The Benz Bz.II was a six-cylinder, water-cooled, inline engine developed in Germany for use in aircraft in 1913. With a displacement of 14.3 L (875 cu in), it developed 75 kW (100 hp) at 1,200 rpm. It had cast-iron cylinders and the valves were operated by dual camshafts.
Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 22–23.
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