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CNA D

From Wikipedia, the free encyclopedia
D
CNA D.4 on display at Museo Nazionale Scienza e Tecnologia Leonardo da Vinci
Type 4-cylinder air-cooled horizontally opposed piston engine
National origin Italy
Manufacturer Compagnia Nazionale Aeronautica (CNA)

The CNA D, often known as the CNA D.4, was a four-cylinder, air-cooled, horizontally opposed engine built in Italy by Compagnia Nazionale Aeronautica (CNA) between 1940 and 1951 to power light aircraft.[1]

Applications

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Data from Erickson[1]

Specifications

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Data from [1]

General characteristics

  • Type: 4-cyl. air-cooled horizontally-opposed piston engine
  • Bore: 100 mm (3.9 in)
  • Stroke: 95 mm (3.7 in)
  • Displacement: 3 L (180 cu in)
  • Dry weight: 80 kg (180 lb)

Performance

See also

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Related lists

References

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  1. ^ a b c Erickson, Jack. "Horizontally Opposed Piston Aero Engines: C.N.A." Archived from the original on 23 April 2012. Retrieved 21 March 2012.
  2. ^ Bridgman, Leonard (1942). Jane's All the World's Aircraft 1942. London: Sampson Low, Marston & Co. p. 36d.