| Meadowlark | |
|---|---|
| Role | Ultralight aircraft |
| National origin | United States |
| Manufacturer | Meadowlark Ultralight Corporation |
| Designer | Jim Higgs |
| Introduction | 1982 |
| Status | Production completed |
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. [1] [2]
The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 251 lb (114 kg). It features a strut-braced high-wing, a single-seat, open cockpit, tricycle landing gear and a single engine in tractor configuration. [1] [2]
The aircraft fuselage is made from aluminum tubing. Its 35 ft (10.7 m) 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 30 hp (22 kW) is mounted in front of the wing, above the pilot. [1] [2]
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. [1]
Data from Cliche and the Virtual Ultralight Museum [1] [2]
General characteristics
Performance
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