Jump to content

Davis DA-5

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Bhcishere (talk | contribs) at 08:10, 30 January 2018 (Added external links heading and link to website with plans and information on the Davis DA-5). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

DA-5
Role Sport aircraft
Manufacturer Homebuilt
Designer Leeon D. Davis
First flight 22 July 1974

The Davis DA-5, a.k.a. DA-5A, is a single-seat sport aircraft designed in the United States in the 1970s and marketed for homebuilding. Like designer Leeon D. Davis's successful DA-2, it is a low-wing monoplane with fixed tricycle undercarriage and a V-tail, but with a much narrower fuselage accommodating only the pilot, and a lengthened nose. Design work was carried out in 1972, but the prototype was not built until 1974, when it was completed in only 67 days.


Specifications (prototype)

General characteristics

  • Crew: One pilot

Performance

References

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 305.
  • Jane's All the World's Aircraft 1977-78. London: Jane's Yearbooks. pp. 534–35.

Source for plans and information on the Davis DA-5 http://davisda2.com