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D-136-2 turboshaft engine is intended for improving the performance of civil transport helicopters.
D-136-2 engine has been developed on the basis of production engines D-136 series 1 and D-436T1 and features a high degree of commonalty with them, which will permit to radically reduce time and cost of building and certifying it.

Basic specifications:

Emergency power rating (H=0, M=0, ISA+15°C):
Power rating, hp (kW) 12500 (9190)
Maximum takeoff power rating (H=0, Mfl=0, ISA):
Power rating (at tAMB=30°C), hp (kW) 11650 (8560)
Specific fuel consumption, kg/hp·h (kg/kW·h) 0.198 (0.269)
Dry weight, kg 1100

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