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 (60hp) piston engine driving a two-blade, pusher propeller.

EQUIPMENT: Ballistic parachute.