Turmo IV C is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Gas generator stages: 2
Compressor stages: 2
Control system: Hydromechanical
Dry weight: 230 kilogram
Height: 0.72 metre
Length: 2.18 metre
Max. continuous power: 960 kilowatt
Max. takeoff power: 1115 kilowatt
Power turbine stages: 1
Width: 0.64 metre
ICAO: PUMA
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