Pratt & Whitney Canada PT6C-67E
Pratt & Whitney Canada PT6C-67E is the exact turboshaft variant in the PT6C-67 family and the engine listed by Pratt & Whitney for the Airbus H175. The current Pratt & Whitney product page lists the PT6C-67E in the 1,800 SHP thermodynamic and 1,300 SHP mechanical power classes, with a 21,000 rpm output shaft, 25 inch diameter, and 65 inch length at takeoff, sea-level standard-day static, uninstalled conditions. The typed shaft-power value uses the 1,300 SHP mechanical class converted to 969.41 kW. Airbus separately publishes two PT6C-67E engines and 1,324 kW / 1,776 shp takeoff power per engine for the H175; that installed-aircraft rating is retained as context only and is not copied into the engine field. Current Pratt & Whitney and Airbus product pages establish active current product and in-service application context for this exact variant.
Identity
- Aliases
- PT6C-67EPratt & Whitney Canada PT6C-67EPT6C-67 series PT6C-67E
- Domains
- aviation
- Identity Level
- variant
- Kind
- turboshaft
- Name
- Pratt & Whitney Canada PT6C-67E
- Status
- active
Details
- Air Breathing Specs
- Shaft Power Kw
- 969.41
- Description
- Pratt & Whitney Canada PT6C-67E is the exact turboshaft variant in the PT6C-67 family and the engine listed by Pratt & Whitney for the Airbus H175. The current Pratt & Whitney product page lists the PT6C-67E in the 1,800 SHP thermodynamic and 1,300 SHP mechanical power classes, with a 21,000 rpm output shaft, 25 inch diameter, and 65 inch length at takeoff, sea-level standard-day static, uninstalled conditions. The typed shaft-power value uses the 1,300 SHP mechanical class converted to 969.41 kW. Airbus separately publishes two PT6C-67E engines and 1,324 kW / 1,776 shp takeoff power per engine for the H175; that installed-aircraft rating is retained as context only and is not copied into the engine field. Current Pratt & Whitney and Airbus product pages establish active current product and in-service application context for this exact variant.
- Developers
- Family
- Length M
- 1.651
- Manufacturers
Links
- Official Url
- https://www.prattwhitney.com/pt6c
Assets & Meta
- Creation Time
- August 8, 2026 at 07:38:48 UTC
- Updated Time
- August 21, 2026 at 02:15:43 UTC
Other
- Diameter M
- 0.635
- Sources
- Accessed Date
- 2026-08-08
- Note
- Current EASA type-certificate listing identifies the PT6C-67 series and Pratt & Whitney Canada as type-certificate holder.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.IM.E.022 — Pratt and Whitney Canada PT6C-67 series engines
- Accessed Date
- 2026-08-08
- Note
- The official TCDS explicitly lists PT6C-67E as a distinct model alongside PT6C-67C, PT6C-67C1, and PT6C-67A.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.IM.E.022 PT6C-67 Series engines — Issue 06 TCDS
- Accessed Date
- 2026-08-08
- Note
- Official EC175 certification record independently specifies Pratt & Whitney Canada 2 x Model PT6C-67E without making an AeroVia vehicle-family mutation in this identity packet.
- Publisher
- European Union Aviation Safety Agency
- Title
- EASA.R.150 EC175 TCDS — PT6C-67E
- Accessed Date
- 2026-08-20
- Note
- Current Pratt & Whitney product page gives exact PT6C-67E values: 1,800 SHP thermodynamic power class, 1,300 SHP mechanical power class, 21,000 rpm output shaft, 25 inch diameter, and 65 inch length at takeoff, sea-level standard-day static, uninstalled conditions; it also lists Airbus H175 as the model application.
- Publisher
- Pratt & Whitney
- Title
- PT6C Engine
- Accessed Date
- 2026-08-20
- Note
- Current Airbus H175 technical information identifies two Pratt & Whitney PT6C-67E engines and publishes 1,324 kW / 1,776 shp takeoff power per engine; retained as installed-aircraft context rather than copied into the exact engine shaft-power field.
- Publisher
- Airbus
- Title
- H175 technical information