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D-136/D-136 series 1

The D-136 and D-136 series 1, turboshaft engines are used to power the civil transport helicopters. Perfect design and highly developed production ensure the engine`s quality and reliability.
Easy maintenance and high repairability 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 repairability;
  • 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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