About: Windecker Eagle

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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The Eagle AC-7 Eagle 1 (USAF designation YE-5) is an aircraft that was manufactured by Windecker Industries. It was the first composite airplane (foam and fiberglass construction) to receive FAA certification in December 1969 at a reported development cost of US$20,000,000. The fiberglass process was named "Fibaloy" by Windecker.

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
rdfs:label	Windecker Eagle (de) ウィンデッカーイーグル (ja) Windecker Eagle (en)
rdfs:comment	Die Windecker AC-7 Eagle 1 ist ein viersitziges Leichtflugzeug des US-amerikanischen Herstellers . Sie war das erste von der FAA zertifizierte Flugzeug, dessen Zelle aus glasfaserverstärktem Kunststoff (GFK) bestand. (de) ウィンデッカーイーグル（Windecker Eagle）は、初めて繊維強化プラスチックを主要構造材として実用化された飛行機。商業的には成功せず、生産数は派生型のステルス実験機YE-5を含めても9機にとどまった。 (ja) The Eagle AC-7 Eagle 1 (USAF designation YE-5) is an aircraft that was manufactured by Windecker Industries. It was the first composite airplane (foam and fiberglass construction) to receive FAA certification in December 1969 at a reported development cost of US$20,000,000. The fiberglass process was named "Fibaloy" by Windecker. (en)
dcterms:subject	Low-wing aircraft Single-engined tractor aircraft 1960s United States civil utility aircraft Aircraft first flown in 1967 Windecker aircraft
Wikipage page ID	16632695 (xsd:integer)
Wikipage revision ID	1095270252 (xsd:integer)
Link from a Wikipage to another Wikipage	United States Constant-speed propeller Lone Star Flight Museum Type certificate Low-wing aircraft US$ Windecker Industries Fuselage Single-engined tractor aircraft 1960s United States civil utility aircraft Aircraft first flown in 1967 China Windecker aircraft Windecker YE-5 Tricycle gear Flat-six Continental IO-520C
Link from a Wikipage to an external page	http://www.nasm.si.edu http://www.eaglebehindthecurtain.com/ https://web.archive.org/web/20080605175518/http:/www.eaglebehindthecurtain.com/WindeckerEagle/tabid/55/Default.aspx http://www.nasm.si.edu/collections/artifact.cfm%3Fid=A19850619000
sameAs	Windecker Eagle Windecker Eagle Windecker Eagle Windecker Eagle Windecker Eagle
span ft	32 (xsd:integer)
span in	0 (xsd:integer)
stall speed mph	66 (xsd:integer)
stall speed note	(en)
variants with their own articles	Windecker YE-5
wing area sqft	167 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Convert dbt:Reflist dbt:Short_description dbt:Use_American_English dbt:Use_mdy_dates dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	imp (en)
first flight	1967-10-07 (xsd:date)
national origin	United States
capacity	3 (xsd:integer)
crew	1 (xsd:integer)
designer	Leo and Fairfax Windecker (en)
height ft	9 (xsd:integer)
height in	5 (xsd:integer)
length ft	28.500000 (xsd:double)
manufacturer	Windecker Industries
ref	Jane's All the World's Aircraft 1971–72 (en)
type	Light aircraft (en)
has abstract	Die Windecker AC-7 Eagle 1 ist ein viersitziges Leichtflugzeug des US-amerikanischen Herstellers . Sie war das erste von der FAA zertifizierte Flugzeug, dessen Zelle aus glasfaserverstärktem Kunststoff (GFK) bestand. (de) ウィンデッカーイーグル（Windecker Eagle）は、初めて繊維強化プラスチックを主要構造材として実用化された飛行機。商業的には成功せず、生産数は派生型のステルス実験機YE-5を含めても9機にとどまった。 (ja) The Eagle AC-7 Eagle 1 (USAF designation YE-5) is an aircraft that was manufactured by Windecker Industries. It was the first composite airplane (foam and fiberglass construction) to receive FAA certification in December 1969 at a reported development cost of US$20,000,000. The fiberglass process was named "Fibaloy" by Windecker. (en)
airfoil	NACA 642415 (en)
aspect ratio	5.820000 (xsd:double)
ceiling ft	18000 (xsd:integer)
climb rate ftmin	1220 (xsd:integer)
cruise speed mph	204 (xsd:integer)
empty weight lb	2150 (xsd:integer)
eng1 hp	285 (xsd:integer)
eng1 name	Continental IO-520C
eng1 number	1 (xsd:integer)
eng1 type	air-cooled flat-six engine (en)
length m	8.700000 (xsd:double)
max speed mph	211 (xsd:integer)
max takeoff weight lb	3400 (xsd:integer)
more performance	Takeoff run to 50 ft : Landing run from 50 ft : (en)
never exceed speed mph	260 (xsd:integer)
number built	Two prototypes and six production aircraft (en)
prop blade number	2 (xsd:integer)
prop dia ft	7 (xsd:integer)

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