LOM M137

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LOM M137
Avia M-137A.JPG
Avia M-137A
Type Aircraft engine
National originCzech Republic
Manufacturer LOM Praha s.p.

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]

Contents

Design and development

The engine is a six-cylinder four-stroke, in-line, 5,970 cc (364.3 cu in) displacement, air-cooled, direct drive, gasoline engine design. It employs dual magneto ignition and produces 132.4 kW (178 hp) 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

Specifications (M132A)

Data from Tacke and manufacturer [1] [2]

General characteristics

Components

Performance

See also

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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. "M137A / M137AZ". www.pistovemotory.cz. Retrieved 19 March 2018.