FJ44-2A is a turbofan engine model used in aircraft.
Engine Family: turbofan
Control system: Single channel EECU + HMU
Dry weight: 240 kilogram
Fan stages: 1
HP compressor stages: 1
HP turbine stages: 1
Height: 0.75 metre
LP compressor stages: 3
LP turbine stages: 2
Length: 1.52 metre
Max. continuous thrust: 10.23 kilonewton
Max. takeoff thrust: 10.23 kilonewton
Width: 0.55 metre
N1 RPM: 17245
N2 RPM: 41200
ICAO: PRM1
View Type →ICAO: C25A
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