Verner JCV 360

JCV 360
Type Aircraft engine
National origin Czech Republic
Manufacturer Verner Motor
Major applications Airsport Song
North Wing Maverick
Spacek SD-1 Minisport
Produced up until about 2013


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, 360 cc (22.0 cu in), 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 35 hp (26 kW) 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

Specifications (JCV 360)

Data from World Directory of Leisure Aviation 2011-12[1]

General characteristics

Components

Performance

See also


Related lists

References

  1. 1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. "Internet Archive Wayback Machine". archive.org. Retrieved 30 June 2015.

External links

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