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Aircraft record

N786SK2009 Bombardier INC CL-600-2C11

Registration validNot yet verified by ownerSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 198230 ADs may apply96 service difficulty reports

Registration
Valid
expires Apr 30, 2028
Based in
St George, UT
owner city / state
Owners
1
since 2009
NTSB events
None
since 1982
ADs may apply
30
confirm with A&P
Service reports
96
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Skywest Airlines INC
Owner type
Corporation
City, state
St George, UT
Certificate issued
Sep 24, 2009
Expires
Apr 30, 2028
Airworthiness
Standard · Transport
Airworthiness date
Aug 31, 2026

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Bombardier INC
Model
CL-600-2C11
Year
2009
Serial number
10286
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
55
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
AAA86A

Engine

Make and model
Ge Cf34-8c5b1
Type
Turbo-fan
Power
13,790 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2009 – nowSkywest Airlines INCSt George, UT · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (30)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2026-15-16Time Limits/ Maintenance ChecksSep 3, 2026Airframe (CL-600-2C11)
2026-05-05Flight controlsMar 23, 2026Airframe (CL-600-2C11)
2026-02-03Flight controlFeb 5, 2026Airframe (CL-600-2C11)
2025-25-03Time Limits/ Maintenance ChecksJan 16, 2026Airframe (CL-600-2C11)
2025-22-02StabilizersNov 20, 2025Airframe (CL-600-2C11)Serial numbers per Transport Canada AD CF-2025-38
Show all 30 ADs
ADSubjectEffectiveApplies to
2025-13-04Flight ControlsAug 5, 2025Airframe (CL-600-2C11)
2025-11-11Time Limits/ Maintenance ChecksJul 15, 2025Airframe (CL-600-2C11)
2025-09-09CommunicationsJun 18, 2025Airframe (CL-600-2C11)
2025-04-08NavigationApr 25, 2025Airframe (CL-600-2C11)Certain serial numbers: CL-600-2B19 7002–8113; CL-600-2C10 10002–10999; CL-600-2C11 10002–10999; CL-600-2D15 15001–15990; CL-600-2D24 15001–15990; CL-600-2E25 19013–19990. Only with: Equipped with a radio altimeter and not determined to be a radio altimeter tolerant airplane as defined in paragraph (g) of the AD.
2024-03-02MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) AirplanesApr 9, 2024Airframe (CL-600-2C11)
2023-25-01MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) AirplanesFeb 6, 2024Airframe (CL-600-2C11)Certain serial numbers: CL-600-2C10 10001–10348; CL-600-2C11 10001–10348; CL-600-2D15 15001–15499; CL-600-2D24 15001–15499; CL-600-2E25 19001–19064
2023-24-03Fire ProtectionJan 22, 2024Airframe (CL-600-2C11)
2023-19-08Fire ProtectionNov 9, 2023Airframe (CL-600-2C11)
2023-10-03Fire ProtectionJul 11, 2023Airframe (CL-600-2C11)
2023-09-02Fire ProtectionJun 26, 2023Airframe (CL-600-2C11)
2023-07-07PneumaticJun 20, 2023Airframe (CL-600-2C11)Certain serial numbers: CL-600-2B19 7002–7990; CL-600-2B19 8000–8113; CL-600-2C10 10002–10347; CL-600-2C11 10002–10347; CL-600-2D15 15001–15494; CL-600-2D24 15001–15494; …
2023-06-06MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) AirplanesApr 28, 2023Airframe (CL-600-2C11)
2023-02-05Turbine Engine Combustion SectionMar 14, 2023Engine (CF34-8C5B1)
2022-24-10Fire protectionJan 18, 2023Airframe (CL-600-2C11)
2022-21-10Landing gearDec 21, 2022Airframe (CL-600-2C11)
2022-18-15FuelNov 25, 2022Airframe (CL-600-2C11)Certain serial numbers: CL-600-2B19 7002–7990; CL-600-2B19 8000–8112; CL-600-2C10 10002–10347; CL-600-2C11 10002–10347; CL-600-2D15 15001–15499; CL-600-2D24 15001–15499; …
2022-12-03MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) AirplanesNov 3, 2022Airframe (CL-600-2C11)Only with: Equipped with inertial reference system (IRS) P/N 465020-0400-0400, -0401, -0402, or -0403 (CL-600-2B19); P/N 465020-0400-0401, -0402, or -0403 (CL-600-2C10, -2C11, -2D15, -2D24); P/N 465020-0400-0402 or -0403 (CL-600-2E25).
2022-13-02Fuel systemAug 31, 2022Airframe (CL-600-2C11)Certain serial numbers: CL-600-2C10 10002–10325; CL-600-2C11 10002–10325; CL-600-2D15 15001–15263; CL-600-2D24 15001–15263; CL-600-2E25 19001–19013
2021-22-24Periodic InspectionsDec 29, 2021Airframe (CL-600-2C11)Certain serial numbers: CL-600-2C10 10002–on; CL-600-2C11 10002–on; CL-600-2D15 15001–on; CL-600-2D24 15001–on; CL-600-2E25 19001–on
2021-19-12Landing GearNov 10, 2021Airframe (CL-600-2C11)Certain serial numbers: CL-600-2C10 10002–on; CL-600-2C11 10002–on; CL-600-2D15 15001–on; CL-600-2D24 15001–on; CL-600-2E25 19001–on
2021-11-02Auto FlightJul 13, 2021Airframe (CL-600-2C11)
2021-08-03Rain and Ice ProtectionMay 25, 2021Airframe (CL-600-2C11)
2020-17-15NavigationNov 3, 2020Airframe (CL-600-2C11)
2020-08-13Flight controlsJun 10, 2020Airframe (CL-600-2C11)Certain serial numbers: CL-600-2B19 7003–7990; CL-600-2B19 8000–on; CL-600-2C10 10002–10347; CL-600-2D15 15001–15469; CL-600-2D24 15001–15469. Only with: Model CL-600-2C11 airplanes apply to all serial numbers.
2017-23-06Compressor bleed governorNov 30, 2017Engine (CF34-8C5B1)Certain serial numbers: 965101–965670; 194101–194999; 195101–195653

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (96)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Windows · window · crackedSep 21, 2026

    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 & R THE LT SIDE WINDOW IAW AMM 56-12-01 &…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · abnormalAug 7, 2026

    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 FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · abnormalAug 7, 2026

    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 FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · skin · abnormalAug 7, 2026

    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 FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · demodificationAug 7, 2026

    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 SKIN LOCATED BETWEEN BS 100000 - BS 101500…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Structures (general) · skin · demodificationAug 7, 2026

    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 INSTALLATION TO FUSLEAGE SKIN LOCATED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · windshield · crackedMay 17, 2025

    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 WORK IN PROGRESS

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · windshield · crackedMay 17, 2025

    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 WAS TRANSFERRED TO CAMP ITEM 30160648 WITH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · hinge · gougedFeb 8, 2025

    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 THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · transducer · faultedDec 15, 2024

    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.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 96 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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