Astazou II E is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 2
Dry weight: 158 kilogram
Height: 0.5 metre
Length: 1.76 metre
Max. continuous power: 353 kilowatt
Max. takeoff power: 390 kilowatt
Output shaft RPM: 2058
Power turbine stages: 3
Width: 0.5 metre
ICAO: PC6T
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