The LOM M132 is a Czech aircraft engine, designed and produced by LOM Praha (Letecke Opravny Malesice, Praha) of Prague for use in light aircraft.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015.
Design and development The engine is a four-cylinder four-stroke, in-line, displacement, air-cooled, direct drive gasoline engine design. It employs dual magneto ignition and produces for take-off at 2700 rpm, with a compression ratio of 6.3.
Variants M132A Model for limited aerobatics, to a maximum of 5 seconds inverted flight. M132AK Model for advanced aerobatics, including inverted flight. Applications Fisher R-80 Tiger Moth Considered for Phönix-Aviatechnica LKhS-4 (unbuilt)
Specifications (M132A)
See also
References
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