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.
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 |