Is designed for An-38, An-3, T-101 Grach regional aircraft.
Small-size high efficient turboprop engine of modular design in 1500 h.p. power class is designed on the base of a core providing high parameters of thermodynamic cycle and efficiency of the assemblies.
The engine comprises:
- two-channel FADEC with a reserve hydromechanical channel which ensures a certification in accordance with international standards and operation of the engine with no limitations worldwide;
- a developed control and diagnostic system which allows the engine operation in accordance with technical status;
- modular design which provides removal and replacement of modules under operation without disassembly of the modules.