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) |
