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AIRCRAFT












ENGINE AND PROPELLER
* The top and bottom engine cowls are quickly and easily removable making any maintenance easier to accomplish. The top cowl has 2 large hinged openings for easy access to the engine compartment, without the need for tools to allow effective pre-flight inspections.
* The engine's mount is steel-tubing with shock mounts. It also supports the nose wheel that is not anchored directly to the cabin's structure.
* The power plant is a Rotax 912 ULS2 four-cylinder, four-stroke engine.
* The engine is a liquid and air cooled engine with an integrated 1:2.4286 reduction gear.
* A fixed pitch wood and composite propeller comes as standard.
* The quick drain gascolator is installed in the engine compartment with easy outside access.
* The fuel system uses a mechanical engine driven pump along is with an electrical back-up pump.
* The engine installation allows the option for an additional 40 Ah alternator.
* The battery is located in the rear of the fuselage with easy access through a hinged door.