About: Comp Air 10

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The Comp Air 10 is a turboprop-powered light civil utility aircraft manufactured in kit form. Very large for a homebuilt aircraft, it is configured as a mainly conventional high-wing monoplane with either taildragger or tricycle undercarriage. Its close-set twin tails are an unusual design feature for an aircraft in its class, intended to ensure that the aircraft can be parked inside standard-size hangars. A total of eleven examples had been completed and flown by the end of 2011. The company website does not list it as being in production in 2022.

Attributes	Values
rdfs:label	Comp Air 10 (en) Aerocomp Comp Air 10 (fr)
rdfs:comment	The Comp Air 10 is a turboprop-powered light civil utility aircraft manufactured in kit form. Very large for a homebuilt aircraft, it is configured as a mainly conventional high-wing monoplane with either taildragger or tricycle undercarriage. Its close-set twin tails are an unusual design feature for an aircraft in its class, intended to ensure that the aircraft can be parked inside standard-size hangars. A total of eleven examples had been completed and flown by the end of 2011. The company website does not list it as being in production in 2022. (en) L'Aerocomp Comp Air 10 est un avion monoplan utilitaire léger turbopropulsé commercialisé en kit pour la construction amateur par la société américaine Aerocomp. Cet appareil est en fait un Comp Air 8 dont le fuselage est élargi pour transporter 1 pilote et 9 passagers. Il est disponible soit avec train classique soit avec train tricycle, sa caractéristique principale étant de posséder un empennage bidérive pour faciliter le parking dans un hangar classique. L'élargissement du fuselage a en effet entraîné la nécessité d'accroître la surface verticale de l'empennage. (fr)
foaf:homepage	https://web.archive.org/web/20210920030336/http:/www.aerocompinc.com/airplanes/CA10/index.htm
dcterms:subject	Single-engined turboprop aircraft High-wing aircraft Homebuilt aircraft 1990s United States civil utility aircraft Comp Air aircraft
Wikipage page ID	1885618 (xsd:integer)
Wikipage revision ID	1104719504 (xsd:integer)
Link from a Wikipage to another Wikipage	Monoplane Turboprop Conventional landing gear Single-engined turboprop aircraft High-wing aircraft Homebuilt aircraft Hangar Archive.org 1990s United States civil utility aircraft Landing gear Comp Air aircraft Cessna 207 Walter M601D Kitplane
Link from a Wikipage to an external page	https://web.archive.org/web/20210920030336/http:/www.aerocompinc.com/airplanes/CA10/index.htm
sameAs	Comp Air 10 Comp Air 10 Comp Air 10 Comp Air 10
similar aircraft	*Cessna 207 (en)
span m	11.890000 (xsd:double)
wing area sqft	242 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Reflist dbt:Short_description dbt:Comp_Air dbt:Aero-1990s-stub dbt:Aircontent dbt:Aircraft_specs
dbp:primeUnits%3F_	kts (en)
capacity	nine passengers (en)
crew	one (en)
has abstract	The Comp Air 10 is a turboprop-powered light civil utility aircraft manufactured in kit form. Very large for a homebuilt aircraft, it is configured as a mainly conventional high-wing monoplane with either taildragger or tricycle undercarriage. Its close-set twin tails are an unusual design feature for an aircraft in its class, intended to ensure that the aircraft can be parked inside standard-size hangars. A total of eleven examples had been completed and flown by the end of 2011. The company website does not list it as being in production in 2022. (en) L'Aerocomp Comp Air 10 est un avion monoplan utilitaire léger turbopropulsé commercialisé en kit pour la construction amateur par la société américaine Aerocomp. Cet appareil est en fait un Comp Air 8 dont le fuselage est élargi pour transporter 1 pilote et 9 passagers. Il est disponible soit avec train classique soit avec train tricycle, sa caractéristique principale étant de posséder un empennage bidérive pour faciliter le parking dans un hangar classique. L'élargissement du fuselage a en effet entraîné la nécessité d'accroître la surface verticale de l'empennage. Le prototype [N4105T] vole en 2002, un second exemplaire a été immatriculé en 2004 et deux en 2005. (fr)
climb rate ftmin	2000 (xsd:integer)
empty weight lb	2750 (xsd:integer)
eng1 name	Walter M601D
eng1 shp	657 (xsd:integer)
eng1 type	turboprop (en)
height m	2.640000 (xsd:double)
length m	9.450000 (xsd:double)
max speed mph	222 (xsd:integer)
max takeoff weight lb	5200 (xsd:integer)
range miles	918 (xsd:integer)
prov:wasDerivedFrom	wikipedia-en:Comp_Air_10?oldid=1104719504&ns=0
page length (characters) of wiki page	2777 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Comp_Air_10
is Link from a Wikipage to another Wikipage of	List of aircraft (Co–Cz) Comp Air Aerocomp Comp Air 10
is Wikipage redirect of	Aerocomp Comp Air 10
is foaf:primaryTopic of	wikipedia-en:Comp_Air_10

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