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, 3980 cc displacement, air-cooled, direct drive gasoline engine design. It employs dual magneto ignition and produces 90 kW 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)