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INSTALLATION, OPERATING, MAINTENANCE—JCV 360
JCV MOTOR s.r.o. , Vikýřovice 562, 788 13, Šumperk, Czech Republic—Europe, www.vernermotor.com, [email protected]
WARNING :
THIS AIRCRAFT ENGINE DOES NOT COMPLY WITH FEDERAL SAFETY
REGULATIONS FOR STANDARD AIRCRAFT. THIS IS FOR USE IN EXPERIMENTAL
AND MICROLIGHT UNCERTIFIED AIRCRAFT ONLY IN CIRCUMSTANCES IN
WHICH ENGINE FAILURE WILL NOT COMPROMISE SAFETY. READ OPERATOR‘S
MANUAL BEFORE OPERATING THE ENGINE.
1. Basic Technical Specifications
The following notes are the installation, operating and maintenance instructions for the JCV
360 engine. It is highly recommended that users of the engine familiarize themselves with
the contents of these pages before installing the engine and adhere to the given instructions
fully and in every respect throughout the operational life of the engine.
Type
JCV 360
Displacement
360 cc / 23.06 cubic inches
Bore
63 mm / 2.47 inches
Stroke
58 mm / 2.28 inches
Compression ratio
1:11
Maximum power
35 BHP (25,7 kW) @ 7800 RPM
Max. continuous power
26 BHP (19,1kW) @ 6000 RPM
Torque
33 Nm @ 7000 RPM
Propeller rotation
CCW (tractor propeller)
Weight
dry weight: 26,4 kg (58 lb)
Spark plugs
NGK CR9EK or equivalent
Spark plug gap
0.5 mm (0.02 inch)
Electric starter
18V - 24V / 370W
Generator (alternator)
12V / 100W 50 VAC no load
Lubrication
semi-synthetic 4 stroke motorcycle JASO MA oil
Fuel
motor petrol, octane number 95 (USA 92)
Fuel pump
vacuum Mikuni
Carburetors
2 x Walbro WB-37-1
Reduction drive
2,76 : 1, via belt (width 42 mm, lenght 610 PJ), (USA 240J/18)
Propeller hub
Ø75 - 6 x M8, Ø70 - 6 x M6, Ø50 - 6 x M6
Weight
cooler - 0.74 kg, oil 1l ~ 0.8 kg, water 1l ~ 1 kg, exhaust - 1.6 kg