Egvoyager Voyager 203

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.

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.

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

Variants

Voyager 203 CF

Fixed landing gear model

Voyager 203 CR

Retractable landing gear model, at an additional cost of €7000.

Specifications (Voyager 203)

Data from Bayerl

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

Cruising speed: 240 km/h (149 mph; 130 kn)

Stall speed: 63 km/h (39 mph; 34 kn)

Never exceed speed: 300 km/h (186 mph; 162 kn)

Rate of climb: 7 m/s (1,400 ft/min)