|First flight||August 2008|
Design and development
The aircraft was designed to comply with the US FAR Part 103 Ultralight Vehicles rules as well as the German 120 kg class (called the Solo 120) and deregulated 115 kg class in the United Kingdom. It features a strut-braced high wing, a single-seat open cockpit, tricycle landing gear and a single engine in tractor configuration.
The aircraft is built with a composite fuselage and an aluminum wing. Its 8.97 m (29.4 ft) span wing has flaperons and employs a single strut on each side supported by an optional jury strut. The standard engines used when the type was introduced were the 28 hp (21 kW) Hirth F33 and the 50 hp (37 kW) Hirth F23 two-stroke powerplants.
The design offers combinations of three types of wings, three types of engines and four types of wheels.
Data from Bayerl
- Crew: one
- Wingspan: 8.97 m (29 ft 5 in)
- Wing area: 10.76 m2 (115.8 sq ft)
- Empty weight: 115 kg (254 lb)
- Gross weight: 220 kg (485 lb)
- Fuel capacity: 12 litres (2.6 imp gal; 3.2 US gal)
- Powerplant: 1 × Hirth F33 single cylinder, air-cooled, two stroke aircraft engine, 21 kW (28 hp)
- Maximum speed: 130 km/h (81 mph, 70 kn)
- Cruise speed: 100 km/h (62 mph, 54 kn)
- Stall speed: 44.8 km/h (27.8 mph, 24.2 kn)
- Rate of climb: 3 m/s (590 ft/min)
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 17. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Aeroplanes DAR (2014). "Company History". Retrieved 21 September 2015. CS1 maint: discouraged parameter (link)
- Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 20. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
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