Antonov-2
Multipurpose aircraft Antonov-2 was developed in 1946 to meet the challenges of peacetime. Due to the high reliability and safety has become the world’s only aircraft manufactured 61 years (now made in China). There are 16 modifications.
| Flight performance Antonov-2 | |
| Cruising speed, km/h | 150-190 |
| Practical flight range, km | 990 |
| Maximum altitude, meters | 4500 |
| Technical characteristics Antonov-2 | |
| Crew, people | 2 |
| Maximum takeoff weight, kg | 5500 |
| Empty weight, kg | 3400-3690 |
| Number of passengers | 12 |
| Load capacity, kg | 1500 |
| Length, meters | 12,4 |
| Wingspan, meters | 8,425 м |
| Aircraft height | 5,35 м |
| The area of the aircraft wing | 71,52 м? |
| Fuel tanks volume | 1240 л |
| Power aircraft engines | АШ-62ИР 735,45 к |
| Dimensions cabin for passengers | |
| Length | 4,1 м (грузовая) |
| Width | 1,8 м (грузовая) |
| Height | 1,6 м (грузовая) |
Documentation for Antonov-2
| Document title | Size |
| Ан-2. КУЛП 1979.1980 | 1,19 Mb |
| Ан-2. Инструкция по эксплуатации А и РЭО.1973 | 2,17 Mb |
| Ан-2. Конструкция. Радченко. 1969 | 19,20 Mb |
| Ан-2. Краткое тех. описание.издание 2. 1969 | 6,96 Mb |
| Ан-2. Практическая аэродинамика самолета. 1972 | 2,29 Mb |
| Ан-2. Рекомендации по практической аэродинамике. 1985 | 8,28 Mb |
| Ан-2. РЛЭ. 1984 | 2,99 Mb |
| Ан-2. РЛЭ авиации ДОСААФ СССР. 1989 | 2,45 Mb |
| Ан-2. ИЭ и ТО. 1969 | 5,77 Mb |
| Ан-2П. Альбом формулярных схем. | 3,03 Mb |