JT8D-9A is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 1
Dry weight: 1543 kilogram
Fan diameter: 1.08 metre
Fan stages: 2
HP compressor stages: 7
HP turbine stages: 1
Height: 1.36 metre
LP compressor stages: 4
LP turbine stages: 3
Length: 3.14 metre
Max. continuous thrust: 56.05 kilonewton
Max. takeoff thrust: 64.5 kilonewton
Overall pressure ratio: 15.9
Width: 1.08 metre
ICAO: B721
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