Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the North American XSN2-1 Twin-Seat, Single-Engine Military Trainer Aircraft.
1 x Wright R-1820-78 "Cyclone" air-cooled radial piston engine developing 1,100 horsepower driving three-bladed propeller unit at the nose.
Propulsion
267 mph
430 kph | 232 kts
Max Speed
29,856 ft
9,100 m | 6 miles
Service Ceiling
1,616 miles
2,600 km | 1,404 nm
Operational Range