The Molniya-1 six-seat aircraft is a three surface design with a forward balanced canard surface and a square section fuselage with a Vedeneyev M14P nine cylinder radial engine in the rear. Twin booms carry fins with balanced and trim tabbed rudders and a high set tailplane, similarly tabbed and balanced.
It was intended to cover a wide range of tasks including touring, cargo/mail carrying, business flights, aerial photography, patrol and air ambulance services. The three-surface configuration was intended to provide improved safety and fuel efficiency over conventional types, with the rear-mounted engine lowering cabin noise and vibration.It flew for the first time on 18 December 1992.
stats
Crew: 1
Capacity: 5 passenger / 500 kg (1,100 lb) maximum payload
Maximum speed: 322 km/h (200 mph, 174 kn)
Cruise speed: 290 km/h (180 mph, 160 kn)
Stall speed: 115 km/h (71 mph, 62 kn)
Range: 500 km (310 mi, 270 nmi) with maximum payload

