CF6-80A1 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 4.7
Dry weight: 3973 kilogram
Fan blades: 38
Fan diameter: 2.19 metre
Fan stages: 1
HP compressor stages: 14
HP turbine stages: 2
Height: 2.68 metre
LP compressor stages: 3
LP turbine stages: 4
Length: 4.24 metre
Max. continuous thrust: 193.99 kilonewton
N1 RPM: 3432
N2 RPM: 9827
Overall pressure ratio: 27.3
Max. takeoff thrust: 209.02 kilonewton
Width: 2.4 metre
