BR700-710C4-11 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 3.8
Control system: FADEC
Dry weight: 1635 kilogram
Fan diameter: 1.22 metre
Fan stages: 1
HP compressor stages: 10
HP turbine stages: 2
LP turbine stages: 2
Length: 4.66 metre
Max. continuous thrust: 64.3 kilonewton
Max. takeoff thrust: 68.4 kilonewton
N1 RPM: 7431
N2 RPM: 15898
