The Parma Mikron III UL is a Czech aircraft engine, developed from the Walter Mikron and produced by Parma Technik sro of Luhačovice for use in ultralight aircraft.
[1] The Mikron III UL is a four-cylinder four-stroke, in-line, 2,440 cc (148.9 cu in) displacement, air-cooled, direct-drive, gasoline engine design.
It employs dual magnetos and produces 75 hp (56 kW) at 2760 rpm, with a compression ratio of 7.0:1.
[1] Data from Tacke[1] Related development
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