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]
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 912ULSfour-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]
egvoyager, voyager, italian, ultralight, aircraft, designed, produced, egvoyager, introduced, 2011, aircraft, supplied, amateur, construction, complete, ready, aircraft, voyager, 203role, ultralight, aircraftnational, origin, italymanufacturer, egvoyagerintrod. 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 Voyager 203Role Ultralight aircraftNational origin ItalyManufacturer EgvoyagerIntroduction May 2010Status In production Contents 1 Design and development 2 Variants 3 Specifications Voyager 203 4 References 5 External linksDesign and development EditThe aircraft was designed to comply with the Federation Aeronautique 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 EditVoyager 203 CF Fixed landing gear model 1 Voyager 203 CR Retractable landing gear model at an additional cost of 7000 1 Specifications Voyager 203 EditData from Bayerl 1 General characteristicsCrew 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 Edit 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 485XExternal links EditOfficial websitePortals nbsp Italy nbsp Companies nbsp Aviation Retrieved from https en wikipedia org w index php title Egvoyager Voyager 203 amp oldid 1126026862, wikipedia, wiki, book, books, library,
