Zenith Gemini CH-620
Zenith Aircraft · Canada · first flew 1996 · light aircraft
The Zenith Gemini CH 620 is a twin-engine, two-seat light aircraft designed to be competitive in the single-engine market.
Recognition (WEFT)
| W — Wings | Low-mounted, tapered |
|---|---|
| E — Engines | 2 × piston, wing-mounted |
| F — Fuselage | 5.79 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Low-wing monoplane
- Two tractor piston engines of 80 hp each
- Two-seat light aircraft
Look for a very small low-wing two-seater with an engine on each wing.
Specifications
- The Zenith Gemini CH-620 has a length of 5.79 m (19 ft).
- It has a wingspan of 8.31 m (27 ft).
- Its maximum speed is 249 km/h (155 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
The Canadian-designed Gemini was designed by Chris Heintz and flew on 23 July 1996.
Variants
Kit production was never started.
Where you'll see it
It was a twin-engined touring light aircraft built by Zenith Aircraft.
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