Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the North American P-64 Single-Seat, Single-Engine Monoplane Fighter / Trainer.
1 x Wright R-1820-77 9-cylinder air-cooled radial piston engine developing 870 horsepower driving a three-bladed propeller unit at the nose.
Propulsion
267 mph
430 kph | 232 kts
Max Speed
27,559 ft
8,400 m | 5 miles
Service Ceiling
628 miles
1,010 km | 545 nm
Operational Range