Delta Pegass
Delta System-Air · Czech Republic · first flew 1995 · light aircraft
The Delta Pegass is a Czech two-seat ultralight cabin monoplane designed and built by Delta System-Air.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Two seats side by side, with a door on each side of the fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Strut-braced high wing on a cabin monoplane
- Two seats side by side, with a door on each side of the fuselage
- Single three-bladed tractor propeller and fixed tricycle landing gear
It is a strut-braced high-wing monoplane with a cabin seating two side by side. It has a fixed tricycle undercarriage and a three-bladed tractor propeller.
Specifications
- The Delta Pegass has a length of 5.7 m (19 ft).
- It has a wingspan of 10.19 m (33 ft).
- Its maximum speed is 170 km/h (106 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
The Pegass first flew in 1995. It was built by Delta System-Air in the Czech Republic.
Variants
The Pegass could be powered by either an 80 hp Rotax 912UL or a 64 hp Rotax 582UL engine.
Where you'll see it
It was an ultralight with a two-seat cabin and a door on each side of the fuselage.
Related aircraft
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