M601D is a turboprop engine model used in aircraft.
Engine Family: turboprop
Max. continuous power: 490 kilowatt
Max. takeoff power: 540 kilowatt
Dry weight: 197 kilogram
Control system: Hydromechanical
Ng RPM: 36660
Np RPM: 31023
Output shaft RPM: 2080
Compressor stages: 3
Gas generator stages: 1
Power turbine stages: 1
Length: 1.68 metre
Width: 0.59 metre
Height: 0.65 metre
ICAO: -
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