Antonov-12
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
