About: Davis DA-2

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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.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188 umbel-rc:Model_airplane
rdfs:label	Davis DA-2 (en)
rdfs:comment	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. (en)
foaf:depiction
dct:subject	Davis aircraft Low-wing aircraft Homebuilt aircraft Single-engined tractor aircraft V-tail aircraft 1960s United States civil utility aircraft Aircraft first flown in 1966
Wikipage page ID	15812817 (xsd:integer)
Wikipage revision ID	1017236856 (xsd:integer)
Link from a Wikipage to another Wikipage	Homebuilt aircraft Davis aircraft Low-wing aircraft Homebuilt aircraft Single-engined tractor aircraft EAA AirVenture Oshkosh Experimental Aircraft Association Flight International V-tail Leeon D. Davis V-tail aircraft 1960s United States civil utility aircraft Aircraft first flown in 1966 Continental A65
Link from a Wikipage to an external page	http://airbum.com/pireps/PirepDavisDA2.html http://www.yahoogroups.com/da2a http://www.davisda2.com https://www.flightglobal.com/pdfarchive/view/1977/1977%20-%202475.html
sameAs	Davis DA-2 Davis DA-2 Davis DA-2 Davis DA-2
span ft	19 (xsd:integer)
span in	3 (xsd:integer)
span m	5.860000 (xsd:double)
wing area sqft	83 (xsd:integer)
wing area sqm	7.700000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Cite_journal dbt:Cite_magazine dbt:Commons_category dbt:Infobox_aircraft_type dbt:Reflist dbt:Harvid dbt:Davis_aircraft dbt:Aircontent dbt:Aircraft_specs
thumbnail	wiki-commons:Special:FilePath/N2366Q_Davis_DA-2.jpg?width=300
dbp:primeUnits%3F_	imp (en)
first flight	1966-05-21 (xsd:date)
primary user	Private pilot owners (en)
capacity	1 (xsd:integer)
crew	One pilot (en)
designer	Leeon D. Davis
height ft	5 (xsd:integer)
height in	5 (xsd:integer)
length ft	17 (xsd:integer)
manufacturer	Homebuilt aircraft
ref	Popular Mechanics August 1973 (en)
type	Civil utility aircraft (en)
unit cost	$2300 in 1971 (en)
has abstract	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. (en)
cruise speed kmh	177 (xsd:integer)
cruise speed mph	110 (xsd:integer)
empty weight kg	277 (xsd:integer)
empty weight lb	610 (xsd:integer)
eng1 hp	65 (xsd:integer)
eng1 kw	49 (xsd:integer)
eng1 name	Continental A65 horizontally-opposed four-cylinder piston engine (en)
eng1 number	1 (xsd:integer)
gross weight kg	510 (xsd:integer)
gross weight lb	1125 (xsd:integer)
height m	1.650000 (xsd:double)
length in	10 (xsd:integer)
length m	5.440000 (xsd:double)
max speed kmh	193 (xsd:integer)
max speed mph	120 (xsd:integer)

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