Makila 2A1 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 4
Control system: Single channel FADEC + manual backup control
Dry weight: 279 kilogram
Gas generator stages: 2
Height: 0.67 metre
Length: 2.11 metre
Max. continuous power: 1303 kilowatt
Max. continuous torque: 55.1 decanewton-metre
Max. takeoff power: 1303 kilowatt
Max. takeoff torque: 55.1 decanewton-metre
Ng RPM: 33200
Np RPM: 22962
Power turbine stages: 2
Width: 0.79 metre
ICAO: EC25
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