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Technical data Wingspan 8,750 mm Wing area 12,24 m2 Aspect ratio 6.24 Length 5,682 mm Empty weight 300 kgf Max. take-off weight 520 kgf Load factor + 5Gs ; - 3Gs Max fuel capacity 96 litros Cabin widht 1,190 mm

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PERFORMANCE Engine (ROTAX) 912 (80 hp) 912S (100 hp) Propeller warp -drivetripá 068" idem Stall speed flaps up 41 mph 41 mph Stall speed with flaps down 36 mph 36 mph Cruising speed 108 mph 120 mph Max. cruis 115 mph 130 mph VNE 160 mph 160 mph Rate of climb 800 fpm 1000 fpm Take-off distance (land) 100 m 85 m Landing distance (land) 80 m 80 m Take-off distance (water) 150 m 100 m Landing distance (water) 100 m 100m Endurance (with 45 min of reserve) 5 horas 4,5 horas .. Note: some modifications can be made to the aircraft to meet different country requirements

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Items included in the basic kit . One piece hull made of glass fibre/Kevlar/carbon/epoxy Aluminium/glass fibre wing covered with polyester/butyrate Aluminium/glass fibre freeze type differential ailerons covered with polyester/butyrate Slotted flaps covered with polyester/butyrate Glass fibre/carbon rudder Glass fibre/carbon stabilator with antiservo and static balancing White paint finishing with polyurethane base Cushioned adjustable seats Electrical retractable landing gear Green tinted canopy  Cabin ventilation Interior finishing Pilot throttle lever Five positions electrical actuated flaps with negative deflection Manual elevator trim Hydraulic differential wheel brakes, pilot side Four position safety belts Two wing fuel tanks (45 litres each) Kevlar reinforced fuel tanks Fuselage collector fuel tank (six litres) Visual fuel quantity indicators Retractable water rudder Lead ballast for single pilot flight

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