The advantages of ALTO is its simple and comfortable piloting, which is guaranteed by the design of the wing. The rectangular wing plan and the profile with a blunt leading edge provide predictable stall characteristics and behaviour. The wing is a semi-monocoque structure and is equipped with built-in tanks with a capacity of 92 litres of fuel.

Rotax 912ULS2/3

Engine speed indicator, cylinder head temperature indicator, electric fuel gauge, oil temperature indicator, oil pressure indicator, fuel pressure indicator, carburetor preheater indicator

Flight instruments
airspeed indicator, altimeter, vertical speed indicator, compass, transverse inclinometer

Other
analog clock, Aera 660 GPS, TRIG transponder and radio

GLASS COCKPIT
At the customer's request, the dashboard can be made in the GLASS COCKPIT configuration

Access to the cockpit is secured by means of footpaths located at the trailing edge of the wing. The spacious, 110 cm wide cockpit provides plenty of room for comfortable control of the aircraft. The cockpit roof slides forward and it is mounted on rails.

The landing gear is designed as three-wheel, with front steering wheel. The main wheels are fixed to the fuselage on flexible laminate legs.The horizontal and vertical tail surfaces are of a traditional arrangement. They are made as a riveted structure with composite end arcs.Flight control transmission from the "stick" is realized by means of rods and cables. Directional steering of the front landing gear leg is coupled with pedals for changing the aircraft direction. The brakes are hydraulically controlled by a lever located on the center panel.

The rear of the fuselage is designed with a rectangular cross section with an oval upper surface. The stiffness of the structure is secured by diagonal webs. The wing-fuse link is conceived as the interconnection of the wing beams with the center plane of the airplane by means of flanged bolts.