LOM M137 explained
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.
[1] Design and development
The engine is a six-cylinder four-stroke, in-line, 59701NaN1 displacement, air-cooled, direct drive, gasoline engine design. It employs dual magneto ignition and produces 132.40NaN0 for take-off at 2750 rpm, with a compression ratio of 6.3.[1] [2]
Variants
- M137A
Model for limited aerobatics, to a maximum of 5 seconds inverted flight.[1] [2]
- M137AZ
Model for advanced aerobatics, including inverted flight. This model can mount an air filter.[1] [2] Applications
Notes and References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015.
- Web site: M137A / M137AZ. 19 March 2018. LOM Praha . www.pistovemotory.cz.
