Aircraft performance

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.

Antonov-28

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

Document title Size
Самолет Ан-28. Устройство и эксплуатация. 11,81 Mb
Перечень минимального оборудования Ан-28 (MEL) 0,61 Mb
Руководство по летной эксплуатации Ан-28 61,97 Mb