General Electric CT7-2F1
Active General Electric CT7-2F1 turboshaft variant certified for the Bell 525 Relentless super-medium helicopter. Bell current specifications list 1,714 shp (1,278 kW) maximum continuous uninstalled thermodynamic capability, 1,979 shp (1,476 kW) takeoff capability, and 2,129 shp (1,588 kW) 30-second OEI capability; the typed shaft-power field remains the maximum-continuous 1,278 kW value.
Identity
- Aliases
- CT7-2F1GE CT7-2F1CT7-2F1 Turboshaft
- Domains
- aviation
- Identity Level
- variant
- Kind
- turboshaft
- Name
- General Electric CT7-2F1
- Status
- active
Details
- Air Breathing Specs
- Shaft Power
- …
- Description
- Active General Electric CT7-2F1 turboshaft variant certified for the Bell 525 Relentless super-medium helicopter. Bell current specifications list 1,714 shp (1,278 kW) maximum continuous uninstalled thermodynamic capability, 1,979 shp (1,476 kW) takeoff capability, and 2,129 shp (1,588 kW) 30-second OEI capability; the typed shaft-power field remains the maximum-continuous 1,278 kW value.
- Developers
- Family
- Manufacturers
Links
Assets & Meta
- Creation Time
- August 13, 2026 at 19:33:27 UTC
- Updated Time
- August 21, 2026 at 08:22:28 UTC
Other
- Sources
- Accessed Date
- 2026-08-13
- Note
- GE records FAA certification of the CT7-2F1 engine for Bell 525 operations.
- Publisher
- GE Aerospace
- Title
- CT7-2F1 engine receives FAA certification
- Accessed Date
- 2026-08-13
- Note
- GE identifies CT7-2F1 as the 2,000-shp-class engine selected for Bell 525.
- Publisher
- GE Aerospace
- Title
- CT7 Engines to Power Bell 525 Relentless Helicopter
- Accessed Date
- 2026-08-13
- Note
- Bell specification lists two GE CT7-2F1 engines with FADEC for Bell 525.
- Publisher
- Bell Textron
- Title
- BELL 525 specifications
- Accessed Date
- 2026-08-21
- Note
- Bell current product information lists CT7-2F1 maximum continuous capability at 1,714 shp / 1,278 kW, takeoff capability at 1,979 shp / 1,476 kW, and two engines with dual FADEC.
- Publisher
- Bell Textron
- Title
- Bell 525 — Applied Technology for Energy Missions