Astazou II D is a turboprop engine model used in aircraft.
Engine Family: turboprop
Output shaft RPM: 2178
Compressor stages: 2
Dry weight: 161 kilogram
Height: 0.46 metre
Length: 1.76 metre
Max. continuous power: 331 kilowatt
Max. takeoff power: 331 kilowatt
Power turbine stages: 3
Width: 0.46 metre
