Fokker C.VII

The Fokker C.VII-W was a reconnaissance seaplane built in the Netherlands in the late 1920s. Sharing elements of the highly successful C.V design, the C.VII-W was a conventional, single-bay biplane with wings of unequal span braced with N-struts. The undercarriage consisted of a standard twin-pontoon arrangement, and the fin and rudder continued through to the ventral side of the fuselage, creating a cruciform tail. The pilot and observer sat in tandem, open cockpits. The wing structure was wooden with fabric and plywood covering, and the fuselage was of steel tube construction with fabric covering. The first twelve of the thirty examples produced were sent to the Dutch East Indies, with the rest remaining in the Netherlands. The type was withdrawn from front-line service in 1940, but some machines remained active in the East Indies as trainers until the Japanese invasion in 1942.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Fokker
Specifications
- Cruise speed
- 70 kt
- Max speed
- 86 kt
- Service ceiling
- 11,800 ft
- Max takeoff weight
- 3,570 lb
- Empty weight
- 2,429 lb
- Fuel capacity
- 87 US gal
- Powerplant
- Armstrong Siddeley Lynx 7-cylinder air-cooled radial piston engine
- Engines
- 1
- Seats
- 2
- Length
- 32 ft
- Wingspan
- 42 ft
- Height
- 13 ft
- Number built
- 30
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.