About: MacDonald S-20

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An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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The MacDonald S-20 is a single-seat sport aircraft that was designed in the United States in the early 1970s and marketed for home building. The aircraft is a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage and an open cockpit. Construction is of metal throughout, with a forward fuselage of welded steel tube construction, with the rear fuselage built up of aluminium bulkheads and longerons. The wings and tail are also of aluminium construction, and the entire aircraft is skinned in the same material. Pop rivets are used extensively to simplify construction.

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	MacDonald S-20 (en)
rdfs:comment	The MacDonald S-20 is a single-seat sport aircraft that was designed in the United States in the early 1970s and marketed for home building. The aircraft is a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage and an open cockpit. Construction is of metal throughout, with a forward fuselage of welded steel tube construction, with the rear fuselage built up of aluminium bulkheads and longerons. The wings and tail are also of aluminium construction, and the entire aircraft is skinned in the same material. Pop rivets are used extensively to simplify construction. (en)
dcterms:subject	Aircraft first flown in 1972 Low-wing aircraft Homebuilt aircraft 1970s United States sport aircraft
Wikipage page ID	19854745 (xsd:integer)
Wikipage revision ID	1048038461 (xsd:integer)
Link from a Wikipage to another Wikipage	Monoplane Homebuilt aircraft United States Volkswagen air-cooled engine Conventional landing gear Low-wing Aircraft first flown in 1972 Low-wing aircraft Fuselage Aluminium Homebuilt aircraft 1970s United States sport aircraft Longeron Pop rivet
Link from a Wikipage to an external page	http://macdonalds21.com
sameAs	MacDonald S-20 MacDonald S-20 MacDonald S-20 MacDonald S-20
span ft	25 (xsd:integer)
span in	0 (xsd:integer)
span m	7.620000 (xsd:double)
wing area sqft	94 (xsd:integer)
wing area sqm	8.700000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Cite_web dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	imp (en)
first flight	1972-03-09 (xsd:date)
national origin	United States (en)
crew	One pilot (en)
designer	Robert A. MacDonald (en)
height ft	5 (xsd:integer)
height in	3 (xsd:integer)
length ft	18 (xsd:integer)
manufacturer	Homebuilt aircraft
ref	Jane's All the World's Aircraft 1977–78, 547 (en)
type	Sport aircraft (en)
has abstract	The MacDonald S-20 is a single-seat sport aircraft that was designed in the United States in the early 1970s and marketed for home building. The aircraft is a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage and an open cockpit. Construction is of metal throughout, with a forward fuselage of welded steel tube construction, with the rear fuselage built up of aluminium bulkheads and longerons. The wings and tail are also of aluminium construction, and the entire aircraft is skinned in the same material. Pop rivets are used extensively to simplify construction. The S-20 designation was applied to the prototype (registration N106AB), while aircraft built from the plans were designated S-21. In 2009 and 2010 changes were made to the original design to add a cockpit canopy, engine cowling and electrical system, including an avionics bus and starter motor. Aircraft with these changes are designated S-22. (en)
climb rate ftmin	850 (xsd:integer)
climb rate ms	4.300000 (xsd:double)
empty weight kg	206 (xsd:integer)
empty weight lb	456 (xsd:integer)
eng1 hp	53 (xsd:integer)
eng1 kw	40 (xsd:integer)
eng1 name	converted Volkswagen automotive engine (en)
eng1 number	1 (xsd:integer)
gross weight kg	326 (xsd:integer)
gross weight lb	720 (xsd:integer)
height m	1.600000 (xsd:double)
length in	6 (xsd:integer)
length m	5.640000 (xsd:double)
max speed kmh	177 (xsd:integer)
max speed mph	110 (xsd:integer)
number built	100 (xsd:integer)
range km	404 (xsd:integer)
range miles	251 (xsd:integer)
gold:hypernym	Aircraft
prov:wasDerivedFrom	wikipedia-en:MacDonald_S-20?oldid=1048038461&ns=0
page length (characters) of wiki page	3705 (xsd:nonNegativeInteger)
number built	100 (xsd:nonNegativeInteger)
manufacturer	Homebuilt aircraft
origin	United States
foaf:isPrimaryTopicOf	wikipedia-en:MacDonald_S-20
is Link from a Wikipage to another Wikipage of	List of aircraft (Ma) MacDonald S-21
is Wikipage redirect of	MacDonald S-21
is foaf:primaryTopic of	wikipedia-en:MacDonald_S-20

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