Aircraft performance


Aircraft Antonov-74 is a modification of military aircraft Antonov-72, which is designed for operation in Arctic regions. Year established 1983. Produced since 1986. Produced 81 aircraft in almost 20 modifications.


Flight performance Antonov-74
Cruising speed, km/h 720
Practical flight range, km 2700
Maximum altitude, meters 10100
Technical characteristics Antonov-74
Crew, people 4-5
Maximum takeoff weight, kg 32 000
Empty weight, kg 19500
Number of passengers 52
Load capacity, kg 7500
Length, meters 28,07
Wingspan, meters 31,89 м
Aircraft height 8,65 м
The area of the aircraft wing 98,62 кв.м
Fuel tanks volume 13 210 кг
Power aircraft engines 2 * 6500 кгс
Dimensions cabin for passengers
Length 10,5 м
Width 2,15 м
Height 2,2 м

Documentation for Antonov-74

Document title Size
Ан-74 РЛЭ ч.1 22,63 Mb
Ан-74 РЛЭ ч.2 32,11 Mb
Ан-74 схемы ч.1 7,24 Mb
Ан-74 схемы ч.2 6,64 Mb
Ан-74 схемы ч.3 1,14 Mb
Ан-74 Технология работы экипажа 0,35 Mb
Ан-74 РЛЭ Действия в сложных ситуациях 3,23 Mb