The AEP100 engine is a 900 kW class civil turboprop engine derived from the AES100 turboshaft engine. The engine has a takeoff power of 900 kW class and a takeoff fuel consumption rate of 0.310 kg/kW/h. It can meet the powerplant needs of platforms such as UAVs, business jets, and general aviation aircraft. Its overall performance reaches the international advanced level of currently operational engines in the same class, with good economy, safety, reliability, and maintainability.