Ekolot KR-030 Topaz

Source: Wikipedia, the free encyclopedia.

Ekolot KR-030 Topaz
Role
Ultralight aircraft, light-sport aircraft
National origin Poland
Manufacturer Ekolot
Status In production (2014)
Developed from Ekolot JK-05L Junior

The Ekolot KR-030 Topaz is a Polish

ultralight aircraft, designed and produced by Ekolot of Krosno. It was certified in Poland in February 2010. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly aircraft.[1][2]

Design and development

The Topaz is a development of the

side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.[1][2]

Like the Junior, the Topaz is made from composites. Its 10.76 m (35.3 ft) span wing employs an NN-1817

The use of a one-piece wing without struts gives the Topaz a 20 km/h (12.4 mph) higher cruise speed than the Junior, while resulting in the same empty weight.[1][2]

The Topaz has been accepted by the US Federal Aviation Administration as a light-sport aircraft.[4]

Specifications (KR-030 Topaz)

Data from Bayerl[1][3]

General characteristics

Performance

  • Maximum speed: 220 km/h (140 mph, 120 kn)
  • Cruise speed: 180 km/h (110 mph, 97 kn)
  • Stall speed: 65 km/h (40 mph, 35 kn)
  • Rate of climb: 6 m/s (1,200 ft/min)


References

  1. ^ a b c d e Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 44. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^
    ISSN 1368-485X
  3. ^ a b Ekolot (11 September 2008). "Technical Description". Archived from the original on 7 January 2012. Retrieved 7 June 2012.
  4. ^ Federal Aviation Administration (10 September 2014). "SLSA Make/Model Directory". Archived from the original on 16 May 2013. Retrieved 13 January 2015.

External links