D-136 And D-136 Series 1 Turboshaft Engines

The D-136 and D-136 series 1, turboshaft engines are used to power the world’s largest Mi-26 transport helicopter and it’s modifications.
Perfect design and highly developed production ensure the engine’s quality and reliability.
Easy maintenance and high repair ability are ensured by a modular design of the engine.

Main advantages of the engine:
- low specific fuel consumption; 
- high reliability; 
- high power; 
- easy maintenance and high repair ability; 
- low weight-to-power ratio.

BASIC SPECIFICATIONS
Maximum takeoff power conditions (SLS, ISA): 
Power, shp (kW)11400 (8382)
Specific fuel consumption, kg/hp•h (kg/kW•h)0.194 (0.263)
Cruise power conditions (H = 4600 m, Mfl = 0.13, ISA): 
Power, shp (kW) 6100 (4486)
Specific fuel consumption, kg/hp•h (kg/kW•h)0.230 (0.312)
Dry weight, kg     1077
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