MTR390-C01 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Np RPM: 27134
Width: 0.44 metre
Height: 0.75 metre
Length: 1.08 metre
Compressor stages: 2
Control system: FADEC
Dry weight: 188 kilogram
Gas generator stages: 1
Max. continuous power: 873 kilowatt
Max. takeoff power: 958 kilowatt
Ng RPM: 43100
Power turbine stages: 2
