Aircraft performance


Four-engine turboprop aircraft Antonov-12 was developed in 1957, primarily for military purposes. Widely used as a landing aircraft. Until 1973, the aircraft produced in 1248, then manufactured in China (667 aircraft). It produced nearly 49 modifications.


Flight performance Antonov-12
Cruising speed, km/h 686
Practical flight range, km 5000
Maximum altitude, meters 10500
Technical characteristics Antonov-12
Crew, people 5
Maximum takeoff weight, kg 61000
Empty weight, kg 28000
Number of passengers 90
Load capacity, kg 20000
Length, meters 33,109
Wingspan, meters 38,015 м
Aircraft height 10,525 м
The area of the aircraft wing 121,7 кв.м
Fuel tanks volume 22 066 кг
Power aircraft engines 4х4250 э.л.с.
Dimensions cabin for passengers
Length 13,5 м (грузовая
Width 3,5 м (грузовая)
Height 2,6 м (грузовая)

Documentation for Antonov-12

Document title Size
Ан-12. Транспортный самолет Ан-12 6,45 Mb
Ан-12. Инструкция экипажу самолета Ан-12 14,29 Mb
Ан-12. РЛЭ 15,33 Mb
Ан-12. БК ТО Книга-4 33,94 Mb