CNA D
| D | |
|---|---|
| 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 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 (variant)
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
- 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)[2]
References
- 1 2 3 Erickson, Jack. "Horizontally Opposed Piston Aero Engines: C.N.A.". Retrieved 21 March 2012.
- ↑ Bridgman, Leonard (1942). Jane's All the World's Aircraft 1942. London: Sampson Low, Marston & Co. p. 36d.
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