# Service difficulty reports: N780SK

A list on [N780SK](https://openairdocs.org/aircraft/N780SK.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 3 · 126 reports

- [SDR SWIA2026091077384](https://openairdocs.org/sdr/SWIA2026091077384.md): Skin · mechanic error · Sep 10, 2026 · N780SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > MIS-DRILL CONDITION HAS OCCURRED DURING STARLINK WIFI ANTENNA TRAY FWD DOUBLER INSTALLATION AT UPPER FUSELAGE SKIN FS 437 BETWEEN STR 2R AND STR 2L DAMAGE DETERMINED TO BE A MAJOR REPAIR. INSTALLED PERMANENT REPAIR DOUBLER INSTALLATION AT UPPER FUSELAGE SKIN
- [SDR SWIA2026090977116](https://openairdocs.org/sdr/SWIA2026090977116.md): Skin · demodification · Sep 9, 2026 · N780SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847 AND STR 1L - 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSL
- [SDR SWIA2026090977115](https://openairdocs.org/sdr/SWIA2026090977115.md): Skin · demodification · Sep 9, 2026 · N780SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409 AND STR 13R - 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FU
- [SDR SWIA2026090977114](https://openairdocs.org/sdr/SWIA2026090977114.md): Skin · demodification · Sep 9, 2026 · N780SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - 409 AND STR 13L - 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUS
- [SDR SWIA2026090977113](https://openairdocs.org/sdr/SWIA2026090977113.md): Skin · demodification · Sep 9, 2026 · N780SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 1000 - 1015 AND STG 25R - 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN I
- [SDR SWIA2026090977112](https://openairdocs.org/sdr/SWIA2026090977112.md): Skin · demodification · Sep 9, 2026 · N780SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581- 597 AND STG 24R - 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM, DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN IAW
- [SDR SWIA202512090002](https://openairdocs.org/sdr/SWIA202512090002.md): Windshield · failed · Dec 2, 2025 · N780SK · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAIN`S WINDSHIELD SHATTERED ON TAXI IN. (FLIGHT 4807) REFERENCE AML 1763854, REFERENCE AML 1764066, REFERENCE AML 1764068. REMOVED AND INSTALLED CAPTAINS SIDE WINDSHIELD, IAWAMM 56-11-01 & TASK CARD 56-220-1000-SKY OPS AND LEAK CHECK GOOD.
- [SDR SWIA2025120300002](https://openairdocs.org/sdr/SWIA2025120300002.md): Windshield · cracked · Dec 2, 2025 · N780SK · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAIN`S WINDSHIELD SHATTERED ON TAXI IN. (FLIGHT 4807)
- [SDR SWI2025F01654](https://openairdocs.org/sdr/SWI2025F01654.md): Landing Gear · malfunctioned · Nov 26, 2025 · N780SK · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > RECEIVED GEAR DISAGREE WARNING MESSAGE ON GEAR EXTENSION. GEAR SELECTOR LEVER IS LIMP. COMPLETED QRH - LANDED WITH OUT FURTHER ISSUE. DEFERRED PER MEL 32-30-1LOCATION: LANDING GEAR RETRACTION SYSTEMMAINTENANCE ACTION COMPLIED WITH ACCORDING TO MELCAT II DOW
- [SDR SWI2025F01653](https://openairdocs.org/sdr/SWI2025F01653.md): Warning Message · illuminated · Nov 26, 2025 · N780SK · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > RECEIVED GEAR DISAGREE WARNING MESSAGE ON GEAR EXTENSION. GEAR SELECTOR LEVER IS LIMP. COMPLETED QRH - LANDED WITH OUT FURTHER ISSUE. DEFERRED PER MEL 32-30-1LOCATION: LANDING GEAR RETRACTION SYSTEMMAINTENANCE ACTION COMPLIED WITH ACCORDING TO MELCAT II DOW
- [SDR SWIA20241223011](https://openairdocs.org/sdr/SWIA20241223011.md): Web · cracked · Oct 11, 2024 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SMALL CRACK MEASURING 1CM IN LENGTH FOUND IN ELECTRICAL BAY FLOOR WEB FS 193.00 ON LEFT SIDE. (FILED CLOSED) COMPLIED WITH PERMENANT REPAIR TO THE ELECTRICAL BAY FLOOR WEB FS 193.00 ON LEFT SIDE IN REFERENCE TO SRM 53-11-43-201-001-A01 & REO 670-53-11-5
- [SDR SWIA202412161011](https://openairdocs.org/sdr/SWIA202412161011.md): Web · cracked · Oct 11, 2024 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SMALL CRACK MEASURING 1CM IN LENGTH FOUND IN ELECTRICAL BAY FLOOR WEB FS 193.00 ON LEFT SIDE. (FILED OPEN) COMPLIED WITH PERMENANT REPAIR TO THE ELECTRICAL BAY FLOOR WEB FS 193.00 ON LEFT SIDE IN REFERENCE TO SRM 53-11-43-201-001-A01 & REO 670-53-11-509
- [SDR SWIA20241223005](https://openairdocs.org/sdr/SWIA20241223005.md): Skin · damaged · Oct 5, 2024 · N780SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > BIRD STRIKE DAMAGE TO UPPER SKIN PANEL (DWG: CC670-33105 REF), UPPER ELEC. BAY DOOR (DWG: CC670-33070 REF) AND UNDERLYING STRUCTURE (FRAME FS 193 (DWG: CC670-34201 REF) & STRINGER STR 14L (DWG: CC670-33145 REF)), LOCATED BETWEEN FS 193.00 - FS 202.75 AND STR 1
- [SDR SWIA202412161005](https://openairdocs.org/sdr/SWIA202412161005.md): Skin · damaged · Oct 5, 2024 · N780SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > BIRD STRIKE DAMAGE TO UPPER SKIN PANEL (DWG: CC670-33105 REF), UPPER ELEC. BAY DOOR (DWG: CC670-33070 REF) AND UNDERLYING STRUCTURE (FRAME FS 193 (DWG: CC670-34201 REF) & STRINGER STR 14L (DWG: CC670-33145 REF)), LOCATED BETWEEN FS 193.00 - FS 202.75 AND STR 1
- [SDR SWIA202401160005](https://openairdocs.org/sdr/SWIA202401160005.md): Unknown · warning message · Jan 15, 2024 · N780SK · Cndair CL6002C10 · Airfoil Anti/De-ice System
  > RECEIVED WING OVHT WARNING MESSAGE IN FLIGHT. LEFT WING. RAN QRH. MESSAGE CLEARED. REMAINED OUT OF ICING CONDITIONS. (FLIGHT 5726 FILED CLOSED)SEE EAML 1280062 FOR REPLACEMENT OF LT IBD WING A/I TEMP SENSOR. SENSOR FAILED AND WOULD NOT CONTROL WING ANTI-ICE MO
- [SDR SWIA202401020001](https://openairdocs.org/sdr/SWIA202401020001.md): Unknown · warning message · Jan 1, 2024 · N780SK · Cndair CL6002C10 · Landing Gear Brake System
  > D: BRAKE OVHT WARING DURING LANDING ROLLOUT. BTMS #1 READ 20, ALL OTHERS READ 0. CLEARED RUNWAY, RAN QRH. ( INDICATION WAS ----).C: MEL 32-46-1BCAT "C" DUE 01/10/2024BRAKE OVHT WARING DURING LANDING ROLLOUT. BTMS #1 READ 20, ALL OTHERS READ 0. CLEARED RUNWAY,
- [SDR SWIA20230613025](https://openairdocs.org/sdr/SWIA20230613025.md): Unknown · damaged · Jun 5, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > DAMAGE FOUND ON PAX DOOR HINGE LUGS #1, 2, 12, 26 (DOOR SIDE) (C-CHECK RO 6/9/2023) PAX DOOR PINO HINGE LUG DOOR SIDE REPAIRED ORIGINAL MATERIAL IS 0.119" IAW DWG 601R318073 REV. E. LUG #1, 2, 12, 26 MATERIAL THICKNESS REMOVED IS 0.009" TOOL # TUC9237 E
- [SDR SWI2023F00048](https://openairdocs.org/sdr/SWI2023F00048.md): Unknown · corroded · May 16, 2023 · N780SK · Cndair CL6002C10 · Doors
  > CORROSION FOUND AT KICKPLATE ANGLE DOOR SURROUND (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW KICKPLATE ANGLE AT DOOR SURROUND. REF CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV AE. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. COMPLIE
- [SDR SWIA202306130023](https://openairdocs.org/sdr/SWIA202306130023.md): Unknown · corroded · May 16, 2023 · N780SK · Cndair CL6002C10 · Doors
  > SEVERAL CORROSION ON PAX DOOR SURROUND ANGLE MID CAP (STGR 18L). (C-CHECK RO 6/9/2023) REMOVED AND REPLACED PAX DOOR SILL MID CAP ANGLE REF. CRJ 700 SRM 51-41-02-001-001-A01 AND DWG SH670-31810 REV. AE.
- [SDR SWIA202306130022](https://openairdocs.org/sdr/SWIA202306130022.md): Unknown · gouged · May 6, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > PAX DOOR HINGE (FUSELAGE SIDE) WITH GOUGE IN LUG LANDS #13 TO #27 (C-CHECK RO 6/9/2023) BLENDED GOUGES ON PAX DOOR HINGE LUG LANDS (FUSELAGE SIDE) #13 TO #27. MEASURED DEEPEST BLEND DEPTH OF 0.026€?. ALLOWABLE DAMAGE DEPTH OF 0.080€?. HINGE FOUND TO B
- [SDR SWIA202306130021](https://openairdocs.org/sdr/SWIA202306130021.md): Unknown · cracked · May 5, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > STRINGER 3L CRACKED AT FS 280 BULKHEAD (C-CHECK RO 6/9/2023) REPAIRED STRINGER 3L AT F.S 280 REF REO 670-53-21-493 REV-D DATED 2015-07-10. AND SERVICE BULLETIN 670BA-53-040 REVISION C DATED 09-20-2012, FUSELAGE CENTER FUSELAGE PRIMARY STRUCTURE FS280.00
- [SDR SWIA20230613020](https://openairdocs.org/sdr/SWIA20230613020.md): Unknown · corroded · May 3, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > INTERCOSTAL CORRODED - STR 20R FS 319.0 - FS 333.0 (C-CHECK RO 6/9/2023) REMOVED AND REPLACED INTERCOSTAL FS319-FS349 STGR 20R REF. DWG SH670-31950 REV. Y, CRJ 700 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. COMPLIED WITHI TASK CARD 51-900-1002
- [SDR SWI2023F00047](https://openairdocs.org/sdr/SWI2023F00047.md): Unknown · galled · May 2, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > LEFT HAND SIDE SEAT RAIL IS GALLED BTW STA 364 AND 379 (C-CHECK RO 6/9/2023) BLENDED LH SIDE SEAT RAIL BTW STA 364 AND 379, REF CRJ 700 SRM 53-21-49-101-001-A01DAMAGE IS OUT OF LIMITS DUE TO NO DAMAGE REMOVAL ALLOWABLE IN BLENDED AREA REF CJ700 SRM 53-2
- [SDR SWIA202306130018](https://openairdocs.org/sdr/SWIA202306130018.md): Unknown · corroded · May 2, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWD DD2 INTERCOSTAL IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR FWD DD2 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N, NO LEAKS NOTED. COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2023F00046](https://openairdocs.org/sdr/SWI2023F00046.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR FORMER F/S 329.41 BETWEEN MID DD5 AND MID DD6 INTERCOSTAL IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR FORMER F/S 329.41 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. NO LEAKS NOTED. COMPLIED WITH 51-90
- [SDR SWI2023F00045](https://openairdocs.org/sdr/SWI2023F00045.md): Unknown · cracked · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > CRACK FOUND AT CENTER COCKPIT FLOOR BEAM FLANGE LBL12.00 FS280.00 (C-CHECK RO 6/9/2023) INSTALLED NEW FABRICATED ANGLE ASSY AT LBL12 WL 72.10 BETWEEN FS280 AND FS265 REF CRJ700 SRM53-11-43-201-003-A01 INSTALLED NEW COCKPIT FLOOR BEAM LBL12 FS280 AND AL
- [SDR SWIA20230613017](https://openairdocs.org/sdr/SWIA20230613017.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR OUTER HANDLE PRESSURE BOX ANGLE IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR OUTER HANDLE PRESSURE BOX ANGLE IAW CRJ 700 SRM 51-42-21-001-001-A01 AND IAW DWG 601R31740 REV. C. NO LEAKS NOTED. COMPLIED WITH 51-900-1002-S
- [SDR SWI2023F00044](https://openairdocs.org/sdr/SWI2023F00044.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR MID DD7A INTERCOSTAL IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR MID DD7A INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. NO LEAKS NOTED. COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2023F00043](https://openairdocs.org/sdr/SWI2023F00043.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR AFT DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR AFT DD4 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. NO LEAKS NOTED. COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2023F00042](https://openairdocs.org/sdr/SWI2023F00042.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWD DD6 INTERCOSTAL IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR FWD DD6 INTERCOSTAL AND NEW BRACKET IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. NO LEAKS NOTED. COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2023F00041](https://openairdocs.org/sdr/SWI2023F00041.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWD DD5 INTERCOSTAL IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR FWD DD5 INTERCOSTAL AND NEW BRACKET AND NEW CLEAT IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A1 AND DWG 601R31702 REV. N. NO LEA
- [SDR SWIA20230613016](https://openairdocs.org/sdr/SWIA20230613016.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWD DD4 INTERCOSTAL AND QTY 2 CLEATS ARE CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR FWD DD4 INTERCOSTAL AND QTY 2 CLEATS IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. NO LEAKS NOTED. COMPLIED WITH 51-900
- [SDR SWIA202306130015](https://openairdocs.org/sdr/SWIA202306130015.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWD DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR FWD DD3 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. NO LEAKS NOTED. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202306130014](https://openairdocs.org/sdr/SWIA202306130014.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR AFT FORMER AT F/S 347.25 IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER AT F/S 347.25 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N AND PERFORMED PRESSURE LEAK CHECK OF THE PAX DOOR PER CRJ700 AM
- [SDR SWIA202306130013](https://openairdocs.org/sdr/SWIA202306130013.md): Unknown · corroded · Apr 30, 2023 · N780SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWD FORMER AT F/S 311.75 IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER AT F/S 311.75 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N AND PERFORMED PRESSURE LEAK CHECK OF THE PAX DOOR PER CRJ700 AM
- [SDR SWI2023F00056](https://openairdocs.org/sdr/SWI2023F00056.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *FS797.00 RH SIDE SEAT TRACK RETAINER AREA CORRODED (MARKED) (C-CHECK RO 6/9/2023) CORROSION AT FS797.00 ON RH SIDE SEAT TRACK RETAINER FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK RETAINER. REF CRJ700 SRM 51-23-00-001-001-A01. SEE CONTIN
- [SDR SWI2023F00055](https://openairdocs.org/sdr/SWI2023F00055.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *FS785.15 - FS847.00 RH SIDE SEAT TRACK CORRODED/CHAFFED/GOUGED (MARKED) (C-CHECK RO 6/9/2023) REMOVED AND REPLACED DAMAGED RH SIDE SEAT TRACK BETWEEN FS785.15 AND FS847.00 REF CRJ700 AMM 53-00-49-000-801 A03 & CRJ700 AMM 53-00-49-400-801-A03. SEE CON
- [SDR SWI2023F00054](https://openairdocs.org/sdr/SWI2023F00054.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *JUST AFT OF FS708.00 - FS761.85 RH SIDE SEAT TRACK CORRODED/CHAFFED (MARKED) (C-CHECK RO 6/9/2023) REMOVED AND REPLACED WITH NEW R/H SIDE SEAT TRACK FROM APPROX FS708 TO FS761 USING NEW EXTRUDED TRACK STOCK P/N 20276-288-0-0A REF CRJ700 AMM 53-00-49-00
- [SDR SWI2023F00053](https://openairdocs.org/sdr/SWI2023F00053.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *FS677.00 TO AFT OF FS708.00 RH SIDE SEAT TRACK CORRODED/CHAFFED (MARKED) (C-CHECK RO 6/9/2023) R/H SIDE SEAT TRACK CORRODED/CHAFFED FROM FS677.00 TO FS708.00 WAS REMOVED AND REPLACED. SEE CONTINUATION CARD FOR MORE DETAILS.
- [SDR SWI2023F00052](https://openairdocs.org/sdr/SWI2023F00052.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *FS785.15 - FS847.00 LH SIDE SEAT TRACK CORRODED/CHAFFED/GOUGED (MARKED) (C-CHECK RO 6/9/2023) REMOVED AND REPLACED LH SIDE SEAT TRACK BETWEEN FS785.15 - FS847.00 PER CRJ700 AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03 USING CALIBRATED TOOL TU
- [SDR SWI2023F00051](https://openairdocs.org/sdr/SWI2023F00051.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > *FS724.00 - FS761.85 LH SIDE SEAT TRACK CORRODED/CHAFFED (MARKED) (C-CHECK RO 6/9/2023) REMOVED AND REPLACED LH SIDE SEAT TRACK BETWEEN FS724.00 - FS761.85 PER CRJ700 AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03 USING CALIBRATED TOOL TUC8618 DUE:
- [SDR SWI2023F00050](https://openairdocs.org/sdr/SWI2023F00050.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *FS708.00 LH SIDE SEAT TRACK CORRODED (MARKED) (C-CHECK RO 6/9/2023) REMOVED AND REPLACED WITH NEW L/H SIDE SEAT TRACK FROM FS 677.00 TO 708.00, REF CRJ 700 AMM 53-00-49-400-801 (CONFIG A03) SEE CONTINUATION TASKS FOR MORE DETAILS
- [SDR SWI2023F00049](https://openairdocs.org/sdr/SWI2023F00049.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *FS677.00 - FS863.00 RBL 9 SEAT TRACK CORRODED/GOUGED THE ENTIRE STICK (MARKED) (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW SEAT TRACK AT RBL 9 BETWEEN FS677.00 AND FS863.00, REF CRJ700 AMM 53-00-49-400-801 A03 SEE CONTINUATION TASKS FOR MORE DETAIL
- [SDR SWI2023F000053](https://openairdocs.org/sdr/SWI2023F000053.md): Unknown · corroded · Apr 29, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *FS677.00 TO AFT OF FS708.00 RH SIDE SEAT TRACK CORRODED/CHAFFED (MARKED) (C-CHECK RO 6/9/2023) R/H SIDE SEAT TRACK CORRODED/CHAFFED FROM FS677.00 TO FS708.00 WAS REMOVED AND REPLACED. SEE CONTINUATION CARD FOR MORE DETAILS.
- [SDR SWIA202306130012](https://openairdocs.org/sdr/SWIA202306130012.md): Unknown · damaged · Apr 28, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *PAX DOOR HINGE, ON PAX DOOR, LUG #1 AND 13 DAMAGED (MARKED) (C-CHECK RO 6/9/2023) REPAIRED PAX DOOR HINGE DOOR SIDE IAW REO 670-52-11-511 REV. E DATED 2017-08-02 ALL STEPS COMPLIED WITH TYPE I STEPS 1 TROUGH 4. COMPLIED WITH SKYWEST TASK CARD 51-900-1
- [SDR SWIA202306130011](https://openairdocs.org/sdr/SWIA202306130011.md): Unknown · corroded · Apr 27, 2023 · N780SK · Cndair CL6002C10 · Doors
  > AFT BAGGAGE BAY LOWER SILL CORRODED (MARKED IN RED) (C-CHECK RO 6/9/2023) INSTALLED NEW AFT BAGGAGE BAY LOWER SILL REF CRJ 700 SRM 51-42-06-001-001-A01,51-42-13-001-001-A01 AND 51-42-21-001-001-A01 AND DRAWING MM670-35085 REV L. COMPLIED WITH SKYWEST
- [SDR SWIA202306130010](https://openairdocs.org/sdr/SWIA202306130010.md): Unknown · gouged · Apr 27, 2023 · N780SK · Cndair CL6002C10 · Doors
  > AFT BAGGAGE BAY SURROUND EXTERNAL SKIN HAS SEVERAL GOUGES ON FORWARD AND AFT SIDES (MARKED IN RED) (C-CHECK RO 6/9/2023) REMOVED GOUGES FROM FWD AND AFT SIDES OF AFT BAGGAGE BAY DOOR AND FOUND BLENDS OUT OF LIMITS. REPAIRED PER REO 670-53-61-2119 REV --
- [SDR SWIA20230613009](https://openairdocs.org/sdr/SWIA20230613009.md): Unknown · corroded · Apr 27, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > PAX DOOR MID DD6 INTERCOSTAL IS CORRODED (C-CHECK RO 6/9/2023) REMOVED AND INSTALLED NEW PAX DOOR MID DD6 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N. NO LEAKS NOTED. COMPLIED WITH 51-9
- [SDR SWIA20230613008](https://openairdocs.org/sdr/SWIA20230613008.md): Unknown · corroded · Apr 27, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *LH GEAR WELL TIRE BURST PANEL 542AZ FWD ATTACH ANGLE ON THE BACK OF THE WING SPAR IS CORRODED (MARKED) (C-CHECK RO 6/9/2023) REMOVED CORROSION OF LH GEAR WELL TIRE BURST PANEL 542AZ FWD ATTACH ANGLE ON THE BACK OF THE WING SPAR REF CRJ700 SRM51-12-00-
- [SDR SWIA20230613007](https://openairdocs.org/sdr/SWIA20230613007.md): Unknown · cracked · Apr 26, 2023 · N780SK · Cndair CL6002C10 · Powerplant System
  > R/H LOWER TRANSCOWL INBD "A" STANDOFF BRACKET IS CRACKED. (C-CHECK RO 6/9/2023) REMOVED CRACKED I/B STAND-OFF ANGLE & INSTALLED NEW I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. CRJ700 SRM 51-42-28-001-001-A01 & REO 670-54-21-971,

Next page: https://openairdocs.org/aircraft/N780SK/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 = 'N780SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N780SK/reports

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