Fokker D.XIV
The Fokker D.XIV was a fighter aircraft developed in the Netherlands in the mid-1920s but which was only produced as a single prototype. It was a low-wing, cantilever monoplane with fixed tailskid undercarriage, the basic concept of which was derived from the Fokker V.25 that had been developed during World War I. The pilot sat in an open cockpit aft of the wing's trailing edge. Flight testing revealed excellent performance, but development was ceased when the prototype crashed, killing the test pilot.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Fokker
Specifications
- Cruise speed
- 150 kt
- Max speed
- 150 kt
- Rate of climb
- 1,400 ft/min
- Max takeoff weight
- 2,980 lb
- Empty weight
- 2,090 lb
- Powerplant
- Hispano-Suiza 12Hb
- Engines
- 1
- Seats
- 1
- Length
- 25.9 ft
- Wingspan
- 35.3 ft
- Height
- 10.4 ft
- Number built
- 1
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.