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The Verner JCV 360 is a Czech aircraft engine, designed and built by Verner Motor of Šumperk for use in ultralight aircraft.

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dbo:abstract
  • The Verner JCV 360 is a Czech aircraft engine, designed and built by Verner Motor of Šumperk for use in ultralight aircraft. (en)
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  • 47120401 (xsd:integer)
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  • 3349 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 959884558 (xsd:integer)
dbo:wikiPageWikiLink
dbp:compression
  • 11 (xsd:integer)
dbp:coolingsystem
  • liquid (en)
dbp:fueltype
  • gasoline (en)
dbp:lists
  • *List of aircraft engines (en)
dbp:majorApplications
dbp:manufacturer
dbp:nationalOrigin
dbp:power
  • at 7800 rpm (en)
dbp:produced
  • up until about 2013 (en)
dbp:reductionGear
  • poly V belt reduction drive, reduction ratio of 2.76:1 (en)
dbp:ref
  • World Directory of Leisure Aviation 2011-12 (en)
dbp:seeAlso
  • *Verner VM 133 (en)
dbp:type
dbp:wikiPageUsesTemplate
dct:subject
gold:hypernym
rdf:type
rdfs:comment
  • The Verner JCV 360 is a Czech aircraft engine, designed and built by Verner Motor of Šumperk for use in ultralight aircraft. (en)
rdfs:label
  • Verner JCV 360 (en)
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