CF6-80E1A1 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 5.3
Dry weight: 5092 kilogram
Fan blades: 34
Fan diameter: 2.44 metre
Fan stages: 1
HP compressor stages: 14
HP turbine stages: 2
Height: 2.87 metre
LP compressor stages: 4
LP turbine stages: 5
Length: 4.28 metre
Max. continuous thrust: 258.09 kilonewton
N1 RPM: 3320
N2 RPM: 9827
Overall pressure ratio: 32.4
Max. takeoff thrust: 281.53 kilonewton
Width: 2.9 metre
