TYPE: Side-by-side ultralight.
DESIGN FEATURES: Low-mounted wing and tailplane; sweptback fin. Fuselage waisted aft of cockpit for weight saving.
FLYING CONTROLS: Conventional and manual. No aerodynamic balances. Trim tab in starboard elevator. Flaps.
STRUCTURE: Composites, except aluminium alloy control surfaces. Sandwich fuselage constuction.
LANDING GEAR: Tricycle type; fixed. Fuselage-mounted, spring composites cantilever mainwheel legs; steerable nosewheel on welded steel leg. Mainwheel hydraulic brakes. Optional wheel fairings.
POWER PLANT: One Rotax flat-four; option of 58.8 kW (78.9 hp) 912 UL, 73.5 kW (98.6 hp) 912 ULS or 76.9 kW (103.1 hp) 914. Integral, composites tank in starboard wing; capacity 68 litres (17.9 US gallons; 15.0 Imp gallons); mechanical pump for Rotax 912/912ULS; electric pump for 914. Fixed-, ground adjustable-, flight adjustable-pitch and constant-speed propeller options.
DIMENSIONS, EXTERNAL:
- Wing span: 7.66 m (25 ft 1½ in)
- Length overall: 6.065 m (19 ft 10¾ in)
- Height overall: 2.16 m (7 ft 1 in)
AREAS:
- Wings, gross: 10.05 m² (108.2 sq ft)
WEIGHTS AND LOADINGS:
- Weight empty: 255 kg (562 lb)
- Max T-O weight: 472.5 kg (1,041 lb)
PERFORMANCE:
- Never-exceed speed (VNE): 145 kt (270 km/h; 167 mph)
- Manoeuvring speed: 84 kt (156 km/h; 97 mph)
- Stalling speed, flaps and gear down: 36 kt (65 km/h; 41 mph)
- Max rate of climb at S/L: 420 m (1,378 ft)/min
- g limits: +4.43/-2.43
