DAR Solo
| Solo | |
|---|---|
| Role | Ultralight aircraft |
| National origin | Bulgaria |
| Manufacturer | Aeroplani DAR |
| Status | In production |
| Unit cost |
€18,500 (2011) |
The DAR Solo is a Bulgarian ultralight aircraft, designed and produced by Aeroplani DAR.
The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1]
Design and development
The aircraft was designed to comply with the US light-sport aircraft rules as well as the German 120 kg class 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.[1]
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 engine is the 28 hp (21 kW) Hirth F33 two-stroke powerplant.[1]
Specifications (Solo)
Data from Bayerl[1]
General characteristics
- 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)
Performance
- Maximum speed: 130 km/h (81 mph; 70 kn)
- Cruising speed: 100 km/h (62 mph; 54 kn)
- Stall speed: 44.8 km/h (28 mph; 24 kn)
- Rate of climb: 3 m/s (590 ft/min)
References
External links
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Wikimedia Commons has media related to DAR. |
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