Shober Willie II

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by John B123 (talk | contribs) at 23:15, 5 November 2019 (→‎Bibliography: Fixed cite error). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Willie II
Role Two-seat sporting or aerobatic aircraft
National origin United States
Manufacturer Shober Aircraft Enterprises
First flight 1971
Number built 1

The Shober Willie II is an American two-seat sporting or aerobatic aircraft designed and built by Shober Aircraft Enterprises.[1] The aircraft was designed to be sold as plans for amateur construction.[1][2]

Design

The Willie II is a braced single-bay biplane with a fabric covered welded steel fuselage.[1] The two-spar wooden wings are fabric covered with wide-span ailerons on the lower wing and a fabric covered wired-braced welded steel tail unit.[1] The prototype is powered by a 180 hp (134 kW) Lycoming O-360-A3A four-cylinder piston engine.[1] It has two open cockpits in tandem and a fixed conventional landing gear with a tailwheel.[1]

Specifications (Prototype)

Data from Jane's All the World's Aircraft 1973-74[1]

General characteristics

  • Crew: 2

Performance

  • g limits: +9 -9g

See also

Aircraft of comparable role, configuration, and era

References

Notes

  1. ^ a b c d e f g Taylor 1973, p. 431
  2. ^ Air Trails: 79. Winter 1971. {{cite journal}}: Missing or empty |title= (help)

Bibliography

  • Taylor, John W.R., ed. (1973). Jane's All the World's Aircraft 1973-74. London, United Kingdom: Jane's Yearbooks. ISBN 0-354-00117-5.