Delta Pegass

Pegass
General information
Type	Two-seat ultralight cabin monoplane
National origin	Czech Republic
Manufacturer	Delta System-Air
History
First flight	1995

The Delta Pegass is a Czech two-seat ultralight cabin monoplane designed and built by Delta System-Air. ^[1]

Design

The Pegass is a strut-braced high-wing monoplane powered by either an 80 hp (60 kW) Rotax 912UL or a 64 hp (48 kW) Rotax 582UL engine driving a three-bladed tractor propeller. It has a fixed tricycle landing gear and a cabin with two seats side-by-side, a door on each side of the fuselage for access. ^[1]

Specifications (Rotax 912UL)

Data fromJane's All the World's Aircraft 2004-05 ^[1]

General characteristics

• Crew: 1
• Capacity: 1
• Length: 5.70 m (18 ft 8.5 in)
• Wingspan: 10.19 m (33 ft 5.25 in)
• Height: 2.37 m (7 ft 9.25 in)
• Wing area: 14.36 m² (153.5 sq ft)
• Empty weight: 225 kg (496 lb)
• Gross weight: 450 kg (992 lb)
• Powerplant: 1 × Rotax 912UL , 60 kW (80 hp)

Performance

• Maximum speed: 170 km/h (105 mph, 91 kn)
• Stall speed: 65 km/h (41 mph, 36 kn)
• Endurance: 4 hours 0 minutes

References

Notes

1. Jackson 2004, p. 107

Bibliography

• Jackson, Paul, ed. (2004). Jane's All the World's Aircraft 2004-2005. Coulsdon, Surrey, United Kingdom: Jane's Information Group. ISBN   978-0-7106-2614-1.