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LOM M132

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.

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

Specifications (M132A)

See also

References

External links