About: CAB Supercab

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An Entity of Type : umbel-rc:TransportationDevice_Vehicle, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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The CAB GY-30 Supercab was a two-seat light aircraft built in France in 1954, as a further development of the CAB Minicab. The design was performed by Yves Gardan, a onetime employee of French aeronautical company SIPA. Changes incorporated in the Supercab (from the Minicab) included a more powerful engine, greater wingspan, manually retractable undercarriage, and slotted flaps that replaced the split flaps of the Minicab.

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	CAB GY-30 Supercab (de) CAB Supercab (en)
rdfs:comment	Die CAB GY-30 Supercab war ein zweisitziges, als Tiefdecker ausgelegtes Leichtflugzeug, das ab 1954 in Frankreich gebaut wurde. (de) The CAB GY-30 Supercab was a two-seat light aircraft built in France in 1954, as a further development of the CAB Minicab. The design was performed by Yves Gardan, a onetime employee of French aeronautical company SIPA. Changes incorporated in the Supercab (from the Minicab) included a more powerful engine, greater wingspan, manually retractable undercarriage, and slotted flaps that replaced the split flaps of the Minicab. (en)
foaf:depiction
dcterms:subject	1950s French sport aircraft Low-wing aircraft Single-engined tractor aircraft Aircraft first flown in 1954 CAB aircraft
Wikipage page ID	11724386 (xsd:integer)
Wikipage revision ID	1079756198 (xsd:integer)
Link from a Wikipage to another Wikipage	Constructions Aéronautiques du Béarn 1950s French sport aircraft Low-wing aircraft CAB Minicab Single-engined tractor aircraft Flap (aircraft) Aircraft first flown in 1954 CAB aircraft Continental C90 SIPA 1000 dbr:Yves_Gardan Piston engine Societé Industrielle par Aeronautique
Link from a Wikipage to an external page	http://www.avionsgardan.free.fr/menu_accueil_eng_avions_gardan.htm http://www.aviafrance.com/9758.htm
sameAs	CAB Supercab CAB Supercab CAB Supercab CAB Supercab CAB Supercab
span m	8.200000 (xsd:double)
wing area sqm	10.300000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Gardan_aircraft dbt:Cite_book dbt:Commons_category dbt:Convert dbt:Dead_link dbt:Infobox_aircraft_type dbt:Reflist dbt:Short_description dbt:Aircontent dbt:Aircraft_specs
thumbnail	wiki-commons:Special:FilePath/CAB_GY-30_Supercab.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	1954-02-05 (xsd:date)
bot	InternetArchiveBot (en)
capacity	1 (xsd:integer)
crew	1 (xsd:integer)
date	January 2018 (en)
designer	dbr:Yves_Gardan
fix-attempted	yes (en)
manufacturer	Constructions Aéronautiques du Béarn
ref	Jane's All The World's Aircraft 1956–57 (en)
type	Utility aircraft (en)
has abstract	The CAB GY-30 Supercab was a two-seat light aircraft built in France in 1954, as a further development of the CAB Minicab. The design was performed by Yves Gardan, a onetime employee of French aeronautical company SIPA. Changes incorporated in the Supercab (from the Minicab) included a more powerful engine, greater wingspan, manually retractable undercarriage, and slotted flaps that replaced the split flaps of the Minicab. Seven units were constructed by CAB before the rights to the design were sold to Gardan's former employer (SIPA), who developed the design into the SIPA 1000. However, due to a downturn in the light aircraft market at that time, only three of the SIPA variant were produced before production was halted. (en) Die CAB GY-30 Supercab war ein zweisitziges, als Tiefdecker ausgelegtes Leichtflugzeug, das ab 1954 in Frankreich gebaut wurde. (de)
aspect ratio	6.500000 (xsd:double)
ceiling m	5000 (xsd:integer)
climb rate ftmin	767 (xsd:integer)
cruise speed kmh	235 (xsd:integer)
developed into	SIPA 1000
empty weight kg	400 (xsd:integer)
eng1 hp	90 (xsd:integer)
eng1 name	Continental C90
eng1 number	1 (xsd:integer)
eng1 type	air-cooled four-cylinder horizontally opposed piston engine (en)
gross weight kg	613 (xsd:integer)
height m	1.650000 (xsd:double)
length m	5.500000 (xsd:double)
max speed kmh	275 (xsd:integer)
more performance	1200.0 (second)
number built	7 (xsd:integer)
prop blade number	2 (xsd:integer)
prop name	fixed pitch (en)
gold:hypernym	Aircraft
prov:wasDerivedFrom	wikipedia-en:CAB_Supercab?oldid=1079756198&ns=0
page length (characters) of wiki page	4492 (xsd:nonNegativeInteger)
number built	7 (xsd:nonNegativeInteger)
designer	dbr:Yves_Gardan
manufacturer	Constructions Aéronautiques du Béarn
foaf:isPrimaryTopicOf	wikipedia-en:CAB_Supercab
is Link from a Wikipage to another Wikipage of	List of civil aircraft

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