FJ44-4A-32 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Control system: Dual channel FADEC
Dry weight: 304 kilogram
Fan stages: 1
HP compressor stages: 1
HP turbine stages: 1
Height: 0.82 metre
LP compressor stages: 3
LP turbine stages: 2
Length: 1.74 metre
Max. continuous thrust: 14.35 kilonewton
Max. takeoff thrust: 14.37 kilonewton
N1 RPM: 16360
N2 RPM: 37450
Width: 0.67 metre
ICAO: BE4W
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