D-36 Series 1 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Dry weight: 1124 kilogram
Bypass ratio: 6.3
Overall pressure ratio: 18.7
Max. continuous thrust: 15.69 kilonewton
Max. takeoff thrust: 63.76 kilonewton
Fan stages: 1
IP compressor stages: 6
HP compressor stages: 7
HP turbine stages: 1
IP turbine stages: 1
LP turbine stages: 3
Length: 3.47 metre
Width: 1.71 metre
Height: 1.54 metre
N1 RPM: 5650
N2 RPM: 11700
N3 RPM: 14200
ICAO: YK42
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