Antonov-28
Aircraft Antonov-28, Antonov Design Bureau designed based on light multipurpose aircraft Antonov-14 “Bee”. Its predecessor it features lengthened fuselage, a powerful gas turbine instead of a piston. First flew in 1969. Serial production started in 1978 under license in Poland. Produced 191 aircraft.
Flight performance Antonov-28 |
Cruising speed, km/h |
355 |
Practical flight range, km |
510 |
Maximum altitude, meters |
6000 |
Technical characteristics Antonov-28 |
Crew, people |
1-2 |
Maximum takeoff weight, kg |
6100 |
Empty weight, kg |
3500 |
Number of passengers |
18 |
Load capacity, kg |
2000 |
Length, meters |
12,98 |
Wingspan, meters |
22 м |
Aircraft height |
4,6 м |
The area of the aircraft wing |
39,7 кв.м |
Fuel tanks volume |
1529 кг |
Power aircraft engines |
2 х 960 л.с. |
Dimensions cabin for passengers |
Length |
5,26 м |
Width |
1,74 м |
Height |
1,6 м |
Documentation for Antonov-28