UL-Jih Evolution
UL-Jih Sedláček · Czech Republic · first flew 2002 · light aircraft
The UL-Jih Evolution is a conventionally laid out, two-seat, high-wing, single-engine ultralight designed and built in the Czech Republic.
Recognition (WEFT)
| W — Wings | High-mounted, tapered |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 6.98 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Conventional layout with a high wing
- Single Rotax 912ULS engine
- Two-seat ultralight
Look for a conventional two-seat high-wing ultralight with a single engine in the nose.
Specifications
- The UL-Jih Evolution has a length of 6.98 m (23 ft).
- It has a wingspan of 9 m (30 ft).
- Its maximum speed is 290 km/h (180 mph).
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It was designed by Jaroslav Sedláček and first flew on 16 February 2002. It is powered by a Rotax 912ULS engine.
Variants
Two variants were available in 2010.
Where you'll see it
At least six had been built by 2005.
Related aircraft
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