Avions Fairey Junior

The Avions Fairey Junior, also known as the Tipsy Junior was a single-seat light aircraft built in Belgium following World War II.

Tipsy Junior
Tipsy Junior G-AMVP at a UK airshow in 1953
Role Sports plane
Manufacturer Avions Fairey
Designer Ernest Oscar Tips
First flight 30 June 1947
Number built 2

Development

The Junior was one of a series of light aircraft[1] designed by and named after E.O.Tips of Fairey Aviation's Belgian subsidiary, Avions Fairey. Of wood and fabric construction, it was a conventional, low-wing monoplane with a tailwheel undercarriage and a single seat, open cockpit,[2] though there was the option of a bubble hood.[3] The constant chord wings were almost square ended and the tailplane, fin and rudder also angular. Both completed aircraft were initially powered by the 36 hp (27 kW) Aeronca JAP J-99 engine, later replaced by the more powerful, 62 hp (46 kW) Walter Mikron 2.[2][4]

The Junior, registered OO-TIT, flew for the first time on 30 June 1947 from Gosselies in Belgium.[3]

Operational history

The first Junior was written off after a hard landing in 1948.[5]

The second example (construction number J.111, registration OO-ULA) was bought by Fairey and taken to England in 1953, where it was registered as G-AMVP.[2][4] In 1957, it was used in a publicity stunt when Fairey test pilot Peter Twiss landed it on the aircraft carrier HMS Ark Royal. For part of its time it had the bubble canopy. Rebuilt after a long time in storage following a forced landing in 1993,[5] it flew again late in 2006.[5] It had a minor landing accident in 2008[6] but had a permit to fly until May 2009.[7]

The Junior did not sell, and the third airframe was cancelled before completion. It was purchased incomplete by Fairey in 1961 and has been under construction in the hands of a number of owners in the intervening years, but never finished.[5]

Specifications
Flying scale model of Avions Fairey Tipsy Junior, built by Donald Granlund

Data from British Civil Aircraft 1919-59 Vol.II.[2]

General characteristics

  • Crew: 1
  • Length: 5.65 m (18 ft 6 in)
  • Wingspan: 6.9 m (22 ft 8 in)
  • Height: 1.48 m (4 ft 10 in)
  • Wing area: 10.5 m2 (113 sq ft) [5]
  • Empty weight: 220 kg (485 lb)
  • Gross weight: 350 kg (772 lb)
  • Powerplant: 1 × Walter Mikron II 4-cylinder air-cooled inverted in-line piston engine, 46 kW (62 hp)
  • Propellers: 2-bladed fixed pitch propeller

Performance

  • Maximum speed: 174 km/h (108 mph, 94 kn)
  • Cruise speed: 158 km/h (98 mph, 85 kn)
  • Range: 430 km (270 mi, 230 nmi)
  • Service ceiling: 1,800 m (5,900 ft)

References
  1. Taylor 1974, pp. 39–44
  2. Jackson 1960, p. 448
  3. "Tipsy Junior: Advanced Performance of Diminutive Single-seater on 60 h.p." Flight. 31 July 1947. p. 115. Archived from the original on 5 March 2016.
  4. Taylor 1974, pp. 44
  5. The Ultimate Tipsy Site Archived September 29, 2007, at the Wayback Machine
  6. G-AMVP accident
  7. CAA G-AMVP

Bibliography
Wikimedia Commons has media related to Tipsy Junior.
  • Taylor, H.O. (1974). Fairey Aircraft since 1915. London: Putnam Publishing. ISBN 0-370-00065-X.
  • Jackson, A.J. (1960). British Civil Aircraft 1919-59 Vol.II. London: Putnam Publishing.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 90.
  • Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. p. 387.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.