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