Avions Fairey Junior
| Tipsy Junior | |
|---|---|
| 300px | |
| Tipsy Junior G-AMVP at a UK airshow in 1953 | |
| Role | Sports plane |
| Manufacturer | Avions Fairey |
| Designer | Ernest Tips |
| First flight | 30 June 1947 |
| Number built | 2 |
The Avions Fairey Junior, also known as the Tipsy Junior was a single-seat light aircraft built in Belgium following World War II.
Contents
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
Data from [2]
General characteristics
- Crew: one pilot
- Length: 5.65 m (18 ft 6 in)
- Wingspan: 6.90 m (22 ft 8 in)
- Height: 1.48 m (4 ft 10 in)
- Wing area: 10.5[5] m2 (113 ft2)
- Empty weight: 220 kg (486 lb)
- Gross weight: 350 kg (770 lb)
- Powerplant: 1 × Walter Mikron II inverted inline engine, 46 kW (62 hp)
Performance
- Maximum speed: 174 km/h (108 mph)
- Cruising speed: 158 km/h (98 mph)
- Range: 690[5] km (430 miles)
- Service ceiling: 1,800[5] m (6,000 ft)
References
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Wikimedia Commons has media related to Tipsy Junior. |
Notes
- ↑ Taylor 1974, pp. 39–44
- ↑ 2.0 2.1 2.2 2.3 Jackson 1960, pp. 448
- ↑ 3.0 3.1 Flight Tipsy Junior
- ↑ 4.0 4.1 Taylor 1974, pp. 44
- ↑ 5.0 5.1 5.2 5.3 5.4 5.5 5.6 The Ultimate Tipsy Site
- ↑ G-AMVP accident
- ↑ CAA G-AMVP
Bibliography
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