DAR Solo

Last updated

Solo
DAR Solo hangar.jpg
Role Ultralight aircraft
National origin Bulgaria
Manufacturer Aeroplanes DAR
DesignerTony Ilieff
First flightAugust 2008
StatusIn production
Produced2008-present

The DAR Solo is a Bulgarian ultralight aircraft, designed by Tony Ilieff and produced by Aeroplanes DAR, first flying in August 2008. [1] [2]

Contents

The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft. [1] [3]

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. [1] [3]

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. [1] [3]

The design offers combinations of three types of wings, three types of engines and four types of wheels. [1]

Specifications (Solo)

DAR Solo 120 powered by the Polini Thor 250 DS powerplant DAR Solo 120.jpg
DAR Solo 120 powered by the Polini Thor 250 DS powerplant

Data from Bayerl [3]

General characteristics

Performance

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References

  1. 1 2 3 4 5 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 17. Flying Pages Europe SARL, 2015. ISSN   1368-485X
  2. Aeroplanes DAR (2014). "Company History". Archived from the original on 10 August 2015. Retrieved 21 September 2015.
  3. 1 2 3 4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 20. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X