Astazou II K is a turboprop engine model used in aircraft.
Engine Family: turboprop
Output shaft RPM: 2178
Compressor stages: 2
Dry weight: 151 kilogram
Height: 0.52 metre
Length: 1.89 metre
Max. continuous power: 353 kilowatt
Max. takeoff power: 390 kilowatt
Output shaft RPM: 2193
Power turbine stages: 3
Width: 0.53 metre
