# Service difficulty reports: N609SK

A list on [N609SK](https://openairdocs.org/aircraft/N609SK.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 8 · 373 reports

- [SDR SWIA2026080776754](https://openairdocs.org/sdr/SWIA2026080776754.md): Window · cracked · Aug 7, 2026 · N609SK · Cndair CL6002C10 · Flight Compartment Windows
  > FO SIDE WINDOW CRACKED INFLIGHT IN TWO PLACES. ONE IS AN ARC AND THE OTHER IS VERTICAL (FLIGHT 6234) TRANSFERRED TO CAMP ITEM 32787656. R & R FO SIDE WINDOW IAW AMM 56-12-01.
- [SDR SWIA2026052976109](https://openairdocs.org/sdr/SWIA2026052976109.md): Skin · scratched · May 29, 2026 · N609SK · Cndair CL6002C10 · Leading Edge Devices
  > FOUND SCRATCH ON LE SLAT 3 MEASURING 1.2"L X 0.100"W X 0.013"D. COMPLIED WITH REO 670-57-42-2512 DATED: 2026-05-29 REV: -- DISPOSITION FOR BLENDED SCRATCH DAMAGES TO OUTER SKIN OF LH SLAT #3 BETWEEN TRACK 3-3 & SS446.38. BLENDED THE SCRATCH/GOUGE DAMAGE TO A
- [SDR SWIA2026052976108](https://openairdocs.org/sdr/SWIA2026052976108.md): Skin · gouged · May 29, 2026 · N609SK · Cndair CL6002C10 · Leading Edge Devices
  > FOUND GOUGE ON LE SLAT 3 MEASURING 1.6"L X.150"W X.025"D. BLENDED SCRATCH DAMAGES TO OUTER SKIN OF LH SLAT NR 3 BETWEEN TRACK 3-3 & SS446.38. BLENDED THE SCRATCH/GOUGE DAMAGE TO A SMOOTH TRANSITION ON THE LH #3 SLAT SKIN LEADING EDGE FROM SLAT STATION NEAR
- [SDR SWIA2026022705384](https://openairdocs.org/sdr/SWIA2026022705384.md): Stringer · fom · Feb 3, 2026 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REMOVED STRINGER 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) TO FOM. (C-CHECK RO 02/25/2026)INSTALLED STR 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337. REFERENCE CP# 316
- [SDR SWIA202602275365](https://openairdocs.org/sdr/SWIA202602275365.md): Frame · damaged · Feb 3, 2026 · N609SK · Cndair CL6002C10 · Fuselage Main, Frame
  > REMOVED SUB-FRAME, FS 317 REFERENCE SRM 53-21-23 ITEM 34. INSTALLED SUB-FRAME BS 317 IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR SWIA2026020375360](https://openairdocs.org/sdr/SWIA2026020375360.md): Fitting · fom · Feb 3, 2026 · N609SK · Cndair CL6002C10 · Passenger/Crew Doors
  > REMOVED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 TO FOM. INSTALLED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026013075371](https://openairdocs.org/sdr/SWIA2026013075371.md): Lintel · corroded · Jan 30, 2026 · N609SK · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN BS 333 - 343.13, STR 3L UNDERNEATH AFT SPIGOT. COMPLIED WITH REO 670-53-21-2805, REV -. REPAIR FOR CORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN FS333.00 - FS343.13 AT STR3L (UNDERNEATH AFT SPIGOT).
- [SDR SWIA2026022705387](https://openairdocs.org/sdr/SWIA2026022705387.md): Frame · damaged · Jan 29, 2026 · N609SK · Cndair CL6002C10 · Fuselage Main, Frame
  > REMOVED SUB-FRAME BS 317 REFERENCE SRM 53-21-23 ITEM 34. INSTALLED SUB-FRAME BS 317 WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202602275377](https://openairdocs.org/sdr/SWIA202602275377.md): Stringer · fom · Jan 29, 2026 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REMOVED STRINGER 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) TO FOM. INSTALLED STR 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026012975361](https://openairdocs.org/sdr/SWIA2026012975361.md): Fitting · fom · Jan 29, 2026 · N609SK · Cndair CL6002C10 · Passenger/Crew Doors
  > REMOVED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 TO FOM. INSTALLED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026012975105](https://openairdocs.org/sdr/SWIA2026012975105.md): Lintel · corroded · Jan 29, 2026 · N609SK · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN FS315.95 - FS323.43 AT STR 3L (UNDERNEATH FWD SPIGOT. (C-CHECK RO 02/25/2026)REPAIRED CORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN FS315.95 - FS323.43 AT STR 3L (UNDERNEATH FWD SPIGOT). COMPLIED WITH REO
- [SDR SWIA202602274765](https://openairdocs.org/sdr/SWIA202602274765.md): Floor Support · corroded · Dec 18, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > COMPLY WITH REO 670-53-11-745 DATED: 2016-10-28 REV: A GENERIC REPAIR FOR NOSE FUSELAGE CENTER FLOOR ANGLE REPLACEMENT AND DOOR POST AT FS 28.00 ( LBL 11.128 AND RBL 11.128) DUE TO CORROSION FOUND ON THE DOOR POST. (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670
- [SDR SWI2025F01831](https://openairdocs.org/sdr/SWI2025F01831.md): Angle · corroded · Dec 18, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > COMPLY WITH REO 670-53-11-745 DATED: 2016-10-28 REV: A GENERIC REPAIR FOR NOSE FUSELAGE CENTER FLOOR ANGLE REPLACEMENT AND DOOR POST AT FS 28.00 ( LBL 11.128 AND RBL 11.128) DUE TO CORROSION FOUND ON THE DOOR POST. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROG
- [SDR SWIA2026022705383](https://openairdocs.org/sdr/SWIA2026022705383.md): Floor Support · corroded · Nov 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR BEAM AT WL 73.00 AND RBL 9.00 FROM FS 565.00 - FS 581.00 (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670-53-31-1142 DATED: 2025-12-16 REV"A" DISPOSITION FOR ELONGATED HOLES AND LOW E.D. CONDITION ON RBL9.0 FLOOR BEAM AND REPAIR SPLICE B
- [SDR SWIA202602274474](https://openairdocs.org/sdr/SWIA202602274474.md): Buttstrap · corroded · Nov 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON BUTTSTRAP AT FS280.00 BTW STR 25R - STR 23R (C-CHECK RO 02/25/2026)CHAFFING UNDER FUSELAGE SKIN ON STRG 27, FS 977.00 TO 989.00 BLEND-OU AND FOUND WITHIN LIMITS IAW MHICRJ700 SRM 53-00-01-101-001-A01, L:3" W:2" D:0.016",SURFACE REPROTECTED IA
- [SDR SWIA202512011126](https://openairdocs.org/sdr/SWIA202512011126.md): Buttstrap · corroded · Nov 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON BUTTSTRAP AT FS280.00 BTW STR 25R - STR 23R (FILED CLOSED)CHAFFING UNDER FUSELAGE SKIN ON STRG 27, FS 977.00 TO 989.00 BLEND-OU AND FOUND WITHIN LIMITS IAW MHICRJ700 SRM 53-00-01-101-001-A01, L:3" W:2" D:0.016",SURFACE REPROTECTED IAW SRM CRJ
- [SDR SWIA2025112800006](https://openairdocs.org/sdr/SWIA2025112800006.md): Buttstrap · corroded · Nov 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON BUTTSTRAP AT FS280.00 BTW STR 25R - STR 23R (FILED OPEN)
- [SDR SWIA2025110675378](https://openairdocs.org/sdr/SWIA2025110675378.md): Bracket · damaged · Nov 6, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD FACE RH FS 280.00 BULKHEAD BRACKET ASSY, FIRE EXT HAS ELONGATED SCREW HOLES AND REQUIRES REPLACEMENT. REMOVED AND REPLACED THE FWD FACE RH FS 280 BULKHEAD BRACKET ASSY, FIRE EXT IAW SRM 51-42-06.
- [SDR SWIA202602275372](https://openairdocs.org/sdr/SWIA202602275372.md): Skin · corroded · Oct 31, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON INNER FUSELAGE BELLY SKIN 2 INCHES FWD OF BS 265 RIGHT NEXT TO STR 27. COMPLIED REO 670-53-11-2208, REV-. DISPOSITION FOR BLENDED CORROSION DAMAGE TO FUSELAGE SKIN PANEL NEAR BS 265 BTWN STR 26R-STR27. PERFORMED EDDY CURRENT INSPECTION WI
- [SDR SWIA202602275375](https://openairdocs.org/sdr/SWIA202602275375.md): Bracket · cracked · Oct 30, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BS 280 STICK PUSHER BRACKET CRACKED. REMOVED AND REPLACED THE RT FWD BS 280 STICK PUSHER BRACKET IAW SRM 51-42-06.
- [SDR SWIA2020227675364](https://openairdocs.org/sdr/SWIA2020227675364.md): Stringer · corroded · Oct 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 27 CORRODED BETWEEN FS 250.00 & FS 265. COMPLIED WITH REO 670-53-11-2202, REV -. REPAIRED BS 250 LOWER FRAME SECTOR BETWEEN STRINGER 27 - 25R AND STRINGER SPLICE 27. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026022705379](https://openairdocs.org/sdr/SWIA2026022705379.md): Frame · corroded · Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 250, STR 26L - STR 26R AFT FACE OF FRAME AND SKIN FLANGE CORRODED. COMPLIED WITH REO 670-53-11-2202 DATED:2025-12-16 REV: -- REPAIR TO FS250.00 LOWER FRAME SECTOR BETWEEN STR27 - STR25R AND STRINGER STR27 SPLICE.
- [SDR SWIA202602275374](https://openairdocs.org/sdr/SWIA202602275374.md): Floorbeam · corroded · Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280 RT CAP ANGLE REF SRM 53-11-10, ITEM 121, CORRODED AND DISTORTED. REMOVED AND REPLACED THE BS 280 RT CAP ANGLE. WORK DONE IAW SRM 51-42-06, SRM 51-42-21, SRM 53-11-10, GREO 670-53-11-594, REV A, AND REO 670-53-11-2182, REV--.
- [SDR SWIA202510275362](https://openairdocs.org/sdr/SWIA202510275362.md): Floorbeam · corroded · Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRAWLWAY FLOOR ANGLE SUPPORT AT FS280.00 IN AVIONICS BAY CORRODED. REMOVED AND REPLACED CRAWLWAY FLOOR SUPPORT AT FS280.00 IN AVIONICS BAY WITH REFERENCE TO SRM 51-42-06, SRM 51-42-13 AND SRM 51-42-21.
- [SDR SWIA20202274125](https://openairdocs.org/sdr/SWIA20202274125.md): Floorbeam · corroded · Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280.00 RH FLOOR BEAM CORRODED (REF SRM 53-11-10 ITEM 119). (C-CHECK RO 02/25/2026)REMOVED AND REPLACED THE FS280.00 RH FLOOR BEAM. WORK DONE IN REFERENCE WITH THE CRJ-700 SRM 51-42-06, SRM 51-42-21, SRM 53-11-10 AND GREO 670-53-11-594 DATED: 2015/06/26 REV
- [SDR SWIA202602274124](https://openairdocs.org/sdr/SWIA202602274124.md): Floorbeam · corroded · Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280.00 LH FLOOR BEAM CORRODED (REF SRM 53-11-10 ITEM 118). (C-CHECK RO 02/25/2026)REMOVED AND REPLACED THE FS280.00 LH FLOOR BEAM. WORK DONE IN REFERENCE WITH THE CRJ-700 SRM 51-42-06, SRM 51-42-21, SRM 53-11-10 AND GREO 670-53-11-594 DATED: 2015/06/26 REV
- [SDR SWI2025F01456](https://openairdocs.org/sdr/SWI2025F01456.md): Floorbeam · corroded · Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280.00 RH FLOOR BEAM CORRODED (REF SRM 53-11-10 ITEM 119). OPEN)
- [SDR SWIA2025102400023](https://openairdocs.org/sdr/SWIA2025102400023.md): Floorbeam · corroded · Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280.00 LEFT FLOORBEAM CORRODED (REF SRM 53-11-10 ITEM 118). OPEN
- [SDR SWIA2026022705382](https://openairdocs.org/sdr/SWIA2026022705382.md): Floorbeam · cracked · Oct 16, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LEFT COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR BS 280 & LBL 11.128 AND AT WL 72.10 IS CRACKED. REMOVED AND REPLACED THE LT COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR BS 280 & LBL 11.128 AND AT WL 72.10 IAW SRM 51-42-06.
- [SDR SWIA2025101675370](https://openairdocs.org/sdr/SWIA2025101675370.md): Floorbeam · cracked · Oct 16, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RIGHT COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR FS 280.00 & RBL 11.128 AND AT WL 72.10 IS CRACKED. REMOVED AND REPLACED THE RH COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR FS 280.00 & RBL 11.128 AND AT WL 72.10 IN REFERENCE WITH THE SRM 51-42-06.
- [SDR SWIA2025101475368](https://openairdocs.org/sdr/SWIA2025101475368.md): Floorbeam · cracked · Oct 14, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 280 AND RBL 12 CRACKED ON THE AFT OUTBOARD FLANGE FROM APPROX WL 70.00 - WL 72.50. COMPLIED WITH REO 670-53-11-896 REV-. GENERIC REPAIR TO CENTER COCKPIT FLOORBEAM BS 280, WL70 - 72.50. AND REO 670-53-11-2195 REV -. REPAIR TO CENTER COCKPI
- [SDR SWIA2026227873969](https://openairdocs.org/sdr/SWIA2026227873969.md): Stringer · corroded · Sep 28, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21L IS CORRODED BETWEEN FS437.00 & FS453.00. (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670-53-21-2698 DATED: 2025-10-07 REV: A, REPAIR FOR CORROSION DAMAGE TO STRINGER STR21L BETWEEN FS 437.00 - FS 453.00. COMPLIED WITH TASK CARD 51-900-1002-SKY. CO
- [SDR SWIA2025F01395](https://openairdocs.org/sdr/SWIA2025F01395.md): Stringer · corroded · Sep 28, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21L IS CORRODED BETWEEN FS437.00 & FS453.00. (FILED OPEN)
- [SDR SWIA2025092375386](https://openairdocs.org/sdr/SWIA2025092375386.md): Hinge Arm · gouged · Sep 23, 2025 · N609SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP. INBOARD HINGE ARM (WS178.00) HAS GOUGES ON EDGE OF HOUSING FOR SPHERICAL BEARING. REPAIRED DAMAGE ON LH OUTBOARD FLAP. INBOARD HINGE ARM (WS178.00) IN COMPLIANCE WITH REO 670-57-53-428 REV-- DATED 2025-09-26. PERFORMED EDDY CURRENT INSPECTI
- [SDR SWIA2025092375359](https://openairdocs.org/sdr/SWIA2025092375359.md): Floorbeam · corroded · Sep 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LEFT & RIGHT BS 280, COCKPIT FLOOR POST REINFORCEMENT PLATE/SKIN HAS CORROSION. COMPLIED WITH REO 670-53-11-2182 REV--. DISPOSITION FOR RE-INCORPORATION OF BULKHEAD LOWER WEB REPAIR AT FS280.00 (LHS AND RHS) PER SRM TASK 53-11-10-201-004-A01 (GREO 670-53-11-5
- [SDR SWIA202602275358](https://openairdocs.org/sdr/SWIA202602275358.md): Skin · chafed · Sep 22, 2025 · N609SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RH INBOARD FLAP LOWER SKIN HAS CHAFE DAMAGE AT INBOARD INTERFACE OF FAIRING. (C-CHECK RO 02/25/2026)REPAIRED RH INBOARD FLAP LOWER SKIN WITH REFERENCE TO SRM 57-52-01 AND REO 670-57-52-628 REV "--" DATED 2025-10-15. REPLACED RH INBOARD FLAP LOWER SKIN WITH
- [SDR SWIA2025091875385](https://openairdocs.org/sdr/SWIA2025091875385.md): Hinge Fitting · gouged · Sep 18, 2025 · N609SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > LEFT WING #5 FLAP HINGE BOX AFT IB ATTACHMENT FITTING LUG IS GOUGED. BLENDED GOUGE ON LT WING NR 5 FLAP HINGE BOX AFT IB ATTACHMENT FITTING LUG IN REFERENCE TO SRM 51-12-00. PERFORMED EDDY CURRENT IN REFERENCE TO NDTM 51-20-006 AND FOUND REWORKED AREA TO BE C
- [SDR SWIA2025091675369](https://openairdocs.org/sdr/SWIA2025091675369.md): Floorbeam · corroded · Sep 16, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FWD CENTER FLOOR PANEL SUPPORT ANGLE AT FS280.00 HAS SURFACE CORROSION. REMOVED AND REPLACED THE FWD CENTER FLOOR PANEL SUPPORT ANGLE AT BS 280 IAW SRM 51-42-06, SRM 53-11-10 AND SRM 53-11-43.
- [SDR SWIA2025090375391](https://openairdocs.org/sdr/SWIA2025090375391.md): Roller · damaged · Sep 3, 2025 · N609SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK ROLLER 1-2 OUTBOARD AFT SIDE ROLLER HAS FLAT SPOTS. REPLACED RH 1-2 OUTBOARD AFT SIDE SLAT TRACK ROLLER AS PER AMM 27-81-44. SEE TASK CARD 27-630-101 IN CP 30270403-1 FOR OPS CHECK.
- [SDR SWIA2025090375390](https://openairdocs.org/sdr/SWIA2025090375390.md): Roller · worn · Sep 3, 2025 · N609SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-2 INBD AFT SIDE ROLLER IS WORN. REMOVED AND REPLACED RT SLAT TRACK 3-2, INBD AFT SIDE ROLLER IN REFERENCE TO AMM 27-81-44.
- [SDR SWIA2026022705389](https://openairdocs.org/sdr/SWIA2026022705389.md): Roller · damaged · Sep 3, 2025 · N609SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 INBOARD FORWAD SIDE ROLLER IS FLAT SPOTTED. REMOVED AND REPLACED LT SLAT TRACK 2-2 INBOARD FORWARD SIDE ROLLER IN REFERENCE TO AMM 27-81-44.
- [SDR SWIA2026022705388](https://openairdocs.org/sdr/SWIA2026022705388.md): Roller · damaged · Sep 3, 2025 · N609SK · Cndair CL6002C10 · Leading Edge Devices
  > L/H SLAT TRACK 1-2 INBOARD AFT SIDE ROLLER IS FLAT SPOTTED. (C-CHECK RO 02/25/2026)REMOVED AND REPLACED L/H SLAT TRACK 1-2 INBOARD AFT SIDE ROLLER, REFERENCE CP 30270403 FOR COMPLETION OF TASK CARD 27-520-120.
- [SDR SWIA2026022705380](https://openairdocs.org/sdr/SWIA2026022705380.md): Frame · damaged · Aug 28, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Frame
  > REMOVED FRAME SEGMENT 18-20L STGR FS 295.00 TO FACILITATE REPLACEMENT OF STGR 20L. INSTALLED FRAME SEGMENT BS 295, STGR 18L - STGR 20L IAW SRM 51-42-06, SRM 51-42-21 AND REO 670-53-21-2688 REV--. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM 53-0
- [SDR SWIA2026022775381](https://openairdocs.org/sdr/SWIA2026022775381.md): Stop Fitting · cracked · Aug 27, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR SURROUND FWD UPPER STOP BRACKET IS CRACKED. REMOVED AND REPLACED PAX DOOR SURROUND FWD UPPER STOP BRACKET WITH REFERENCE TO SRM 51-42-21.
- [SDR SWIA202602273555](https://openairdocs.org/sdr/SWIA202602273555.md): Door Frame · cracked · Aug 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Structure
  > AFT BAGGAGE BAY DOOR CUTOUT SURROUND STRUCTURE FS1047.00 LOWER CHANNEL CRACKED (SRM 53-61-58 ITEM 16). (C-CHECK RO 02/25/2026)REMOVED AND REPLACED AFT BAGGAGE BAY DOOR CUTOUT SURROUND STRUCTURE FS1407.00 LOWER CHANNEL (SRM 53-61-58 ITEM 16) WITH REFERENCE TO
- [SDR SWIA2025082700006](https://openairdocs.org/sdr/SWIA2025082700006.md): Channel · cracked · Aug 26, 2025 · N609SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE BAY DOOR CUTOUT SURROUND STRUCTURE FS1047.00 LOWER CHANNEL CRACKED (SRM 53-61-58 ITEM 16). (FILED OPEN)
- [SDR SWIA202602275357](https://openairdocs.org/sdr/SWIA202602275357.md): Skin · dented · Aug 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN BETWEEN FS349.00 AND FS 364.00 AND BETWEEN STGR 22L AND STGR 23L. (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670-53-21-2681 DATED: 2025-08-28 REV -- PERMANENT DISPOSITION FOR REWORKED DENTS ON LOWER FUSELAGE SKIN BETWEEN FS349.00 - FS409.
- [SDR SWIA2025082075376](https://openairdocs.org/sdr/SWIA2025082075376.md): Hinge Fitting · gouged · Aug 20, 2025 · N609SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR FUSELAGE SIDE HINGE AFT LUG LANDING HAS A SMALL GOUGE FROM HINGE PIN RETAINER PIN CONTACT/WEAR. PERFORMED REPAIR OF PAX DOOR FUSELAGE SIDE HINGE AFT LUG LANDING WITH REFERENCE TO REO 670-53-21-582 REV "-G" DATED 2024-02-18 TYPE IV: DISPOSITION FOR
- [SDR SWIA2025082075373](https://openairdocs.org/sdr/SWIA2025082075373.md): Doubler · gouged · Aug 20, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TWO SMALL SCREW GOUGES ON A DOUBLER AT STGR 27 BETWEEN BS 969 AND 985 ON THE EXTERIOR OF THE AIRCRAFT. COMPLIED WITH REO 670-53-61-352, REV A. REPAIRED THE FUSELAGE SKIN AT BS 977 AND STR 27 BY REMOVING AND REPLACING A NEW SERVICEABLE DOUBLER. MAJOR REPAIR.
- [SDR SWIA2025081375366](https://openairdocs.org/sdr/SWIA2025081375366.md): Mount · broken · Aug 13, 2025 · N609SK · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > GALLEY 1, MOST AFT INBD MOUNTING NUT PLATE IS BROKEN. UPON INSPECTION FOUND THE NUTPLATE BROKEN AND GALLEY 1, MOST AFT INBD MOUNTING FITTING ASSEMBLY TO BE CORRODED AND NEEDS TO BE REPLACED. REMOVED AND REPLACED THE GALLEY 1, MOST AFT INBD MOUNTING FITTING AS

Next page: https://openairdocs.org/aircraft/N609SK/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 = 'N609SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N609SK/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.