Wing Derringer

Wing D-1 Derringer
Wing D-1 Derringer at Lakeland, Florida in April 2009
Role Light twin-engined touring monoplane
Manufacturer Wing Aircraft
Designer John Thorp
First flight 1962
Number built 12

The Wing Derringer is an American light twin-engined two-seat monoplane tourer designed by John Thorp and developed by the Hi-Shear Corporation and built by the Wing Aircraft Company.

Contents

Development

The D-1 Derringer light twin design was originally designed in 1958 by John Thorp as the Thorp T-17 a twin-engined development of his Thorp T-11 Sky Scooter. The design was taken over by George Wing of the Hi-Shear Corporation. The Derringer is a low-wing cantilever monoplane with a retractable tricycle landing gear. It had room for two in an enclosed cockpit with an unusual up and backward opening canopy. It was powered by two 115hp Continental O-200 engines, one mounted on the leading edge of each wing. The prototype aircraft (registered N3621G) first flew on 1 May 1962 at Torrance. A second prototype flew in November 1964 but crashed a few weeks later. A static test aircraft and two more aircraft were built for testing which resulted in the award of a type certificate in December 1966. The aircraft did not go into production due to internal problems within the Hi-Shear Corporation.

Development of a two-seat Coin/military trainer version designated Wing D-2M Derringer was begun but failed to develop further than the design stage.[1]

In 1978 George Wing left Hi-Shear and started the Wing Aircraft Company. The company built one-pre-production aircraft followed by six production aircraft, enterring bankruptcy in July 1982, after which only one further aircraft was built before seven unfinished airframes were sold.

Nine D-1 aircraft were on the U.S. civil aircraft register in May 2009.

Specifications (D-1)

Data from Jane's All The World's Aircraft 1980-81 [2]

General characteristics

Performance

See also

Aircraft of comparable role, configuration and era

References

  1. ^ Taylor, John W. R.. Jane's All the World's Aircraft 1982-83. Jane's Publishing Company. London. 1983. ISBN 0710607482
  2. ^ J W R Taylor 1980, p.454.
  3. ^ 65% power at 13,000 ft