AECC ATP120A
AECC's ATP120A is a 1,230 kW-class turboprop under development for general-aviation aircraft and UAVs. AECC reports successful cold-start and maximum-state ground performance testing in May 2026, with high-altitude simulation and airworthiness certification still ahead; service status remains development.
Identity
- Aliases
- ATP120AATP-120A
- Domains
- aviation
- Identity Level
- model
- Kind
- turboprop
- Name
- AECC ATP120A
- Status
- development
Details
- Air Breathing Specs
- Shaft Power Kw
- 1,230
- Description
- AECC's ATP120A is a 1,230 kW-class turboprop under development for general-aviation aircraft and UAVs. AECC reports successful cold-start and maximum-state ground performance testing in May 2026, with high-altitude simulation and airworthiness certification still ahead; service status remains development.
Links
Assets & Meta
- Creation Time
- August 14, 2026 at 20:23:31 UTC
- Updated Time
- August 14, 2026 at 20:23:31 UTC
Other
- Sources
- Accessed Date
- 2026-08-14
- Note
- AECC reports ATP120A's May 2026 ground performance test, stable maximum-state operation, 1,230 kW output, successful low-temperature ignition, and intended general-aircraft/UAV applications; high-altitude simulation and airworthiness certification remain future milestones.
- Publisher
- Aero Engine Corporation of China
- Title
- ATP120A Turboprop Engine Reaches Ground Performance Target