AL5512 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 8
Dry weight: 354 kilogram
Gas generator stages: 2
Length: 1.18 metre
Max. continuous power: 2218 kilowatt
Max. takeoff power: 3039 kilowatt
Ng RPM: 18720
Np RPM: 16000
Output shaft RPM: 14750
Power turbine stages: 2
ICAO: H47
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