CNA D
From Wikipedia, the free encyclopedia
The CNA D was a four-cylinder, air-cooled, horizontally-opposed engine built in Italy between 1939 and 51 to power aircraft.
[edit] Specifications
- Bore: 100 mm (3.9 in)
- Stroke: 95 mm (3.7 in)
- Displacement: 3.0 L (182 cu in)
- Power: 45 kW (60 hp)
- Weight: 80 kg (180 lb)
[edit] Applications
- Adam RA-14 Loisirs
- Ambrosini SAI.10
- CNA PM.1
- CNA MPL
- CVV Tartaca
- Druine Condor
- GCA Pedro
- GCA Etabeta
- Lombardi FL.3
- Lombardi FL.5
- Lombardi FL.7
- Macchi MB.308
- Viberti Muscal
[edit] References
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