# Service difficulty reports: N786SK

A list on [N786SK](https://openairdocs.org/aircraft/N786SK.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 2 · 96 reports

- [SDR SWIA2026092177226](https://openairdocs.org/sdr/SWIA2026092177226.md): Window · cracked · Sep 21, 2026 · N786SK · Cndair CL6002C11 · Flight Compartment Windows
  > CLIMBING THROUGH 18,000 FT WE NOTICED STATIC WITH SMALL FIRE ON THE CA SIDE LEFT WINDSHIELD FOLLOW QRH PROCEDURE AND NOT GETTING WORSEN BUT CRACKED ON THE LEFT SIDE FLIGHT 5763. INSPECTED LT WINDSHIELD & SIDE WINDOW, FOUND LT SIDE WINDOW TO BE CRACKED. R &
- [SDR SWIA2026080776758](https://openairdocs.org/sdr/SWIA2026080776758.md): Skin · demodification · Aug 7, 2026 · N786SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 100000 - 101500 AND STR 25R - 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKI
- [SDR SWIA2026080777071](https://openairdocs.org/sdr/SWIA2026080777071.md): Skin · demodification · Aug 7, 2026 · N786SK · Cndair CL6002C11 · Standard Practices/Structures
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR IN
- [SDR SWIA2026080776757](https://openairdocs.org/sdr/SWIA2026080776757.md): Skin · abnormal · Aug 7, 2026 · N786SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, 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 FUSLE
- [SDR SWIA2026080776756](https://openairdocs.org/sdr/SWIA2026080776756.md): Skin · abnormal · Aug 7, 2026 · N786SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13R - 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLE
- [SDR SWIA2026080776755](https://openairdocs.org/sdr/SWIA2026080776755.md): Skin · abnormal · Aug 7, 2026 · N786SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847, 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 FUSLEA
- [SDR SWIA2025052100017](https://openairdocs.org/sdr/SWIA2025052100017.md): Windshield · cracked · May 17, 2025 · N786SK · Cndair CL6002C10 · Flight Compartment Windows
  > AT FL280, LEFT WINDSHIELD DEVELOPED SINGLE CRACK, FOLLOWED QUICKLY BY LEFT WINDSHIELD HEAT CAUTION, FOLLOWED BY TOTAL SHATTERING OF INNER CORE OF WINDSHIELD. COMPLIED WITH QRH, NO PRESSURIZATION LOSS OCCURRED. (FLIGHT 4788 - FILED CLOSED)THIS DISCREPANCY WA
- [SDR SWI2025F00645](https://openairdocs.org/sdr/SWI2025F00645.md): Windshield · cracked · May 17, 2025 · N786SK · Cndair CL6002C10 · Flight Compartment Windows
  > AT FL280, LEFT WINDSHIELD DEVELOPED SINGLE CRACK, FOLLOWED QUICKLY BY LEFT WINDSHIELD HEAT CAUTION, FOLLOWED BY TOTAL SHATTERING OF INNER CORE OF WINDSHIELD. COMPLIED WITH QRH, NO PRESSURIZATION LOSS OCCURRED. (FLIGHT 4788 - FILED OPEN)THIS IS CURRENTLY A W
- [SDR SWIA2025021408](https://openairdocs.org/sdr/SWIA2025021408.md): Hinge · gouged · Feb 8, 2025 · N786SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > FOUND GOUGING DAMAGE ON FWD SIDE OF FUSELAGE PAX DOOR HINGE AT FS310-FS313. (FILED CLOSED) BLENDED GOUGING DAMAGE ON FWD SIDE OF FUSLAGE PAX DOOR SKIN CUTOUT AT FS310-FS313 BETWEEN STR 17L AND STR 19L WITH REFERENCE TO SRM 51-12-00. PERFORMED UT THICKNE
- [SDR SWIA2024121600015](https://openairdocs.org/sdr/SWIA2024121600015.md): Transducer · faulted · Dec 15, 2024 · N786SK · Cndair CL6002C10 · Landing Gear Brake System
  > A/SKID OB CAUTION IN FLIGHT DIVERTED TO MSP. (FLIGHT 5378 - FILED CLOSED) REMOVED AND REPLACED LHOB WHEEL SPEED TRANSDUCER ASSEMBLY PER AMM 32-44-01. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SWIA202412101355](https://openairdocs.org/sdr/SWIA202412101355.md): Intercostal · corroded · Oct 24, 2024 · N786SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD5 INTERCOSTAL AND CLEAT IS CORRODED HN00196557 (C-CHECK RO 12/8/2024) REPLACED PAX DOOR AFT DD5 INTERCOSTAL AND CLEAT REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202412101354](https://openairdocs.org/sdr/SWIA202412101354.md): Intercostal · corroded · Oct 19, 2024 · N786SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DD4 HAS CORROSION BETWEEN FS338-347 SKIN ATTACHMENT FLANGE (C-CHECK RO 12/8/2024) REPLACED PAX DOOR INTERCOSTAL AT DD4 BETWEEN FS338-FS347 REF CRJ700 SRM 51-42-06-001-001-A01, AND DWG 601R31702 REV. N. COMPLIED WITH 51-900-1002-S
- [SDR SWIA202412101353](https://openairdocs.org/sdr/SWIA202412101353.md): Intercostal · corroded · Oct 19, 2024 · N786SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DD6 BETWEEN FS320-338 HAS CORROSION AT FS320 ON BOTH SIDES AND AT FS338 ON LOWER SIDE (C-CHECK RO 12/8/2024) REPLACED PAX DOOR INTERCOSAL DD6 BETWEEN FS320-FS338 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPL
- [SDR SWIA202412101352](https://openairdocs.org/sdr/SWIA202412101352.md): Door Frame · gouged · Oct 17, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR (FUSELAGE SIDE) LAND 27 IS GOUGED. (C-CHECK RO 12/8/2024) REPAIRED PASSENGER DOOR (FUSELAGE SIDE) LAND 27 REF CRJ 700 SRM 53-21-23-201-010-A01 REPAIR TYPE IV. COMPLIED WITH SKY CARD 51-900-1002-SKY
- [SDR SWIA2024121015](https://openairdocs.org/sdr/SWIA2024121015.md): Striker · corroded · Oct 15, 2024 · N786SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AT ATTACHMENT HOLES AS MARKED (C-CHECK RO 12/8/2024) REPLACED SERVICE DOOR LOWER SEAL STRIKER REF DWG SH670-31950 REV. Y, CRJ700 SRM 51-42-06-001-001-A01. LEAK CHECK FAILED SEE HN00204233, CAMP#29221755. COM
- [SDR SWIA202412101316](https://openairdocs.org/sdr/SWIA202412101316.md): Floorbeam · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL9 LONGITUDINAL FLOOR BEAM TOP CAP IS CORRODED AT APPROX. FS1031 (C-CHECK RO 12/8/2024) REPAIRED LBL 9.0 FLOOR BEAM CAP AT APPROX F/S 1031 AND INSTALLED ALL REPAIRED PARTS IAW CRJ 700 SRM 53-00-41-201-001-A01 AND IAW REO 670-53-61-2392 REV. -- DATED
- [SDR SWIA202412101315](https://openairdocs.org/sdr/SWIA202412101315.md): Floorbeam · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL27 LONGITUDINAL FLOOR BEAM TOP CAP IS CORRODED AT APPROX. FS1031 (C-CHECK RO 12/8/2024) CORROSION ON LBL27 BEAM AT APPROX FS1031 FOUND TO BE OUT OF LIMITS, PERFORMED SPICE REPAIR REF CRJ700 SRM 53-00-41-201-001-A01, COMPLIED WITH 51-900-1002-SKY CARD
- [SDR SWIA202412101314](https://openairdocs.org/sdr/SWIA202412101314.md): Floorbeam · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL9 LONGITUDINAL FLOOR BEAM TOP CAP IS CORRODED AT APPROX. FS1031 (C-CHECK RO 12/8/2024) REPAIRED RBL 9.0 FLOOR BEAM TOP CAP AT FS 1031 AND INSTALLED ALL REPAIR PARTS IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2392 REV. -- DATED 2024-10-21
- [SDR SWIA202412101313](https://openairdocs.org/sdr/SWIA202412101313.md): Floorbeam · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL27 LONGITUDINAL FLOOR BEAM TOP CAP IS CORRODED AT APPROX. FS1031 (C-CHECK RO 12/8/2024) REPAIRED RBL 27 FLOOR BEAM AT F/S 1031 IAW REO 670-53-61-2390 REV. -- DATED 2024-10-20 STEPS 1, 2, 3, 4, 5, 6. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202412101312](https://openairdocs.org/sdr/SWIA202412101312.md): Bracket · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BRACKET CORRODED FS533, STGR22L - 23L. (MARKED) (C-CHECK RO 12/8/2024) REMOVED CORRODED CARGO TIE DOWN BRACKET, AND INSTALLED NEW CARGO TIE DOWN BRACKET (P/N SH670-33390-1) AT FS 533, BETWEEN STGR 22L-23L REF CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 S
- [SDR SWIA202412101311](https://openairdocs.org/sdr/SWIA202412101311.md): Door Sill · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 12/8/2024) REPLACED AFT CARGO DOOR SILL REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, AND DWG MM670-35085 REV. L. COMPLIED
- [SDR SWIA202412101310](https://openairdocs.org/sdr/SWIA202412101310.md): Floorbeam · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 BEAM IS CORRODED BETWEEN BL.0 AND LBL9 (C-CHECK RO 12/8/2024) BLENDED CORROSION AND FOUND OUT OF LIMITS. REPLACED WITH NEW CROSSBEAM AT FS 280.00 LBL9 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-
- [SDR SWIA202412101309](https://openairdocs.org/sdr/SWIA202412101309.md): Web · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LH LOWER FS.280 WEB (C-CHECK RO 12/8/2024) REPLACED LH LOWER FS280 WEB. REF CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202412101308](https://openairdocs.org/sdr/SWIA202412101308.md): Seat Track · corroded · Oct 11, 2024 · N786SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK STRUCTURE IS CORRODED FS793 (C-CHECK RO 12/8/2024) REPAIRED LH SIDE SEAT RAIL STRUCTURE BETWEEN FS785.15 - FS797.00 REF REO 670-53-41-691 REV--, DATED 2024-10-22. COMPLIED WITH ALL STEPS. COMPLIED WITH TASK 51-900-1002-SKY. SEE CONTIN
- [SDR SWIA202412101351](https://openairdocs.org/sdr/SWIA202412101351.md): Stringer Splice · corroded · Oct 10, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE FOR STGR25R AT FS333.00 HAS GALVANIC CORROSION. (MARKED) (C-CHECK RO 12/8/2024) REPLACED STRINGER SPLICE FFOR STGR 25R AT FS333.00 REF CRJ700 SRM 51-42-06-001-001-A01, DWG SH670-32420 REV-E. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SK
- [SDR SWIA202412101350](https://openairdocs.org/sdr/SWIA202412101350.md): Floorbeam · cracked · Oct 10, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 CLIP IS CRACKED LBL9 OTBD SIDE (C-CHECK RO 12/8/2024) REMOVED AND REPLACED WITH 1 EA OF NEW CLIP AT FS 280.00 LBL9. CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV-K. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002
- [SDR SWIA2024121001349](https://openairdocs.org/sdr/SWIA2024121001349.md): Floorbeam · corroded · Oct 10, 2024 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR SUPPORT ANGLE IS CORRODED FWD SIDE OF FS280 BEAM BETWEEN RBL9 AND LBL9 (C-CHECK RO 12/8/2024) REMOVED AND REPLACED COCKPIT FLOOR SUPPORT ANGLE (FWD OF FS.280 BETWEEN LBL.9 AND RBL.9) REF CRJ700 SRM 51-42-06-001-001-A01 REVISION 38: JUL 25/
- [SDR SWIA202412101345](https://openairdocs.org/sdr/SWIA202412101345.md): Stand Off · cracked · Oct 9, 2024 · N786SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/8/2024) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CAR
- [SDR SWIA202412101344](https://openairdocs.org/sdr/SWIA202412101344.md): Stand Off · cracked · Oct 9, 2024 · N786SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > L/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/8/2024) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD
- [SDR SWI2024F01343](https://openairdocs.org/sdr/SWI2024F01343.md): Stand Off · cracked · Oct 9, 2024 · N786SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/8/2024) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD
- [SDR SWIA202412101363](https://openairdocs.org/sdr/SWIA202412101363.md): Stand Off · cracked · Oct 8, 2024 · N786SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/8/2024) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLETED SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA2024121008](https://openairdocs.org/sdr/SWIA2024121008.md): Stand Off · cracked · Oct 8, 2024 · N786SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/8/2024) REMOVED CRACKED INBD "A" BRACKET STANDOFF, AND INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON THE L/H UPPER TRANSCOWL REF MHIRJ GREO #670-54-21-971 REV
- [SDR SWIA202412101303](https://openairdocs.org/sdr/SWIA202412101303.md): Skin · dented · Sep 26, 2024 · N786SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP, LOWER INBOARD SKIN HAS DENTS, HN00190905 (C-CHECK RO 12/8/2024) ON R/H WING I/B FLAP, REMOVED AND REPLACED DAMAGED I/B PORTION OF LOWER SKIN, REF. CRJ700 SRM 57-52-01-201-005-A01, REPAIR 005-A01. C/W 51-900-1002-SKY
- [SDR SWIA20241210925](https://openairdocs.org/sdr/SWIA20241210925.md): Track · cracked · Sep 25, 2024 · N786SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > THE AFT BAG BAY DOOR SURROUND AFT TRACK LOWER ATTACHMENT BRACKET IS CRACKED. (C-CHECK RO 12/8/2024) REMOVED AND REPLACED LOWER ATTACH CHANNEL FOR AFT CARGO DOOR AFT TRACK SUPPORT REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, DWG
- [SDR SWIA202412100920](https://openairdocs.org/sdr/SWIA202412100920.md): Skin · dented · Sep 20, 2024 · N786SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > ADM #7780. #1 ENGINE LOWER FAN COWL DOOR AT 6 O'CLOCK POSITION. DENT MEASURES 4" LONG, 3.5" WIDE, 0.145" DEEP. W/D RATION IS 24. CRJ700 SRM 54-14-00-101-001-A01. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE ALL EVIDENCE USI
- [SDR SWIA2023121101](https://openairdocs.org/sdr/SWIA2023121101.md): Unknown · warning message · Dec 10, 2023 · N786SK · Cndair CL6002C10 · Landing Gear Door Actuator
  > AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING MESSAGE ACCOMPANIED WITH A NWS STEERING INOP CAUTION MESSAGE. RAN THE QRH PUT THE GEAR SELECTOR IN THE DOWN POSITION GEAR SHOWED DOWN AND LOCKED. NWS STEERING INOP MESSAGE PERSISTED RAN THE QRH. RETURNED TO THE FIEL
- [SDR SWIA20230815004](https://openairdocs.org/sdr/SWIA20230815004.md): Unknown · dented · Aug 14, 2023 · N786SK · Cndair CL6002C10 · Nacelle/Pylon Structure
  > REMOVED LH LOWER FAN COWL DOOR TO FACILITATE PERMANENT REPAIR FOR DENT ON LT ENG COWL DOOR ASSY (FILED CLOSED)INSTALLED NEW LH FAN COWL DOOR SEE CP 27023226-1 FOR MX PERFORMED AND PARTS INFO
- [SDR SWIA202162956](https://openairdocs.org/sdr/SWIA202162956.md): None · arced · Dec 3, 2021 · N786SK · Cndair CL600* · Window/Windshield System
  > TRANSFER FROM EAML 794229: ARCING OCCURRING AT RT WINDSHIELD CONNECTOR BLOCK. ARCING CEASES WHEN WINDSHIELD HEAT IS TURNED OFF. (FILED - CLOSED) / REMOVED AND REPLACED RH WINDSHIELD IN REFERENCE WITH CRJ 700 AMM CH 56-11-01 AND TASK CARD 56-220-1000-SKY O
- [SDR SWIA202054128](https://openairdocs.org/sdr/SWIA202054128.md): Skin · chafed · Nov 2, 2020 · N786SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LT INBOARD FLAP LEADING EDGE PANEL 584GB HAS CHAFE MARK. C-CHECK RO 11/16/2020. REPLACED LT INBOARD FLAP LEADING EDGE PANEL 584GB, REF CRJ700 SRM. INSTALLATION ACCOMPLISHED ON JOB 71028670 OP 7005. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA202054113](https://openairdocs.org/sdr/SWIA202054113.md): Retainer · out of tolerance · Nov 1, 2020 · N786SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR AFT LT SEAL RETAINER WAS FOUND TO BE OUT OF LIMITS. C-CHECK RO 11/16/2020. REPLACED AVIONICS BAY DOOR AFT LT SEAL RETAINER, IAW CRJ700 SRM DWG. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA202054112](https://openairdocs.org/sdr/SWIA202054112.md): Retainer · out of tolerance · Nov 1, 2020 · N786SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR AFT RT SEAL RETAINER WAS FOUND TO BE OUT OF LIMITS. C-CHECK RO 11/16/2020. REPLACED AVIONICS BAY DOOR AFT RT SEAL RETAINER, IAW CRJ700 SRM DWG. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA202054111](https://openairdocs.org/sdr/SWIA202054111.md): Retainer · out of tolerance · Nov 1, 2020 · N786SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR, FWD LT SEAL RETAINER WAS FOUND TO BE OUT OF LIMITS. C-CHECK RO 11/16/2020. REPLACED AVIONICS BAY DOOR FWD LT SEAL RETAINER, IAW CRJ700 SRM DWG. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA202054110](https://openairdocs.org/sdr/SWIA202054110.md): Retainer · out of tolerance · Nov 1, 2020 · N786SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR, FWD RT SEAL RETAINER WAS FOUND TO BE OUT OF LIMITS. C-CHECK RO 11/16/2020. REPLACED AVIONICS BAY DOOR FWD RT SEAL RETAINER, IAW CRJ700 SRM, DWG. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA202054109](https://openairdocs.org/sdr/SWIA202054109.md): Slat Track · cracked · Oct 27, 2020 · N786SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RT WING, SLAT TRACK 1-3 CANISTER BRACKET, IN FUEL TANK PANEL 651AB, HAS EVIDENCE OF CRACKS ON TOP AND BOTTOM CORNERS. C-CHECK RO 11/16/2020. COMPLIED WITH THE REO FOR REPLACEMENT CANISTER BRACKET AT RT WING SLAT TRACK 1-3. LEAK CHECK AND OPERATIONS CHEK GOO
- [SDR SWIA202054125](https://openairdocs.org/sdr/SWIA202054125.md): Seat Track · corroded · Oct 26, 2020 · N786SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FS 581-677 HAS CORROSION IN SEVERAL SPOTS. C-CHECK RO 11/16/2020. REMOVED AND REPLACED LBL 9 SEAT TRACK FROM FS 581-677, REF CRJ700 AMM. TOOL NR TUC2049 DATE DUE 31-JUL-21.
- [SDR SWIA202054124](https://openairdocs.org/sdr/SWIA202054124.md): Seat Track · corroded · Oct 26, 2020 · N786SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FS 863-953 HAS CORROSION IN SEVERAL SPOTS. C-CHECK RO 11/16/2020. REPLACED LT FLOOR SEAT TRACK LOCATED AT LBL 9.0 FROM FS 863 TO FS 953 WITH NEW, REF CRJ-700 AMM. TUC8605 31/JAN/2021.
- [SDR SWIA202054108](https://openairdocs.org/sdr/SWIA202054108.md): Bulkhead Web · corroded · Oct 26, 2020 · N786SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > CORROSION FOUND ON RT FS 280 BULKHEAD WEB. C-CHECK RO 11/16/2020. REMOVED CORROSION FROM RT FS 280 LOWER BULKHEAD WEB AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPAIRED RT FS 280 LOWER BULKHEAD WEB, REF REO. COMPLIED WITH TASK CARD.
- [SDR SWIA202054107](https://openairdocs.org/sdr/SWIA202054107.md): Hinge · gouged · Oct 26, 2020 · N786SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > GOUGE ON FUSELAGE SIDE OF PAX DOOR HINGE JUST AFT OF AFT LUG. C-CHECK RO 11/16/2020. REMOVED AND REPLACED PAX DOOR HINGE FUSELAGE SIDE, REF-CRJ-700 SRM AND DWG. SEE CONTINUATON CARD FOR DETAILS. LEAK & OPERATIONS CHECK GOOD.
- [SDR SWIA202054106](https://openairdocs.org/sdr/SWIA202054106.md): Floorbeam · cracked · Oct 25, 2020 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL 12.00 FS 274 FLOOR BEAM IS CRACKED, FOUND WHILE REMOVING 221ALF FLOOR SUPPORT ANGLE AT FS 280 ON JOB: 71028674 OP: 16 MX TRANS NR 21720630. C-CHECK RO 11/16/2020. REPAIRED RBL 12.00 FS 274 FLOOR BEAM, REF CRJ-700 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA202054105](https://openairdocs.org/sdr/SWIA202054105.md): Floorbeam · corroded · Oct 25, 2020 · N786SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RT 280 FLOOR BEAM IS CORRODED, FOUND DURING REMOVAL OF 221ALF FLOOR SUPPORT ANGLE ON JOB: 71028674 OP: 16 MX TRANS NR 21720630. C-CHECK RO 11/16/2020. REMOVED AND REPLACED RT 280 FLOOR BEAM, REF DWG CRJ 700 SRM. COMPLIED WITH TASK CARD.

Next page: https://openairdocs.org/aircraft/N786SK/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 = 'N786SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N786SK/reports

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