Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Boeing VC-25A (Air Force One) Presidential Air Transport Aircraft.
4 x General Electric CF6-80C2B1 non-afterburning turbofan engines developing 56,700 pounds of thrust each.
Propulsion
629 mph
1,013 kph | 547 kts
Max Speed
45,098 ft
13,746 m | 9 miles
Service Ceiling
7,798 miles
12,550 km | 6,776 nm
Operational Range