# Service difficulty reports: N813SK

A list on [N813SK](https://openairdocs.org/aircraft/N813SK.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 · 300 reports

- [SDR SWIA2026021776587](https://openairdocs.org/sdr/SWIA2026021776587.md): Window Frame · cracked · Feb 17, 2026 · N813SK · Cndair CL6002D24 · Fuselage Main, Structure
  > PILOTS SIDE WINDSHIELD SIDE POST LOWER OUT BOARD CLIP CRACKED. REMOVED CRACKED CLIP AND INSTALLED NEW OUTBOARD CLIP AT PILOTS SIDE WINDSHIELD LOWER POST IAW SRM 51-42-21-001-001-A01, AND DWG CC670-33055 REV -F. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA2026070676520](https://openairdocs.org/sdr/SWIA2026070676520.md): Beam · chafed · Feb 17, 2026 · N813SK · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > RIGHT ENGINE LOWER C DUCT, THE INBD INNER BEAM ARE CHAFED, WHERE IT MEETS THE FIRE SEAL. BLENDED CHAFE ON RT ENGINE LOWER C DUCT INBD INNER BEAM IAW SRM 51-12-00-001-001-A01L 16. NO DAMAGE ALLOWED IN THIS AREA. REPAIRED PER REO 690-54-22-122 REV--. SEE CONT
- [SDR SWIA2026020176480](https://openairdocs.org/sdr/SWIA2026020176480.md): Skin · damaged · Feb 1, 2026 · N813SK · Cndair CL6002D24 · Rudder, Plate/Skin
  > UPON INSTALLATION OF THE RUDDER, FOUND LOWER HINGE ACCESS HOLE TO HAVE A BEND ON EDGE OF SKIN. PERFORMED REPAIR OF RUDDER LOWER HINGE ACCESS HOLE PER REO 690-55-41-109 REV-- BY TRIM OUT OF DAMAGE USING MINIMUM OF.500 CORNER RADIUS ENSURING COMPLETE DAMAGE
- [SDR SWIA2026070676566](https://openairdocs.org/sdr/SWIA2026070676566.md): Angle · corroded · Jan 6, 2026 · N813SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON ANGLE, KICKPLATE (STGR 17L TO 18L) PAX DOOR SURROUND FS 311.25 - FS347.25. (C-CHECK RO 07/02/2026)EXFOLIATION CORROSION AT PAX DOOR SURROUND ANGLE KICKPLATE, ALONG THE ENTIRE LENGTH OF THE PART. REPLACEMENT REQUIRED.REMOVED AND REPLACED PA
- [SDR SWIA2026010276509](https://openairdocs.org/sdr/SWIA2026010276509.md): Stringer Splice · corroded · Jan 2, 2026 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE STRINGER 19R, BS 477. REMOVED AND INSTALLED NEW STRINGER SPLICE IAW DWG SH690-302006, REV C, & SRM 51-42-06-001-001-A01. PERFORMED LEAK CHECK IAW SRM 51-23-03-001-001-A01. LEAK CHECK GOOD WITH NO DEFECTS NOTED. COMPLIED WITH
- [SDR SWIA2025122876590](https://openairdocs.org/sdr/SWIA2025122876590.md): Drag Angle · cracked · Dec 28, 2025 · N813SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > RT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE SHOWS POSSIBLE CRACK. REMOVED, CRACKED RIGHT, AFT DRAG ANGLE ON THE VERTICAL STAB, AND INSTALLED SERVICABLE DRAG ANGLE. SRM 51-42-21-001-001-A01 REV 38, SRM 51-42-13-001-001-A01 REV. 38, SRM 51-42-22-001-001-A01 RE
- [SDR SWIA2025122076513](https://openairdocs.org/sdr/SWIA2025122076513.md): Frame · corroded · Dec 20, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Frame
  > EXFOLIATED CORROSION FOUND AT FRAME 379.00 INSIDE FWD WASTE SERVICE AREA. STRINGER 25R TO 27R. INSTALLED NEW FRAME 379 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, DWG SH670-32280, REV H, AND DWG SH670-32050 REV. J. COMPLIED WITH SKYWEST TASK CARD
- [SDR SWIA2026070606541](https://openairdocs.org/sdr/SWIA2026070606541.md): Stringer Splice · corroded · Dec 17, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT STR20R AND FS477 IS CORRODED. REMOVED AND INSTALLED NEW STRINGER SPLICE ON STR20R AT FS477 IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND DWG SH690-30006 REV C. PERFORMED LEAK CHECK IAW SRM 51-23-03-001-001-A01. LEAK CHECK GOOD
- [SDR SWIA2025121776533](https://openairdocs.org/sdr/SWIA2025121776533.md): Seat Track · corroded · Dec 17, 2025 · N813SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > UPON REMOVAL OF SEAT RAIL AT RBL9 BETWEEN FS838.00 TO FS852.00 FLOORBEAM FOUND TO BE CORRODED. REMOVED AND INSTALLED NEW FLOOR BEAM SECTION AT RBL 9 F/S 847 TO F/S 847+56 UNDER SEAT RAIL AT RBL9 BETWEEN FS838.00 TO FS852.00 IAW SRM 53-00-41-201-001-A03. C
- [SDR SWIA2025121576470](https://openairdocs.org/sdr/SWIA2025121576470.md): Window Frame · cracked · Dec 15, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Structure
  > DURING AUDIT OF TASK CARD 53-220-504 (CONFIG A01) GENERAL VISUAL INSPECTION OF THE INTERNAL FRAME STRUCTURE OF THE WINDSHIELD AND SIDE WINDOWS IT WAS FOUND THAT THE LT INTERNAL WINDOW FRAME STRUCTURE ON THE AFT SIDE OF BS 235 IS CRACKED. REPAIRED LT INTERNAL
- [SDR SWIA2026070676558](https://openairdocs.org/sdr/SWIA2026070676558.md): Stringer · corroded · Dec 13, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS STR 24R HAS CORROSION BETWEEN FS349 - FS364. INSTALLED NEW MAIN AVIONICS STRINGER 24R BETWEEN FS333.00 TO FS477.40. IAW. SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH690-31350 REV. M. LEAK CHECK GOOD, COMPLIED WITH SKYWEST TRACK C
- [SDR SWIA2025121276556](https://openairdocs.org/sdr/SWIA2025121276556.md): Door Sill · corroded · Dec 12, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Structure
  > FWD OUTBOARD DOOR SILL LONGERON AT FWD BAGGAGE DOOR FS 477 TO FS 517 IS CORRODED. INSTALLED NEW FWD OUTBOARD DOOR SILL LONGERON AT FWD BAGGAGE DOOR FS 477 TO FS 517 REF. SRM 51-42-21-001-001-A01 AND DWG SH690-33750 REV -AF. COMPLIED WITH SKYWEST TASK CARD 51
- [SDR SWIA2025120876572](https://openairdocs.org/sdr/SWIA2025120876572.md): Rib · cracked · Dec 8, 2025 · N813SK · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > RT WING BATTERY RIB IS CRACKED AT WS 14.50. INSTALLED NEW RT WING BATTERY RIB AT WS 14.50. IAW SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01. AND DWG CC690-10610, REV. D..SEE CONTINUE CARD FOR DETAILSCOMPLIED WITH TASK CARD 51-900-1002.
- [SDR SWIA2025120776453](https://openairdocs.org/sdr/SWIA2025120776453.md): Cleat · corroded · Dec 7, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > EXFOLIATED CORROED CLEAT BS 319, S21R. CORROSION OVER 50% OF THICKNESS, LIMIT ALLOW. DAMAGE 10% OF CLEAT BS 319, S21R. OUT OF LIMITS IAW SRM 53-21-23-101-002-A02. REQ. REPLACEMENT.INSTALLED NEW CLEAT BS 319, S21R, IAW. SRM 51-42-06-001-001-A01, SRM 51-42-21-0
- [SDR SWIA2025120676586](https://openairdocs.org/sdr/SWIA2025120676586.md): Stringer Splice · corroded · Dec 6, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS STRINGER SPLICE STR 22R HAS CORROSION AT FS333 MX 31317120. INSTALLED NEW MAIN AVIONICS STRINGER SPLICE S22R AT BS 333 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-32420, REV. E. COMPLIED WITH SKYWEST TASK CARD 51-900-100
- [SDR SWIA2025120676529](https://openairdocs.org/sdr/SWIA2025120676529.md): Stringer · corroded · Dec 6, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS STR 22R HAS CORROSION BETWEEN FS280 - FS3295. INSTALLED NEW MAIN AVIONICS STR 22R BETWEEN FS280 - FS333 REF CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV. K. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA2025120576568](https://openairdocs.org/sdr/SWIA2025120576568.md): Stringer · corroded · Dec 5, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS STRINGER 22R HAS CORROSION BETWEEN BS 333 - 349. INSTALLED NEW MAIN AVIONICS STRINGER 22R BETWEEN BS 333 - 349. IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH690-31350 REV. M. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CAR
- [SDR SWIA2025120576544](https://openairdocs.org/sdr/SWIA2025120576544.md): Stringer Splice · corroded · Dec 5, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS STRINGER SPLICE 21R HAS CORROSION AT FS333. INSTALLED NEW SPLICE STGR 21R FS333.00. IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV. E. LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026070676497](https://openairdocs.org/sdr/SWIA2026070676497.md): Stringer · corroded · Dec 5, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS STRINGER 21R HAS CORROSION BETWEEN BS 310 - 319. INSTALLED NEW STRINGER 21R BS 280 TO 333 IAW SRM 51-42-06-001-001A01.AND DWG SH670-31630, REV. K. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA2025120576450](https://openairdocs.org/sdr/SWIA2025120576450.md): Intercostal · corroded · Dec 5, 2025 · N813SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MAIN AVIONICS INTERCOSTALS 20R HAS CORROSION BETWEEN BS 319 - 333. MAIN AVIONICS INTERCOSTAL S20R, BS 310 - 319 HAS EXFOLIATED CORROSION AT FASTENERS LOCATION. DAMAGE IS NOT ALLOWED WITHIN A 2D RADIUS OF A FASTENER THEREFORE FOUIND TO BE OUT OF LIMITS IAW SRM
- [SDR SWIA2025120376581](https://openairdocs.org/sdr/SWIA2025120376581.md): Structure · corroded · Dec 3, 2025 · N813SK · Cndair CL6002D24 · Cargo/Baggage Doors
  > EXFOLIATED CORROSION FOUND AT AFT BAGGAGE DOOR INNER CHORD BETWEEN BS 1031 TO 1047. REMOVED AND INSTALLED NEW AFT BAGGAGE DOOR INNER CHORD IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG MM670-35085 REV. L. COMPLIED WITH TASK CARD 51-900-1002
- [SDR SWIA2025120276547](https://openairdocs.org/sdr/SWIA2025120276547.md): Bulkhead Web · corroded · Dec 2, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > LH BULKHEAD LOWER WEB AT FS 280.00 HAS CORROSION. REMOVED LT LOWER WEB AND LT BUTTSTRAP AT BS 280 IAW SRM 51-42-06-001-001-A01, INSTALLED NEW ITEM -1 LOWER WEB AND ITEM -3 LH BUTTSTRAP AT LH BULKHEAD FS 280.00 REF CRJ900 SRM 53-11-10-201-004-A01, FABRICATED,
- [SDR SWIA2026070676554](https://openairdocs.org/sdr/SWIA2026070676554.md): Strap · cracked · Dec 1, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 3L AT FS280 TO FS282 CIRCUMFERENTIAL JOINT STRAP CRACKED. COMPLIED WITH PERMANENT REPAIR OF STGR 3L AT FS282 CIRCUMFERENTIAL JOINT STRAP REF REO 670-53-21-493 REV -D, AND SERVICE BULLETIN 670BA-53-040, REVISION C, FUSELAGE - CENTER FUSELAGE, PRIMARY S
- [SDR SWIA2025120176516](https://openairdocs.org/sdr/SWIA2025120176516.md): Floorbeam · corroded · Dec 1, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH CROSSBEAM AT FS 280.00 HAS CORROSION AND ELONGATED HOLES. REMOVED AND INSTALLED NEW LH CROSSBEAM AT BS 280 REF SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV -K. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025113076583](https://openairdocs.org/sdr/SWIA2025113076583.md): Slat Track · corroded · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT WING, SLAT TRACK 1-2 IS CORROSION ON THE LOWER FACE, REPAIRED RIGHT WING SLAT TRACK 1-2 IAW REO 690-57-42-1353 REV -. COMPLIED WITH ALL STEPS OF REO 690-57-42-1353 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025113076564](https://openairdocs.org/sdr/SWIA2025113076564.md): Slat Track · gouged · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING SLAT TRACK 1-1 SECTOR GEAR GOUGED. REPAIRED LEFT WING SLAT TRACK 1-1 SECTOR GEAR IAW REO 690-57-42-1361 REV -- DATED 2026-01-15. COMPLIED WITH ALL STEPS OF REO 690-57-42-1361 REV -- DATED 2026-01-15. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONT
- [SDR SWIA2025113076539](https://openairdocs.org/sdr/SWIA2025113076539.md): Slat Track · gouged · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-1 GOUGED. REPAIRED LEFT WING SLAT TRACK 3-1 IAW REO 690-57-42-1360 REV -. COMPLIED WITH ALL STEPS OF REO 690-57-42-1360 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025113076536](https://openairdocs.org/sdr/SWIA2025113076536.md): Slat Track · dented · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT WING, SLAT TRACK 3-1 IS INDENTED ON THE LOWER FACE, REPAIRED RIGHT WING SLAT TRACK 3-1 IAW REO 690-57-42-1357 REV -. COMPLIED WITH ALL STEPS OF REO 690-57-42-1357 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025113076522](https://openairdocs.org/sdr/SWIA2025113076522.md): Slat Track · dented · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT WING, SLAT TRACK 1-3 IS INDENTED ON THE LOWER FACE, REPAIRED RIGHT WING SLAT TRACK 1-3 IAW REO 690-57-42-1355 REV -. COMPLIED WITH ALL STEPS OF REO 690-57-42-1355 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025113076507](https://openairdocs.org/sdr/SWIA2025113076507.md): Slat Track · damaged · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT WING, SLAT TRACK 2-2 HAS PITTING ON THE LOWER FACE. REPAIRED RIGHT WING SLAT TRACK 2-2 IAW REO 690-57-42-1358 REV --. COMPLIED WITH ALL STEPS OF REO 690-57-42-1358 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025113076466](https://openairdocs.org/sdr/SWIA2025113076466.md): Window Post · cracked · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Structure
  > COCKPIT PILOT WINDOW SIDEPOST POSSIBLE CRACK AT TOP AFT, REMOVED LT WINDSHIELD POST IAW SRM 51-42-21-001-001-A01. INSTALLED NEW LT WINDSHIELD POST. IAW SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV. F. LEAK CHECKED GOOD. COMPLIED WITH SKYWEST TASK CARD 51-
- [SDR SWIA2025113076461](https://openairdocs.org/sdr/SWIA2025113076461.md): Slat Track · dented · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT WING, SLAT TRACK 1-1 IS DENTED ON THE LOWER FACE, REPAIRED RIGHT HAND WING SLAT TRACK 1-1 IAW REO 690-57-42-1354 REV -. COMPLIED WITH ALL STEPS OF REO 690-57-42-1354 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA2025113076457](https://openairdocs.org/sdr/SWIA2025113076457.md): Slat Track · dented · Nov 30, 2025 · N813SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT WING, SLAT TRACK 2-1 IS DENTED ON THE LOWER FACE, REPAIRED RIGHT WING SLAT TRACK 2-1 IAW REO 690-57-42-1356 REV -. COMPLIED WITH ALL STEPS OF REO 690-57-42-1356 REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA2025112876588](https://openairdocs.org/sdr/SWIA2025112876588.md): Stringer · corroded · Nov 28, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 19R BETWEEN BS 501 AND 517. REPAIRED THE STRINGER IAW REO 690-53-31-1096 REV -, AND SRM 53-00-03-201-001-A02. COMPLIED WITH ALL STEPS OF REO 690-53-31-1096, REV -. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD..
- [SDR SWIA2025112876585](https://openairdocs.org/sdr/SWIA2025112876585.md): Stringer · corroded · Nov 28, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON S18R BETWEEN BS 581 AND BS 661+32. PERFORMED STRINGER SPLICE REPAIR 18R BETWEEN BS 477.40 - 661+90 IAW REO 690-53-31-1111 REV -. COMPLIED WITH ALL STEPS REO 690-53-31-1111 REV -. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA2026070676504](https://openairdocs.org/sdr/SWIA2026070676504.md): Stringer Splice · corroded · Nov 28, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON GUSSETS ATTACHED TO STRINGER 19R BETWEEN BS 661+74 TO BS 677. INSTALLED NEW 3EA GUSSETS AND NEW STRINGER SPLICE AT STRINGER 19R, BS 677 IAW DWG SH690-39100, REV G, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. LEAK CHECK GOOD. COMPLIED
- [SDR SWIA2025112876478](https://openairdocs.org/sdr/SWIA2025112876478.md): Frame Splice · fom · Nov 28, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Frame
  > REMOVE AND SPLICE FRAMES BS 485 AND 501, S16R TO S20R TO FOM. REMOVED AND SPLICED FRAMES BS 485 AND 501, S16R TO S20R IAW SRM 53-00-06-201-001-A03, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, REO 690-53-31-1101, REV - AND DWG SH690-33101, REV M. COMP
- [SDR SWIA2025112876473](https://openairdocs.org/sdr/SWIA2025112876473.md): Stringer · corroded · Nov 28, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 20R BETWEEN FS581.00 AND FS597. REMOVED AND INSTALLED NEW STR20R BETWEEN BS 581 AND 597 IAW REO 690-53-31-1095 REV --A, DWG SH690-33302, REV C, SRM 51-42-21-001-001-A01, SRM 53-00-03-201-001-A02, AND SRM 51-42-06-001-001-A01. COMPLIED WI
- [SDR SWIA2025112876455](https://openairdocs.org/sdr/SWIA2025112876455.md): Stringer · corroded · Nov 28, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L BTWN BS 319 - 333 CORRODED. INSTALLED NEW MAIN AVIONICS STRINGER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-31630, REV K. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY, LEAK CHECKED GOOD.
- [SDR SWIA2025112676562](https://openairdocs.org/sdr/SWIA2025112676562.md): Intercostal · corroded · Nov 26, 2025 · N813SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR MID DD3 INTERCOSTAL IS CORRODED. REMOVED AND INSTALLED NEW MID DD3 INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 REV. 38 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2025112676535](https://openairdocs.org/sdr/SWIA2025112676535.md): Floorbeam · corroded · Nov 26, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH CROSSBEAM AT FS 280.00 HAS CORROSION TRANS 31259851 (C-CHECK RO 07/02/2026)REMOVED AND INSTALLED NEW RH CROSSBEAM AT FS 280.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-22-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV -K.
- [SDR SWIA2025112576582](https://openairdocs.org/sdr/SWIA2025112576582.md): Stiffener · damaged · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT BL 0, DAMAGED AT THE BOTTOM, FROM THE FLOATATION VALVE HINGE PIN BORING A HOLE. REPAIRED AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT BL 0, BOTTOM, FROM THE FLOATATION VALVE HINGE PIN IAW REO 690-53-61-1711 REV -. CO
- [SDR SWIA2025112576574](https://openairdocs.org/sdr/SWIA2025112576574.md): Intercostal · corroded · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD DD4 INTERCOSTAL IS CORRODED. REMOVED AND INSTALLED NEW PAX DOOR FWD DD4 INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA2025112576555](https://openairdocs.org/sdr/SWIA2025112576555.md): Stand Off · cracked · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Engine Thrust Reverser
  > LEFT UPPER TRANSCOWL OTBD A, BRACKET IS CRACKED. REMOVED CRACKED OTBD A BRACKET STANDOFF FROM LT UPPER TRANSCOWL AND INSTALLED 1 EA NEW OTBD A BRACKET STANDOFF ON LT UPPER TRANSCOWL, REF.GREO 670-54-21-971 REV (-B), STEPS 1-3. COMPLIED WITH SKY CARD #51-900-
- [SDR SWIA2026070676550](https://openairdocs.org/sdr/SWIA2026070676550.md): Stiffener · damaged · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT LBL 9, DAMAGED AT THE BOTTOM, FROM THE FLOATATION VALVE HINGE PIN BORING A HOLE (MARKED) (C-CHECK RO 07/02/2026)REPAIRED AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT LBL 9, DAMAGED AT THE BOTTOM, FROM THE FLOATATION
- [SDR SWIA2025112576538](https://openairdocs.org/sdr/SWIA2025112576538.md): Intercostal · corroded · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD DD7 INTERCOSTAL IS CORRODED. REMOVED AND INSTALLED NEW PAX DOOR FWD DD7 INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH SKYTRACK TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2026070676519](https://openairdocs.org/sdr/SWIA2026070676519.md): Drag Angle · cracked · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LH VERTICAL STAB - TO - FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK. REMOVED, CRACKED LEFT, AFT DRAG ANGLE ON THE VERTICAL STAB., AND INSTALLED SERVICABLE DRAG ANGLE. IAW SRM 51-42-21-001-001-A01, REV. 38, SRM 51-42-13-001-001-A01 REV. 38, SRM 51-42-22-001-001
- [SDR SWIA2025112576503](https://openairdocs.org/sdr/SWIA2025112576503.md): Rivet · loose · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Engine Thrust Reverser
  > RIGHT UPPER TRANSCOWL Z STIFFENER RIVETS ARE PULLED LOOSE. REPAIRED FASTENER HOLES COMMON TO ZED STIFFENER ON INNER SKIN OF RT UPPER TRANSCOWL, IAW REO 690-54-21-620, REV. A, 2026-01-20.COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2026070676501](https://openairdocs.org/sdr/SWIA2026070676501.md): Intercostal · corroded · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD DD6 INTERCOSTAL IS CORRODED. REMOVED AND INSTALLED NEW PAX DOOR FWD DD6 INTERCOSTAL SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV N. COMPLIED WITH SKY TRACK TASK CARD 51-900-1002-SKY. LEAK CHECKED GOOD.
- [SDR SWIA2025112576494](https://openairdocs.org/sdr/SWIA2025112576494.md): Drag Angle · cracked · Nov 25, 2025 · N813SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > RIGHT VERTICAL STAB - TO - FUSELAGE FWD DRAG ANGLE POSSIBLE CRACK. REMOVED DAMAGE FROM THE RIGHT FORWARD VERTICAL STAB. DRAG ANGLE, FABRICATED AND INSTALLED REPAIR PARTS. REF. SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Next page: https://openairdocs.org/aircraft/N813SK/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 = 'N813SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N813SK/reports

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