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Makila 1A1

Makila 1A1 is a turboshaft engine model used in aircraft.

Specifications

Engine Family: turboshaft

Compressor stages: 4

Control system: Hybrid hydromechanical + analogue electronic

Dry weight: 241 kilogram

Gas generator stages: 2

Height: 0.67 metre

Length: 2.12 metre

Max. continuous power: 1185 kilowatt

Max. takeoff power: 1357 kilowatt

Ng RPM: 33200

Np RPM: 22850

Power turbine stages: 2

Width: 0.5 metre

Manufacturer

Safran Helicopter Engines

Compatible Aircraft Types

Compatible Aircraft Models