# N710EV: 2002 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: 10071
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 7, 2024
- Certificate issued: February 12, 2019
- Expires: February 28, 2029
- Mode S code: A97C85
- 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=710EV
- Page: https://openairdocs.org/aircraft/N710EV

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 N710EV.

## FAA accident and incident reports

None matched to N710EV.

## Service difficulty reports (223, 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 SWIA202265928](https://openairdocs.org/sdr/SWIA202265928), May 12, 2022: NONE. WORN. PASSENGER DOOR HINGE (AIRFRAME SIDE) PIN HOLES ARE WORN. (FILED CLOSED)REMOVED AND REPLACED PASSENGER DOOR HINGE (AIRFRAME SIDE) IN REF TO SRM 53-21-23 AND REO 
- [SDR SWIA202265927](https://openairdocs.org/sdr/SWIA202265927), Apr 14, 2022: NONE. CUT. COMPLY WITH REPAIR AUTHORIZATION: RA75921-670-53-21-2206 N710EV MXCODEID60842-PR - PASSENGER DOOR F.S. 310, BETWEEN STRINGER 17 LH AND STRINGER 18LH, REQUIRE FU
- [SDR SWIA202164817](https://openairdocs.org/sdr/SWIA202164817), Dec 13, 2021: NONE. DAMAGED. PASSENGER DOOR F.S. 310, BETWEEN STRINGER 17 LH AND STRINGER 18LH, REQUIRE FURTHER EVALUATION DUE TO DAMAGE. (C-CHECK RO 3/10/2022) REPAIRED DAMAGED PAX DOOR CU
- [SDR SWIA202164816](https://openairdocs.org/sdr/SWIA202164816), Dec 2, 2021: NONE. CORRODED. DURING INSPECTION WAS FOUND CORROSION ON STRINGER 20L AT FS. 310.00 TO FS. 349.00 REQUIRES CLEANING AND EVALUATION. (C-CHECK RO 3/10/2022) REMOVED CORRODED STRI
- [SDR SWIA202164815](https://openairdocs.org/sdr/SWIA202164815), Nov 28, 2021: EXTENSION. CORRODED. FS 863 TO FS 954, LBL 9 FLOOR BEAM UNDER SEAT TRACK SEVERAL SPOTS OF CORROSION. (C-CHECK RO 3/10/2022) REMOVED CORRODED FLOOR BEAM SUPPORT AND REPLACED WITH NEW
- [SDR SWIA202164814](https://openairdocs.org/sdr/SWIA202164814), Nov 18, 2021: FRAME. CORRODED. DURING INSPECTION WAS FOUND CORROSION ON FRAME LOCATION FS 319.00 BETWEEN STGR 21L TO STGR 18L NEED TOBE EVALUATED. (C-CHECK RO 3/10/2022) REMOVED AND REPLACED 
- [SDR SWIA202164813](https://openairdocs.org/sdr/SWIA202164813), Nov 13, 2021: NONE. CORRODED. CORROSION ON STRINGER STRG20R BETWEEN FUSELAGE FS879 THRU FS893 (C-CHECK RO 3/10/2022) REMOVED CORRODED STGR20R FROM FS879-FS893 AND REPLACED WITH NEW STGR SECT
- [SDR SWIA202164812](https://openairdocs.org/sdr/SWIA202164812), Nov 12, 2021: NONE. CORRODED. INTERCOSTAL ON STRG20R FROM FS319 TO FS349, UNDER SERVICE DOOR, CORRODED. FOUND OUT OF LIMITS ON CAMP#23764037, REQUIRES TO BE REPLACED. (C-CHECK RO 3/10/2022) 
- [SDR SWIA202164811](https://openairdocs.org/sdr/SWIA202164811), Nov 12, 2021: NONE. CORRODED. INTERCOSTAL AT STRG20R FROM FS310 TO FS319, UNDER SERVICE DOOR, CORRODED AND OUT OF LIMITS, REF CAMP #23764037. REQUIRES TO BE REPLACED. (C-CHECK RO 3/10/2022) 
- [SDR SWIA202164810](https://openairdocs.org/sdr/SWIA202164810), Nov 9, 2021: NONE. CHAFED. FS 975 - FS 981, STR 27 EXT SKIN DOUBLER CHAFED/GOUGED BY WING TO BODY FAIRINGS 196DL/DR SPLICE STIFFENER. (C-CHECK RO 3/10/2022) REMOVED GOUGED DOUBLER AND TOP
- [SDR SWIA202164809](https://openairdocs.org/sdr/SWIA202164809), Nov 3, 2021: NONE. CORRODED. CORROSION FOUND ON STRINGER STR19 BETWEEN FS333 AND FS349 UNDER SERVICE DOOR. (C-CHECK RO 3/10/2022) REMOVED AND REPLACED SGTR19R FROM FS333-FS349 PER CRJ700 SR
- [SDR SWIA202164808](https://openairdocs.org/sdr/SWIA202164808), Nov 3, 2021: NONE. CORRODED. CORROSION AT FS310 TO FS349 & L/H STRINGER 21LH (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED BACK UP SILL AT FS 310.00 TO FS 349.00 STGR 21L WITH NEW BA
- [SDR SWIA202164807](https://openairdocs.org/sdr/SWIA202164807), Nov 1, 2021: NUT. DENTED. L/H SIDE FUSELAGE FS533, BETWEEN STR16L & 17L DENT; MEASURE AT 7"X 4" ; .012" IN DEPTH; NO ALLOWABLE DAMAGE IN AREA. (C-CHECK RO 3/10/2022) PERFORMED REPAIR ON 
- [SDR SWIA202164806](https://openairdocs.org/sdr/SWIA202164806), Nov 1, 2021: NONE. DENTED. L/H SIDE FUSELAGE FS453, BETWEEN STR14L & 15L DENT; MEASURE AT 3"X 4" .010" DEPTH; NO ALLOWABLE DAMAGE IN AREA. (C-CHECK RO 3/10/2022) PERFORMED REPAIR ON FRAME
- [SDR SWIA202164805](https://openairdocs.org/sdr/SWIA202164805), Nov 1, 2021: NONE. CRACKED. ABOVE FLOOR FS333.00 FRAME CRACKED BEBOW STGR 1RH (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CRACKED FRAME AT FS333 FROM STGR0 TO STGR9R WITH NEW FRAME SECTION
- [SDR SWIA202164804](https://openairdocs.org/sdr/SWIA202164804), Oct 27, 2021: NONE. CRACKED. FORWARD FUSELAGE LEFT WINDSHIELD SUPPORT POST BETWEEN PILOT'S SIDE WINDSLIELD AND FORWARD WINDSHIELD IS CRACKED. (C-CHECK RO 3/10/2022) REMOVED CRACKED PILOT SI
- [SDR SWIA202164803](https://openairdocs.org/sdr/SWIA202164803), Oct 21, 2021: NONE. CORRODED. FS565 AND STGR18L FRAME CORROSION /BARE METAL (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED FRAME AT FS565, STGR18L TO STGR8L REF CRJ700 SRM 51-42-06-001
- [SDR SWIA202164802](https://openairdocs.org/sdr/SWIA202164802), Oct 21, 2021: NONE. CORRODED. FS549 AND STGR18L FRAME CORROSION /BARE METAL (C-CHECK RO 3/10/2022) REMOVED CORRODED FRAME SECTOR AT FS549 FROM STGR9L TO STGR18L AND REPLACED WITH NEW FRAME S
- [SDR SWIA202164801](https://openairdocs.org/sdr/SWIA202164801), Oct 16, 2021: NONE. WORN. RIGHT HAND SLAT NO.# 3 AT SLAT SATATION SS337.66 INBOARD CONNER RUBBING ON TOP OF THE WING LEADING EDGED AREA (C-CHECK RO 3/10/2022) PERFORMED REPAIR TO RIGHT H
- [SDR ASOA201809057164](https://openairdocs.org/sdr/ASOA201809057164), Sep 5, 2018: STRINGER. DAMAGED. TYS-DAMAGED FOUND AT STRINGER 6L, BETWEEN FR 1144.00 AND FR 1162. MAINTENANCE BLENDED THE DAMAGED TO STR 6L AT STA 1144.00 TO 1162.00. PERFORMED A NDT INSPECTIO
- [SDR ASOA201809057163](https://openairdocs.org/sdr/ASOA201809057163), Sep 5, 2018: STRINGER. DAMAGED. DAMAGED FOUND AT STR 7L BETWEED FS 1144-1162. BLENDED DAMAGE TO STR 7L BETWEEN FS 1144-1162. PERFORMED NDI NO DEFECTS FOUND. INSTALLED REPAIR AND RETURNED TO OR
- [SDR ASOA201809057162](https://openairdocs.org/sdr/ASOA201809057162), Sep 5, 2018: STRINGER. DAMAGED. FOUND DAMAGE AT STR 7R BETWEEN FS 1144-1162. BLENDED DAMAGE TO 7R FS 1144-1162. PERFORMED NDI NO DEFECTS FOUND. INSTALLED REPAIR AND RESTORED TO ORIGINL FINISH 
- [SDR ASOA201801255041](https://openairdocs.org/sdr/ASOA201801255041), Jan 25, 2018: CONNECTOR. DAMAGED. DURING MX INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW 9 WAS FOUND INOPERATIVE. MX CRIMPED NEW PINS IN THE CONNECTOR. OPS CHECKED GOOD.
- [SDR ASOA201712075248](https://openairdocs.org/sdr/ASOA201712075248), Dec 7, 2017: STRAP. DAMAGED. REF: CO# EJA150D JOB# EJA050D OP# 51: STRAP LANDING FIXED LEADING EDGE PN CC670-12107-3 REQUIRES FABRICATION DUE TO PART AVAILABILITY.C/A: FABRICATED STRAP LAND
- [SDR ASOA201712075247](https://openairdocs.org/sdr/ASOA201712075247), Dec 7, 2017: STRAP. DAMAGED. REF: CO# EJA150D JOB# EJA050D OP# 49: STRAP LANDING FIXED LEADING EDGE PN CC670-12106-3 REQUIRES FABRICATION DUE TO PART AVAILABILITY.C/A: FABRICATED STRAP LAND
- [SDR ASOA201712075246](https://openairdocs.org/sdr/ASOA201712075246), Dec 7, 2017: RIB. DAMAGED. REF: CO# EJA150D JOB# EJA050D OP# 14: LEFT WING STATION 15.5 RIB IS DAMAGED. C/A: REMOVED AND REPLACED LEFT WING STATION 15.5 RIB IAW CRJ 700 SRM 51-40-11-001-0
- [SDR ASOA201702081298](https://openairdocs.org/sdr/ASOA201702081298), Feb 8, 2017: SMOKE DETECTOR. FAILED. FIRE SYS FAULT STATUS MSG. REMOVED AND REPLACED FWD CARGO SMOKE DET 2 (A227 ) IAW AMM 26-17-01, IPC REF 26-17-01 ITEM 5, OPS CHECK GOOD DEFER CLEARED, PLACARD R
- [SDR ASOA201611076146](https://openairdocs.org/sdr/ASOA201611076146), Nov 7, 2016: CHANNEL. CORRODED. NUT PLATE CHANNEL CORRODED BETWEEN 193AB AND 194AB. COMPLIED WITH EC/TC EA 32-2016-202 AND EA 32-2016-202. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076145](https://openairdocs.org/sdr/ASOA201611076145), Nov 7, 2016: FLOORBEAM. CORRODED. FLOORBEAM CORRODED FS 797-813. COMPLIED WITH EC/TC REO 670-53-41-289 AND REO 670-53-41-289. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076144](https://openairdocs.org/sdr/ASOA201611076144), Nov 7, 2016: SEAT TRACK. CORRODED. RT SEAT RAIL CORRODED FS 785-863. REMOVED RAIL. COMPLIED WITH EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076143](https://openairdocs.org/sdr/ASOA201611076143), Nov 7, 2016: SEAT TRACK. CORRODED. RT SEAT RAIL CORRODED FS 677-708. REMOVED RAIL. C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076142](https://openairdocs.org/sdr/ASOA201611076142), Nov 7, 2016: SEAT TRACK. CORRODED. RT SEAT RAIL CORRODED FS 581-677. REMOVED RAIL. C/W EC/TC REO 670-53-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076141](https://openairdocs.org/sdr/ASOA201611076141), Nov 7, 2016: SEAT TRACK. CORRODED. LT SEAT RAIL CORRODED FS 785-863. REMOVED RAIL. C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076140](https://openairdocs.org/sdr/ASOA201611076140), Nov 7, 2016: SEAT TRACK. CORRODED. LT SEAT RAIL CORRODED FS 708-761. REMOVED RAIL. COMPLIED WITH EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076139](https://openairdocs.org/sdr/ASOA201611076139), Nov 7, 2016: SEAT TRACK. CORRODED. LT SEAT RAIL CORRODED FS 677-708. REMOVED RAIL AND C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076138](https://openairdocs.org/sdr/ASOA201611076138), Nov 7, 2016: DOOR SILL. CORRODED. RT FLOOR SILL CORRODED FS 1000-1080. C/W EC/TC REO 970-53-00-390 AND REO 670 53-00-390. A/C APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076137](https://openairdocs.org/sdr/ASOA201611076137), Nov 7, 2016: DOOR SILL. CORRODED. AFT CARGO FLOOR SILL CORRODED. REMOVED AND REPLACED AFT CARGO FLOOR SILL PER SRM 700 51-42-06-001-001, 51-42-13-001-001. P/N MM670-35655-003 DRAWING MM670-35655
- [SDR ASOA201611076136](https://openairdocs.org/sdr/ASOA201611076136), Nov 7, 2016: FLOORBEAM. CORRODED. FLOORBEAM CORRODED FS 1000-1031. COMPLIED WITH EC/TC 700-53-0356 AND REO 670-53-029.
- [SDR ASOA201611076135](https://openairdocs.org/sdr/ASOA201611076135), Nov 7, 2016: FLOOR SUPPORT. CORRODED. LBL 9 FLOOR SUPPORT CORRODED AT BS 549 - 638. REPAIRED IAW EC/TC EO 700-53-0358 AND EO 700-53-0359. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076134](https://openairdocs.org/sdr/ASOA201611076134), Nov 7, 2016: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT CORRODED AT BS 547. REPAIRED IAW EC/TC REO 970-53-00-390. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076133](https://openairdocs.org/sdr/ASOA201611076133), Nov 7, 2016: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT CORRODED BS 351 RBL 45. REPAIRED IAW EC/TC REO 670-53-00-390. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076132](https://openairdocs.org/sdr/ASOA201611076132), Nov 7, 2016: FRAME. CORRODED. FRAME CORRODED AT BS 333 STRINGER 26-27R. REPAIRED THE FRAME IAW EC/TC 25-2016-247. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076131](https://openairdocs.org/sdr/ASOA201611076131), Nov 7, 2016: DOOR FRAME. CORRODED. LEFT FLIGHT DECK DOOR POST CORRODED AT BOTTOM, BS 280 LBL 9. REPAIRED IAW EC/TC EA 25-2016-248. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076130](https://openairdocs.org/sdr/ASOA201611076130), Nov 7, 2016: BUTTSTRAP. CORRODED. BUTTSTRAP CORRODED FS 280 BETWEEN STRINGERS 26-27L. REPAIRED THE BUTTSTRAP IAW EA 12-2016-146 AND EC/TC EA 12-2016-146. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076129](https://openairdocs.org/sdr/ASOA201611076129), Nov 7, 2016: ANGLE. CORRODED. AVIONICS BAY FLOORBEAM ANGLE ON AFT SIDE OF BS 280 IS CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01 AND DRAWING CC670-34010. AIRCRAFT AP
- [SDR ASOA201611076128](https://openairdocs.org/sdr/ASOA201611076128), Nov 7, 2016: DOUBLER. CORRODED. TCAS ANTENNA DOUBLER CORRODED AT STRINGER 27L BETWEEN BS 295-310. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-001-001-A01 AND 51-42-06-001-001-A01. AIRCRAFT APPR
- [SDR ASOA201611076127](https://openairdocs.org/sdr/ASOA201611076127), Nov 7, 2016: SKIN. DENTED. RIGHT INBD FLAP DENTED. REPAIRED IAW SRM 57-52-01-201-001-A01 REPAIR IV. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201611076126](https://openairdocs.org/sdr/ASOA201611076126), Nov 7, 2016: HEAT SHIELD. DAMAGED. HOLE WORN THROUGH RT ENGINE LOWER CORE COWL INNER HEAT SHIELD. REPAIRED HOLE TO LOWER CORE COWL IAW REO 670-54-23-959 AND ECTC REO 670-54-23-959. AIRCRAFT APPRO
- [SDR ASOA201610180595](https://openairdocs.org/sdr/ASOA201610180595), Oct 18, 2016: CHARGER. INOPERATIVE. DURING MX INSPECTION, THE NR 1 EMERGENCY FLOOD LIGHT WOULD NOT ILLUMINATE. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPS CHECKED GOOD. RETURNED TO SERVIC
- [SDR ASOA201610120835](https://openairdocs.org/sdr/ASOA201610120835), Oct 12, 2016: FLOOR SUPPORT. CORRODED. DURING C CHECK INSPECTION, AFT CARGO FLOOR SUPPORT HAS CORROSION. R & R THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. ACFT WAS APPROVED FOR RETURN TO SERVICE.

All 223: https://openairdocs.org/aircraft/N710EV/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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