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Aircraft record

N796SK2010 Bombardier INC CL-600-2C11

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:1 NTSB accident (substantial damage, Jul 2017)30 ADs may apply103 service difficulty reports

Registration
Valid
expires Apr 30, 2029
Based in
St George, UT
owner city / state
Engine
CF34-8C5B1 · 13,790 lb thrust
Ge
Owners
1
since 2010
NTSB events
1
substantial, 2017
ADs may apply
30
confirm with A&P
Service reports
103
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Skywest Airlines INC
Owner type
Corporation
City, state
St George, UT
Certificate issued
Jan 22, 2010
Expires
Apr 30, 2029
Airworthiness
Standard · Transport
Airworthiness date
Feb 24, 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
2010
Serial number
10300
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
AACFE9

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. 2010 – 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 (1)

Accident · substantial damage

Jul 2, 2017 · Denver, CO

The fuel supply tube fitting pulling out of the left engine’s operability bleed valve (OBV) during the landing rollout, allowing fuel to leak and contact hot engine cases, which ignited a fire that caused thermal damage to the engine pylon. Contributing to the fitting pullout from the OBV was an undetected progressive environmental control system (ECS) support link wear condition that allowed…

Damage
Substantial
Injuries
None
Report
DCA17LA182

From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA17LA182)

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 (103)

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.

  • Fuselage · floorbeam · corrodedJul 10, 2026

    UPON REMOVAL LH CROSSBEAM FOUND SIGNS OF CORROSION ON LH SIDE FLOOR BEAM AT FS295 LBL9. PERFORMED REPAIR LH CROSSBEAM AT FS295 IAW REO 670-53-21-2941 REV.--(P2), SRM 53-00-00, AMM 20-70-00 AND REO 670-53-21-2941 REV.--(P1). REO 670-53-21-2941 REV--.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · striker · gougedMay 28, 2026

    PAX DOOR FS310 FWD DOOR SEAL STREAKER GOUGE BETWEEN STR7-8. PERFORMED REPAIR OF FWD DOOR SEAL STREAKER FS.310 BETWEEN STGR7-8 OF PAX DOOR IAW CRJ700 550 SERIES SRM 53-21-23, 51-21-11, 51-25-06, 51-42-06, 51-25-16N

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · skin · erodedMay 23, 2026

    RH ENG INLET LEADING EDGE ERODED. REMOVED AND REPLACED NOSE COWL LIPSKIN AT RT ENG INLET LEADING EDGE IAW SRM 54-11-05, AMM 71-61-01, SRM 51-42-06, REO 670-54-11-1456 REV - , REO 670-54-11-1456 REV -A AND SRM 51-21-11.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · bulkhead web · corrodedMay 22, 2026

    L/H FS 280 BULKHEAD WEB AT FLOOR HAS SIGNS OF CORROSION (C-CHECK RO 08/17/2026)PERFORMED REPAIR LH LOWER WEB FS280. FOUND TO BE WITHIN LIMITS IAW BOMBARDIER REO 670-53-11-594 REV -A, DATED 2015-06-26, CRJ 550 AMM 20-70-00, SRM 51-42-06, 51-42-13, 53-00-00. SEE REPORT FOR DETAILS. 7 DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead web · corrodedMay 22, 2026

    R/H FS280 BULKHEAD WEB AT FLOOR HAS SIGNS OF CORROSION. REMOVED AND REPLACED RH BUTTSTRAP AND RH LOWER WEB ON RH FS 280 BULKHEAD WEB IAW SRM 51-25-16, 51-42-06, 51-42-13, 53-00-00, AMM 20-70-00, REO 670-53-11-594, REV -A,

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor panel · gougedMay 20, 2026

    ON FWD EQUIPMENT BAY FLOOR JUST AFT OF ACCESS DOOR 211AL THERE IS A GOUGE (C-CHECK RO 08/17/2026)PERFORMED REPAIR ON FWD EQUIPMENT BAY FLOOR JUST AFT OF ACCESS DOOR 211AL, IAW CRJ-550, SRM 51-42-06, BOMBARDIER REO 670-53-11-509, REV -E, DATE: 2018-02-08 AND MHI RJ AVIATION ULC REO 670-53-11-2352…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · drag angle · crackedMay 18, 2026

    VERT STAB RH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AFT DRAG ANGLE AT RH VERT STAB IAW BOMBARDIER REO 670-55-31-018 DATE: 2016-11-10, CRJ550 SRM 51-26-01, NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S072326-2 DATE INSPECTION: 23-JUL-2026, SEE REPORT FOR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · drag angle · crackedMay 18, 2026

    VERT STAB LH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AT VERT STAB LH AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018, REV -A, DATE: 2016-11-10.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · skin · dentedMay 13, 2026

    ADM N796SK-9240 MCD TWO DENTS ON OUTER SKIN 24.5" FROM TOP, 11" FROM FRONT LEADING EDGE. 1ST DENT IS 11.5" FROM LEADING EDGE OF DOOR .750" TALL, .187" WIDE, .025" DEEP. 2ND DENT IS 11.0" FROM LEADING EDGE OF DOOR 1.250" TALL, .375" WIDE, .115" DEEP. SRM 52-11-01, PERFORMED REPAIR AREA ON PAX DOOR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · reversedFeb 6, 2026

    PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581 - 597, S24R - 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581 - 597, S24R - 25R IAW DWG 601-2365-02-343 REV IR AND SRM…

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

Showing the 10 most recent of 103 reports.

Related aircraft

Show all 8 related aircraft
All 109 registered Bombardier INC CL-600-2C11 aircraft

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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