# Service difficulty reports: N613SK

A list on [N613SK](https://openairdocs.org/aircraft/N613SK.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 6 · 286 reports

- [SDR SWIA2026022175319](https://openairdocs.org/sdr/SWIA2026022175319.md): Screw · unsecure · Feb 21, 2026 · N613SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SCREW PROTRUDING FROM AFT CARGO SCUFF PLATE AT FORWARD UPPER CORNER ADJACENT TO CARGO DOOR EDGE. (C-CHECK RO 02/22/2026)COMPLIED WITH TEMP REPAIR REO 670-53-61-2683 REV-- DATED 2026-02-21 FOR CRACK TO INNER DOUBLER OF FUSELAGE SKIN BETWEEN FS1000.00 TO FS1015
- [SDR SWIA2026022575329](https://openairdocs.org/sdr/SWIA2026022575329.md): Skin · corroded · Feb 7, 2026 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND MINOR CORROSION AROUND 3 SCREW HOLES OF VHF-1 ANTENNA (C-CHECK RO 02/22/2026)REPAIRED CORROSION AROUND 3 SCREW HOLES VHF-1 ANTENNA WITH REFERENCE TO REO 670-53-21-2811 REV "--" DATED 2026-02-08 "DISPOSITION FOR BLENDED DAMAGE TO UPPER FUSELAGE SKIN PAN
- [SDR SWIA2026022575324](https://openairdocs.org/sdr/SWIA2026022575324.md): Skin · scratched · Feb 7, 2026 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > SURFACE SCRATCHES ON FUSALAGE SKIN UNDER UPPER VHF-1 ANTENNA (C-CHECK RO 02/22/2026)REPAIRED SURFACE SCRATCHES ON FUSELAGE SKIN UNDER UPPER VHF-1 ANTENNA WITH REFERENCE TO REO 670-53-21-2811 REV "--" DATED 2026-02-08 "DISPOSITION FOR BLENDED DAMAGE TO UPPER
- [SDR SWIA2026022575323](https://openairdocs.org/sdr/SWIA2026022575323.md): Skin · scratched · Feb 7, 2026 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > SURFACE SCRATCHES ON FUSALAGE SKIN UNDER LH ATC L-BAND ANTENNA (C-CHECK RO 02/22/2026)REPAIRED SURFACE SCRATCHES ON FUSELAGE SKIN UNDER LH ATC L-BAND ANTENNA WITH REFERENCE TO REO 670-53-21-2811 REV "--" DATED 2026-02-08 "DISPOSITION FOR BLENDED DAMAGE TO UP
- [SDR SWIA2026025775318](https://openairdocs.org/sdr/SWIA2026025775318.md): Skin · corroded · Feb 7, 2026 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND CORROSION AROUND 3 SCREW HOLES UNDER RH ATC L-BAND ANTENNA (C-CHECK RO 02/22/2026)REPAIRED CORROSION DAMAGE AROUND 3 SCREW HOLES UNDER RH ATC L-BAND ANTENNA WITH REFERENCE TO REO 670-53-21-2810 REV "A" DATED 2026-02-08 "REPAIR FOR ELONGATED HOLE AND TO
- [SDR SWIA2026020775317](https://openairdocs.org/sdr/SWIA2026020775317.md): Antenna · corroded · Feb 7, 2026 · N613SK · Cndair CL6002C10 · Navigation System
  > FOUND CORROSION AROUND 3 SCREW HOLES UNDER LH ATC L-BAND ANTENNA (C-CHECK RO 02/22/2026)REPAIRED CORROSION AROUND 3 SCREW HOLES UNDER LH ATC L-BAND ANTENNA WITH REFERENCE TO REO 670-53-21-2811 REV "--" DATED 2026-02-08 "DISPOSITION FOR BLENDED DAMAGE TO UPPE
- [SDR SWIA2026022575313](https://openairdocs.org/sdr/SWIA2026022575313.md): Skin · scratched · Feb 7, 2026 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > SURFACE SCRATCHES ON FUSALAGE SKIN UNDER RH ATC L-BAND ANTENNA (C-CHECK RO 02/22/2026)REPAIRED SURFACE SCRATCHES ON FUSELAGE SKIN UNDER RH ATC L-BAND ANTENNA WITH REFERENCE TO REO 670-53-21-2810 REV "A" DATED 2026-02-08 "REPAIR FOR ELONGATED HOLE AND TOOLIN
- [SDR SWIA2026022575315](https://openairdocs.org/sdr/SWIA2026022575315.md): Dome Nut · damaged · Feb 5, 2026 · N613SK · Cndair CL6002C10 · Fuselage Structure (General)
  > SCREW SHANK STUCK IN THE RH ATC L-BAND ANTENNA DOME NUT (MARKED). (C-CHECK RO 02/22/2026)REMOVED THE RH ATC L-BAND ANTENNA INNER DOUBLER. COMPLIED WITH REO 670-53-21-2810 DATED: 2026-02-08 REV: -A REPAIR FOR ELONGATED HOLE AND TOOLING & CORROSIOIN DAMAGE TO
- [SDR SWIA2026022575326](https://openairdocs.org/sdr/SWIA2026022575326.md): Spigot · corroded · Jan 17, 2026 · N613SK · Cndair CL6002C10 · Passenger/Crew Doors
  > POSSIBLE SIGNS OF CORROSION FOUND AROUND THE BOLT HOLES OF THE PAX DOOR AFT SPIGOT ASSEMBLY. (C-CHECK RO 02/22/2026)COMPLIED WITH REO 670-53-21-2786 REV "--" DATED 2026-01-23 REPAIR FOR CORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN FS333.00-FS343.13 AT ST
- [SDR SWIA2026022574933](https://openairdocs.org/sdr/SWIA2026022574933.md): Floor Support · corroded · Dec 29, 2025 · N613SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY FLOOR SUPPORT FWD OUTBOARD FITTING IS CORRODED. REMOVED AND REPLACED GALLEY FLOOR SUPPORT FWD OUTBOARD FITTING WITH REFERENCE TO SRM 51-42-21.
- [SDR SWIA2025123000029](https://openairdocs.org/sdr/SWIA2025123000029.md): Floor Support · corroded · Dec 29, 2025 · N613SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY FLOOR SUPPORT FWD OUTBOARD FITTING IS CORRODED. OPEN.
- [SDR SWIA2025121175316](https://openairdocs.org/sdr/SWIA2025121175316.md): Stiffener · cracked · Dec 11, 2025 · N613SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 280.00 FWD STIFFENER ANGLE, BL26.00 IS CRACKED. (C-CHECK RO 02/22/2026)REMOVED AND REPLACED THE FS 280.00 FWD STIFFENER ANGLE,(CORRECTED LOCATION) LBL26.00 IN REFERERENCE WITH THE CRJ-700 SRM 51-42-06 AND SRM 53-11-10. COMPLIED WITH TASK CARD 51-900-1002-S
- [SDR SWIA2026022575312](https://openairdocs.org/sdr/SWIA2026022575312.md): Floorbeam · cracked · Nov 29, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > SUPPORT ANGLE CRACKED ON COCKPIT FLOORBEAM, RBL 12 - LBL 12. REMOVED AND REPLACED THE BS 280 LH & RH COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR LBL 12 AND RBL 12, WL 72.10 IAW SRM 51-42-06, AND SRM 53-11-43.
- [SDR SWIA2026022575309](https://openairdocs.org/sdr/SWIA2026022575309.md): Floorbeam · cracked · Nov 29, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > GUSSETS CRACKED FOR SUPPORT ANGLE ON COCKPIT FLOORBEAM AT RBL 12 AND LBL 12. REMOVED AND REPLACED THE BS 280 LT & RT GUSSETS FOR COCKPIT CENTER FLOOR PANEL LANDING/ANGLE IAW SRM 51-42-06 AND SRM 53-11-43.
- [SDR SWIA2026022575336](https://openairdocs.org/sdr/SWIA2026022575336.md): Floorbeam · corroded · Nov 27, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND SURFACE CORROSION ON THE LH FLOOR BEAM UPPER FLANGE/SEAT TRACK MOUNTING SURFACE FS 571.50 - FS 584.00 & LBL 9.00. (C-CHECK RO 02/22/2026)PERFORMED FLOOR BEAM SPLICE REPAIR OF LH BEAM FS 571.50 - FS584.00 & LBL 9.00 WITH REFERENCE TO SRM 53-00-41 AND C
- [SDR SWIA2026022575327](https://openairdocs.org/sdr/SWIA2026022575327.md): Floorbeam · corroded · Nov 26, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND SURFACE CORROSION ON THE RH FLOOR BEAM UPPER FLANGE/SEAT TRACK MOUNTING SURFACE FS 582.00 RBL 9.00 & FS 585.00 RBL 9.00. (C-CHECK RO 02/22/2026)COMPLIED WITH REO 670-53-31-1131 REV-- DATED 2025-11-28 AND BLENDED SURFACE CORROSION ON THE RH FLOOR BEAM U
- [SDR SWIA2026022575314](https://openairdocs.org/sdr/SWIA2026022575314.md): Pressure Blkhd · corroded · Nov 26, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FOUND SURFACE CORROSION ON THE LH FORWARD PRESSURE BULKHEAD FITTING UPPER SURFACE FLANGE FS 686.00 - FS 698.00 & LBL 9.00 (C-CHECK RO 02/22/2026)COMPLIED WITH REO 670-53-41-777 REV-- DATED 2025-11-28. AND BLENDED SURFACE CORROSION ON THE LH FORWARD PRESSURE
- [SDR SWIA2026022574317](https://openairdocs.org/sdr/SWIA2026022574317.md): Skin · dented · Nov 21, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND DENT ON FUSALAGE SKIN NEXT TO BS 565, STRINGER 21R. DENT IS 1 INCH IN LENGTH,.25 INCH WIDE, &.018 INCH DEEP. COMPIED WITH REO 670-53-31-1123 REV-. REPAIR TO RT FUSELAGE SKIN PANEL, LOWER, FWD BARREL AT BS 565, S21R - 22R. COMPLIED WITH TASK CARD 5
- [SDR SWIA2025112400021](https://openairdocs.org/sdr/SWIA2025112400021.md): Skin · dented · Nov 21, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND DENT ON FUSALAGE SKIN NEXT TO FS565 STRINGER 21R. DENT IS 1" IN LENGTH.25" WIDE AND.018" DEEP. REF SRM 53-31-01. (FILED OPEN)
- [SDR SWIA2026022575330](https://openairdocs.org/sdr/SWIA2026022575330.md): Floorbeam · cracked · Nov 18, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOOR BEAM (REFERENCE SRM 53-11-43 ITEM 108) AT FS280.00 AND LBL12.00 CRACKED ON THE AFT OUTBOARD FLANGE FROM APPROX WL70.00 - WL72.50 (C-CHECK RO 02/22/2026)COMPLIED WITH GREO 670-53-11-896 DATED: 2015-03-17 REV: -- GENERIC REPAIR TO THE CENTER COCKPIT FLOOR
- [SDR SWIA2026022575335](https://openairdocs.org/sdr/SWIA2026022575335.md): Angle · cracked · Nov 17, 2025 · N613SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE, BL26.00 FS280.00 (REFERENCE SRM 53-11-10 ITEM 81A) CRACKED. (C-CHECK RO 02/22/2026)REMOVED AND REPLACED THE ANGLE, (CORRECTED LOCAITON) RBL26.00 FS280.00 IN REFERENCE WITH THE CRJ-700 SRM 51-42-06 AND SRM 53-11-10. COMPLIED WITH TASK CARD 51-900-1002
- [SDR SWIA2026022575308](https://openairdocs.org/sdr/SWIA2026022575308.md): Floorbeam · cracked · Nov 13, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM, BS 280 AND RBL 12 CRACKED ON THE AFT OTBD FLANGE FROM APPROX WL 70 - WL 72.50. COMPLIED WITH GREO 670-53-11-896 REV -. COMPLIED WITH REO 670-53-11-2231, REV -. REPAIR TO CENTER COCKPIT FLOORBEAMS AT LBL12. & RBL 12. PERFORMED EDDY CURRENT INSP
- [SDR SWIA2026022575321](https://openairdocs.org/sdr/SWIA2026022575321.md): Skin · dented · Nov 12, 2025 · N613SK · Cndair CL6002C10 · Rudder, Plate/Skin
  > THERE ARE 2 ADJACENT DENTS ON THE R/H RUDDER SKIN BETWEEN STA 60.73 AND STA 66.76 LOCATED 6" FORWARD OF THE TRAILING EDGE. (C-CHECK RO 02/22/2026)PERFORMED REPAIR ON THE R/H RUDDER SKIN BETWEEN STA 60.73 AND STA 66.76, 6" FWD OF TRAILING EDGE WITH REFERENCE T
- [SDR SWIA2026022575328](https://openairdocs.org/sdr/SWIA2026022575328.md): Web · corroded · Nov 7, 2025 · N613SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS280.00 RH LOWER WEB INSERT AT WL 73.00 IS CORRODED IN TWO SPOTS AT RBL 11.128 AND RBL 45.00. (REF. DWG CC670-34170) (C-CHECK RO 02/22/2026)COMPLIED WITH REO 670-53-11-2214 DATED: (12-18-2025) REV (--) DISPOSITION FOR RE-INCORPORATION OF RHS BULKHEAD LOWER
- [SDR SWIA2026022575325](https://openairdocs.org/sdr/SWIA2026022575325.md): Floorbeam · corroded · Nov 7, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280.00 RH FLOOR CROSS BEAM AT WL 73.00 CORRODED AND HAS SEVERAL CRACKS ON NUTPLATE HOLES FROM RBL 11.128 TO RBL 45.00 (REF. CRJ-700 SRM 53-11-10 ITEM 119). (C-CHECK RO 02/22/2026)REMOVED AND REPLACED THE RH FS 280.00 RH FLOOR CROSS BEAM @ WL 73.00 AND RBL
- [SDR SWIA2025110175307](https://openairdocs.org/sdr/SWIA2025110175307.md): Skin · dented · Nov 1, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > SMALL DENT ON FUSELAGE SKIN BETWEEN BS 581 & 597, S19R - 18R. REPAIRED THE DENT IAW REO 670-53-31-1119 REV--. ENSURED DRESS BACK PERFORMED IAW REO 670-51-00-085, REV A. CP 31112613 FOR EDDY CURRENT INSPECTION.
- [SDR SWIA2026022575310](https://openairdocs.org/sdr/SWIA2026022575310.md): Door Frame · corroded · Oct 29, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON PAX DOOR SURROUND STRUCTURE AROUND FWD PAX DOOR LATCH SPIGOT BOLT HOLES. COMPLIED WITH REO 670-53-21-2736 REV--. REPAIR FOR CORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN FS315.95-FS323.43 AT STR3L (UNDERNEATH FWD SPIGOT).
- [SDR SWIA2026022575331](https://openairdocs.org/sdr/SWIA2026022575331.md): Structure · corroded · Oct 19, 2025 · N613SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > LARGE AMOUNT OF CORROSION ALONG THE LOWER EDGE SPAR ON FWD BAGGAGE-BAY DOOR (C-CHECK RO 02/22/2026)REMOVED AND REPLACED LOWER EDGE SPAR ON FWD BAGGAGE BAY DOOR (P/N LE670-39500-2, S/N 054) WITH REFERENCE TO SRM 51-42-06, SRM 51-42-13, AND REO 670-52-35-591
- [SDR SWIA2026022575332](https://openairdocs.org/sdr/SWIA2026022575332.md): Skin · dented · Oct 15, 2025 · N613SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RH INBOARD FLAP LOWER SKIN HAS 4 DENTS LOCATED 14" FROM INBD EDGE AND 4" FROM TRAILING EDGE, 32" FROM INBD EDGE AND 2" FROM TRAILING EDGE, 20.5" FROM INBD EDGE AND 24" FROM TRAILING EDGE, 26" FROM INBD EDGE AND 24" FROM TRAILING EDGE. (C-CHECK RO 02/22/2026)
- [SDR SWIA2026022575322](https://openairdocs.org/sdr/SWIA2026022575322.md): Skin · dented · Oct 15, 2025 · N613SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LH INBOARD FLAP LOWER SKIN HAS 5 DENTS LOCATED 19" FROM INBD EDGE AND 2.5" FROM TRAILING EDGE, 16" FROM INBD EDGE AND 13" FROM TRAILING EDGE, 18" FROM INBD AND 15" FROM TRAILING EDGE, 17.5" FROM INBD EDGE AND 16.5" FROM TRAILING EDGE, 19" FROM INBD EDGE AND 24
- [SDR SWIA2026022575320](https://openairdocs.org/sdr/SWIA2026022575320.md): Rivet · sheared · Oct 10, 2025 · N613SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FO'S OB SEAT TRACK WEAR STRIP FWD RIVET HEAD IS SHEARED (C-CHECK RO 02/22/2026)UPON REMOVAL OF THE FO'S OB SEAT TRACK, FOUND SEVERAL HOLES ELOGATED THAT SECURE THE TRACK TO THE COCKPIT FLOOR. COMPLIED WITH REO 670-53-11-2206 DATED: 2025-12-02 REV: "--" REPA
- [SDR SWIA2026022575349](https://openairdocs.org/sdr/SWIA2026022575349.md): Roller · damaged · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > RIGHT SLAT 3-2 INBD AFT SIDE ROLLER IS DAMAGED. RT SLAT-TRACK ROLLER REMOVED AND REPLACED IAW AMM 27-81-44.
- [SDR SWIA2026022575348](https://openairdocs.org/sdr/SWIA2026022575348.md): Roller · damaged · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > RIGHT SLAT 2-2 OTBD AFT SIDE ROLLER IS DAMAGED. RT SLAT-TRACK 2-2 ROLLER REMOVED AND REPLACED IAW AMM 27-81-44.
- [SDR SWIA2026022575347](https://openairdocs.org/sdr/SWIA2026022575347.md): Roller · damaged · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > RH SLAT 2-2 OB FWD SIDE ROLLER IS DAMAGED. RT SLAT-TRACK 2-2 OB FWD SIDE ROLLER REMOVED AND REPLACED IAW AMM 27-81-44.
- [SDR SWIA2025100975346](https://openairdocs.org/sdr/SWIA2025100975346.md): Roller · damaged · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > RH SLAT 2-2 IB FWD SIDE ROLLER IS DAMAGED. RT SLAT TRACK 2-2 INBD FWD SIDE ROLLER REMOVED AND REPLACED PER AMM 27-81-44.
- [SDR SWIA2026022575345](https://openairdocs.org/sdr/SWIA2026022575345.md): Roller · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > L/H SLAT-TRACK 3-2 AFT OB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)L/H SLAT-TRACK 3-2 AFT OB SIDE ROLLER REMOVED AND REPLACED PER AMM 27-81-44. SEE C-CHECK TASK CARD 27-520-120
- [SDR SWIA2026022575344](https://openairdocs.org/sdr/SWIA2026022575344.md): Roller · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > L/H SLAT-TRACK 3-2 AFT IB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)L/H SLAT-TRACK 3-2 AFT IB SIDE ROLLER REMOVED AND REPLACED PER AMM 27-81-44. SEE C-CHECK TASK CARD 27-520-120
- [SDR SWIA2026022575343](https://openairdocs.org/sdr/SWIA2026022575343.md): Roller · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > L/H SLAT-TRACK 3-2 FWD OB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)L/H SLAT-TRACK 3-2 FWD OB SIDE ROLLER REMOVED AND REPLACED PER AMM 27-81-44. SEE C-CHECK TASK CARD 27-520-120
- [SDR SWIA2026022575342](https://openairdocs.org/sdr/SWIA2026022575342.md): Roller · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > L/H SLAT-TRACK 3-2 FWD IB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)L/H SLAT-TRACK 3-2 FWD IB SIDE ROLLER REMOVED AND REPLACED PER AMM 27-81-44. SEE C-CHECK TASK CARD 27-520-120
- [SDR SWIA2026022575341](https://openairdocs.org/sdr/SWIA2026022575341.md): Rub Block · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > L/H SLAT-TRACK 2-2 AFT OB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)L/H SLAT-TRACK 2-2 AFT OB SIDE ROLLER REMOVED AND REPLACED PER AMM 27-81-44. SEE C-CHECK TASK CARD 27-520-120
- [SDR SWIA2026022575340](https://openairdocs.org/sdr/SWIA2026022575340.md): Roller · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > L/H SLAT-TRACK 2-2 AFT IB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)L/H SLAT-TRACK 2-2 AFT IB SIDE ROLLER REMOVED AND REPLACED PER AMM 27-81-44. SEE C-CHECK TASK CARD 27-520-120
- [SDR SWIA2026022575339](https://openairdocs.org/sdr/SWIA2026022575339.md): Roller · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > L/H SLAT-TRACK 2-2 FWD OB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)L/H SLAT-TRACK 2-2 FWD OB SIDE ROLLER REMOVED AND REPLACED PER AMM 27-81-44. SEE C-CHECK TASK CARD 27-520-120
- [SDR SWIA2026022575338](https://openairdocs.org/sdr/SWIA2026022575338.md): Roller · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > LEFT SLAT-TRACK 1-2 AFT OB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)REMOVED L/H SLAT-TRACK 1-2 AFT OB SIDE ROLLER ASSEMBLY IN REFERENCE WITH AMM 27-81-44.REMOVED AND REPLACED BEARING IN REFERENCE WITH RIL #2631, REV: B, DATE: 01-AUG-2019 AND SRM 51-42-07.REIN
- [SDR SWIA2026022575337](https://openairdocs.org/sdr/SWIA2026022575337.md): Roller · worn · Oct 9, 2025 · N613SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > L/H SLAT-TRACK 1-2 FWD IB SIDE ROLLER WORN. (C-CHECK RO 02/22/2026)REMOVED L/H SLAT-TRACK 1-2 FWD IB SIDE ROLLER ASSEMBLY IN REFERENCE WITH AMM 27-81-44.REMOVED AND REPLACED BEARING IN REFERENCE WITH RIL #2631, REV: B, DATE: 01-AUG-2019 AND SRM 51-42-07.REIN
- [SDR SWIA2026022575334](https://openairdocs.org/sdr/SWIA2026022575334.md): Frame · gouged · Oct 7, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND GOUGE ON FRONT FACE OF RH FRAME AT FS1108.00 BEHIND COWL ANTI ICE VALVE (C-CHECK RO 02/22/2026)PERFORMED REPAIR FOR FRAME ASSY FS1108 BETWEEN STR9R - STRG10R AND COMPLIED WITH REO 670-53-61-2599 REV "--" DATED 2025-12-04. PERFORMED EDDY CURRENT INSPECT
- [SDR SWIA2025090275311](https://openairdocs.org/sdr/SWIA2025090275311.md): Skin · gouged · Sep 2, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA91625-REO 670-53-21-2419 REV-, COMPLY WITH PERMANENT REPAIR ON GOUGE ON FUSELAGE SKIN BELOW PASSENGER DOOR, BETWEEN BS333 AND 349, S19L AND S20L. BLENDED DISCREPANT AREA PER REO 670-53-21-2419 REV-. THIS TEMPORARY DISP
- [SDR SWIA2026022575333](https://openairdocs.org/sdr/SWIA2026022575333.md): Skin · dented · Jun 30, 2025 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA71070-670-53-21-2078 N613SK MXCODEID57339-PR - 6 EACH DENTS FOUND ABOVE REPLACED STR 21L BETWEEN FS421 AND FS453. COMPLIED WITH MHIRJ REO 670-53-21-2078, REV--, DATED 2021-07-07. THIS IS A TEMPORARY DISPOSITION VA
- [SDR SWI2025F00642](https://openairdocs.org/sdr/SWI2025F00642.md): Indicator · out of adjust · May 14, 2025 · N613SK · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON TAKEOFF AFTER RETRACTING LANDING GEAR. NOSE GEAR RED INDICATION (FLIGHT 6335 - FILED CLOSED)INTERROGATED MDC AND FOUND B1-CODE 007437. TROUBLESHOT GEAR DISAGREE IN REFERENCE TO FIM 32-61-05. FOUND PX22 OUT-OF-RIG. ADJUSTED PX22 AND TARGET IN R
- [SDR SWIA20240614](https://openairdocs.org/sdr/SWIA20240614.md): Skin · gouged · Jun 14, 2024 · N613SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > GOUGE IN FUSELAGE SKIN BELOW PASSENGER DOOR, BETWEEN FS333.00 AND FS349.00, STRGR 19LH AND STRGR 20LH.PERFORMED TEMPERARY REPAIR FUSELAGE SKIN BELOW PASSENGER DOOR, BETWEEN FS333.00 AND FS349.00, STRGR 19LH AND STRGR 20LH IAW REO 670-53-21-2419 REV-- DATED 20
- [SDR SWIA2024051700016](https://openairdocs.org/sdr/SWIA2024051700016.md): Warning Message · false activation · May 16, 2024 · N613SK · Cndair CL6002C10 · Ice/Rain Protection System
  > ANTI-ICE DUCT RED WARNING EICAS. AT CRUISE FL340. COMPLIED WITH QRH. MESSAGE DID NOT REAPPEARTROUBLESHOT ANTI-ICE DUCT WARNING IN REF TO CRJ 700 FIM 36-21-05. NO DAMAGE FOUND. COULD NOT DUPLICATE FAULT. RAN ENGINES IN REF TO CRJ 700 AMM 71-00-00. PERFORME

Next page: https://openairdocs.org/aircraft/N613SK/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 = 'N613SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N613SK/reports

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