The Aviatika-890U

Aviatika-890U is a dual seater multipurpose airplane combines the advantages of "ultralights" and of traditional light planes. This airplane is made to be used in pilot training flights, air tourism, aerial photography, patrolling of forests, roads, electric- and pipelines, etc.

It's a wire-braced with a fabric covering of wings, control surfaces and tail units, with tricycle fixed undercarriage and controllable nose wheel airplane. The planes have a closed heated cockpit with an excellent pilot view.

Performed calculations and static tests provide high strength of the plane, including a force "triangle" to protect pilots in emergency.

The planes are easy to fly, its flight characteristics allow to perform aerobatics elements. Nicely harmonized controls and an excellent pilot view from the cockpit make the plane extremely safe and pleasant for piloting.

Aviatika-890U may to be delivered with float and ski landing gear.

The airplanes are being produced by a leading aviation company in Russia, Federal State Unitary Enterprise Russian Aircraft Corp. "MIG", well-known in the world for its MIG-29 fighter.

The Aviatika-890U is designed in accordance with JAR VLA and FAR-23 regulations.

The fuselage is made from aluminum tubes. The cockpit is fully enclosed with two doors with glazing. The cockpit is made from glass-fibre glass.

Wings are wire-braced. Beams are made from aluminum tubes. Ribs are the pressed components, made from aluminum alloy. Wings are fabric covered.

Tail is strut- and wire-braced, made from fabric covering aluminum tubes.

Landing gear - tricycle. The spring of main gear is made from titanium alloy. Main wheels (tire 300x125) are equipped with brakes. The nose wheel (tire 300x125) is controlled by pedals.

Standard Instruments

• speed indicator
• compass
• vertical speed indicator
• altimeter
• bank indicator
• tachometer
• VDO CHT
• VDO oil temperature indicator
• VDO oil pressure indicator

Power plant

Aviatika-890U is delivered with Rotax-912UL engine.

Rotax-912UL engine is a four stroke, petrol, four-cylinder engine. A three-blade Warp propeller, ground adjustable, is used for engine.

Specifications

Engine type	Rotax-912UL
Engine power, hp	80(95)
Max takeoff weight, kg	540
Empty weight, kg	298
Mass of fuel (in main tanks), kg	37
Maximal speed of horizontal flight, km/h	130
Cruising speed of flight, km/h	90...100
Take-off speed, km/h	70...75
Landing speed, km/h	70...75
Maximal rate-of-climb, m/sec	3.2...3.5
Take-off run, m	90
Landing run, m	150
Allowed speed of cross-wind at take-off, m/sec	6
Allowed speed of head wind at take-off and landing, m/sec	10
Allowed speed of tail wind at landing, m/sec	2
Service ceiling, m	2600
Duration of flight	3h. 04min.
Total wing area, sq. m	14.29
Upper wing span, m	8.11
Plane length, m	5.5
Parking height, m	2.25