Astazou II A is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 2
Control system: Mechanical control system
Dry weight: 142 kilogram
Height: 0.56 metre
Length: 1.43 metre
Max. continuous power: 353 kilowatt
Max. takeoff power: 390 kilowatt
Power turbine stages: 3
Width: 0.52 metre
ICAO: ALO2
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