About: Ameur Altania

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.org associated with source document(s)
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The Ameur Altania was a single-engine light aircraft of pusher configuration with side-by-side seats for two and a V-tail, designed in France in the 1990s. Several prototypes were built and flown, including a 15 m span motorglider version; the final prototype was constructed from carbon composites rather than glass fibre. Another version, the UCA Carbon Bird has been built by Universal Composite Aviation after the bankruptcy of Ameur Aviation.

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	Ameur Altania (en)
rdfs:comment	The Ameur Altania was a single-engine light aircraft of pusher configuration with side-by-side seats for two and a V-tail, designed in France in the 1990s. Several prototypes were built and flown, including a 15 m span motorglider version; the final prototype was constructed from carbon composites rather than glass fibre. Another version, the UCA Carbon Bird has been built by Universal Composite Aviation after the bankruptcy of Ameur Aviation. (en)
foaf:depiction
dcterms:subject	Low-wing aircraft 1990s French sport aircraft Aircraft first flown in 1995 Single-engined pusher aircraft Motor gliders V-tail aircraft
Wikipage page ID	33842097 (xsd:integer)
Wikipage revision ID	1114160816 (xsd:integer)
Link from a Wikipage to another Wikipage	Rotax 912 Monoplane Prehistory of Corsica Error analysis for the Global Positioning System Lycoming O-235 Composite material Low-wing aircraft 1990s French sport aircraft Aircraft first flown in 1995 Transponder (aviation) Fuselage Glass cockpit Single-engined pusher aircraft Aircraft canopy France V-tail Dorsal (anatomy) Pusher configuration Hydraulic brake Flap (aircraft) Motor gliders V-tail aircraft Jabiru 2200 Williams FJ22 Spar (aviation) Tricycle gear Flat four Ventral Motorglider Glass fibre Winglets dbr:Strakes
sameAs	Ameur Altania Ameur Altania Ameur Altania
span m	7.700000 (xsd:double)
stall speed kmh	65 (xsd:integer)
wing area note	gross (en)
wing area sqm	6.220000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs
thumbnail	wiki-commons:Special:FilePath/Salon_du_Bourget_20090619_016.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	1995-07-09 (xsd:date)
national origin	France
capacity	two (en)
designer	Bousad Ameur (en)
fuel capacity	328 (xsd:integer)
manufacturer	Ameur Aviation SA (en)
ref	Jane's All the World's Aircraft 2006/7 Unbuilt variant, estimated data. (en)
type	Two/four seat ultralight (en)
has abstract	The Ameur Altania was a single-engine light aircraft of pusher configuration with side-by-side seats for two and a V-tail, designed in France in the 1990s. Several prototypes were built and flown, including a 15 m span motorglider version; the final prototype was constructed from carbon composites rather than glass fibre. Another version, the UCA Carbon Bird has been built by Universal Composite Aviation after the bankruptcy of Ameur Aviation. (en)
aspect ratio	9.500000 (xsd:double)
avionics	GPS and transponder standard. Glass cockpit optional (en)
ceiling m	5500 (xsd:integer)
cruise speed kmh	260 (xsd:integer)
cruise speed note	150000.0 (second)
empty weight kg	265 (xsd:integer)
eng1 hp	80 (xsd:integer)
eng1 name	Jabiru 2200
eng1 number	1 (xsd:integer)
eng1 type	flat four piston (en)
g limits	+6/-4 (en)
glide ratio	18.500000 (xsd:double)
height m	2.300000 (xsd:double)
length m	6 (xsd:integer)
max speed kmh	287 (xsd:integer)
max takeoff weight kg	472 (xsd:integer)
max takeoff weight note	approximately (en)
never exceed speed kmh	320 (xsd:integer)
number built	c.5 (en)
prop blade number	3 (xsd:integer)

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