JT8D-219

JT8D-219 is a turbofan engine model used in aircraft.

Specifications

Engine Family: turbofan

Bypass ratio: 1.8

Dry weight: 2125 kilogram

Fan diameter: 1.25 metre

Fan stages: 1

HP compressor stages: 7

HP turbine stages: 1

Height: 1.71 metre

LP compressor stages: 6

LP turbine stages: 3

Length: 3.92 metre

Max. continuous thrust: 84.07 kilonewton

Max. takeoff thrust: 96.53 kilonewton

Overall pressure ratio: 19.2

Width: 1.5 metre