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The CNA C.II was a small, air-cooled, two cylinder horizontally opposed aircraft engine designed and built in Italy in the late 1930s.

C.II
Type Horizontally opposed air-cooled twin
National origin Italy
Manufacturer Compagnia Nazionale Aeronautica (CNA)
Produced 1937-41

Design


The low power, unsupercharged C.II had offset cylinders with special steel barrels and light alloy cylinder heads. The pistons were light alloy castings; the connecting rods were heat treated chrome-nickel steel, with split big ends. The CN.II had a one piece chrome-nickel steel crankshaft running in two roller bearings, with a ball thrust bearing. The crankcase was a one piece light alloy casting.[1]


Applications


Data from Erickson[2]


Specifications


Data from Jane's All the World's Aircraft 1938[1]

General characteristics

Components

Performance


References


  1. Grey, C.G. (1972). Jane's All the World's Aircraft 1938. London: David & Charles. p. 68d. ISBN 0715 35734 4.
  2. Erickson, Jack. "Horizontally Opposed Piston Aero Engines: C.N.A." Retrieved 21 March 2012.



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