JT8D-217 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 1.8
Dry weight: 2097 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: 80.07 kilonewton
Max. takeoff thrust: 97.75 kilonewton
Overall pressure ratio: 18.6
Width: 1.5 metre
ICAO: MD81
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View Type →ICAO: MD83
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