Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Dornier Do 28D-2 Short Take-Off and Landing (STOL) Light Utility Aircraft.
2 x Lycoming IGSO-540-A1E 6-cylinder piston engines developing 380 horsepower each.
Propulsion
201 mph
323 kph | 174 kts
Max Speed
25,197 ft
7,680 m | 5 miles
Service Ceiling
652 miles
1,050 km | 567 nm
Operational Range
1,160 ft/min
354 m/min
Rate-of-Climb