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LOM M137





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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]

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

Design and development

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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

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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

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Specifications (M132A)

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Data from Tacke and manufacturer[1][2]

General characteristics

Components

Performance

See also

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Related development

Related lists

References

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  1. ^ a b c d e Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  • ^ a b c d LOM Praha. "M137A / M137AZ". www.pistovemotory.cz. Retrieved 19 March 2018.
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    Retrieved from "https://en.wikipedia.org/w/index.php?title=LOM_M137&oldid=1021136310"
      



    Last edited on 3 May 2021, at 02:54  





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    ●This page was last edited on 3 May 2021, at 02:54 (UTC).
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