Egvoyager Voyager 203
From Wikipedia the free encyclopedia
| Voyager 203 | |
|---|---|
| Role | Ultralight aircraft |
| National origin | Italy |
| Manufacturer | Egvoyager |
| Introduction | May 2010 |
| Status | In production |
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
[edit]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
[edit]- 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)
[edit]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)
