Verner JCV 360 explained

The Verner JCV 360 is a Czech aircraft engine, designed and built by Verner Motor of Šumperk for use in ultralight aircraft.[1]

Design and development

The engine is a twin cylinder, 3601NaN1, horizontally-opposed four-stroke, liquid-cooled, gasoline engine design, with a poly V belt reduction drive with reduction ratio of 2.76:1. It employs a single electronic ignition and produces 350NaN0 at 7800 rpm.[1]

The engine was still advertised for sale on the company website in 2013, but by 2015 was no longer listed as available and it is likely that production has ended.[2]

Applications

External links

Notes and References

  1. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011.
  2. Web site: Verner Motor. archive.org. 30 June 2015.