D-136 Turboshaft Engine

Designed for use as a sustainer propulsion system on twin-engine helicopters of various applications in the class of load capacity up to 20000 kg. It powers Mi-26, Mi-26T helicopters. It meets the effective environmental requirements of ICAO standards. In commercial production since  1978.

Takeoff (SLS, ISA)
Power, h.p. 11,400
Specific fuel consumption, kg/hp/h 0.198
Dimensions, mm 3,715 x 1,382 x 1,124
Weight, dry, kg 1,077
Specified service life, h 3,000
SAAU Type Certificate

SAAU Type Certificate

IAC AR Type Certificate

IAC AR Type Certificate

СААС Type Certificate

СААС Type Certificate


  • Mi-26


  • Mi-26T


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