Astazou XIV H is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 3
Control system: Hydromechanical
Dry weight: 160 kilogram
Height: 0.57 metre
Length: 1.47 metre
Max. continuous power: 440 kilowatt
Max. takeoff power: 440 kilowatt
Output shaft RPM: 6334
Power turbine stages: 3
Width: 0.5 metre
ICAO: GAZL
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