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Manufacturer: Alfa Romeo
Developed: 1930s
Type: 14-cylinder air-cooled radial
Bore: 140 mm (5.512 in)
Stroke: 145 mm (5.709 in)
Displacement: 31.25 L (1,906.9 cu in)
Length: 1,044mm (41.13 in)
Width: 653mm (25.71 in)
Height: 1,195 mm (47.05 in)
Dry weight: 565 kg (1,246 lb)
Components:
Valvetrain: One intake and one sodium-cooled exhaust valve per cylinder
Fuel system: 1 Stromberg carburettor
Fuel type: 87 octane
Cooling system: air-cooled
Performance:
Take-off power: 858 hp at 2,520 rpm at sea level
Emergency Power: 947 hp at 2520 rpm at 3,000 m
Compression ratio: 6.7:1
Power-to-weight ratio: 0.67 hp/lb
Variants:
The Italian engine designation system includes a suffix indicating major components or attributes. The most common were R for Riduttore - reduction gear and C for Compressore - compressor/supercharger, followed by a number indicating the rated altitude in hundreds of metres, two speed superchargers were indicated by a double figure such as 10/34.
A.74 R.C.38
With reduction gear and supercharger, rated altitude 3,800 m (12,500 ft).
A.74 R.I.C.38
With reduction gear, fuel injection and supercharger, rated altitude 3,800 m (12,500 ft).
A.74 R.C.42
With reduction gear and supercharger, rated altitude 4,200 m (13,800 ft).
Applications:
CANSA FC.20
Fiat CR.42
Fiat G.50
Fiat RS.14
Macchi C.200
Sources:
Bridgman, Leonard (ed.) (1938). Jane's All The World's Aircraft 1938. London: Sampson Low and Marston Co. Ltd.
Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens.
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