Top speed 195 km/h Length 6.38 m | Wingspan 9.45 m | |
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201109 ikarus c52 c42b tracting a banner blois
The Ikarus C52 is a German ultralight aircraft, designed and produced by Comco Ikarus, introduced at the Aero show held in Friedrichshafen in 2011. The aircraft is supplied as a complete ready-to-fly-aircraft.
Contents
- 201109 ikarus c52 c42b tracting a banner blois
- Ikarus c52 auf der aero 2012
- Design and development
- Specifications C 52 Club
- References
Ikarus c52 auf der aero 2012
Design and development
An evolution of the Ikarus C42, the C52 was designed to comply with the Fédération Aéronautique Internationale microlight rules. It not only updates the older design, but offers more comforts. The C-52 is not intended to replace the C42 in production, but instead to act as a higher-end complimentary model. Like the C42, it features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed open cockpit, fixed tricycle landing gear and a single engine in tractor configuration.
The aircraft differs from the earlier C42 primarily in that the landing gear is a cantilever design, the tail is constructed of carbon fibre and the engine mount was redesigned. Its 9.45 m (31.0 ft) span wing employs V-struts with jury struts and has an area of 12.5 m2 (135 sq ft). Standard engines available are the 80 hp (60 kW) Rotax 912UL and the 100 hp (75 kW) Rotax 912ULS four-stroke powerplants.
Specifications (C-52 Club)
Data from Bayerl and Comco Ikarus
General characteristics
Performance
