History

The Fokker C.VII was developed by Fokker after the disappointing Fokker C.Vw. The type was meant for reconnaissance and continuing training.
The device was built in the proven Fokker construction of a linen-covered, welded steel tube fuselage and wooden wings.
Between 1930 and 1932 thirty examples were delivered to the MLD.

 

Technical information
Dimensions:
Length: 9,55 m Wingspan: 12,9 m
Height: 4,01 m Wing area: 37 m2
Weights:
Empty weight: 1200 kg Max. start weight: 1700 kg
Performances:
Max. speed: 160 km/hr Climbing speed: - m/min
Cruising speed: 130 km/hr    
Range: 800 km Service ceiling: - m
Miscellaneous:
Engine type: One Lorraine Mizar rated 280 hp
Crew: Two men: one aviator plus one observer/air gunner
Armament: Two machine guns