Aircraft is single engine, single seat braced biplane with beam type fuselage, empennage of the standard cruciform design, with wing/control surfaces/empennage fabric covering, three wheel non-retractable LG of the spring type with the nose steering and closed type cockpit.

Aircraft was designed in compliance with the standards JAR and VLA FAR-23. On aircraft, in the rear and above the cockpit the "ROTAX-912A" four-stroke opposed (two cylinders opposite other two) piston engine of 80 h.p, with pusher prop, single central camshaft beneath the crankshaft is installed. Engine has liquid-cooling for cylinders head and air-cooling for cylinders walls.

Prop drive is provided thru the gearbox with impact integral absorber.

Prop – double blade, made of wood, constant pitch, pusher type.

Fuel: ROTAX-582 – avgas with octane number 92, not less, in mixture with oil  SUPER or ROTAX-912 – avgas with octane number 92, not less.

Aircraft structure and equipment allow to climb up to altitude of 3,000 m in VFR conditions from ground and paved RWY.

Good aerodynamic design allows high maneuverability and perfect take-off and landing performance.

Aircraft is good for TO and landing from paved, ground and grass RWYs.

On the Customer’s request aircraft can be equipped with float and ski LG.

The "Aviatika-MAI-890" aircraft family designers and manufacture developers were granted the Government Premium of Russian Federation in the science and technics for 1999 year. Aircraft is in operation with more than 20 countries, including USA, SAR, UK, France, Italy, Spain, Brazil and is certified there in the  "Ultra-light" category. The "Aviatika-MAI-890" aircraft is certified in Russian Federation.

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