|Type||National origin|| Manufacturer
Design and development
The engine has two cylinders in a horizontally-opposed configuration, with cooling fins on the cylinders. The single ignition system uses capacitor discharge ignition. Fuel is metered by a single Tillotson carburetor. Starting is only by electric start, without recoil start as an option.
- Twin-cylinder, horizontally-opposed aircraft engine introduced in the mid-1990s and currently out of production. Power output is Script error: No such module "convert". at 6600 rpm.
- Twin-cylinder, horizontally-opposed aircraft engine, improved variant, currently in production. Power output is Script error: No such module "convert". at 6500 rpm.
Data from JPX
- Type: twin-cylinder, two-stroke engine
- Displacement: 319 cc (19.47 cu inches)
- Dry weight: Script error: No such module "convert". complete with standard reduction drive, carburettor, air filter, electronic ignition, starter motor and exhaust system.
- Valvetrain: 6-blade reed valve induction
- Fuel system: Tillotson carburetor
- Oil system: premixed 2.5% oil and fuel
- Cooling system: air cooled
- Power output: Script error: No such module "convert". at 6500 rpm
- Compression ratio: 8.5:1
- Fuel consumption: 2.5 litres to 6 litres per hour depending on load and cruising speed