About: ANEC I

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An Entity of Type : umbel-rc:TransportationDevice_Vehicle, within Data Space : dbpedia.org associated with source document(s)
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The ANEC I and ANEC II were 1920s British single-engine ultralight aircraft designed and built by Air Navigation and Engineering Company Limited at Addlestone Surrey. One was privately constructed in Brisbane, Australia.

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 umbel-rc:TransportationDevice_Vehicle
rdfs:label	ANEC I (en)
rdfs:comment	The ANEC I and ANEC II were 1920s British single-engine ultralight aircraft designed and built by Air Navigation and Engineering Company Limited at Addlestone Surrey. One was privately constructed in Brisbane, Australia. (en)
foaf:depiction
dct:subject	High-wing aircraft Single-engined tractor aircraft 1920s British civil utility aircraft ANEC aircraft Aircraft first flown in 1923
Wikipage page ID	10702160 (xsd:integer)
Wikipage revision ID	1110160866 (xsd:integer)
Link from a Wikipage to another Wikipage	English Electric Wren Anzani Horrie Miller (aviator) Richard Ormonde Shuttleworth United Kingdom Genairco Biplane Monoplanes Australia Brisbane Brooklands Addlestone High-wing aircraft Single-engined tractor aircraft Air Ministry Air Navigation and Engineering Company Bristol Cherub ABC Scorpion 1920s British civil utility aircraft ANEC aircraft Aircraft first flown in 1923 Blackburne Tomtit Surrey RAAF Base Richmond The Shuttleworth Collection Ultralight aviation Shuttleworth Collection Lympne light aircraft trials Grosvenor Trophy dbr:George_Beohm Lympne Aerodrome
Link from a Wikipage to an external page	http://www.airteamimages.com/4042.html https://web.archive.org/web/20070210110913/http:/www.britishaircraft.co.uk/aircraftpage.php%3FID=715 https://web.archive.org/web/20070210110923/http:/www.britishaircraft.co.uk/aircraftpage.php%3FID=716
sameAs	ANEC I ANEC I ANEC I ANEC I
span ft	32 (xsd:integer)
span in	10 (xsd:integer)
stall speed mph	32 (xsd:integer)
time to altitude	480.0 (second)
wing area sqft	145 (xsd:integer)
wing loading lb/sqft	3.210000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:AUS dbt:Commons_category dbt:Cvt dbt:Reflist dbt:UK dbt:Use_British_English dbt:Use_dmy_dates dbt:ANEC_aircraft dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/ANEC_II.jpg?width=300
dbp:primeUnits%3F_	imp (en)
first flight	1923 (xsd:integer)
crew	1 (xsd:integer)
designer	W.S. Shackleton (en)
height ft	3 (xsd:integer)
length ft	15 (xsd:integer)
manufacturer	Air Navigation and Engineering Company
ref	Jane's all the World's Aircraft 1924, British Civil Aviation since 1919 Volume 1 (en)
type	ultralight aircraft (en)
has abstract	The ANEC I and ANEC II were 1920s British single-engine ultralight aircraft designed and built by Air Navigation and Engineering Company Limited at Addlestone Surrey. One was privately constructed in Brisbane, Australia. (en)
empty weight lb	290 (xsd:integer)
eng1 hp	16 (xsd:integer)
eng1 name	Blackburne Tomtit
eng1 number	1 (xsd:integer)
eng1 type	2 (xsd:integer)
gross weight lb	470 (xsd:integer)

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