D-136 Turboshaft


Designed for helicopters of various applications, in the load class up to 20,000 kg. It is mounted on a Mi-26, Mi-26T helicopter. Conforms to current ICAO environmental standards. Has Type Certificate. It has been produced in series since 1978.

30-minute maximum power H=0, Vn=0, ISA.
Power, hp 11,400
Supports up to temperature, 0C 17
Taking off power H=0, Vn=0, ISA
Power, hp 10,000
Supports up to temperature, 0C 22
Specific fuel consumption, kg/h/hp 0.210
Weight, kg 1,077
Dimensions, mm 3,715 x 1,124 x 1,382
Specified service life, h 6,000
Сертификат типа Госавислужбы Украины

Certificate of State Service of Ukraine

Сертификат типа АР МАК

Certificate of type AR MAK (D-136)

Сертификат типа СААС

Certificate of type CAAC (D-136)

Applicability

  • Mi-26T

    Mi-26T

  • Мі-26Т

    Мі-26Т