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・ Robin and Linda Williams
・ Robin and Marian
・ Robin and the 7 Hoods
・ Robin and the 7 Hoods (album)
・ Robin and Wendy's Wet Weekends
・ Robin Anderson
・ Robin Andrew
・ Robin Antin
・ Robin Appleyard
・ Robin Archer
・ Robin Aristorenas
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・ Robin Armstrong (alpine skier)
・ Robin Askwith
・ Robin Atkin Downes
Robin ATL
・ Robin Attfield
・ Robin Auld
・ Robin Auld (musician)
・ Robin Austin
・ Robin Ayres
・ Robin Backhaus
・ Robin Backhaus (German swimmer)
・ Robin Bacul
・ Robin Baggett Stadium
・ Robin Bailey
・ Robin Bailey (disambiguation)
・ Robin Bailhache
・ Robin Bailie
・ Robin Bain


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Robin ATL : ウィキペディア英語版
Robin ATL

The Robin ATL (''Avion Très Léger'', "very light aircraft") is a French two-seat light aircraft designed by Avions Robin in the 1980s to meet a need for an economical two-seat aircraft to equip flying clubs. It is a single-engined monoplane with a fixed tricycle undercarriage, conventional control stick, and is, unusually, fitted with a V-tail. Due to the large bubble canopy, visibility is excellent. Its benign flight characteristics, moderate speeds and low fuel consumption, as well as some unique details, like an engine starter button which can only be pressed when the fuel selector switch is open, made the ATL a good trainer.
==Development and design==
In the early 1980s, Avions Pierre Robin started design of an ultra-lightweight two-seat light aircraft intended to meet the requirements of French flying clubs for a low-cost light trainer, as existing American training aircraft were becoming increasingly expensive, which was not helped by an unfavourable exchange rate, which resulted in a competition to supply a new light trainer, which could be mass-produced for supply to subsidised French flying clubs. Robin won the competition in 1983 with their ATL design, a single-engined low-winged monoplane with a fixed undercarriage and a V-tail. The ATL's fuselage was of Glass-reinforced plastic construction, with a wooden wing, while the V-tail is a conventional all-metal construction.〔Blech 1985, p.26.〕
The first prototype flew on 17 June 1983, powered by a single 35 kW (47 hp) JPX PAL 1300, a new design of two stroke, three-cylinder radial engine.〔 However, testing showed that the new engine was prone to vibration, and in order to speed development and certification, the prototype was re-engined with a converted Volkswagen car engine,〔''Flight International'' 26 November 1983, p.1418.〕 which formed the basis for production. As the four-cylinder car engine was heavier than the original engine, the aircraft's wings were swept forward to maintain the aircraft's centre of gravity in an acceptable position.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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