The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.^[1][2][3]

The aircraft is made predominantly from welded steel tubing, with its flying surfaces covered in doped aircraft fabric. Its 9.40 m (30.8 ft) span wing, has an area of 15.04 m² (161.9 sq ft) and it constructed using a welded steel tube lattice spar, aluminium tube ribs and a laminate leading edge. The standard engine is the 80 hp (60 kW) Rotax 912UL four-stroke powerplant. The cockpit is 1.15 m (45.3 in) wide and is intended to accommodate "bulky crew".^[1][2][3]

The aircraft comes with its own open-frame trailer for ground transport.^[1][2][3]

Data from Bayerl^[1]

General characteristics

• Crew: one
• Capacity: one passenger
• Wingspan: 9.40 m (30 ft 10 in)
• Wing area: 15.04 m² (161.9 sq ft)
• Empty weight: 275 kg (606 lb)
• Gross weight: 450 kg (992 lb)
• Fuel capacity: 53 litres (12 imp gal; 14 US gal)
• Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp)
• Propellers: 3-bladed composite

Performance

• Maximum speed: 175 km/h (109 mph, 94 kn)
• Cruise speed: 150 km/h (93 mph, 81 kn)
• Stall speed: 65 km/h (40 mph, 35 kn)
• Rate of climb: 5 m/s (980 ft/min)

• Official website