Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Antonov An-28 Light Utility, Short Take-Off and Landing (STOL) Aircraft.
2 x Glushenkov TVD-10B OR2 x Pratt & Whitney Canada (PWC) PT6A-65B turboprop engines developing 960 horsepower each driving three-bladed propeller units.
Propulsion
221 mph
355 kph | 192 kts
Max Speed
19,685 ft
6,000 m | 4 miles
Service Ceiling
317 miles
510 km | 275 nm
Operational Range
2,360 ft/min
719 m/min
Rate-of-Climb