# Service difficulty reports: N790SK

A list on [N790SK](https://openairdocs.org/aircraft/N790SK.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 · 105 reports

- [SDR SWIA2026022675573](https://openairdocs.org/sdr/SWIA2026022675573.md): Skin · damaged · Feb 26, 2026 · N790SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581 - FS 597 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEE
- [SDR SWIA2026022675572](https://openairdocs.org/sdr/SWIA2026022675572.md): Skin · damaged · Feb 26, 2026 · N790SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000 - FS 1015 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETW
- [SDR SWIA2026022675571](https://openairdocs.org/sdr/SWIA2026022675571.md): Skin · damaged · Feb 26, 2026 · N790SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - FS 409 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN
- [SDR SWIA2026022675570](https://openairdocs.org/sdr/SWIA2026022675570.md): Skin · damaged · Feb 26, 2026 · N790SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - FS 409 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN
- [SDR SWIA2026022675569](https://openairdocs.org/sdr/SWIA2026022675569.md): Skin · damaged · Feb 26, 2026 · N790SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LO
- [SDR SWIA2026020975232](https://openairdocs.org/sdr/SWIA2026020975232.md): Frame · fom · Dec 4, 2025 · N790SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FS485.00 FRAME SEGMENT NEEDS REMOVED FROM STR 20R TO STR 25R TO FACILITATE STR 21R REPLACEMENT. REMOVED AND REPAIRED FS 485.00 FRAME SEGMENT IAW MHIRJ REO 670-53-31-1138 REV -- DATED 2025-12-04. REFERENCE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA2026020975231](https://openairdocs.org/sdr/SWIA2026020975231.md): Stringer · corroded · Dec 1, 2025 · N790SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R CORRODED BETWEEN BS 409 - BS 421. REMOVED STRINGER 21R BTWN BS 394 - BS 477 IAW SRM 51-42-06-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE STRINGER IAW SRM 51-40-11-001-001-A01, INSTALLED THE NEW STRINGER IAW SRM 51-42-06-001-001-A01.
- [SDR SWIA2026020975230](https://openairdocs.org/sdr/SWIA2026020975230.md): Floorbeam · cracked · Nov 28, 2025 · N790SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK ON LBL 12 COCKPIT FLOORBEAM (PREVIOUS REPAIR) AT BS 280. REPAIRED LBL 12 COCKPIT FLOORBEAM (PREVIOUS REPAIR) AT BS 280 IAW SRMS 53-11-43-201-003-A01, 51-25-21-001-001-A01, 51-21-00-001-001-A01, REV 38. COMPLETED TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026020975226](https://openairdocs.org/sdr/SWIA2026020975226.md): Floorbeam · cracked · Nov 27, 2025 · N790SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK AT BS 280, COCKPIT FLOORBEAM AT RBL 9 AT FLOORPOST ATTACHMENT POINT. REPAIRED THE FLOORBEAM IAW SRM 53-11-43-201-003-A01, 51-42-13-001-001-A01, REV 38. COMPLETED TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026020975234](https://openairdocs.org/sdr/SWIA2026020975234.md): Bearing · damaged · Nov 21, 2025 · N790SK · Cndair CL6002C10 · Leading Edge Devices
  > THE RIGHT SLAT TRACK 2-2 AFT OUTBOARD, FWD INBOARD AND FWD OUTBOARD SIDE ROLLERS HAVE FLAT SPOT WIDTH GREATER THAN 0.060 IN. REMOVED AND REPLACED RT SLAT TRACK 2-2 AFT OTBD, FWD INBD AND FWD OTBD ROLLERS IAW AMM 27-81-44-000/400-802-A01.
- [SDR SWIA2026020975233](https://openairdocs.org/sdr/SWIA2026020975233.md): Roller · damaged · Nov 20, 2025 · N790SK · Cndair CL6002C10 · Leading Edge Devices
  > THE LEFT SLAT TRACK 3-2 ALL 4 SIDE ROLLERS HAVE FLAT SPOT WIDTH GREATER THAN 0.060 IN OR MULTIPLE FLAP SPOTS. REPLACEMENT IS REQUIRED. REPLACED THE LT SLAT TRACK 3-2 OB SIDE ROLLERS 2EA, IB AFT SIDE ROLLER IAW AMM 27-81-44-400-803-A01. REPLACED LT SLAT TRAC
- [SDR SWIA2026020975225](https://openairdocs.org/sdr/SWIA2026020975225.md): Frame · chafed · Nov 19, 2025 · N790SK · Cndair CL6002C10 · Fuselage Main, Frame
  > RIGHT ACM WATER INJECTOR LINE HAS CHAFED INTO FRAME BS 1144 AT STR 11R. REPAIRED THE FRAME AT BS 1144, STR 11R IAW REO 670-53-61-2636 REV--.
- [SDR SWIA2026020975229](https://openairdocs.org/sdr/SWIA2026020975229.md): Slat Track · worn · Nov 18, 2025 · N790SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-3 SHOWS SIGNS OF WEAR. REPAIRED LT SLAT TRACK 3-3 IAW SRM 51-21-06-001-001-A01, REV 38. AND REO 670-57-42-2285, REV -.
- [SDR SWIA2026020975228](https://openairdocs.org/sdr/SWIA2026020975228.md): Slat Track · corroded · Nov 18, 2025 · N790SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 SHOWS SIGNS OF CORROSION. REPAIRED THE LT SLAT TRACK 2-2 IAW SRM 51-21-06-001-001-A01, REV --, AND REO 670-57-42-2284 REV --.
- [SDR SWIA2026020975224](https://openairdocs.org/sdr/SWIA2026020975224.md): Slat Track · corroded · Nov 18, 2025 · N790SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK AT 1-2 HAS EVIDENCE OF CORROSION. REPAIRED LT SLAT TRACK AT 1-2 IAW SRM 51-21-06-001-001-A01 REV 38, AND REO 670-57-42-2283 REV A.
- [SDR SWIA2026020975222](https://openairdocs.org/sdr/SWIA2026020975222.md): Slat Track · corroded · Nov 18, 2025 · N790SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT, 1-2 SLAT LOWER AREA HAS CORROSION ON TRACK. REPAIRED RT 1-2 SLAT LOWER AREA IAW SRM 51-21-06-001-001-A01 REV 38 AND REO 670-57-42-2281 REV -.
- [SDR SWIA2026020975221](https://openairdocs.org/sdr/SWIA2026020975221.md): Slat Track · worn · Nov 18, 2025 · N790SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-1 SHOWS SIGNS OF WEAR. REPAIRED LT SLAT TRACK 3-1 IAW MHIRJ REO 670-57-42-2282 REV -- DATE 2025-11-25. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2026020975223](https://openairdocs.org/sdr/SWIA2026020975223.md): Skin · gouged · Nov 13, 2025 · N790SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LOWER SKIN GOUGED AT APPROXIMATELY BS 969, STGR 27. REPAIRED LOWER SKIN GOUGE AT APPROX BS 969, STGR 27 IAW REO 670-53-00-290 REV F.
- [SDR SWIA2026020975227](https://openairdocs.org/sdr/SWIA2026020975227.md): Skin · damaged · Sep 26, 2025 · N790SK · Cndair CL6002C10 · Passenger/Crew Doors
  > MAIN PAX DOOR 1 1/2 IN LONG.007 IN DEEP NEAR TOP MIDDLE OF DOOR.SRM 52-00-01. PERFORMED A MAJOR REPAIR TO THE PAX DOOR OUTER SKIN BETWEEN FS320.163 TO FS338.963 AND DD2 TO DD3 IAW REO 670-52-11-1529 REV--, AND REO 670-51-00-085 REV-A.
- [SDR SWIA20250922019](https://openairdocs.org/sdr/SWIA20250922019.md): Loop · faulted · Sep 19, 2025 · N790SK · Cndair CL6002C10 · Pneumatic System
  > LEFT BLEED DUCT WARNING, SWITCHED TO LT BLEED DUCT CAUTION. RAN QRH. (FLIGHT 5322) NO LT BLEED DUCT WARNING NOR CAUTION MESSAGES APPARENT. TROUBLESHOT LT BLEED DUCT WARNING IAW FIM 36-21-01. INTERROGATED MDC, FLAGGED B1 CODE 349536 (LT BLEED LOOP A FAILE
- [SDR SWIA202504180324](https://openairdocs.org/sdr/SWIA202504180324.md): Pressure Deck · dented · Mar 24, 2025 · N790SK · Cndair CL6002C10 · Fuselage Main, Structure
  > DENT DAMAGE FOUND ON AFT PRESSURE SILL DECK P/N SH670-36142-3 AT APPROXIMATE FS813.70 LHS. (C-CHECK RO 04/18/2025)REPAIRED DAMAGE FOUND ON AFT PRESSURE SILL DECK P/N SH670-36142-3 AT APPROXIMATE FS813.70 LHS PER REO 670-53-41-726 REV -A DATED 2025-04-10 ALL S
- [SDR SWIA202504180323](https://openairdocs.org/sdr/SWIA202504180323.md): Diaphragm · damaged · Mar 23, 2025 · N790SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > TOOLING DAMAGE ON FWD SIDE OF DIAPHRAGM P/N SH670-36115-1 AT FS736.00 BETWEEN BL36 AND BL45 RHS. (C-CHECK RO 04/18/2025)REMOVED AND INSTALLED NEW DIAPHRAGM AT RH FS736.00 REF. CRJ700 SRM 51-42-20-001-001-A01 AND DWG SH670-36110 REV. NCW TASKCARD 51-900-1002-SK
- [SDR SWIA2021072259726](https://openairdocs.org/sdr/SWIA2021072259726.md): Attach Angle · cracked · May 15, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > F.S.280 RBL12.00 INTERCOSTAL ATTACH ANGLE CRACKED AND CORRODED. (C-CHECK RO 7/20/2021) REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT F.S.280 RBL12.00 INTERCOSTAL WITH NEW REF. CRJ 700 SRM 51-42-21-001-001-A01.
- [SDR SWIA2021072259720](https://openairdocs.org/sdr/SWIA2021072259720.md): Floor Support · corroded · May 14, 2021 · N790SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF LWR DOOR POST FOUND THE COCKPIT FLOOR SUPPORT @ RBL12 @ FS 274 CORRODED AND CRACKED (C-CHECK RO 7/20/2021) REMOVED AND INSTLLED NEW COCKPIT FLOOR SUPPORT AT RBL12 AT FS274. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG CC670-33199 REV
- [SDR SWIA2021072259719](https://openairdocs.org/sdr/SWIA2021072259719.md): Floor Support · corroded · May 14, 2021 · N790SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF LWR DOOR POST FOUND THE COCKPIT FLOOR SUPPORT @ LBL12 @ FS 274 CORRODED AND CRACKED (C-CHECK RO 7/20/2021) REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT AT LBL12 AT FS274. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG CC670-33199 REV
- [SDR SWIA2021072259717](https://openairdocs.org/sdr/SWIA2021072259717.md): Support · corroded · May 10, 2021 · N790SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BACKUP SILL STGR 21L, FS310.00 TO FS333.00 HAS EVIDENCE OF CORROSION (C-CHECK RO 7/20/2021) REMOVED AND REPLACED WITH NEW BACK-UP SILL STGR 21L, FS310.00 TO FS333.00 HAS EVIDENCE OF CORROSION REF CRJ-700 SRM 51-42-06-001-001-A01 & BOMBARDIER DWG SH670-3
- [SDR SWIA2021072259716](https://openairdocs.org/sdr/SWIA2021072259716.md): Channel · corroded · May 9, 2021 · N790SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INNER FUSELAGE CHANNEL FOR DRAIN MAST BETWEEN FS1031.00 - FS1051.30 AND STGR 27 - 26R HAS CORROSION (C-CHECK RO 7/20/2021) REMOVED AND REPLACED WITH NEW INNER FUSELAGE CHANNEL FOR DRAIN MAST BETWEEN FS1031.00 - FS1051.30 AND STGR 27 - 26R HAS CORROSION
- [SDR SWIA2021072259741](https://openairdocs.org/sdr/SWIA2021072259741.md): Support · corroded · May 8, 2021 · N790SK · Cndair CL6002C10 · Aerodynamic Fairings
  > CORROSION ON SUPPORT STRUCTURE, AFT WING-TO-FUSELAGE FAIRING FS 909 MID ANGLES. MARKED. (C-CHECK RO 7/20/2021) CORROSION COVERS MORE THAN 30% OF AFT WING-TO-FUSELAGE FAIRING FS 909 MID ANGLES AND IN MULTIPLE SPOTS NEXT TO FASTENER HOLES CORROSION IS 10
- [SDR SWIA2021072259740](https://openairdocs.org/sdr/SWIA2021072259740.md): Bulkhead · corroded · May 7, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > ANGLE AT RBL26.00 FS280.00 LOWER BULKHEAD HAS CORROSION. (C-CHECK RO 7/20/2021) REMOVED AND REPLACED THE ANGLE AT RBL26.00 FS280.00 LOWER BULKHEAD WITH NEW REF. CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR SWIA2021072259715](https://openairdocs.org/sdr/SWIA2021072259715.md): Floorbeam · corroded · May 7, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > THE LBL9 FLOOR BEAM UPPER SURFACE HAS EVIDENCE OF CORROSION AT APPROXIMATELY FS 928.00 (MARKED). (C-CHECK RO 7/20/2021) REPAIRED LBL9 FLOOR BEAM FS928 REF CRJ700 SRM 51--23-00-001-001-A01,SRM 51-42-21-001-001-A01 REF MHI REO 670-53-51-220 REV -- DATE
- [SDR SWIA2021072259714](https://openairdocs.org/sdr/SWIA2021072259714.md): Floor Support · cracked · May 6, 2021 · N790SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER FLOOR SILL, CLIP AT FS 1000 JUST INBOARD OF STGR 17, IS CRACKED. (MARKED) (C-CHECK RO 7/20/2021) REMOVED OLD BRACKET AND INSTALLED AFT CARGO LOWER FLOOR SILL NEW BRACKET WITH P/N MM670-35642-001 FS1000 JUST INBOARD OF STGR 17LH RE
- [SDR SWIA2021072259713](https://openairdocs.org/sdr/SWIA2021072259713.md): Intercostal · corroded · May 6, 2021 · N790SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD7 INTERCOSTAL HAS CORROSION (C-CHECK RO 7/20/2021) REPLACED PAX DOOR FWD DD7 REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2021072259712](https://openairdocs.org/sdr/SWIA2021072259712.md): Skin · corroded · May 5, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON FUSELAGE SKIN UNDER TCAS ANTENNA AT APPROX. FS295.00 AND STRG 27. (C-CHECK RO 7/20/2021) REPAIRED CORROSION FOUND ON FUSELAGE SKIN UNDER TCAS ANTENNA AT APPROX. FS295.00 AND STRG 27 REF CRJ-700 SRM 51-42--21-001-001-A01 AND MHIRJ RE
- [SDR SWIA2021072259711](https://openairdocs.org/sdr/SWIA2021072259711.md): Door Sill · corroded · May 4, 2021 · N790SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL FWD TOP CAP ANGLE HAS CORROSION ON EDGE (C-CHECK RO 7/20/2021) REMOVED AND REPLACED PAX DOOR SILL FWD TOP CAP ANGLE. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV AE. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2021072259710](https://openairdocs.org/sdr/SWIA2021072259710.md): Bulkhead Web · corroded · May 3, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > F.S.280 R/H LOWER WEB CORRODED AT APPROX RBL 11. (C-CHECK RO 7/20/2021) REPLACED FS.280 RH LOWER WEB. WITH NEW REF. CRJ 700 SRM 53-11-10-201-004-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND SKYWEST M-337 FORM.
- [SDR SWIA2021072259709](https://openairdocs.org/sdr/SWIA2021072259709.md): Intercostal · corroded · May 2, 2021 · N790SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD6 INTERCOSTAL AND CLEAT HAS CORROSION (C-CHECK RO 7/20/2021) REMOVED CORROSION ON PAX DOOR FWD DD6 INTERCOSTAL IAW CRJ 700 SRM 51-21-06-001-001-A01. PAX DOOR FWD DD6 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050" IAW CRJ 700 SRM 52-11-
- [SDR SWIA2021072259708](https://openairdocs.org/sdr/SWIA2021072259708.md): Intercostal · corroded · May 2, 2021 · N790SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD5 INTERCOSTAL HAS CORROSION (C-CHECK RO 7/20/2021) REPLACED PAX DOOR FWD DD5 INTERCOSTAL (P/N 601R318091-5) REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2021072259707](https://openairdocs.org/sdr/SWIA2021072259707.md): Intercostal · corroded · May 2, 2021 · N790SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD1A INTERCOSTAL AND CLEAT HAS CORROSION (C-CHECK RO 7/20/2021) REMOVED CORROSION ON PAX DOOR FWD DD1A INTERCOSTAL IAW CRJ 700 SRM 51-21-06-001-001-A01. PAX DOOR FWD DD1A INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050" IAW CRJ 700 SRM 52-
- [SDR SWIA2021072259706](https://openairdocs.org/sdr/SWIA2021072259706.md): Bulkhead Web · corroded · May 2, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > F.S.280 L/H LOWER WEB CORRODED AT APPROX LBL 11. (C-CHECK RO 7/20/2021) EXFOLIATION CORROSION FOUND AND 100% MATERIAL LOSS. REMOVED EXISTING SPLICE PLATE AND PERFORMED REPAIR ON FS280.00 L/H LOWER WEB AND BUTTSTRAP. REF: CRJ700 SRM 51-42-06-001-001-A01,
- [SDR SWIA2021072259705](https://openairdocs.org/sdr/SWIA2021072259705.md): Window Post · cracked · May 2, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Structure
  > * CO-PILOT WINDSHIELD SIDE POST HAS SUSPECTED CRACK AT TOP BARREL NUT HOLE. (C-CHECK RO 7/20/2021) REMOVE AND REPLACED DAMAGED CO-PILOT WINDSHIELD SIDE POST REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV F. / COMPLIED WITH 51-900-1002 SKY.
- [SDR SWIA202159704](https://openairdocs.org/sdr/SWIA202159704.md): Retainer · corroded · May 1, 2021 · N790SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > A BAY DOOR HAS CORROSION ON SEAL RETAINER (C-CHECK RO 7/20/2021) REMOVED AND REPLACED FWD RHS SEAL RETAINER ANGLE ON MAIN AVIONIC BAY DOOR. REF. CRJ 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG # CC670-38651 REV. E SHEET 1. / COMPLIED WITH SK
- [SDR SWIA2021072259703](https://openairdocs.org/sdr/SWIA2021072259703.md): Door Frame · corroded · May 1, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FORMER F/S 320.163 AND FWD CLIP COMMON TO FORMER ARE CORRODED (C-CHECK RO 7/20/2021) REPLACED PAX DOOR FORMER FS320.163 AND CLIP WITH NEW REF CRJ-700 SRM 52-11-06-001-001-A01, 51-42-21-001-001-A01 AND DWG# 601R31702 REV N. COMPLIED WITH TASK C
- [SDR SWIA2021072259702](https://openairdocs.org/sdr/SWIA2021072259702.md): Floorbeam · corroded · May 1, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > REPLACE LH AND RH FS.280 FLOOR CROSSBEAM WITH SREVICEABLE DUE TO OUT OF LIMITS CORROSION. (C-CHECK RO 7/20/2021) REMOVED AND REPLACED THE LH AND RH FS.280 FLOOR CROSSBEAMS WITH NEW REF CRJ 700 SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01, 51-42-22-00
- [SDR SWIA2021072259701](https://openairdocs.org/sdr/SWIA2021072259701.md): Cleat · corroded · May 1, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR CLEAT COMMON TO FRAME F/S 313.56 IS CORRODED (C-CHECK RO 7/20/2021) REMOVED AND INSTALLED NEW PAX DOOR CLEAT COMMON TO FRAME F/S313.56 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N AND RESTORED FINISH ALL FASTENERS AN
- [SDR SWIA2021072259739](https://openairdocs.org/sdr/SWIA2021072259739.md): Slat Track · corroded · Apr 30, 2021 · N790SK · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 2-2 HAS CORROSION AND GOUGING. (C-CHECK RO 7/20/2021) RECEIVED CANNED RH SLAT TRACK 2-2 PN:CC670-12051-9,SN:M638 FROM N806SK FOR USE ON N790SK AND IT IS REMOVED AND INSTALLED ON CAMP#22712841 JOB 71029265 OP 66. NO FURTHER ACTION IS
- [SDR SWIA2021072259700](https://openairdocs.org/sdr/SWIA2021072259700.md): Post · corroded · Apr 30, 2021 · N790SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FS 280 RH BL12L POST HAS EVIDENCE OF CORROSION AT FLOOR LEVEL. (C-CHECK RO 7/20/2021) PERFORMED DOOR POST REPAIR AT FS280.00 RH BL 12L. REF CRJ700 SRM 53-11-10-201-006-A01. SEE CONTINUATION CARD FOR WORK PERFORMED. COMPLIED WITH SKYWEST TASKCARD 51-900-
- [SDR SWIA2021072259699](https://openairdocs.org/sdr/SWIA2021072259699.md): Hinge · gouged · Apr 26, 2021 · N790SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > *PAX DOOR PIANO HINGE ON FUSELAGE SIDE HAS GOUGES ON LANDINGS BETWEEN LUGS. AREAS MARKED. (C-CHECK RO 7/20/2021) REPLACED PAX DOOR PIANO HINGE ON FUSELAGE SIDE REF CRJ-700 SRM 53-21-23-201-007-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY AND SWA M-337.
- [SDR SWIA2021072259698](https://openairdocs.org/sdr/SWIA2021072259698.md): Hinge · gouged · Apr 26, 2021 · N790SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > *PAX DOOR PIANO HINGE ON DOOR SIDE HAS A GOUGE BETWEEN LUGS ON AFT SECTION. MARKED. (C-CHECK RO 7/20/2021) REPLACED PAX DOOR PIANO HINGE ON DOOR SIDE WITH NEW HINGE REF CRJ-700 SRM 52-11-01-201-002-A01 AND BOMBARDIER DWG 60131702 REV N. COMPLIED WITH TA
- [SDR SWIA2021072259697](https://openairdocs.org/sdr/SWIA2021072259697.md): Intercostal · corroded · Apr 23, 2021 · N790SK · Cndair CL6002C10 · Passenger/Crew Doors
  > *CORROSION ON INTERCOSTAL DD3 FOR PAX DOOR UNDER ACCESS PANEL 832DL (C-CHECK RO 7/20/2021) REPLACED PAX DOOR FWD DD3 INTERCOSTAL (P/N 601R318054-1) REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2021072259696](https://openairdocs.org/sdr/SWIA2021072259696.md): Structure · damaged · Apr 23, 2021 · N790SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > *DAMAGE ON UPPER RH ENGINE TRANS COWL AT HINGE POINT (MARKED) (C-CHECK RO 7/20/2021) REMOVED AND REPLACED THE UPPER RH ENGINE TRANS COWL HINGE FAIRING WITH NEW REF. CRJ 700 SRM 54-21-00-201-001-A01 AND DWG CN624-2003 REV. AG. COMPLIED WITH SKYWEST TASK

Next page: https://openairdocs.org/aircraft/N790SK/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 = 'N790SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N790SK/reports

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