About: Agusta GA.40

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An Entity of Type : yago:WikicatAgustaAircraftEngines, within Data Space : dbpedia.org associated with source document(s)
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The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 1960s.

Attributes	Values
rdf:type	mean of transportation yago:WikicatBoxerEngines yago:AircraftEngine102687423 yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:Instrumentality103575240 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:Whole100003553 yago:WikicatAgustaAircraftEngines
rdfs:label	Agusta GA.40 (en) Agusta GA.40 (in)
rdfs:comment	The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 1960s. (en) Agusta GA.40 adalah mesin horizontal 2-silinder, berpendingin udara, dikembangkan di Italia oleh Agusta digunakan untuk pesawat ringan. Mesin itu dimaksudkan untuk digunakan dalam motorgliders. Mesin ini diproduksi pada 1950-an dan 60-an. (in)
dcterms:subject	1950s aircraft piston engines Agusta aircraft engines Boxer engines
Wikipage page ID	31732111 (xsd:integer)
Wikipage revision ID	1113330209 (xsd:integer)
Link from a Wikipage to another Wikipage	Corby Starlet 1950s aircraft piston engines Agusta aircraft engines Agusta Aircraft engine Italy Boxer engines dbr:M._Ginnini Stromberg NAS 3A1 carburettor dbr:Octane Horizontally opposed Motorglider dbr:Kokkola_Ko-04
sameAs	Agusta GA.40 Agusta GA.40 Agusta GA.40 Agusta GA.40 Agusta GA.40 Agusta GA.40
specpower	20.990000 (xsd:double)
valvetrain	pushrod operated overhead valve, 1x inlet + 1x exhaust per cylinder (en)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Convert dbt:Refbegin dbt:Refend dbt:Reflist dbt:Infobox_Aircraft_Engine dbt:Pistonspecs dbt:AgustaWestland_aircraft
national origin	Italy
designer	dbr:M._Ginnini M. Ginnini (en)
manufacturer	Agusta
power	at 2,700rpm (en)
ref	Jane's All the World's Aircraft 1962-63 (en)
type	2 (xsd:integer)
unit cost	$685 in 1958 (en)
weight	dry (en)
has abstract	The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 1960s. (en) Agusta GA.40 adalah mesin horizontal 2-silinder, berpendingin udara, dikembangkan di Italia oleh Agusta digunakan untuk pesawat ringan. Mesin itu dimaksudkan untuk digunakan dalam motorgliders. Mesin ini diproduksi pada 1950-an dan 60-an. (in)
coolingsystem	Air-cooled (en)
first run	1955 (xsd:integer)
fuelsystem	Stromberg NAS 3A1 carburettor
fueltype	80 (xsd:integer)
oilsystem	Pressure lubrication with a gear driven pump (en)
power/weight	0.559000 (xsd:double)
gold:hypernym	Cylinder
prov:wasDerivedFrom	wikipedia-en:Agusta_GA.40?oldid=1113330209&ns=0
page length (characters) of wiki page	2434 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Agusta_GA.40
is Link from a Wikipage to another Wikipage of	List of aircraft engines Agusta
is foaf:primaryTopic of	wikipedia-en:Agusta_GA.40

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