Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the AEG C.IV Two-Seat Biplane Fighter Aircraft.
1 x Mercedes D.III water-cooled in-line engine developing 160 horsepower driving a two-bladed propeller unit at the nose.
Propulsion
98 mph
158 kph | 85 kts
Max Speed
16,404 ft
5,000 m | 3 miles
Service Ceiling
280 miles
450 km | 243 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).