FJ44-4M-34 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: 1.67 metre
Max. continuous thrust: 15.22 kilonewton
Max. takeoff thrust: 15.22 kilonewton
N1 RPM: 16360
N2 RPM: 37450
Width: 0.67 metre
