Antonov-24
Antonov An-24 was developed in the Antonov Design Bureau as a passenger aircraft designed for use on short-haul passenger lines. In the period from 1959 to 1979 it was built more than 1,000 aircraft. Prior to 2000, he produced in China.
| Flight performance Antonov-24 | |
| Cruising speed, km/h | 498 |
| Practical flight range, km | 640 |
| Maximum altitude, meters | 8400 |
| Technical characteristics Antonov-24 | |
| Crew, people | 5 |
| Maximum takeoff weight, kg | 21000 |
| Empty weight, kg | 13300 |
| Number of passengers | 48 |
| Load capacity, kg | 4612 |
| Length, meters | 23,53 |
| Wingspan, meters | 29.20 м |
| Aircraft height | 8.32 м |
| The area of the aircraft wing | 72.46 кв.м |
| Fuel tanks volume | 4760 кг |
| Power aircraft engines | 2 х 2550 л.с. |
| Dimensions cabin for passengers | |
| Length | 9.96 м |
| Width | 2.76 м |
| Height | 1.91 м |
