Ease of inspection; immediate access for servicing that is efficient and inexpensive at the same time. The comfort of the controls, the high roll rate and well-matched stick force allow for pleasant flight and easy manoeuvring even in demanding situations. A marked longitudinal stability allows for prolonged stick free flying.

All load-bearing structures are light alloy and built to meet International Standards of Air navigation.

Flight controls are traditional type with dual stick, dual rudder pedals and dual throttle knobs on dashboard. Longitudinal trim and electrical flap controls with position indicators are also located on dashboard.
Instrument panel meets General Aviation standards both in size and quality allowing for installation of a wide variety of flight instrumentation inclusive of IFR, engine controls and com/nav apparatus.
Main gear features steel springs while nose gear features a steerable wheel with rubber damper. Specifically designed wheel fairing complete their efficiency.

Wing profile and tips feature new design and meet requirements for added speed.
New engine cowling, greater windshield slope and new fairing that joins harmoniously the cabin area with the vertical tail tangibly reduce aerodynamic drag.
Rear visibility is improved with the addition of a third window on the aft fairing.
The cabin features a wide windshield with view unhindered by structural elements. Visibility while turning is also improved by the tapering of the inboard wing roots. Doors feature elbow housings for added comfort and allow for easy access to cabin. Side-by-side seats are adjustable and feature three point attachment safety belts.

Engine cowling is made up two parts and allows for quick and complete opening.
Fuel tanks are integral part of the wing structure and feature 35 or 50 litre capacity per each half wing. Fuel feed is via an engine driven pump.

ENGINE IS FOUR STROKE, FOUR OPPOSING CYLINDERS
AUTOMOBILE GRADE FUEL
* ROTAX 912 S - 73,5 kW (100 hp) REDUCTION GEARBOX 1:2,428