Turmo IV A is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 2
Dry weight: 230 kilogram
Gas generator stages: 2
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
View Type →