LOM M132

LOM M132
TypeAircraft engine
National originCzech Republic
ManufacturerLOM Praha s.p.

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, 3,980 cc (242.9 cu in) displacement, air-cooled, direct drive gasoline engine design. It employs dual magneto ignition and produces 90 kW (121 hp) 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)

Data from Tacke and manufacturer

General characteristics

Components

Performance

See also

Related development

Related lists

References

  1. 1 2 3 4 5 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. 1 2 3 4 LOM Praha. "M132A / M132AK". www.pistovemotory.cz. Retrieved 19 March 2018.
  3. ↑ Gordon, Yefim; Komissarov, Sergey (2013). Unflown Wings: Soviet and Russian Unrealised Aircraft Projects 1925-2010. Manchester: Créey Publishing. p. 472.