Jump to content

Focke-Wulf Fw 43 Falke

From Wikipedia, the free encyclopedia
The printable version is no longer supported and may have rendering errors. Please update your browser bookmarks and please use the default browser print function instead.
A 43 Falke
Role Civil utility aircraft
Manufacturer Focke-Wulf
First flight 1932
Number built 1

The Focke-Wulf A 43 Falke (Falcon) was a light utility aircraft developed in Germany in 1932. The last project undertaken by the company under the technical direction of Henrich Focke, was a high-wing strut-braced monoplane of conventional design, with a fixed tailwheel undercarriage. The pilot and two passengers sat in a fully enclosed cabin. Only a single example was built. In 1932, it was the fastest airliner in Europe[1]

Specifications

General characteristics

  • Crew: one, pilot
  • Capacity: two passengers
  • Length: 8.30 m (27 ft 3 in)
  • Wingspan: 10.00 m (32 ft 10 in)
  • Height: 2.30 m (7 ft 7 in)
  • Wing area: 14.0 m2 (151 sq ft)
  • Empty weight: 725 kg (1,600 lb)
  • Gross weight: 1,125 kg (2,480 lb)
  • Powerplant: 1 × Argus As 10c , 164 kW (220 hp)

Performance

  • Maximum speed: 256 km/h (158 mph, 137 kn)
  • Range: 1,050 km (652 mi, 567 nmi)
  • Service ceiling: 5,100 m (16,730 ft)

References

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 395.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 894 Sheet 29.
  • Zuerl, Walter (1941). Deutsche Flugzeug Konstruktteuire. München: Curt Pechstein Verlag. pp. Teil 336.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 395.
  1. ^ a b Zuerl 1941, p. 201.