Its constant chord wing has twin tubular aluminium spars with wooden ribs and, like the rest of the aircraft, is fabric covered.

[3] After trials with Rotax and Volkswagen engines, Lambert chose the Belgian 61 kW (82 hp) ULPower UL260i flat-four to power the M106.

The development period also produced changes to the undercarriage, which initially had V-strut main legs and half-axles.

[1][2][3] Production began in late 2005 with a batch of eight aircraft built in the Slovak Republic and assembled in Belgium.

The M106 is built to meet the European ULM maximum takeoff weight (MTOW) limits of 450 kg (992 lb) and is available only in flyaway form; the M108 variant is heavier, intended for areas which allow higher MTOWs, and may be kit built.