Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Armstrong Whitworth AW.16 Single-Seat, Single-Engine Biplane Fighter.
1 x Armstrong Siddeley "Panther IIA" 14-cylinder air-cooled radial piston engine developing 525 horsepower driving a two-bladed propeller unit at the nose.
Propulsion
199 mph
320 kph | 173 kts
Max Speed
26,247 ft
8,000 m | 5 miles
Service Ceiling
267 miles
430 km | 232 nm
Operational Range
1,665 ft/min
507 m/min
Rate-of-Climb