Honeywell T55-L-714C
Honeywell T55-L-714C is a T55-family turboshaft in the 6,000-shaft-horsepower class for commercial and military helicopters. Honeywell technical material describes the T55 architecture with a seven-stage axial compressor and two-stage gas-producer turbine; its current T55 product page presents the 714C as a current enhancement/upgrade for the 714A with a 15,066 rpm output shaft. The structured shaft-power value is normalized to 4,474 kW from 6,000 shaft horsepower, and the active status reflects current Honeywell product and upgrade support.
Identity
- Aliases
- T55-L-714C
- Domains
- aviation
- Identity Level
- model
- Kind
- turboshaft
- Name
- Honeywell T55-L-714C
- Status
- active
Details
- Air Breathing Specs
- Shaft Power
- …
- Description
- Honeywell T55-L-714C is a T55-family turboshaft in the 6,000-shaft-horsepower class for commercial and military helicopters. Honeywell technical material describes the T55 architecture with a seven-stage axial compressor and two-stage gas-producer turbine; its current T55 product page presents the 714C as a current enhancement/upgrade for the 714A with a 15,066 rpm output shaft. The structured shaft-power value is normalized to 4,474 kW from 6,000 shaft horsepower, and the active status reflects current Honeywell product and upgrade support.
- Developers
- Family
- Manufacturers
Links
Assets & Meta
- Creation Time
- August 13, 2026 at 18:28:33 UTC
- Updated Time
- August 23, 2026 at 20:12:15 UTC
Other
- Sources
- Accessed Date
- 2026-08-13
- Note
- Lists T55-L-714C as a distinct 6,000-shaft-horsepower-class turboshaft rating for commercial and military helicopters; no exact lifecycle or airframe installation is asserted.
- Published Date
- 2022
- Publisher
- Honeywell Aerospace
- Title
- Honeywell T55 Turboshaft Engine
- Accessed Date
- 2026-08-22
- Note
- Honeywell’s T55 brochure table lists the T55-L-714C as a commercial and military helicopter turboshaft in the 6,000-shaft-horsepower class; this record stores the normalized equivalent of 4,474 kW.
- Publisher
- Honeywell Aerospace
- Title
- Honeywell T55 Turboshaft Engine
- Accessed Date
- 2026-08-23
- Note
- Honeywell’s current T55 product page presents the 714C as a 6,000-shaft-horsepower-class enhancement/upgrade for the 714A and lists a 15,066 rpm output shaft; paired with the exact L-714C brochure row, this supports active current product and upgrade context.
- Publisher
- Honeywell Aerospace
- Title
- T55 Turboshaft Engine