TYPE: Tandem-seat ultralight.

PROGRAMME: Production aircraft built at Kazan.

CUSTOMERS: At least two flying with aero club at Podolsk, Moscow region.

DESIGN FEATURES: High wing, open cockpit (with optional enclosure), pusher configuration with constant-chord, V-strut braced wings and strut-braced tailboom. Rear occupant's seat is raised.

FLYING CONTROLS: Conventional and manual. Flaps.

STRUCTURE: Duralumin tube and fabric; composites nacelle.

LANDING GEAR: Tricycle type; fixed.

POWER PLANT: One 44.7 kW (60 hp) piston engine driving a two-blade, pusher propeller.

EQUIPMENT: Ballistic parachute.

DIMENSIONS, EXTERNAL:

• Wing span: 9.80 m (32 ft 1¾ in)
• Length overall: 6.80 m (22 ft 3¾ in)

AREAS:

• Wings, gross: 14.85 m² (159.8 sq ft)

WEIGHTS AND LOADINGS:

• Weight empty: 240 kg (529 lb)
• Max T-O weight: 420 kg (925 lb)

PERFORMANCE:

• Max level speed: 65 kt (120 km/h; 75 mph)
• Normal cruising speed: 49 kt (90 km/h; 60 mph)
• Max rate of climb at S/L: 180 m (591 ft)/sec
• T-O run: 60 m (200 ft)
• Range: with max fuel: 540 n miles (1,000 km; 621 miles)
• with two crew: 162 n miles (300 km; 186 miles)

The article appears in the following publication:
Jane's All the World's Aircraft 2004-2005. Jane's Information Group Ltd. 2004. ISBN: 0-7106-2614-2