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Purpose:
Passenger aircraft
Description:
It is intended for carriage of passengers in conditions of increased comfort.
FUNCTIONAL FEATURES
The An-74TK-300D aircraft is an all-metal cantilever high-wing monoplane with single-finned T-tailed empennage. The aircraft is intended for operation in all-weather conditions.
Technical details:
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Maximum payload weight, t
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6
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Engines:
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type
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D-36 ser. 4A double-flow turbojet engine
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quantity x thrust, tf
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2x6.5
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Maximum cruissng flight speed, km/h
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725
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Maximum flight altitude, m
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10100
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Fuselage length, m
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25.735
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Flight range at 10100 m altitude and 580-615 km/h airspeed in ISA condition, 37 500 kg take-off weight and 1 hour flight fuel reserve (1400 kg), km:
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with maximum playload 4800 kg
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2640
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Quantity of passengers, persons, not more than
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24
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Crew, persons
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2
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