FJ44-1A is a turbofan engine model used in aircraft.
Engine Family: turbofan
LP compressor stages: 1
Bypass ratio: 3.3
Control system: Hydromechanical
Dry weight: 209 kilogram
Fan stages: 1
HP compressor stages: 1
HP turbine stages: 1
Height: 0.75 metre
LP turbine stages: 2
Length: 1.36 metre
Max. continuous thrust: 8.45 kilonewton
Max. takeoff thrust: 8.45 kilonewton
Overall pressure ratio: 12.8
Width: 0.55 metre
N1 RPM: 17245
N2 RPM: 41200
ICAO: C525
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