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

Applicability

  • Mi-26

    Mi-26

  • Mi-26T

    Mi-26T


Subscribe to our website news

(no more than one letter per month)

Name:(required)

E-Mail (required)

-Country

field of activity / interests

Firm (Enterprise)