PW1120 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Overall pressure ratio: 26.8
Bypass ratio: 0.2
Afterburner:
Max. thrust: 61.18 kilonewton
Max. thrust (wet): 91.56 kilonewton
Control system: FADEC
Dry weight: 1292 kilogram
Fan diameter: 0.78 metre
Fan stages: 3
HP compressor stages: 10
HP turbine stages: 2
LP turbine stages: 2
Length: 4.11 metre
