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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 10.15 L (619.4 cu in) it developed about 75–82 kW (100–110 hp).
It had cast-iron cylinders with sheet metal cooling jackets welded to them. The two overhead valves per cylinder were operated via pushrods and rocker arms by a single camshaft embedded in the engine block on the right-hand side.
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