AROUND FASTENER ON 202 BULKHEAD, FS235, AFT FACE LH SIDE. (C-CHECK RO 11/30/2025)REPAIRED 202 BULKHEAD AT FS235 AFT FACE LH SIDE REF-CRJ-700 REO 670-53-11-2196 REV -- DATE 2025-10-17 AND REO 670-53-11-2197 REV -- DATE 2025-10-15, LE
- [SDR SWIA2025120100011](https://openairdocs.org/sdr/SWIA2025120100011.md): Stringer Splice · corroded · Oct 11, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE 25R, BS 333 CORRODED. REPLACED STRINGER SPLICE IAW DWG SH670-32420, REV E, & SRM 51-42-06-001-001-A01. CHECKED GOOD.
- [SDR SWIA2025120119](https://openairdocs.org/sdr/SWIA2025120119.md): Frame · corroded · Oct 9, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ALONG FRAME FS319.70, STGR 18L TO 21L ON WEB AND ATTACH FLANGE. (C-CHECK RO 11/30/2025)REPLACED FRAME SECTOR AT FS319, STGR 18L - 21L REF DWG: SH670-31810 REV AE, CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WI
- [SDR SWI2025F01669](https://openairdocs.org/sdr/SWI2025F01669.md): Web · corroded · Oct 8, 2025 · N606SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPPER SURFACE OF BACKUP SILL WEB CORRODED STR 21L FS310.00 TO FS333.00 (C-CHECK RO 11/30/2025)REPLACED UPPER SURFACE OF BACKUP SILL WEB AT STR 21L FS310.00 TO FS 333.00 REF. DWG# SH670-31810 REV AE AND CRJ700 SRM 51-42-06-001-001-A01. C/W 51-900-1002-SKY
- [SDR SWIA202512011008](https://openairdocs.org/sdr/SWIA202512011008.md): Stringer · damaged · Oct 8, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > ELONGATED HOLES FOUND ON VERTICAL FLANGE OF STRINGER 21L FWD OF FS333.00 (C-CHECK RO 11/30/2025)REPAIRED VERTICAL FLANGE STGR21L BETWEEN FS295-FS333 REF-CRJ-700 DWG SH670-32420 REV E, SRM 51-42-06-001-001 A01 AND REO 670-53-21-2720 REV -- DATE 2025-11-10,
- [SDR SWIA202512011002](https://openairdocs.org/sdr/SWIA202512011002.md): Hinge · chafed · Oct 2, 2025 · N606SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > AFTER REMOVAL OF THE PAX DOOR NOTED THE PAX DOOR HINGE (PAX DOOR SIDE) TO HAVE CHAFES ON ALL LUG LANDINGS (C-CHECK RO 11/30/2025)PERFORMED PASSENGER DOOR HINGE (PAX DOOR SIDE) REPAIR PER CRJ700 SRM 52-11-01-201-007-A01 STEP 5.D. TYPE IV, ALL STEPS COMPLIED W
- [SDR SWIA202512010001](https://openairdocs.org/sdr/SWIA202512010001.md): Hinge · chafed · Oct 1, 2025 · N606SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > AFTER REMOVAL OF THE PAX DOOR NOTED THE PAX DOOR HINGE TO HAVE CHAFES ON ALL LUG LANDINGS. REMOVED DAMAGE AT PAX DOOR HINGE ON ALL LUG LANDINGS IAW SRM 51-12-00-001-001-A01, AND FOUND TO BE WITHIN LIMITS PER SRM 53-21-23-201-010-A01.
- [SDR SWI2025F01697](https://openairdocs.org/sdr/SWI2025F01697.md): Stringer Splice · damaged · Sep 30, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > ELONGATED HOLES FOUND ON STRINGER SPLICE 21L. REPLACED THE STRINGER SPLICE 21L, FS333 IAW DWG SH670-32420, REV E, AND SRM 51-42-06-001-001-A01.
- [SDR SWIA2025120100930](https://openairdocs.org/sdr/SWIA2025120100930.md): Floor Support · corroded · Sep 30, 2025 · N606SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF SEAT TRACK FOUND CORROSION ON FLOOR SUPPORT LBL9, FS549. REPAIRED THE FLOOR SUPPORT BS 533 - 581 IAW SRM 53-00-41-201-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG: SH670-33415 REV E.
- [SDR SWIA20251201929](https://openairdocs.org/sdr/SWIA20251201929.md): Frame · damaged · Sep 29, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Frame
  > REMOVE AND PERFORM SRM FRAME SPLICE REPAIR ON FRAME FS333 TO FOM (C-CHECK RO 11/30/2025)REMOVED AND INSTALLED NEW FRAME SECTOR AT FS333 FROM STGR21L TO STGR25L REF-CRJ-700 DWG SH670-32420 REV E, SRM 51-42-06-001-001 A01 AND SRM 53-00-06-201-006 A01, LEAK CHE
- [SDR SWIA2025120100927](https://openairdocs.org/sdr/SWIA2025120100927.md): Hinge · gouged · Sep 27, 2025 · N606SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > THE PAX DOOR PIANO HINGE ON THE DOOR SIDE LUGS 1,2,3,5,9,21,22,23,24,25,26, AND 27 ARE GOUGED AND CHAFED. (C-CHECK RO 11/30/2025) GOUGING AND CHAFING ON THE PAX DOOR PIANO HINGE ON THE DOOR SIDE LUGS,2,3,5,9,21,22,23,24,25,26, AND 27 REMOVED. REF SRM 51-12-
- [SDR SWIA202512010925](https://openairdocs.org/sdr/SWIA202512010925.md): Stringer · corroded · Sep 25, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R, BS 280 - 333 HAS CORROSION ON ATTACH FLANGE. REPLACED S25R, BS 280 - 333 IAW DWG SH670-31630, REV K. AND SRM 51-42-06-001-001-A01; SRM 51-42-21-001-001-A01. LEAK CHECKED GOOD.
- [SDR SWI2025F01676](https://openairdocs.org/sdr/SWI2025F01676.md): Floorbeam · corroded · Sep 24, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS1051.30 BETWEEN RBL27.00 AND RT OTBD FLOOR SILL HAS CORROSION ON TOP EDGE. REMOVED CORROSION FROM FLOOR CROSS BEAM AT FS1051.30 BETWEEN RBL27 AND RT OTBD FLOOR SILL ON TOP EDGE, IAW SRM 51-21-06-001-001-A01, FLOORBEAM WAS OUT OF LIMITS IAW 53-61
- [SDR SWIA2025120100924](https://openairdocs.org/sdr/SWIA2025120100924.md): Floor Support · corroded · Sep 24, 2025 · N606SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR BEAM LBL27.00 BETWEEN APPROXIMATELY FS977.00 AND FS1088.20 HAS CORROSION AND SCRATCHES IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 11/30/2025)REPAIRED FLOOR BEAM LBL27.00 BETWEEN APPROXIMATELY FS977.00 AND FS1088.20 REF CRJ700 SRM 51-42-06-001-001-A01
- [SDR SWI2025F01668](https://openairdocs.org/sdr/SWI2025F01668.md): Floorbeam · cracked · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT SHEAR BOX LBL9, FS280.00 OUTBOARD ATTACHING ANGLE IS CRACKED IN RADIUS FROM THE TOP TO BOTTOM. REMOVED & INSTALLED NEW FLOOR SUPPORT SHEAR BOX LBL9 FS280 OUTBOARD ATTACHING ANGLE IAW SRM 51-42-21-001-001-A01, & DWG CC670-34010, REV -K. COMPLIED
- [SDR SWI2025F01667](https://openairdocs.org/sdr/SWI2025F01667.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-3 INTERNAL FACE BOTH SIDES OF SECTOR GEAR WITH ROLLER MARKS. BLENDED REPAIR AS REQUIRED PER REO 670-57-42-2268 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01666](https://openairdocs.org/sdr/SWI2025F01666.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 2-3 INTERNAL FACE BOTH SIDES OF SECTOR GEAR WITH ROLLER MARKS. BLENDED REPAIR AS REQUIRED PER REO 670-57-42-2249 REV -- DATED 2025-10-07. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01665](https://openairdocs.org/sdr/SWI2025F01665.md): Slat Track · corroded · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 2-3 EXTERNAL FWD FACE WITH SUSPECT OF SURFACE CORROSION. BLENDED REPAIR AS REQUIRED LH SLAT TRACK 2-3 PER REO 670-57-42-2249 REV -- DATED 2025-10-07. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01664](https://openairdocs.org/sdr/SWI2025F01664.md): Slat Track · corroded · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 2-2 INTERNAL FACE WITH SUSPECT OF SURFACE CORROSION (TWO SPOTS). BLENDED REPAIR AS REQUIRED LH SLAT TRACK 2-2 PER REO 670-57-42-2248 REV A DATED 2025-11-21. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01663](https://openairdocs.org/sdr/SWI2025F01663.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 1-1 INTERNAL FACE BOTH SIDES OF SECTOR GEAR WITH ROLLER MARKS. BLENDED REPAIR AS REQUIRED LH SLAT TRACK 1-1 PER REO 670-57-42-2245 REV -- DATED 2025-10-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01662](https://openairdocs.org/sdr/SWI2025F01662.md): Housing · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Galley Doors
  > GALLEY SERVICE DOOR EXTERNAL DOOR HANDLE HOUSING UPPER FORWARD EDGE HAS DAMAGE FROM THE OUTER HANDLE CHAFING. MARKED IN RED (C-CHECK RO 11/30/2025)REPLACED THE SERVICE DOOR HANDLE HOUSING AND HANDLE ASSY REF CRJ-700 CRJ-700 SRM 51-42-06-001-001-A01 AND DWG: C
- [SDR SWI2025F01661](https://openairdocs.org/sdr/SWI2025F01661.md): Slat Track · worn · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-3 EXTERNAL FWD FACE WITH BARE METAL EXPOSED (AS MARKED) (C-CHECK RO 11/30/2025)BLENDED REPAIR AS REQUIRED PER REO 670-57-42-2268 REV -- DATED 2025-10-30. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01660](https://openairdocs.org/sdr/SWI2025F01660.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-2 INTERNAL FACE WITH ROLLER MARKS (AS MARKED) (C-CHECK RO 11/30/2025)BLENDED REPAIR AS REQUIRED PER REO 670-57-42-2250 REV -- DATED 2025-10-07. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01659](https://openairdocs.org/sdr/SWI2025F01659.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 1-3 INTERNAL FACE BOTH SIDES OF SECTOR GEAR WITH ROLLER MARKS (AS MARKED) (C-CHECK RO 11/30/2025)BLENDED REPAIR AS REQUIRED PER REO 670-57-42-2246 REV -- DATED 2025-10-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS T
- [SDR SWI2025F01658](https://openairdocs.org/sdr/SWI2025F01658.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-1 EXTERNAL FWD FACE WITH SUSPECT OF SURFACE CORROSION (AS MARKED) (C-CHECK RO 11/30/2025)BLENDED REPAIR AS REQUIRED PER REO 670-57-42-2251 REV -- DATED 2025-10-10. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01657](https://openairdocs.org/sdr/SWI2025F01657.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-1 INTERNAL FACE BOTH SIDES OF SECTOR GEAR WITH ROLLER MARKS (AS MARKED) (C-CHECK RO 11/30/2025)BLENDED REPAIR AS REQUIRED LH SLAT TRACK 3-1 PER REO 670-57-42-2251 REV -- DATED 2025-10-10. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CH
- [SDR SWI2025F01656](https://openairdocs.org/sdr/SWI2025F01656.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 2-1 INTERNAL FACE BOTH SIDES OF SECTOR GEAR WITH ROLLER MARKS (AS MARKED) (C-CHECK RO 11/30/2025)BLENDED REPAIR AS REQUIRED PER REO 670-57-42-2244 REV -- DATED 2025-10-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TI
- [SDR SWI2025F01655](https://openairdocs.org/sdr/SWI2025F01655.md): Slat Track · corroded · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > LEFT WING SLAT TRACK 3-2 EXTERNAL AND INTERNAL FWD & AFT FACE WITH SUSPECT OF SURFACE CORROSION (AS MARKED) (C-CHECK RO 11/30/2025)BLENDED REPAIR AS REQUIRED LH SLAT TRACK 3-2 PER REO 670-57-42-2250 REV -- DATED 2025-10-07. COMPLIED WITH TASK CARD 51-900-100
- [SDR SWIA202512010923](https://openairdocs.org/sdr/SWIA202512010923.md): Slat Track · damaged · Sep 23, 2025 · N606SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 2-2 INTERNAL FACE WITH ROLLER MARK. BLENDED REPAIR AS REQUIRED LH SLAT TRACK 2-2 PER REO 670-57-42-2248 REV -- DATED 2025-10-08. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPS CHECK GOOD AT THIS TIME.
- [SDR SWI2025F01675](https://openairdocs.org/sdr/SWI2025F01675.md): Floorbeam · corroded · Sep 22, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR SUPPORT ANGLE ON THE FORWARD SIDE OF THE FS280 BEAM BL9L - BL9R IS CORRODED. (C-CHECK RO 11/30/2025)REMOVED AND REPLACED COCKPIT FLOOR SUPPORT ANGLE REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-42-13-00
- [SDR SWI2025F01674](https://openairdocs.org/sdr/SWI2025F01674.md): Intercostal · corroded · Sep 22, 2025 · N606SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 21LH BETWEEN FS333.00 AND FS349.00 HAS CORROSION ON UPPER WEB. (MARKED) (C-CHECK RO 11/30/2025)REPLACED INTERCOSTAL AT STGR 21 LH BETWEEN FS333.00 AND FS349.00 REF. DWG# SH670-31810 REV AE AND CRJ700 SRM 51-42-06-001-001-A01. C/W 51-900-
- [SDR SWI2025F01673](https://openairdocs.org/sdr/SWI2025F01673.md): Stringer · corroded · Sep 22, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER STGR 23RH HAS CORROSION ON ATTACH FLANGE BETWEEN FS333.00 AND FS349.00. (MARKED) (C-CHECK RO 11/30/2025)REPLACED STGR 23RH BETWEEN FS333.00 AND FS349.00 REF DWG# SH670-31350 REV-A AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-
- [SDR SWIA202512010922](https://openairdocs.org/sdr/SWIA202512010922.md): Stringer · corroded · Sep 22, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER STGR 22LH HAS CORROSION IN MULTIPLE SPOTS ON UPPER ATTACH FLANGE BETWEEN FS333.00 AND FS364.00. (MARKED) (C-CHECK RO 11/30/2025)REPAIRED STRINGER STGR 22LH FROM FS333.00 AND FS394.00. REF CRJ700 SRM 53-00-03-201-001-A01. COMPLIED WITH ALL STEPS OF 5
- [SDR SWI2025F01672](https://openairdocs.org/sdr/SWI2025F01672.md): Frame · corroded · Sep 21, 2025 · N606SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FS349.00 FRAME FORWARD WEB OUTBOARD OF STGR26R. REPAIRED FS 349 FRAME BETWEEN STR26R TO STR25R. REF CRJ 700 SRM 53-00-06-201-004-A01, SRM 51-42-06-001-001 A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-10002-SKY. SEE CONTINUATION CARD FOR DETA
- [SDR SWI2025F01671](https://openairdocs.org/sdr/SWI2025F01671.md): Striker · corroded · Sep 21, 2025 · N606SK · Cndair CL6002C10 · Galley Doors
  > SERVICE DOOR SURROUND LOWER SEAL STRIKER HAS CORROSION AROUND MULTIPLE FASTENER HOLES. (C-CHECK RO 11/30/2025)REPLACED GALLEY SERVICE DOOR LOWER SEAL STRIKER REF DWG: SH670-31950 REV Y, CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-S
- [SDR SWI2025F01670](https://openairdocs.org/sdr/SWI2025F01670.md): Support Angle · corroded · Sep 21, 2025 · N606SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SURROUND HAS CORROSION ON 3EA STEP PLATE SUPPORT ANGLES. (MARKED) (C-CHECK RO 11/30/2025)REMOVED & REPLACED 03 EA. STEP PLATE SUPPORT ANGLES PN: SH670-31982-1 AT SERVICE DOOR SURROUND REF CRJ700 SRM 51-42-06-001-001-A01.COMPLIED WITH 51-900-1002
- [SDR SWIA202512010921](https://openairdocs.org/sdr/SWIA202512010921.md): Angle · corroded · Sep 21, 2025 · N606SK · Cndair CL6002C10 · Galley Doors
  > GALLEY SERVICE DOOR SURROUND HAS CORROSION ON THE KICK ANGLE. (MARKED) (C-CHECK RO 11/30/2025)REPLACED GALLEY SERVICE DOOR LOWER KICK ANGLE AND MOUNTING ANGLE REF DWG SH670-31950 REV Y, CRJ700 SRM 51-42-06-001-001-A01, REV 38, JUL 25/2020, CRJ-700 SRM 51-42-
- [SDR SWI2025F01678](https://openairdocs.org/sdr/SWI2025F01678.md): Transcowl · chafed · Sep 17, 2025 · N606SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT UPPER TRANSCOWL INBD SLIDER IS CHAFED/GOUGED (C-CHECK RO 11/30/2025)COMPLIED WITH REPAIR OF THE LH ENGINE UPPER TRANSCOWL INBD SLIDER REF CRJ 700 REO 670-54-21-1767, REV. --, 2025-09-26. CLEARANCE AND GAP CHECKS ARE GOOD. COMPLIED WITH SKYWEST TASK CARD
- [SDR SWIA2025120100917](https://openairdocs.org/sdr/SWIA2025120100917.md): Transcowl · punctured · Sep 17, 2025 · N606SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT UPPER TRANSCOWL INNER PERFORATED SKIN IS PUNCTURED (C-CHECK RO 11/30/2025)REPAIRED INNER PERFORATE SKIN ON L/H UPPER TRANSCOWL, REF. REO 670-54-21-1767, REV. --, 2025-09-26. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-SKY. JOB HN00267022, CAMP 30858321
- [SDR SWIA2025120100903](https://openairdocs.org/sdr/SWIA2025120100903.md): Skin · dented · Sep 3, 2025 · N606SK · Cndair CL6002C10 · Trailing Edge Flaps
  > ADM# N606SK-8233. LEFT INBOARD FLAP AT FS 27 NEAR THE TRAILING EDGE. DENT ON LOWER SKIN MEASURES WIDTH 1/4 IN. X DEPTH.035". SRM 57-53-01. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES
- [SDR SWIA20231116](https://openairdocs.org/sdr/SWIA20231116.md): Unknown · warning message · Nov 16, 2023 · N606SK · Cndair CL6002C10 · Airfoil Anti/De-ice System
  > ANTI-DUCT WARNING MESSAGE AT FL250 WHILE IN ICING CONDITIONS. OAT -26° AT THE TIME WITH LIGHT TO MODERATE RIME ICING. EXITING ICING CONDITIONS, RAN QRH AND DIVERTED TO OKC. (FLIGHT 3295)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27437244 WITH THE FOLLOWING
- [SDR SWIA2023070503](https://openairdocs.org/sdr/SWIA2023070503.md): Unknown · warning message · Jul 3, 2023 · N606SK · Cndair CL6002C10 · Pneumatic System
  > DURING INITIAL CLIMB OUT OF KPHX AFTER REDUCING POWER TO CLIMB THRUST, RECEIVED A R BLEED DUCT WARNING MESSAGE. AFTER ABOUT 30 SECONDS MESSAGE CHANGED TO R BLEED DUCT CAUTION MESSAGE. RAN QRH, THEN RETURNED TO DEPARTURE AIRPORT. (FLT 4954 FILED CLOSED)INTEROGA
- [SDR SWIA2023061412](https://openairdocs.org/sdr/SWIA2023061412.md): Windshield · cracked · Jun 12, 2023 · N606SK · Cndair CL6002C10 · Flight Compartment Windows
  > TRANSFER FROM EAML 1154630: RECEIVED R WSHLD HEAT CAUTION MESSAGE AT FL280. SIMULTANEOUSLY NOTICED APPROXIMATE 2 FT DELAMINATION. RAN QRH. WINDSHIELD THEN CRACKED AT APPROXIMATELY 10,000 FEET. (FLT 4997 FILED CLOSED)REMOVED AND REPLACED R/H WINDSHIELD IN REFE
- [SDR SWIA2023052200001](https://openairdocs.org/sdr/SWIA2023052200001.md): Landing · damaged · May 15, 2023 · N606SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > RH UPPER ELECTRIC ACCESS DOOR SURROUND STRUCTURE FS173.00 TO FS193.00 DOOR LANDING DAMAGED. REMOVED AND REPLACED RH TRU DOOR LAND PN CC670-33151-6 WITH NEW IAW SRM 51-42-06-001-001, DWG CC670-33040, AND REO 670-53-11-1855 REV A DATED 2023-05-16. COMPLIED WITH
- [SDR SWIA202305160015](https://openairdocs.org/sdr/SWIA202305160015.md): Angle · damaged · May 15, 2023 · N606SK · Cndair CL6002C10 · Doors
  > RH UPPER ELECTRIC ACCESS DOOR SURROUND STRUCTURE FS173.00, FWD UPPER ZEE DAMAGED. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Next page: https://openairdocs.org/aircraft/N606SK/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 = 'N606SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N606SK/reports

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