D-136 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Max. continuous power: 6252 kilowatt
Max. takeoff power: 8385 kilowatt
Dry weight: 1264 kilogram
Length: 3.72 metre
Width: 1.38 metre
Height: 1.12 metre
Np RPM: 9375
Power turbine stages: 2
Nh RPM: 13978
Nl RPM: 12167
HP compressor stages: 7
HP turbine stages: 1
LP compressor stages: 6
LP turbine stages: 1
ICAO: MI26
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