Davis DA-2
http://dbpedia.org/resource/Davis_DA-2 an entity of type: Thing
The Davis DA-2 is a light aircraft designed in the United States in the 1960s and was marketed for homebuilding. While it is a low-wing monoplane of largely conventional design with fixed tricycle undercarriage, the DA-2 is given a distinctive appearance by its slab-like fuselage construction and its V-tail. The pilot and a single passenger sit side-by-side. Construction of the aircraft is sheet aluminum throughout, with the sole compound curves formed a fiberglass cowling and fairings.
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Davis DA-2
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15812817
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imp
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1966-05-21
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Private pilot owners
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1
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One pilot
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5
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5
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17
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Popular Mechanics August 1973
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Civil utility aircraft
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$2300 in 1971
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The Davis DA-2 is a light aircraft designed in the United States in the 1960s and was marketed for homebuilding. While it is a low-wing monoplane of largely conventional design with fixed tricycle undercarriage, the DA-2 is given a distinctive appearance by its slab-like fuselage construction and its V-tail. The pilot and a single passenger sit side-by-side. Construction of the aircraft is sheet aluminum throughout, with the sole compound curves formed a fiberglass cowling and fairings. The prototype made its first flight on May 21, 1966, and was exhibited at that year's Experimental Aircraft Association annual fly-in, where it won awards for "most outstanding design" and "most popular aircraft". A major design consideration was ease of assembly for a first time home aircraft builder. Examples of this include: few curved components, a V-tail is one less control surface to build, and each wing is made from two sheets of aluminum with no trimming involved. The DA-3 was a single DA-2 enlarged to accommodate four people. Work proceeded through 1973-74, but the aircraft was never completed. Plans have been intermittently available over the years. They are as of August 2019, available from D2 Aircraft.
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Continental A65 horizontally-opposed four-cylinder piston engine
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1
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510
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1125
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1.65
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ca. 45 by 1985
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2300.0