JT4A-12 is a turbojet engine model used in aircraft.
Engine Family: turbojet
Dry weight: 2220 kilogram
Fan diameter: 1.08 metre
HP compressor stages: 7
HP turbine stages: 1
LP compressor stages: 8
LP turbine stages: 2
Length: 4.8 metre
Max. continuous thrust: 66.28 kilonewton
Max. takeoff thrust: 77.84 kilonewton
Overall pressure ratio: 12.5
ICAO: B703
View Type →ICAO: -
View Type →ICAO: -
View Type →