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

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

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

• Airsport Song
• North Wing Maverick
• Spacek SD-1 Minisport
• TechProAviation Merlin 100

Specifications (JCV 360)

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

General characteristics

• Type: Twin cylinder, horizontally-opposed, four stroke aircraft engine
• Bore: 63 mm (2.5 in)
• Stroke: 58 mm (2.3 in)
• Displacement: 360 cc (22.0 cu in)
• Length: 580 mm (22.8 in)
• Width: 340 mm (13.4 in)
• Height: 360 mm (14.2 in)
• Dry weight: 30.5 kg (67.2 lb)

Components

• Fuel type: gasoline
• Cooling system: liquid
• Reduction gear: poly V belt reduction drive, reduction ratio of 2.76:1

Performance

• Power output: 35 hp (26 kW) at 7800 rpm
• Compression ratio: 11:1

See also

• Verner VM 133

Related lists

• List of aircraft engines

References

External links

• Photo of the JCV 360

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