JT12A-6 is a turbojet engine model used in aircraft.
Engine Family: turbojet
Dry weight: 203 kilogram
HP compressor stages: 9
HP turbine stages: 2
Length: 1.99 metre
Max. continuous thrust: 10.68 kilonewton
Max. takeoff thrust: 13.34 kilonewton
ICAO: L29A
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