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Purpose:
Turbofan аero еngine
Description:
Designed to power An-74TK-300 convertable 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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thrust, kgf
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6500
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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/kgf-h
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0.358
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Max cruise (H8000m,M0.75,ISA):
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thrust, kgf
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1600
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specific fuel consumption, kg/kgf-h
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0.63
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Dimensions, mm
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3732.5x1802.3x1987.4
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Weight, dry, kg
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1130
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Assigned service life, h
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40000
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