The Egvoyager Voyager 203 is an Italian ultralight aircraft, designed and produced by Egvoyager and introduced in May 2011. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly aircraft.[1]

Design and development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy with gull-winged doors, fixed, or optionally retractable, tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft is made from composites. Its 8.0 m (26.2 ft) span wing employs flaps. The standard engine available is a 100 hp (75 kW) Rotax 912ULS four-stroke powerplant. The basic model is the Voyager Fly, with the Voyager Club and the Voyager Style being models with options included as standard equipment.[1]

A light-sport aircraft category version is planned for the United States market.[1]

Variants

Voyager 203 CF
Fixed landing gear model[1]
Voyager 203 CR
Retractable landing gear model, at an additional cost of €7000.[1]

Specifications (Voyager 203)

Data from Bayerl[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wingspan: 8.0 m (26 ft 3 in)
  • Empty weight: 278 kg (613 lb)
  • Gross weight: 472.5 kg (1,042 lb)
  • Fuel capacity: 88 litres (19 imp gal; 23 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)

Performance

  • Cruise speed: 240 km/h (150 mph, 130 kn)
  • Stall speed: 63 km/h (39 mph, 34 kn)
  • Never exceed speed: 300 km/h (190 mph, 160 kn)
  • Rate of climb: 7 m/s (1,400 ft/min)


References

  1. ^ a b c d e f g Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 44. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
Allikas: http://en.wikipedia.org/wiki/Egvoyager_Voyager_203
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