About: ADI Stallion

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.org associated with source document(s)
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http://dbpedia.org/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FADI_Stallion

The ADI Stallion is a US civil utility aircraft that first flew in July 1994. It is marketed in kit form for homebuilding by Aircraft Designs Inc.

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	ADI Stallion (en) ADI Stallion (fr)
rdfs:comment	The ADI Stallion is a US civil utility aircraft that first flew in July 1994. It is marketed in kit form for homebuilding by Aircraft Designs Inc. (en) L'ADI Stallion est un quadriplace utilitaire dont le prototype [N408S] a effectué son premier vol en 1994. C'est un monoplan à aile haute cantilever et train tricycle escamotable de construction composite. Cet appareil peut transporter jusqu’à 6 personnes, à condition de supprimer le coffre à bagages à l’arrière de la cabine et devient Super Stallion avec un moteur Continental TSIO-550-E. Le Stallion est commercialisé en kit par Aircraft Designs Inc et plusieurs exemplaires étaient en construction aux États-Unis et en Nouvelle-Zélande début 2001. Aucun n’avait encore obtenu de certification en janvier 2007. (fr)
foaf:depiction
dcterms:subject	High-wing aircraft Homebuilt aircraft Single-engined tractor aircraft 1990s United States civil utility aircraft Aircraft Designs aircraft
Wikipage page ID	1026942 (xsd:integer)
Wikipage revision ID	997883213 (xsd:integer)
Link from a Wikipage to another Wikipage	Monoplane Homebuilt aircraft United States of America Continental IO-550 High-wing aircraft Homebuilt aircraft Single-engined tractor aircraft 1990s United States civil utility aircraft Aircraft Designs aircraft Lancair ES Lancair IV Tricycle landing gear Walter M601 Aircraft Designs Inc Flat-six
sameAs	ADI Stallion ADI Stallion ADI Stallion ADI Stallion ADI Stallion
span ft	35 (xsd:integer)
span in	0 (xsd:integer)
span m	10.670000 (xsd:double)
stall speed kmh	115 (xsd:integer)
stall speed kts	62 (xsd:integer)
stall speed mph	71 (xsd:integer)
wing area sqft	140.100000 (xsd:double)
wing area sqm	13 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:ISBN dbt:Infobox_aircraft_type dbt:Reflist dbt:ADI_aircraft dbt:Aircontent dbt:Aircraft_specs
thumbnail	wiki-commons:Special:FilePath/2004_Hollmann_Super_Stallion.jpg?width=300
dbp:primeUnits%3F_	imp (en)
first flight	July 1994 (en)
national origin	United States of America
capacity	5 (xsd:integer)
crew	one pilot (en)
designer	Martin Hollmann (en)
height ft	9 (xsd:integer)
height in	6 (xsd:integer)
length ft	25 (xsd:integer)
manufacturer	Aircraft Designs Inc
ref	Jane's All The World's Aircraft 2003–2004. (en)
related	*Lancair IV (en)
type	Light utility aircraft (en)
has abstract	The ADI Stallion is a US civil utility aircraft that first flew in July 1994. It is marketed in kit form for homebuilding by Aircraft Designs Inc. (en) L'ADI Stallion est un quadriplace utilitaire dont le prototype [N408S] a effectué son premier vol en 1994. C'est un monoplan à aile haute cantilever et train tricycle escamotable de construction composite. Cet appareil peut transporter jusqu’à 6 personnes, à condition de supprimer le coffre à bagages à l’arrière de la cabine et devient Super Stallion avec un moteur Continental TSIO-550-E. Le Stallion est commercialisé en kit par Aircraft Designs Inc et plusieurs exemplaires étaient en construction aux États-Unis et en Nouvelle-Zélande début 2001. Aucun n’avait encore obtenu de certification en janvier 2007. (fr)
aspect ratio	8.800000 (xsd:double)
ceiling ft	32000 (xsd:integer)
ceiling m	9750 (xsd:integer)
climb rate ftmin	2600 (xsd:integer)
climb rate ms	13.200000 (xsd:double)
cruise speed kmh	474 (xsd:integer)
cruise speed kts	256 (xsd:integer)
cruise speed mph	295 (xsd:integer)
empty weight kg	998 (xsd:integer)
empty weight lb	2200 (xsd:integer)
eng1 hp	350 (xsd:integer)
eng1 kw	224 (xsd:integer)
eng1 name	Continental IO-550
eng1 number	1 (xsd:integer)
eng1 type	air-cooled turbocharged flat-six engine (en)
height m	2.900000 (xsd:double)
length in	0 (xsd:integer)
length m	7.620000 (xsd:double)
max speed kmh	493 (xsd:integer)
max speed kts	266 (xsd:integer)
max speed mph	306 (xsd:integer)
max takeoff weight kg	1784 (xsd:integer)
max takeoff weight lb	3800 (xsd:integer)

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