Development of the Pegazair started in 1985 by Serg Dufour of Mont-Saint-Michel, Quebec. Originally it consisted of a new set of Pega-STOL wings with retractable leading edge slats to be installed on Zenair CH 701 STOLs to replace their wings which have fixed leading edge slots. Dufour went on to develop a new fuselage and tail to match the wings. The Pegazair is a two seats in side-by-side configuration, strut-braced, high-wing monoplane with conventional landing gear. Fuselage construction is welded steel tubing with aluminum skin. The wings employ full length flaperons and leading edge slats that deploy automatically. The tailplane is slotted for slow speed authority. The prototype was outfitted with a 65 hp (48 kW) Continental A-65 engine. The design was later developed into the four-seat Tapanee Levitation 4. VARIANTS. Pegazair P80 Powered by an 80 hp (60 kW) Rotax 912UL Pegazair P100 Powered by an 80 hp (60 kW) Continental O-200 or 115 hp (86 kW) Rotax 914
