AECC AES100
AECC's AES100 is a civil turboshaft with 1,000 kW takeoff power, designed for multipurpose helicopters. AECC specifies 5–6-ton twin-engine and 3–4-ton single-engine helicopter classes; Chinese civil authorities document its type-certification work, while current production and service status remain unestablished.
Identity
- Aliases
- AES100AES-100
- Domains
- aviation
- Identity Level
- model
- Kind
- turboshaft
- Name
- AECC AES100
- Status
- unknown
Details
- Air Breathing Specs
- Shaft Power Kw
- 1,000
- Description
- AECC's AES100 is a civil turboshaft with 1,000 kW takeoff power, designed for multipurpose helicopters. AECC specifies 5–6-ton twin-engine and 3–4-ton single-engine helicopter classes; Chinese civil authorities document its type-certification work, while current production and service status remain unestablished.
Links
Assets & Meta
- Creation Time
- August 14, 2026 at 20:18:44 UTC
- Updated Time
- August 14, 2026 at 20:18:44 UTC
Other
- Sources
- Accessed Date
- 2026-08-14
- Note
- AECC identifies AES100 as a civil turboshaft with 1,000 kW takeoff power, suitable for 5–6-ton twin-engine and 3–4-ton single-engine multipurpose helicopters.
- Publisher
- Aero Engine Corporation of China
- Title
- AES100 Engine
- Accessed Date
- 2026-08-14
- Note
- CAAC describes AES100 as China's first independently developed advanced civil turboshaft and reports high-altitude simulated airworthiness testing during type-certification work.
- Publisher
- Civil Aviation Administration of China
- Title
- AES100 Engine Completes High-Altitude Simulated Airworthiness Test
- Accessed Date
- 2026-08-14
- Note
- CAAC reports completion of extensive materials and process airworthiness verification for AES100, supporting the model's distinct certification boundary without asserting operational service.
- Publisher
- Civil Aviation Administration of China
- Title
- AES100 Engine Materials Airworthiness Tests Complete