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| Meadowlark Ultralight Meadowlark ： ウィキペディア英語版 |
Meadowlark Ultralight Meadowlark
The Meadowlark Ultralight Meadowlark is an American ultralight aircraft that was designed by Jim Higgs and produced by the Meadowlark Ultralight Corporation. The Meadowlark was supplied only as a factory completed aircraft.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-24. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕
==Design and development==
The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . It features a strut-braced high-wing, a single-seat, open cockpit, tricycle landing gear and a single engine in tractor configuration.〔〔
The aircraft fuselage is made from aluminum tubing. Its span wing is constructed in a similar manner to the Ultraflight Lazair's wing. It is built from D-cell spar and leading edge, with foam ribs bonded to the spar. The wing is then covered with transparent Mylar film for covering. The wing incorporates a quick-folding mechanism that allows it to be folded back along the fuselage for ground transport or for storage. The pilot is accommodated on an open seat without a windshield. The landing gear features suspension on all wheels and a steerable nosewheel. The Cuyuna 430R engine of is mounted in front of the wing, above the pilot.〔〔
Due to its introduction just before the collapse of the US ultralight industry in 1984, the design was not a commercial success and only a small number were completed and sold.〔
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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