MTR390-2C is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 2
Control system: FADEC
Dry weight: 169 kilogram
Gas generator stages: 1
Height: 0.68 metre
Length: 1.08 metre
Max. continuous power: 873 kilowatt
Max. takeoff power: 958 kilowatt
Power turbine stages: 2
Width: 0.44 metre
ICAO: TIGR
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