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.