08/31/2010. Remarks by Johan Visschedijk: "Filip Lambert of Lambert Aircraft Engineering at Wevelgem, Belgium, used a Slovakian design as basis for the M106. This side-by-side two-seat ultralight is of metal construction covered with fabric, and is fitted with a new power plant of Belgian design, an 82 hp four-cylinder air-cooled ULPower UL260i. The airframe is produced in Slovakia, can be equipped with a nose or tail wheel, while the engine and instruments are installed in Belgium. It has foldable wings for storage or transport on a trailer."

Span: 30 ft 6.9 in (9.32 m)
Span: 8 ft 6.4 in (2.60 m) (wings folded)
Length: 20 ft 0.2 in (6.10 m)
Height: 6 ft 4.8 in (1.95 m) (tail wheel)
Height: 7 ft 0.6 in (2.15 m) (nose wheel)
Wing area: 127.01 sq.ft (11.8 sq.m)
Weight empty: 551 lb (250 kg)
Loaded weight: 1,042 lb (472.5 kg)
Max speed: 115 mph (185 kmh)
Cruise speed: 99 mph (160 kmh)
Climb: 1,000 ft (305 m)/min
Range: 435 mls (700 km)