# N707EV: 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: 10057
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 8, 2024
- Certificate issued: August 4, 2020
- Expires: August 31, 2027
- Mode S code: A96F07
- 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=707EV
- Page: https://openairdocs.org/aircraft/N707EV

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ENG26LA011](https://openairdocs.org/ntsb/ENG26LA011), Nov 23, 2025: Bombardier CL-600-2C11 (N707EV), Hibbing, MN, incident, no damage. Probable cause: The elevator control restriction was caused by the failure of an elevator autopilot servo control cable which failed due to cyclic fatigue. The slack in the cable wrapped around the servo mount in…

## 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 20251123020789I](https://openairdocs.org/incident/20251123020789I), Nov 23, 2025: Bombardier Inc CL-600-2C11 (N707EV), Hibbing, MN, No damage. On 11/23/2025 a CRJ550 aircraft en-route from minneapolis, MN (msp) to Range Regional Airport, Hibbing, MN (hib) encountered autopilot anomalies and a loss of…

## Service difficulty reports (227, 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 SWIA2026050176636](https://openairdocs.org/sdr/SWIA2026050176636), May 1, 2026: BULKHEAD WEB. CORRODED. UPON REMOVAL OF THE BS 280 CROSSBEAM LT THE COCKPIT BULKHEAD LOWER WEB HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE CROSSBEAM, THE COCKPIT BULKHEAD LOWER WE
- [SDR SWIA2026041676633](https://openairdocs.org/sdr/SWIA2026041676633), Apr 16, 2026: POST. CORRODED. FLIGHT COMPARTMENT LT DOOR POST HAS SIGNS OF CORROSION. PERFORMED REPAIR AT FLIGHT COMPARTMENT LT DOOR POST IAW SRM 53-00-00, & 51-21-11, 51-25-06, IAW AMM 20-7
- [SDR SWIA2026030576627](https://openairdocs.org/sdr/SWIA2026030576627), Mar 5, 2026: DOOR FRAME. GOUGED. NLG AFT DOOR CUTOUT ON LH SIDE EDGE IS GOUGED. REMOVED, EVALUATED AND REPAIRED DAMAGE ON LT SIDE EDGE AT NLG AFT DOOR CUTOUT IAW REO 670-53-11-2318 REV -- AND S
- [SDR SWIA2026030476630](https://openairdocs.org/sdr/SWIA2026030476630), Mar 4, 2026: FRAME. FOM. FRAME AT BS 333. REQUIRES CUT OUT DUE TO MULTIPLE STRINGER REPLACEMENTS. PERFOMED REPAIR AT FRAME BS 333 IAW AMM 20-70-00, SRM 51-42-06, 51-42-13, 51-42-21, IAW
- [SDR SWIA2026022776624](https://openairdocs.org/sdr/SWIA2026022776624), Feb 27, 2026: PLATE. CRACKED. AFT EQUIPMENT BAY LH PROTECTIVE PLATE ABOVE COCKPIT VOICE RECORDER IS CRACKED. REMOVED AND REPAIRED DAMAGE ON AFT EQUIPMENT BAY LT PROTECTIVE ABOVE COCKPIT VOIC
- [SDR SWIA2026012776639](https://openairdocs.org/sdr/SWIA2026012776639), Jan 27, 2026: STRUCTURE. CORRODED. RBL9 SIGNS OF CORROSION FROM BS 6770 TO 693. BLENDED OUT AND EVALUATED DAMAGE ON FLOOR SUPPORT AND BULKHEAD BEAM AT RBL9 BETWEEN F.S.677 TO 693, REWORKED CONDIT
- [SDR SWIA2026012776637](https://openairdocs.org/sdr/SWIA2026012776637), Jan 27, 2026: SUPPORT. CORRODED. MULTIPLE NUTPLATE HOLES HAVE SIGNS OF CORROSION ON LBL9 FROM FS579.00 TO FS661. REPAIRED DAMAGE AROUND NUTPLATE HOLES ON LBL 9 FROM BS 579 TO BS 661 IAW REO 670
- [SDR SWIA2026012776634](https://openairdocs.org/sdr/SWIA2026012776634), Jan 27, 2026: STRINGER. CORRODED. STRINGER 19R SIGNS OF CORROSION BETWEEN BS 437 TO 453 UNDER FLOORBOARD 252CFR. REMOVED AND REPLACED STR 19R BETWEEN BS 349 TO 485 IAW SRM 53-21-03, 51-42-06, 51
- [SDR SWIA2026012776631](https://openairdocs.org/sdr/SWIA2026012776631), Jan 27, 2026: STRINGER. CORRODED. AVIONICS BAY STR 24R BETWEEN BS 333 - 364 HAS MULTIPLE SIGNS OF CORROSION. REPAIRED DAMAGE ON AVIONICS BAY STRG 24R BETWEEN FS 333 AND FS 364 IAW REO 670-53-21-
- [SDR SWIA2026012776626](https://openairdocs.org/sdr/SWIA2026012776626), Jan 27, 2026: FLOOR SUPPORT. CORRODED. ON RBL9, MULTIPLE NUTPLATE HOLES HAVE SIGNS OF CORROSION FROM BS 613 TO 693. BLENDED OUT AND EVALUATED DAMAGE ON FLOOR SUPPORT AT RBL9 BETWEEN BS 613 TO 693, RE
- [SDR SWIA2026012276628](https://openairdocs.org/sdr/SWIA2026012276628), Jan 22, 2026: STRINGER. CORRODED. SIGNS OF CORROSION ON STGR 26R AT F.S.1047.0, JUST FORWARD AND TO THE RIGHT OF THE POTABLE WATER TANK. REMOVED AND REPLACED REPAIR SPLICE, REPAIR FILLER, REPAIR
- [SDR SWIA2026011976638](https://openairdocs.org/sdr/SWIA2026011976638), Jan 19, 2026: STRINGER. CORRODED. SIGNS OF CORROSION IN THE FORWARD CARGO BAY AT BS 581, STGR 22LH ON THE STRINGER FOOT. PERFORMED REPAIR IN THE FORWARD CARGO BAY AT BS 581 STGR 22L ON THE STRIN
- [SDR SWIA2026011976625](https://openairdocs.org/sdr/SWIA2026011976625), Jan 19, 2026: SHEAR TIE. CORRODED. SIGNS OF CORROSION IN THE FWD CARGO BAY AT BS 549, S26L, ON FRAME FOOT OF FRAME 549. PERFORMED REPAIR ON FWD CARGO BAY AT BS 549 ON FRAME BETWEEN STGR 26L AND S
- [SDR SWIA2026011776629](https://openairdocs.org/sdr/SWIA2026011776629), Jan 17, 2026: HINGE. GOUGED. PAX DOOR PIANO HINGE HAS MULTIPLE LUGS WITH GOUGES DOWN ENTIRE LENGTH FUSELAGE SIDE. BLENDED AND REMOVED DAMAGE ON PAX DOOR HINGE LUGS IAW REO 670-53-21-582, RE
- [SDR SWIA2026011176635](https://openairdocs.org/sdr/SWIA2026011176635), Jan 11, 2026: FLOORBEAM. CRACKED. LBL 12 COCKPIT FLOORBEAM IS CRACKED AT BS 280 ATTACH POINT. PERFORMED REPAIR ON LBL 12 COCKPIT FLOORBEAM IAW REO 670-53-11-896, REV --, AMM 20-70-00, AND SRM 51
- [SDR SWIA2026010876641](https://openairdocs.org/sdr/SWIA2026010876641), Jan 8, 2026: WEB. CRACKED. FWD EQUIPMENT COMPARTMENT LT FLOOR WEB CRACKED BY THE BRAKE ACCUMULATOR GAUGES. PERFORMED REPAIR ON FWD EQUIPTMENT COMPARTMENT LT FLOOR WEB IAW REO 670-53-11-50
- [SDR SWIA2026010876623](https://openairdocs.org/sdr/SWIA2026010876623), Jan 8, 2026: WEB. CRACKED. FWD EQUIPMENT COMPARTMENT RT SIDE FLOOR WEB REPAIR DOUBLER UNDER ADG PUMP APPEARS TO BE CRACKED. REMOVED AND REPLACED DOUBLER AT FWD EQUIPMENT COMPARTMENT RT SI
- [SDR SWIA2025111876640](https://openairdocs.org/sdr/SWIA2025111876640), Nov 18, 2025: SKIN. DENTED. COMPLY WITH PERMANENT REPAIR ON RA 78977, FOUND DENT ON EXTERIOR OF FUSELAGE AT INTERSECTION OF BS 501 AND STR 21R. COMPLIED WITH TEMPORARY REPAIR PER REO670-53
- [SDR SWIA2025111876632](https://openairdocs.org/sdr/SWIA2025111876632), Nov 18, 2025: SKIN. DENTED. FOUND DENT ON EXTERIOR OF FUSELAGE 2 INCHES FWD OF BS2 80 AND 1 INCH ABOVE STGR 26R. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-11-1678 REV A DATED 2022-06-0
- [SDR SWIA202307050626](https://openairdocs.org/sdr/SWIA202307050626), Jun 26, 2023: UNKNOWN. UNKNOWN. GEAR DID NOT RETRACT ON TAKE OFF. WE RECEIVED GEAR DISAGREE WARNING MSG. COMPLIED WITH QRH PROCEDURE. PROX SYS FAULT STATUS MSG WAS PRESENT WITH GEAR DOWN BUT A
- [SDR SWIA20230627006](https://openairdocs.org/sdr/SWIA20230627006), Jun 26, 2023: UNKNOWN. UNKNOWN. GEAR DID NOT RETRACT ON TAKE OFF. WE RECEIVED GEAR DISAGREE WARNING MSG. COMPLIED WITH QRH PROCEDURE. PROX SYS FAULT STATUS MSG WAS PRESENT WITH GEAR DOWN BUT A
- [SDR SWIA2023062603](https://openairdocs.org/sdr/SWIA2023062603), Jun 23, 2023: UNKNOWN. DID NOT STOW. DURING TAKEOFF, TRIPLE CHIME AND GEAR DISAGREE DURING GEAR RETRACTION, NOSE GEAR DID NOT SHOW RETRACTED. COMPLIED WITH QRH PROCEDURE, GEAR DISAGREE MESSAGE DISA
- [SDR SWIA202306150014](https://openairdocs.org/sdr/SWIA202306150014), Jun 14, 2023: UNKNOWN. DAMAGED. DAMAGE ON RH SIDE OF AIRCRAFT FUSELAGE BETWEEN FS333.00 AND FS349.00, BETWEEN STGR19R AND STGR21RTHIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 IS RE
- [SDR SWIA202162959](https://openairdocs.org/sdr/SWIA202162959), Dec 3, 2021: NONE. DAMAGED. REF CP 23937463 FOR ORIGINAL DISCREPANCY AND CP23943655 FOR DAMAGE DETERMINATION. FOUND TWO HOLES TO BE ELONGATED WHILE REMOVING THE PAX DOOR AFT SEAL RETAINER 
- [SDR SWIA2021092961356](https://openairdocs.org/sdr/SWIA2021092961356), Sep 28, 2021: TERMINAL. LOOSE. SMELL OF ELECTRICAL SMOKE DETECTED AROUND FL220. AT FL280, SMELL INTENSIFIED AND SMOKE SEEN AROUND WINDOW HEAT IN CA SIDE. (FLIGHT 3084) THIS DISCREPANCY WAS TR
- [SDR SWIA2021092961238](https://openairdocs.org/sdr/SWIA2021092961238), Sep 27, 2021: FILTER. OBSTRUCTED. DURING CLIMB OUT FROM DFW A VERY INTENSE ELECTRICAL BURNING SMELL ENTERED THE FLIGHT DECK. (FLIGHT 3243 - FILED CLOSED) PLEASE REFERENCE AML 743123 PLEASE REFER
- [SDR SWIA2021091561080](https://openairdocs.org/sdr/SWIA2021091561080), Sep 10, 2021: DOUBLER. CRACKED. LH UPPER TRANS COWL €“ POSSIBLE CRACK ON DOUBLER FOR FWD LATCH CUTOUT (FILED CLOSED) REMOVED AND REPLACED DOUBLER FOR FWD LATCH CUTOUT ON LH UPPER TRANSCOWL IN
- [SDR SWIA202154935](https://openairdocs.org/sdr/SWIA202154935), Jan 2, 2021: SMOKE WARNING. FALSE ACTIVATION. WHILE ON LEFT DOWNWIND, THE SMOKE AFT LAV WARNING LIGHT ILLUMINATED. WE ELECTED TO LAND AND THEN RAN THE QRH. NO EVIDENCE OF ANY SMOKE WAS FOUND. RAN THE QRH AN
- [SDR N6WA20200410701](https://openairdocs.org/sdr/N6WA20200410701), Apr 7, 2020: FRAME. CRACKED. DURING SCHEDULED MAINTENANCE IN THE GOJET MAINTENANCE FACILITY IN ST LOUIS INT’L AIRPORT, ST. LOUIS, MO (STL) THE FUSELAGE FRAME UPPER SECTOR AT FS 333.00 BETWE
- [SDR ASOA201809267169](https://openairdocs.org/sdr/ASOA201809267169), Sep 26, 2018: BRAKE. DRAGGING. TYS A/C WAS LANDING WHEN THE RIGHT MAIN OUTBOARD TIRE BLEW OUT. MAINTENANCE FOUND THE NR 4 BRAKE TO BE DRAGGING. MAINTENANCE REMOVED AND REPLACED THE NR 4 BRAKE
- [SDR ASOA201804215108](https://openairdocs.org/sdr/ASOA201804215108), Apr 21, 2018: BULB. INOPERATIVE. PILOT REPORTED OVERHEAD EMERGENCY LIGHTS AT ROWS 9 AND 15 WERE INOPERATIVE. REMOVED AND REPLACED THE BULBS, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SE
- [SDR ASOA20161105207](https://openairdocs.org/sdr/ASOA20161105207), Nov 5, 2016: FLOORBEAM. CORRODED. DURING C CHECK, FOUND FLOORBEAM ANGLE CORRODED BEYOND LIMITS AT FS 280. REMOVED AND REPLACED FLOOBEAM ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 
- [SDR ASOA201610250615](https://openairdocs.org/sdr/ASOA201610250615), Oct 25, 2016: BATTERY. DISCHARGED. CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT TURN ON. THE EMERGENCY LIGHT SYSTEM WAS CHARGED AND FAULT NO LONGER EXIST. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2016051914841](https://openairdocs.org/sdr/ASOA2016051914841), May 19, 2016: FITTING. CRACKED. WHILE WORKING INTERCOSTAL REPAIR AT FS 280, FS 265, RBL1, FOUND FWD JACK FITTING TO BE CRACKED. REMOVED LT & RT ANGLE FROM FS 280.00 AND FROM LT & RT SUPPORTS B
- [SDR ASOA2016051614859](https://openairdocs.org/sdr/ASOA2016051614859), May 16, 2016: RETAINER. CORRODED. AVIONICS BAY DOOR SEAL RETAINER AREAS HAS EXFOLICATED CORROSION. REMOVED DOOR SEAL, DAMAGED IAW AMM 52-42-07-000-801-A01. INSTALLED NEW AVIONICS DOOR SEAL IAW A
- [SDR ASOA2016051614855](https://openairdocs.org/sdr/ASOA2016051614855), May 16, 2016: SUPPORT. CRACKED. DURING REPAIR OF AFT BAGAGE BAY DOOR SILL STRUCTURE FOUND THE MACHINED FITTING SUPPORTING THE SILL AT FS101.5, CRACKED. REMOVED MACHINED FITTING . FITTING SPLIC
- [SDR ASOA2016050214854](https://openairdocs.org/sdr/ASOA2016050214854), May 2, 2016: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON LT FLOOR SILL AT FS 761.93 & 785.07. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2016-079. RECIEVED & COMPLIED WITH E
- [SDR ASOA2016042914853](https://openairdocs.org/sdr/ASOA2016042914853), Apr 29, 2016: FRAME. CORRODED. CORROSION WAS DISCOVERED ON LT FUSELAGE FRAME 549 BELOW FLOOR SILL. RECEIVED REO 670-53-31-367. REO 53-31-367 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCU
- [SDR ASOA2016042514858](https://openairdocs.org/sdr/ASOA2016042514858), Apr 25, 2016: INTERCOSTAL. CORRODED. INTERCOSTAL LBL1 FS 280-265 HAS CORROSION, NOSE JACK FITTING. REMOVED INTERCOSTAL SUPPORT LBL1 BETWEEN FS280.00 AND FS265.00 REF SRM 51-42-06-001-001-A01, 51-42
- [SDR ASOA2016042514852](https://openairdocs.org/sdr/ASOA2016042514852), Apr 25, 2016: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON RBL9 FLOORBEAM AT FS 1015.00, SAND 1031.00. REMOVED CORROSION ON RBL9, FLOORBEAM AT FS 1015.00 AND 1031.00 IAW SRM 51-21-06-001-001 A01. REPA
- [SDR ASOA2016042514851](https://openairdocs.org/sdr/ASOA2016042514851), Apr 25, 2016: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON LBL 27 FLOOR SUPPORT AT BS 1000, 1015, 1031. REMOVED CORROSION ON LBL27, FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01. REPAIRED FLOOR SUPPORT I
- [SDR ASOA2016042514850](https://openairdocs.org/sdr/ASOA2016042514850), Apr 25, 2016: FLOORBEAM. CORRODED. CORRISON FOUND ON LBL 9, FLOORBEAM AT FS 1031.00. REMOVED CORROSION ON LBL9 FLOOR BEAM AT FS 1031.00 IAW SRM 51-21-06-001-001, A01. REMOVED DAMAGED SECTION OF F
- [SDR ASOA2016042514849](https://openairdocs.org/sdr/ASOA2016042514849), Apr 25, 2016: FRAME. CORRODED. 349 FRAME HAS CORROSION LBL2-STR 26R. REMOVED RT SIDE SEAT RAIL AT FS 565-677 IAW AMM 53-00-49-000-801-A01. INSTALLED NEW RT SIDE SEAT RAIL AT FS 565-677 IAW AM
- [SDR ASOA2016042514846](https://openairdocs.org/sdr/ASOA2016042514846), Apr 25, 2016: INTERCOSTAL. CORRODED. INTERCOSTAL CORRODED FS 349-364, LBL2. REMOVED INTERCOSTAL AT 349-364 LBL2 IAW SRM 51-42-06-001-001 A01 & 51-42-21-001-001 A01. DRILLED NEW INTERCOSTAL IAW SRM 
- [SDR ASOA2016042514845](https://openairdocs.org/sdr/ASOA2016042514845), Apr 25, 2016: INTERCOSTAL. CORRODED. INTERCOSTAL RBL1 FS 280-265 HAS CORROSION, AT NOSE JACK FITTING. REMOVED INTERCOSTAL RBL1, BETWEEN FS 265.00 AND 280.00, REF SRM 51-42-06-001-001-A01, 51-42-21-
- [SDR ASOA2016042514819](https://openairdocs.org/sdr/ASOA2016042514819), Apr 25, 2016: STRUCTURE. CORRODED. PACKER CORRODED AT RBL 9, FS 333.00. R & R PACKER AT RBL 9, FS 333.0 IAW AMM 51-42-06-001-001 A01.
- [SDR ASOA2016042514818](https://openairdocs.org/sdr/ASOA2016042514818), Apr 25, 2016: INTERCOSTAL. CORRODED. INTERCOSTAL CORRODED FS 349-364, RBL2. REMOVED INTERCOSTAL AT 349-364, RBL2 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. DRILLED NEW INTERCOSTAL IAW SRM
- [SDR ASOA2016042514817](https://openairdocs.org/sdr/ASOA2016042514817), Apr 25, 2016: FLOORBEAM. CORRODED. AVIONIC BAY CRAWL WAY FLOOR SUPPORT HAS CORROSION AT FS 280. REMOVED CORRODED CRAWLWAY SUPPORT IAW SRM 57-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NE
- [SDR ASOA2016042514816](https://openairdocs.org/sdr/ASOA2016042514816), Apr 25, 2016: SUPPORT. CRACKED. CRACK FOUND ON LT AFT WING TO FUSELAGE FAIRING SUPPORT DIAPHRAGM LBL17.63, FS 923.00. REPAIRED WING TO FUSELAGE AFT FAIRING SUPPORT FS 909.00, LBL 17.63 OR RBL 
- [SDR ASOA2016042214848](https://openairdocs.org/sdr/ASOA2016042214848), Apr 22, 2016: SEAT TRACK. CORRODED. RIGHT SIDE SEAT TRACK FS 565 - FS 677 HAS CORROSION DAMAGE. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A01. INSTALLED NEW RT SIDE SEAT TRACK IAW AMM 53

All 227: https://openairdocs.org/aircraft/N707EV/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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