Jihlavan KP-2 Sova
Originally developed by Kappa 77 as the KP-2U Sova, this Czech ultralight first flew in May 1996 as an all-metal, low-wing, two-seat monoplane with Fowler flaps for a low stall speed and tricycle undercarriage. Jihlavan Aircraft built the type under contract from 1997 and took over full rights in 2005 before it was rebranded under the Skyleader name in 2008, making the KP-2 Sova the direct ancestor of today's Skyleader 200/600 series. Its riveted ultra-thin duralumin skin and integral fuel tanks were unusual construction choices for a homebuilt-class ultralight of its era.
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Did you know?
An all-metal, fixed-gear Czech ultralight whose design was reborn as the Skyleader brand.
Specifications
| Length | 7.2 m (24 ft) |
|---|---|
| Wingspan | 9.9 m (32 ft) |
| Height | 2.6 m (9 ft) |
| Persons on board | 2 |
| Maximum take-off weight | 0.5 t |
| Range | 520 NM (963 km) |
| Service ceiling | 15,000 ft (4,572 m) |
| Optimum ceiling | 10,000 ft (3,048 m) |
| Rate of climb | 1,300 ft/min (6.6 m/s) |
| Take-off distance | 100 m (328 ft) |
| Landing distance | 149 m (489 ft) |
| Fuel capacity | 64 l |
Curated by CatchFlights from manufacturer documents, ICAO Doc 8643 and reference works; values are left out where no source could confirm them. Sources are listed on our credits page.
In CatchFlights
In CatchFlights the Jihlavan KP-2 Sova starts as a Rare catch. The tier is an editorial judgement of how special a sighting of this type is. The more often you catch it, the closer it moves to Common for you.
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