LOM M137
The LOM M137 is a Czech aircraft engine, designed and produced by LOM Praha of Prague for use in light aircraft.
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;M137AZ
Applications
- Zlín Z-50
Specifications (M132A)