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The Ava 4A was a low power flat-four (boxer engine) developed for very light aircraft in France in the 1930s. It was used by several prototypes and at least one production series.

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rdfs:label
  • Ava 4A (en)
rdfs:comment
  • The Ava 4A was a low power flat-four (boxer engine) developed for very light aircraft in France in the 1930s. It was used by several prototypes and at least one production series. (en)
dcterms:subject
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sameAs
specfuelcon
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national origin
designer
length
  • over propeller boss (en)
manufacturer
  • Ava (en)
power
  • Continuous at 2,300 rpm, maximum at 2.500 rpm (en)
ref
type
  • Air-cooled flat-four, two-stroke (en)
  • Flat-four, air-cooled two-stroke (en)
weight
  • including mounting and propeller boss. (en)
has abstract
  • The Ava 4A was a low power flat-four (boxer engine) developed for very light aircraft in France in the 1930s. It was used by several prototypes and at least one production series. (en)
coolingsystem
  • air (en)
fuelsystem
  • Amrac carburettor, rotary inlet distribution valve. One plug per cylinder, two magnetos, each firing two plugs. (en)
fueltype
general other
  • Opposing cylinders offset. Cast iron cylinders with finned, hemispherical alloy heads. Single piece nitrided steel crankshaft with roller bearings and ball thrust bearing. Light alloy crankcase. (en)
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page length (characters) of wiki page
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is Link from a Wikipage to another Wikipage of
is Wikipage redirect of
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