About: Caffort 12Aa

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The Caffort 12Aa was a 12-cylinder, horizontally-opposed, piston aircraft engine designed and built in France during the latter half of the 1920s.

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dbo:abstract
  • The Caffort 12Aa was a 12-cylinder, horizontally-opposed, piston aircraft engine designed and built in France during the latter half of the 1920s. (en)
dbo:wikiPageExternalLink
dbo:wikiPageID
  • 56237528 (xsd:integer)
dbo:wikiPageLength
  • 3998 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 896027861 (xsd:integer)
dbo:wikiPageWikiLink
dbp:coolingsystem
  • water-cooled (en)
dbp:firstRun
  • 1926 (xsd:integer)
dbp:fuelsystem
  • 4 (xsd:integer)
dbp:fueltype
  • Aviation gasoline (en)
dbp:manufacturer
dbp:nationalOrigin
dbp:oilsystem
  • Dry sump pressure system (en)
dbp:power
  • maximum at 2,200 rpm (en)
dbp:reductionGear
  • 0.530000 (xsd:double)
dbp:ref
  • Jane's all the World's Aircraft 1928 (en)
dbp:specfuelcon
  • 0.335000 (xsd:double)
dbp:type
  • 12 (xsd:integer)
dbp:valvetrain
  • 4 (xsd:integer)
dbp:weight
  • dry (en)
dbp:wikiPageUsesTemplate
dct:subject
rdfs:comment
  • The Caffort 12Aa was a 12-cylinder, horizontally-opposed, piston aircraft engine designed and built in France during the latter half of the 1920s. (en)
rdfs:label
  • Caffort 12Aa (en)
owl:sameAs
prov:wasDerivedFrom
foaf:isPrimaryTopicOf
is dbo:wikiPageWikiLink of
is foaf:primaryTopic of
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