FJ44-1AP is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 2.6
Control system: Dual channel FADEC
Dry weight: 212 kilogram
Fan stages: 1
HP compressor stages: 1
HP turbine stages: 1
Height: 0.79 metre
LP compressor stages: 1
LP turbine stages: 2
Length: 1.47 metre
Max. continuous thrust: 8.67 kilonewton
Max. takeoff thrust: 8.74 kilonewton
Width: 0.55 metre
N1 RPM: 17245
N2 RPM: 41200
ICAO: C525
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