CF6-80C2A1 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 5.2
Dry weight: 4300 kilogram
Fan blades: 38
Fan diameter: 2.36 metre
Fan stages: 1
HP compressor stages: 14
HP turbine stages: 2
Height: 2.69 metre
LP compressor stages: 4
LP turbine stages: 5
Length: 4.27 metre
Max. continuous thrust: 237.49 kilonewton
N1 RPM: 3280
N2 RPM: 9827
Overall pressure ratio: 30.4
Max. takeoff thrust: 257.37 kilonewton
Width: 2.67 metre
ICAO: A306
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