Girish Mahajan (Editor)

Delta Pegass

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

Contents

Design

The Pegass is a strut-braced high-wing monoplane powered by either a 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.

Specifications (Rotax 912UL)

Data from Jane's All the World's Aircraft 2004-05

General characteristics

  • Crew: 1
  • Capacity: 1
  • Length: 5.70 m (18 ft 8½ in)
  • Wingspan: 10.19 m (33 ft 5¼ in)
  • Height: 2.37 m (7 ft 9¼ in)
  • Wing area: 14.36 m2 (153.5 ft2)
  • 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)
  • Stall speed: 65 km/h (41 mph)
  • Endurance: 4 hours  0 min

    • References

    Delta Pegass Wikipedia
    (Text) CC BY-SA


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