The LOM M137 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 six-cylinder four-stroke, in-line, displacement, air-cooled, direct drive, gasoline engine design. It employs dual magneto ignition and produces for take-off at 2750 rpm, with a compression ratio of 6.3.
Variants M137A Model for limited aerobatics, to a maximum of 5 seconds inverted flight. M137AZ Model for advanced aerobatics, including inverted flight. This model can mount an air filter.
Applications Zlín Z-50
Specifications (M132A)
See also
References
External links