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Purpose:
Turbofan aero engine
Description:
Designed to power Yak-42 passenger and An-72 and
An-74 transport aircraft. The engine has Type Certificate.
It meets the effective environmental requirements of
ICAO standards.
Technical details:
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Emergency power (SLS,ISA+15
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Series 1
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thrust, kgf
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Takeoff (SLS, ISA):
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thrust, kgf
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6500
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specific fuel consumption, kg/h/kgf
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0.365
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Max cruise (H 8 000 m, M 0.75, ISA):
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thrust, kgf
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1600
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specific fuel consumption, kg/h/kgf
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0.65
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Dimensions, mm
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3 469.5x1541x1411.5
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Weight, dry, kg
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1124.2
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Assigned service life, h
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18000
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