Antonov-74
Aircraft Antonov-74 is a modification of military aircraft Antonov-72, which is designed for operation in Arctic regions. Year established 1983. Produced since 1986. Produced 81 aircraft in almost 20 modifications.
| Flight performance Antonov-74 |
| Cruising speed, km/h |
720 |
| Practical flight range, km |
2700 |
| Maximum altitude, meters |
10100 |
| Technical characteristics Antonov-74 |
| Crew, people |
4-5 |
| Maximum takeoff weight, kg |
32 000 |
| Empty weight, kg |
19500 |
| Number of passengers |
52 |
| Load capacity, kg |
7500 |
| Length, meters |
28,07 |
| Wingspan, meters |
31,89 м |
| Aircraft height |
8,65 м |
| The area of the aircraft wing |
98,62 кв.м |
| Fuel tanks volume |
13 210 кг |
| Power aircraft engines |
2 * 6500 кгс |
| Dimensions cabin for passengers |
| Length |
10,5 м |
| Width |
2,15 м |
| Height |
2,2 м |
Documentation for Antonov-74
