Trisha Shetty (Editor)

CNA D

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CNA D

The CNA D, often known as the CNA D.4, was a four-cylinder, air-cooled, horizontally opposed engine built in Italy between 1940 and 1951 to power light aircraft.

Contents

Applications

Data from Erickson

  • Adam RA-14 Loisirs
  • Ambrosini SAI.10
  • CNA PM.1
  • CNA MPL
  • CVV Tartuca
  • Druine Condor
  • GCA Pedro
  • GCA Etabeta
  • Lombardi FL.3
  • Lombardi FL.5
  • Lombardi FL.7
  • Macchi MB.308
  • Viberti Muscal

    • Specifications

    Data from

    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

  • Power output: 45 kW (60 hp) at 2,100 rpm
  • Compression ratio: 5.3:1
  • Specific fuel consumption: 0.34 kg/kW hr (0.56 lb/hp hr)

    • References

    CNA D Wikipedia
    (Text) CC BY-SA


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