04/30/2011. Remarks by Johan Visschedijk: "The four-seat twin-engine Mercury 6 multipurpose aircraft, developed by the aircraft company Aviation, is designed for wide range of operations: business, mail and parcel service; pilot training; power lines, oil and gas pipelines patrol; forests and fishery control; environmental studies; geological exploration; communications; intelligence. Power plants are two 140 hp LOM Praha M332A four-cylinder inverted in-line engines. Eventual production will reportedly be undertaken at the MAPO (Moscow Aviation Production Association) plant Dementyev."

Span: 33 ft 5.6 in (10.12 m)
Length: 21 ft 9.8 in (6.65 m)
Height: 10 ft 4 in (3.15 m)
Wing area: 136.16 sq.ft (12.65 sq.m)
Empty weight: 1,984 lb (900 kg)
Load: 661 lb (300 kg)
Max weight: 3,307 lb (1,500 kg)
Max speed: 217 mph (350 kmh)
Cruise speed: 162 mph (260 kmh)
Climb: to 1,181 ft (360 m)/min
Service ceiling: 13,123 ft (4,000 m)
Range: 932 mls (1,500 km)