Variants (Jihlavan)
Data from Jane's All the World's Aircraft 2011/12
- Skyleader 100
- Single seat variant, with optional rectangular or trapezoidal wing planform and powered by a the 64 hp (48 kW) Rotax 582 two-stroke engine. Was expected to be marketed starting in 2011 as a kit or complete aircraft.
- KP-2U Skyleader 150
- Original the Kappa 77 KP-2U Sova. Staggered side-by-side seating.
- KP-2 Skyleader 200
- Introduced 1996, widened cockpit to 120 cm (47 in) for true side-by-side seating. It features retractable landing gear.
- Rapid 200FC
- One-off hydrogen powered via fuel cell and electric motor Skyleader 150 conversion, first flight 20 May 2010.
- KP-5 Skyleader 500
- S-LSA version, originally the KP-5 Rapid 500. FAA approved July 2005.
- Skyleader 600
- Light-sport model introduced at the Aero show held in Friedrichshafen in 2010. It features a wider 128 cm (50 in) cockpit, revised wing tips and greater fuel capacity. Engines available include the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS and the turbocharged 115 hp (86 kW) Rotax 914 four-stroke powerplants.
Read more about this topic: Kappa 77 KP 2U-SOVA
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