CNA D
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| CNA D.4 on display at Museo Nazionale Scienza e Tecnologia Leonardo da Vinci |
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
Data from Erickson[1]
- 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 [1]
General characteristics
- Type: 4-cyl. air-cooled horizontally-opposed piston engine
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- Dry weight: Script error: No such module "convert".
Performance
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- Compression ratio: 5.3:1
- Specific fuel consumption: 0.34 kg/kW hr (0.56 lb/hp hr)[2]
See also
Related lists
References
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