# N718EV: 2003 Bombardier CL-600-2C11

- Status: Valid registration
- Airframe: [Bombardier CL-600-2C11](https://openairdocs.org/model/bombardier-cl-600-2c11) (registry code 1390021, 55 seats)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (MHI RJ Aviation ULC) (OpenAirDocs)
- Serial number: 10095
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 6, 2024
- Certificate issued: December 20, 2018
- Expires: December 31, 2028
- Mode S code: A99A3D
- Registered owner: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC)
- Location: [St George, UT](https://openairdocs.org/faa-place/UT/St%20George)
- Owner type: Corporation
- Owner's area on the map: 37.0461° N, 113.5573° W: Placed by OpenAirDocs at the center of ZIP code 84790, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=718EV
- Page: https://openairdocs.org/aircraft/N718EV

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every GE CF34 model are included.

## ADs that may apply (OpenAirDocs): 76 in force

### Matched by airframe (Bombardier CL-600-2C11)

- [AD 2026-15-16](https://openairdocs.org/ad/2026-15-16): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 3 more. Effective Sep 3, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-08-02](https://openairdocs.org/ad/2026-08-02): Stabilizers · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective May 26, 2026
- [AD 2026-05-05](https://openairdocs.org/ad/2026-05-05): Flight controls · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Mar 23, 2026
- [AD 2026-02-03](https://openairdocs.org/ad/2026-02-03): Flight control · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Feb 5, 2026
- [AD 2025-25-03](https://openairdocs.org/ad/2025-25-03): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jan 16, 2026
- [AD 2025-13-04](https://openairdocs.org/ad/2025-13-04): Flight Controls · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Aug 5, 2025
- [AD 2025-11-11](https://openairdocs.org/ad/2025-11-11): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jul 15, 2025
- [AD 2025-09-09](https://openairdocs.org/ad/2025-09-09): Communications · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jun 18, 2025
- [AD 2025-04-08](https://openairdocs.org/ad/2025-04-08): Navigation · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Apr 25, 2025
- [AD 2024-07-08](https://openairdocs.org/ad/2024-07-08): Fuselage · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 3 more. Effective Jun 5, 2024
- [AD 2024-03-02](https://openairdocs.org/ad/2024-03-02): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Apr 9, 2024
- [AD 2023-25-01](https://openairdocs.org/ad/2023-25-01): Equipment/Furnishings · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Feb 6, 2024
- [AD 2023-24-03](https://openairdocs.org/ad/2023-24-03): Fire Protection · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jan 22, 2024
- [AD 2023-19-08](https://openairdocs.org/ad/2023-19-08): Fire Protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Nov 9, 2023
- [AD 2023-10-03](https://openairdocs.org/ad/2023-10-03): Fire Protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jul 11, 2023
- [AD 2023-09-02](https://openairdocs.org/ad/2023-09-02): Fire Protection · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jun 26, 2023
- [AD 2023-07-07](https://openairdocs.org/ad/2023-07-07): Pneumatic · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jun 20, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-06-06](https://openairdocs.org/ad/2023-06-06): Air conditioning · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Apr 28, 2023
- [AD 2022-20-03](https://openairdocs.org/ad/2022-20-03): Oxygen · MHI RJ Aviation ULC CL-600-2C11 (Regional Jet Series 550), CL-600-2C10 (Regional Jet Series 702), CL-600-2C10 (Regional Jet Series 701) and 4 more. Effective Apr 14, 2023
- [AD 2022-24-10](https://openairdocs.org/ad/2022-24-10): Fire protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jan 18, 2023
- [AD 2022-21-10](https://openairdocs.org/ad/2022-21-10): Landing gear · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Dec 21, 2022
- [AD 2022-18-15](https://openairdocs.org/ad/2022-18-15): Fuel · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Nov 25, 2022
- [AD 2022-12-03](https://openairdocs.org/ad/2022-12-03): Navigation System · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Nov 3, 2022
- [AD 2022-13-02](https://openairdocs.org/ad/2022-13-02): Fuel system · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Aug 31, 2022
- [AD 2021-22-24](https://openairdocs.org/ad/2021-22-24): Periodic Inspections · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Dec 29, 2021
- [AD 2021-19-12](https://openairdocs.org/ad/2021-19-12): Landing Gear · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Nov 10, 2021
- [AD 2021-11-02](https://openairdocs.org/ad/2021-11-02): Auto Flight · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jul 13, 2021
- [AD 2021-08-03](https://openairdocs.org/ad/2021-08-03): Rain and Ice Protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective May 25, 2021
- [AD 2021-07-10](https://openairdocs.org/ad/2021-07-10): Ice and Rain Protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 2 more. Effective May 12, 2021
- [AD 2020-21-02](https://openairdocs.org/ad/2020-21-02): Fire protection · Airbus Canada Limited Partnership BD-500-1A10, BD-500-1A11, A330-201 and 45 more. Effective Nov 19, 2020
- [AD 2020-17-15](https://openairdocs.org/ad/2020-17-15): Navigation · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Nov 3, 2020
- [AD 2020-08-13](https://openairdocs.org/ad/2020-08-13): Flight controls · Bombardier CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 5 more. Effective Jun 10, 2020

### Matched by engine (GE CF34 series)

- [AD 2026-21-11](https://openairdocs.org/ad/2026-21-11): Turbine Engine Compressor Section · General Electric Company GE Aerospace CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Nov 27, 2026
- [AD 2025-14-03](https://openairdocs.org/ad/2025-14-03): Turbine Section · General Electric Company GE CF34-10E2A1, CF34-10E6, CF34-10E6A1 and 4 more. Effective Aug 25, 2025
- [AD 2025-12-08](https://openairdocs.org/ad/2025-12-08): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Jul 23, 2025
- [AD 2025-10-04](https://openairdocs.org/ad/2025-10-04): Turbine Section · General Electric Company GE CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 4 more. Effective Jun 26, 2025
- [AD 2023-02-05](https://openairdocs.org/ad/2023-02-05): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 9 more. Effective Mar 14, 2023
- [AD 2022-21-06](https://openairdocs.org/ad/2022-21-06): Turbine Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Nov 15, 2022
- [AD 2022-09-14](https://openairdocs.org/ad/2022-09-14): Compressor Bleed Valve · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Jun 24, 2022
- [AD 2022-08-06](https://openairdocs.org/ad/2022-08-06): Turbine Engine Compression Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Apr 29, 2022
- [AD 2022-05-08](https://openairdocs.org/ad/2022-05-08): Turbine Engine Oil System · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 4 more. Effective Apr 11, 2022
- [AD 2021-26-19](https://openairdocs.org/ad/2021-26-19): Turbine Section · General Electric CF34-8C5, CF34-8C5B1, CF34-8E2 and 6 more. Effective Jan 25, 2022
- [AD 2021-23-51](https://openairdocs.org/ad/2021-23-51): Turbine Engine Compression Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Dec 29, 2021
- [AD 2021-18-13](https://openairdocs.org/ad/2021-18-13): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Oct 22, 2021
- [AD 2020-08-01](https://openairdocs.org/ad/2020-08-01): Turbine Engine Inlet Section · General Electric CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 15, 2020
- [AD 2018-17-14](https://openairdocs.org/ad/2018-17-14): Thrust Reverser · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Nov 7, 2018
- [AD 2018-19-22](https://openairdocs.org/ad/2018-19-22): Turbine Engine Turbine Section · General Electric CF34-10A16, CF34-10E2A1, CF34-10E5 and 5 more. Effective Oct 25, 2018
- [AD 2017-20-09](https://openairdocs.org/ad/2017-20-09): Turbine Engine Bypass Section · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Nov 13, 2017
- [AD 2017-17-18](https://openairdocs.org/ad/2017-17-18): Turbine Engine Compressor Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Oct 6, 2017
- [AD 2013-06-06](https://openairdocs.org/ad/2013-06-06): Operability bleed valves (OBV) · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective May 8, 2013
- [AD 2012-01-10](https://openairdocs.org/ad/2012-01-10): Fan drive shaft · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 4 more. Effective Feb 27, 2012
- [AD 2011-18-02](https://openairdocs.org/ad/2011-18-02): Fan rotor spinner · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 4 more. Effective Sep 26, 2011
- [AD 2009-26-09](https://openairdocs.org/ad/2009-26-09): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Feb 11, 2010
- [AD 2010-01-04](https://openairdocs.org/ad/2010-01-04): Fan blade · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 25, 2010
- [AD 2009-24-06](https://openairdocs.org/ad/2009-24-06): Full authority digital electronic controls · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Dec 28, 2009
- [AD 2009-07-12](https://openairdocs.org/ad/2009-07-12): High-pressure (HP) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 7, 2009
- [AD 2008-05-01](https://openairdocs.org/ad/2008-05-01): Fuel metering units (FMU) · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 8 more. Effective Apr 3, 2008
- [AD 2007-12-15](https://openairdocs.org/ad/2007-12-15): Main fuel pump (MFP) · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 3 more. Effective Jul 19, 2007
- [AD 2007-12-09](https://openairdocs.org/ad/2007-12-09): Combustor case · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 3 more. Effective Jul 10, 2007
- [AD 2006-04-12](https://openairdocs.org/ad/2006-04-12): Stage 5 low pressure turbine (LPT) disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Mar 30, 2006
- [AD 2005-18-16](https://openairdocs.org/ad/2005-18-16): High pressure turbine (HPT) rotating components · General Electric Aircraft Engines CF34-3A1. Effective Oct 13, 2005
- [AD 2005-07-09](https://openairdocs.org/ad/2005-07-09): Master variable geometry (VG) actuators · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Apr 20, 2005
- [AD 2005-07-06](https://openairdocs.org/ad/2005-07-06): Master variable geometry (VG) actuators · General Electric CF34-8C1 and CF34-8C5. Effective Apr 15, 2005
- [AD 2004-26-02](https://openairdocs.org/ad/2004-26-02): Certain high pressure compressor (HPC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 26, 2005
- [AD 2003-05-10 R1](https://openairdocs.org/ad/2003-05-10-R1): B-Sump Scavenge Screens · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Nov 18, 2003
- [AD 2003-09-14](https://openairdocs.org/ad/2003-09-14): Combustion chamber assemblies · General Electric CF34-8C1. Effective Jun 12, 2003
- [AD 2002-23-02](https://openairdocs.org/ad/2002-23-02): Airworthiness Limitations Section (ALS) - Critical Life-Limited Parts · General Electric CF34-8C1. Effective Dec 26, 2002
- [AD 2002-05-02](https://openairdocs.org/ad/2002-05-02): Life-Limited Rotating Parts · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Apr 12, 2002
- [AD 2001-12-06](https://openairdocs.org/ad/2001-12-06): Lubrication System for the Engine Bearings · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jul 20, 2001
- [AD 99-23-26 R1](https://openairdocs.org/ad/99-23-26-R1): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Feb 17, 2000
- [AD 99-22-10](https://openairdocs.org/ad/99-22-10): High Pressure Compressor (HPC) Spool and Disk · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 1 more. Effective Dec 27, 1999
- [AD 97-06-15](https://openairdocs.org/ad/97-06-15): HPC Stage 1 rotor disk · General Electric Aircraft Engines CF34-1A, CF34-3A and CF34-3A2. Effective May 27, 1997
- [AD 97-06-14](https://openairdocs.org/ad/97-06-14): Fan Disk · General Electric Aircraft Engines CF34-1A, CF34-3A and CF34-3A2. Effective May 27, 1997
- [AD 88-06-07](https://openairdocs.org/ad/88-06-07): Fuel Controls · General Electric Aircraft Engines CF34-1A and CF34-3A. Effective Mar 23, 1988

### Historical (superseded or no longer in force)

- [AD 2025-22-02](https://openairdocs.org/ad/2025-22-02) (historical): Stabilizers · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Nov 20, 2025
- [AD 2023-23-02](https://openairdocs.org/ad/2023-23-02) (historical): Flight controls · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jan 18, 2024
- [AD 2019-22-05](https://openairdocs.org/ad/2019-22-05) (historical): Compressor bleed governor · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 3 more. Effective Dec 23, 2019
- [AD 2017-23-06](https://openairdocs.org/ad/2017-23-06) (historical): Compressor bleed governor · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 1 more. Effective Nov 30, 2017
- [AD 2009-24-11](https://openairdocs.org/ad/2009-24-11) (historical): Fan blades · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jan 4, 2010
- [AD 2008-16-01](https://openairdocs.org/ad/2008-16-01) (historical): Full authority digital engine controls (FADECs) · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Aug 15, 2008
- [AD 2007-07-07 R1](https://openairdocs.org/ad/2007-07-07-R1) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Sep 12, 2007
- [AD 2007-07-07](https://openairdocs.org/ad/2007-07-07) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Apr 23, 2007
- [AD 2007-05-16](https://openairdocs.org/ad/2007-05-16) (historical): Fan disks for an arc-out defect · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Mar 12, 2007
- [AD 2007-04-51](https://openairdocs.org/ad/2007-04-51) (historical): Uncontained fan disk failure during flight operation · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1
- [AD 2006-20-06](https://openairdocs.org/ad/2006-20-06) (historical): Main fuel pump (MFP) inlet strainer · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 3 more. Effective Oct 16, 2006
- [AD 2006-05-04](https://openairdocs.org/ad/2006-05-04) (historical): Fan disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Apr 7, 2006
- [AD 2004-15-03 R1](https://openairdocs.org/ad/2004-15-03-R1) (historical): Stage 5 low pressure turbine (LPT) disks · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Aug 31, 2004
- [AD 2004-15-03](https://openairdocs.org/ad/2004-15-03) (historical): Stage 5 Low Pressure Turbine (LPT) Disks · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Aug 16, 2004
- [AD 2004-04-04](https://openairdocs.org/ad/2004-04-04) (historical): Master Variable geometry (VG) actuators · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Mar 9, 2004
- [AD 2003-26-05](https://openairdocs.org/ad/2003-26-05) (historical): Master Variable Geometry (VG) Actuators · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 3 more. Effective Jan 20, 2004
- [AD 2003-05-10](https://openairdocs.org/ad/2003-05-10) (historical): B-sump Oil Scavenge System · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Apr 2, 2003
- [AD 2001-19-02](https://openairdocs.org/ad/2001-19-02) (historical): B-sump Scavenge Screens · General Electric Aircraft Engines CF34-3A1, CF34-3B and CF34-3B1. Effective Oct 9, 2001
- [AD 2000-03-03 R1](https://openairdocs.org/ad/2000-03-03-R1) (historical): Life-limited Parts · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Jun 19, 2001
- [AD 2001-10-03](https://openairdocs.org/ad/2001-10-03) (historical): Fan Disks · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective May 31, 2001
- [AD 2000-03-03](https://openairdocs.org/ad/2000-03-03) (historical): Critical Life-Limited Rotating Engine Parts · General Electric Aircraft Engines CF34-3A1 and CF34-3B1. Effective Mar 13, 2000
- [AD 99-23-26](https://openairdocs.org/ad/99-23-26) (historical): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Dec 6, 1999
- [AD 99-11-08](https://openairdocs.org/ad/99-11-08) (historical): Main Fuel Control (MFC) · General Electric Aircraft Engines CF34-1A, CF34-3A, CF34-3A1 and 3 more. Effective Jul 27, 1999

## Information bulletins (advisory) (1 in force)

- [SAIB NE-04-77](https://openairdocs.org/saib/NE-04-77): . Issued Aug 12, 2004

## NTSB investigations

None matched to N718EV.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20250427008329I](https://openairdocs.org/incident/20250427008329I), Apr 27, 2025: Bombardier Inc CL-600-2C11 (N718EV), Appleton, WI, Minor damage. Aircraft struck a bird during landing which caused damage to the right wing #2 leading edge slat. Aircraft inspected per repair engineering order…

## Service difficulty reports (238, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SWIA2025111200009](https://openairdocs.org/sdr/SWIA2025111200009), Nov 9, 2025: SENSOR. FAULTED. GEAR DISAGREE ON TAKEOFF. NOSE GEAR INDICATOR WAS RED. RAN QRH AND GEAR LOCKED DOWN WITH THREE GREEN DN INDICATORS. (FLIGHT 5998) REF. CP 31173584 FOR TROUBLESH
- [SDR SWIA202157595](https://openairdocs.org/sdr/SWIA202157595), Mar 31, 2021: FLOOR SUPPORT. CORRODED. LBL 9 T-CAP CORRODED NEEDS TO BE REPLACED FROM FS565.00 THRU FS693.00. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED LBL 9 FLOOR BEAM T-CAP FROM FS-565.00 THRU FS
- [SDR SWIA202157594](https://openairdocs.org/sdr/SWIA202157594), Feb 22, 2021: FAIRING. CRACKED. SUPPORT STRUCTURE FOR FAIRING 196AR CRACKED AFT OF FS909.00 LOWER SECTION. REFERENCE STGR24RH. (C-CHECK RO 4/20/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORD
- [SDR SWIA202157593](https://openairdocs.org/sdr/SWIA202157593), Feb 22, 2021: FAIRING. CRACKED. SUPPORT STRUCTURE FOR FAIRING 195AL CRACKED AFT OF FS909.00 LOWER SECTION. REFERENCE STGR24LH. (C-CHECK RO 4/20/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORD
- [SDR SWIA202157592](https://openairdocs.org/sdr/SWIA202157592), Feb 10, 2021: FRAME. CRACKED. POSSIBLE CRACK AT FRAME FS333 BETWEEN STR0 AND STR1 R/H. (C-CHECK RO 4/20/2021) PERFORMED REPAIR IAW REO 670-53-21-1954, SEE ATTACHED FORM M-337.
- [SDR SWIA202157591](https://openairdocs.org/sdr/SWIA202157591), Feb 6, 2021: CHANNEL. CORRODED. FS 1035 TO1045 DOUBLER AND DOME NUTS BETWEEN STR. 27R AND 26R NEEDS CLEANED AND EVALUATED (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED INNER NUT PLATE C
- [SDR SWIA202157590](https://openairdocs.org/sdr/SWIA202157590), Feb 4, 2021: SKIN. DENTED. RIGHT FUSELAGE DENT INSIDE RVSM AREA, LOWER FORWARD BELOW RIGHT TRU DOOR CUT OUT (C-CHECK RO 4/20/2021) COMPLIED WITH REWORK ON DENT ON ADG SKIN PANEL BETWEEN F
- [SDR SWIA202157589](https://openairdocs.org/sdr/SWIA202157589), Jan 29, 2021: ANCHOR FITTING. CORRODED. CORROSION ON TOP SURFACE OF FORWARD CARGO NETTING ANCHOR HOLD DOWNS FS533.00 AND FS581.00. BOTH BETWEEN STRINGERS 23LH AND 22LH. (C-CHECK RO 4/20/2021) REMOVED 
- [SDR SWIA202157588](https://openairdocs.org/sdr/SWIA202157588), Jan 28, 2021: DOUBLER. CORRODED. CORROSION FOUND ON EXTERNAL DOUBLER @ FS 985.00 STGR 26R TO 26L (C-CHECK RO 4/20/2021) REMOVED CORRODED DOUBLER AND TRIPLER FROM F.S. 985.00 STR 26R TO STR26L I
- [SDR SWIA202157587](https://openairdocs.org/sdr/SWIA202157587), Jan 27, 2021: STRINGER. CORRODED. FOUND CORROSION ON STGR 20R @ FS 316.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED STR20R/H FROM FS280 TO FS 319 IAW CRJ700 SRM 51-42-06 AND 51-42-21.
- [SDR SWIA202157586](https://openairdocs.org/sdr/SWIA202157586), Jan 27, 2021: STRINGER. CORRODED. FOUND CORROSION ON STGR 21R AND SPLICE ANGLES @ FS 310.00 TO FS 349.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED SRT 21R/H P/N SH670-31383-1S FROM FS
- [SDR SWIA202157585](https://openairdocs.org/sdr/SWIA202157585), Jan 27, 2021: STRINGER. CORRODED. FOUND CORROSION ON STGR 22R AND SPLICE ANGLES @ FS 319.00 TO FS 349.00 (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED STR22R FROM FS319 TO FS349 IAW CRJ70
- [SDR SWIA202157584](https://openairdocs.org/sdr/SWIA202157584), Jan 26, 2021: BOX BEAM. CORRODED. CORRISION INSIDE OF BOX FRAME ABOVE FWD CARGO DOOR, BETWEEN STR 18 AND 19, F/S 533.00 AND 549.00 (C-CHECK RO 4/20/2021) REPAIRED FWD CARGO DOOR LINTEL DAMAGE AT
- [SDR SWIA202157583](https://openairdocs.org/sdr/SWIA202157583), Jan 26, 2021: FRAME. CORRODED. FS 379.00 FRAME CORRODED BETWEEN STRINGER 22RH AND 20RH. FORWARD OF LAVATORY DRAIN. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED CORRODED FRAME FS379 FROM STR26R
- [SDR SWIA202157582](https://openairdocs.org/sdr/SWIA202157582), Jan 26, 2021: STRINGER. CORRODED. STRINGER 21 LEFT CORREDED BETWEEN FS 310.00 TO FS 319.00. GROUNDING POINTS ON FRAME GS 405 AND GS 445 ARE ALSO CORRODED. (C-CHECK RO 4/20/2021) REMOVED AND REPL
- [SDR SWIA202157581](https://openairdocs.org/sdr/SWIA202157581), Jan 26, 2021: FRAME. CORRODED. CORROSION AT FS 517.00 LOWER FRAME BETWEEN STRINGERS 26LH AND 24RH. (C-CHECK RO 4/20/2021) REMOVED CORRODED LOWER FRAMES AT FS517 L/H AND R/H, FABRICATED AND IN
- [SDR SWIA202157600](https://openairdocs.org/sdr/SWIA202157600), Jan 25, 2021: SEAT TRACK. DAMAGED. RT SIDE SEAT RAIL FS810 NEEDS CLEANING AND EVALUATIONING ( FLAGGED DOT 402 ) (C-CHECK RO 4/20/2021) REMOVED AND REPLACED RH SEAT RAIL AT FS 785.15 THRU FS853.00
- [SDR SWIA202157598](https://openairdocs.org/sdr/SWIA202157598), Jan 25, 2021: SEAT TRACK. DAMAGED. RT SIDE SEAT RAIL FS 785.15 NEED TO BE CLEANED AND EVALUATED ALSO MISSING 2EA FASTENERS ( FLAGGED DOT 401 ) (C-CHECK RO 4/20/2021) REMOVED DAMAGED RH SIDE SEAT 
- [SDR SWIA202157596](https://openairdocs.org/sdr/SWIA202157596), Jan 25, 2021: STRINGER. CORRODED. WING TO BODY FUSELAGE STRINGER @ FS 942.0 HAS CORROSION (C-CHECK RO 4/20/2021) REMOVED DAMAGED ANGLES AND INSTALLED NEW L/H, R/H AND CENTER ANGLES AT WING TO BO
- [SDR SWIA202157580](https://openairdocs.org/sdr/SWIA202157580), Jan 25, 2021: DOOR SILL. CORRODED. FILIFORM CORROSION AND ALUMINUM OXIDE ON THE UPPER SURFACE OF THE INBOARD FLANGE OF THE LOWER SILL OF THE AFT BAGGAGE DOOR FRAME WHERE THE FLOORBOARD OUTBOARD E
- [SDR SWIA202157599](https://openairdocs.org/sdr/SWIA202157599), Jan 15, 2021: VANE. WORN. RIGHT HAND FLAP VANE STOPPER IN THE WING TRAILING EDGE- CENTER AND I/B STOPPER PADS MISSING O/B PAD WORN. (C-CHECK RO 4/20/2021) REMOVED AND REPLACED RIGHT WING
- [SDR SWIA202157597](https://openairdocs.org/sdr/SWIA202157597), Jan 14, 2021: VANE. WORN. LH I/B FLAP VANE STOPPERS IN THE WING TRAILING EDGE- O/B STOPPER PAD WORN AND CENTER AND I/B STOPPER PAD MISSING. (C-CHECK RO 4/20/2021) LH FLAP - REPLACED CENT
- [SDR SWIA202157579](https://openairdocs.org/sdr/SWIA202157579), Jan 13, 2021: INTERCOSTAL. CORRODED. CORROSION FOUND ON INTERCOSTALS FROM FS 295 TO FS 349 ON STRINGER # STGR 19RH BELOW WL 72.00 UNDER THE SERVICE DOOR AREA (C-CHECK RO 4/20/2021) AFTER FURTHER IN
- [SDR ASOA201801135034](https://openairdocs.org/sdr/ASOA201801135034), Jan 13, 2018: DOUBLER. CHAFED. PREVIOUS REPAIR AT F.S. 977.00 STRINGER 27 IS CHAFED. C/A:REO 670-53-00-528 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROU
- [SDR ASOA201801135033](https://openairdocs.org/sdr/ASOA201801135033), Jan 13, 2018: HINGE. GOUGED. PASSENGER DOOR HINGE DOOR SIDE LUGS 2,5,6, AND 12 FROM FRONT ARE GOUGED. REPAIRED THE DOOR HINGE LUGS IAW REO 670-52-11-511, 670-52-11-995, EC/TC REO670-52-11-5
- [SDR ASOA201801115029](https://openairdocs.org/sdr/ASOA201801115029), Jan 11, 2018: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT BETWEEN BS 533 TO 581 IS CORRODED. REPAIRED THE FLOOR SUPPORT IAW REO 670-53-21-1483, AND REO 670-53-21-1483.
- [SDR ASOA201801105028](https://openairdocs.org/sdr/ASOA201801105028), Jan 10, 2018: FRAME. CORRODED. BS 364 FRAME IS CORRODED BETWEEN STRINGERS 25L AND 26R. REMOVED AND REPLACED THE FRAME IAW REO 670-53-21-687, REV, 670-53-21-1481, REV --, REO 670-53-21-687, AN
- [SDR ASOA201801105027](https://openairdocs.org/sdr/ASOA201801105027), Jan 10, 2018: FRAME. CORRODED. BS 280 FRAME WAS CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW REO 670-53-21-1478 AND REO 670-53-21-1478.
- [SDR ASOA201801095026](https://openairdocs.org/sdr/ASOA201801095026), Jan 9, 2018: INTERCOSTAL. CORRODED. INTERCOSTAL AT STRINGER 27L WAS CORRODED BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51
- [SDR ASOA201801095025](https://openairdocs.org/sdr/ASOA201801095025), Jan 9, 2018: INTERCOSTAL. CORRODED. INTERCOSTAL AT STRINGER 27R IS CORRODED BETWEEN BS 349, AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51
- [SDR ASOA201801095024](https://openairdocs.org/sdr/ASOA201801095024), Jan 9, 2018: INTERCOSTAL. CORRODED. LEFT INTERCOSTAL AT STRINGER 26L IS CORRODED BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AN
- [SDR ASOA201801095023](https://openairdocs.org/sdr/ASOA201801095023), Jan 9, 2018: STRINGER SPLICE. CORRODED. STRINGER SPLICE 25R IS CORRODED BETWEEN BS 333 AND 349. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-2
- [SDR ASOA201801065019](https://openairdocs.org/sdr/ASOA201801065019), Jan 6, 2018: FRAME. CORRODED. FRAME BS333 IS CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND REO 670-53-21-799 03.
- [SDR ASOA201801065018](https://openairdocs.org/sdr/ASOA201801065018), Jan 6, 2018: FRAME. CORRODED. FRAME BS 310 IS CORRODED BETWEEN STRINGERS 26L AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND EO 670-53-21-799 01, REV D.
- [SDR ASOA201801055016](https://openairdocs.org/sdr/ASOA201801055016), Jan 5, 2018: FRAME. CORRODED. FRAME BS 319.7 IS CORRODED BETWEEN STRINGERS 27 AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, AND EC/TC REO 670-53-21-799 02.
- [SDR ASOA201801055015](https://openairdocs.org/sdr/ASOA201801055015), Jan 5, 2018: FRAME. CORRODED. FRAME BS 295 IS CORRODED BETWEEN STRINGERS 26L AND 25R. REPAIRED THE FRAME IAW REO 670-53-21-799, AND EC/TC REO 670-53-21-799.
- [SDR ASOA201801045014](https://openairdocs.org/sdr/ASOA201801045014), Jan 4, 2018: BUTTSTRAP. CORRODED. CIRCUMFERENTIAL BUTTSTRAP IS CORRODED AT BS 333 BETWEEN STRINGERS 25L AND 25R. REPAIRED THE CIRCUMFERENTIAL BUTTSTRAP IAW REO 670-53-21-1479, AND EC/TC REO670-5
- [SDR ASOA201801035013](https://openairdocs.org/sdr/ASOA201801035013), Jan 3, 2018: STRINGER. CORRODED. STRINGER 25R CORRODED BETWEEN BS 333 AND 364. REMOVED AND REPLACED THE STRINGER 25R IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01
- [SDR ASOA201801035012](https://openairdocs.org/sdr/ASOA201801035012), Jan 3, 2018: STRINGER. CORRODED. STRINGER 25L IS CORRODED BETWEEN BS 280 AND 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR ASOA201801035011](https://openairdocs.org/sdr/ASOA201801035011), Jan 3, 2018: STRINGER. CORRODED. STRINGER 26R IS CORRODED BETWEEN BS 333 AND 364. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR ASOA201801035010](https://openairdocs.org/sdr/ASOA201801035010), Jan 3, 2018: STRINGER. CORRODED. STRINGER 25R IS CORRODED BETWEEN BS 295 AND 310. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR ASOA201801035009](https://openairdocs.org/sdr/ASOA201801035009), Jan 3, 2018: STRINGER. CORRODED. STRINGER 26R IS CORRODED BETWEEN BS 295 AND 310. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR ASOA201812305006](https://openairdocs.org/sdr/ASOA201812305006), Dec 30, 2017: INTERCOSTAL. CORRODED. RT INTERCOSTAL AT STRINGER 26R IS CORRODED BETWEEN FS 349.00 AND FS 364.00. REMOVED AND REPLACED INTERCOSTAL P/N SH670-32077-4 IAW SRM 51-40-11-001-001-A01 AND 
- [SDR ASOA201812295005](https://openairdocs.org/sdr/ASOA201812295005), Dec 29, 2017: STRINGER. CORRODED. STRINGER 27 FWD SEGMENT FS 310.00-333.00, AFT SEGMENT FS. 333.00-349.00 AND STRINGER SPLICE AT FS 333.00 ARE CORRODED. REMOVED AND REPLACED STRINGER 27 FWD SEGM
- [SDR ASOA201812295004](https://openairdocs.org/sdr/ASOA201812295004), Dec 29, 2017: DOUBLER. CRACKED. RT FORWARD EQUIPMENT COMPARTMENT FLOOR PREVIOUS REPAIR IS CRACKED AT BS 193. REMOVED AND REPLACED THE REPAIR DOUBLER IAW REOS 670-53-11-509, 670-53-11-1355, AND
- [SDR ASOA201812285003](https://openairdocs.org/sdr/ASOA201812285003), Dec 28, 2017: DOOR FRAME. CRACKED. RIGHT FORWARD EQUIPMENT COMPARTMENT DOOR LANDING IS CRACKED IN TWO LOCATIONS NEAR FWD AND AFT DOOR LATCHES. REMOVED AND REPLACED THE DOOR LANDING IAW SRM 51-40-
- [SDR ASOA201812285002](https://openairdocs.org/sdr/ASOA201812285002), Dec 28, 2017: DOOR FRAME. CRACKED. LEFT FORWARD EQUIPMENT BAY DOOR LANDING IS CRACKED NEAR AFT DOOR LATCH. REMOVED AND REPLACED THE DOOR LANDING IAW SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01
- [SDR ASOA201812205001](https://openairdocs.org/sdr/ASOA201812205001), Dec 20, 2017: BRACKET. CORRODED. WEB PROTECTOR BRACKETS ON GALLEY SERVICE DOOR FLOOR SUPPORT ARE CORRODED. REMOVED AND REPLACED THE BRACKETS IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 
- [SDR ASOA201712205254](https://openairdocs.org/sdr/ASOA201712205254), Dec 20, 2017: ANGLE. CORRODED. BS 280 J ANGLE IS CORRODED ON UPPER FLANGE BETWEEN LBL 11 AND RBL 11. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-
- [SDR ASOA201812165020](https://openairdocs.org/sdr/ASOA201812165020), Dec 16, 2017: FLOOR SUPPORT. CORRODED. RIGHT SIDE FLOOR SUPPORT IS CORRODED BETWEEN BS 280 BULKHEAD TO BS 319. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRMS 51-42-06-001-001-A01, 51-42-21-001-001-A

All 238: https://openairdocs.org/aircraft/N718EV/reports.md

## STCs that may be installed (OpenAirDocs) (18)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Bombardier CL-600-2C11)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST04755NY](https://openairdocs.org/stc/ST04755NY): Installation of the SpaceX Starlink Aviation System. Space Exploration Technologies Corp. / Starlink Aviation
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST04790NY](https://openairdocs.org/stc/ST04790NY): Installation Bruce Cabin Lighting. Delta Engineering Corporation
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc
- [STC ST04201AT](https://openairdocs.org/stc/ST04201AT): Installation of the Avionics Innovations DMP500 PRAM (Pre-Recorded Announcement Machine). Chippewa Aerospace Inc
- [STC SA02358LA](https://openairdocs.org/stc/SA02358LA): Installation of Main Landing Gear Wire Harness Assemblies. NIACC Avitech Technologies
- [STC ST04839NY](https://openairdocs.org/stc/ST04839NY): Installation of LED Position/Anti-Collision Lights. Sterling Helicopter
- [STC ST03034AT](https://openairdocs.org/stc/ST03034AT): Installation of the Honeywell Dual Laser Ref V Inertial Reference System (IRU’s). Chippewa Aerospace, Inc
- [STC ST02800LA](https://openairdocs.org/stc/ST02800LA): Installation of USB Ports Type A and Type C and Power Inverters in the cabin. U.S. Technical Consultants Inc
- [STC ST03663AT](https://openairdocs.org/stc/ST03663AT): Installation of an Artex C406-2 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST04418NY](https://openairdocs.org/stc/ST04418NY): Installation of the Three Cabin Class Configuration. GAL Aviation
- [STC ST03336AT](https://openairdocs.org/stc/ST03336AT): Installation of LRU Avionics Protective Covers. Chippewa Aerospace Inc
- [STC SA03642AT](https://openairdocs.org/stc/SA03642AT): Installation of Michelin's tires P/N 029-901-0 on the main gear and P/N 036-897-0 on the nose gear of Bombardier CL-600-2C10/2D15/2D24 aircraft wheel assembly. Michelin North America Inc
- [STC ST03651NY](https://openairdocs.org/stc/ST03651NY): Installation of the Transponder Upgrade for ADS-B Out. Avmax Aviation Services Inc

### Approved for the engine (GE CF34 series)

- [STC SE01271LA](https://openairdocs.org/stc/SE01271LA): Installation of anti-ice shut-off/regulator valve p/n 5399-00-1. Dukes Inc. Lists CF34-3A1

## Related

- Other Bombardier CL-600-2C11 aircraft: https://openairdocs.org/model/bombardier-cl-600-2c11/aircraft.md
- The GE CF34 series engine: https://openairdocs.org/engine/ge-cf34-series.md

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