Aveko VL-3 Sprint

The Aveko VL-3 Sprint also called the VL-3 Evolution is a Czech ultralight aircraft, designed and initially produced by Aveko of Brno. The design is now produced by JMB Aircraft of Choceň. The aircraft is supplied as a complete ready-to-fly-aircraft.^[1][2]

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, fixed or retractable tricycle landing gear and a single engine in tractor configuration.^[1]

The aircraft is made from composites. Its 8.44 m (27.7 ft) span wing has a small wing area of 9.77 m² (105.2 sq ft). The standard engine is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant.^[1]

A fixed gear version with a larger wing span and area as well as a higher gross weight was developed for the US light-sport aircraft category and is marketed as the Gobosh 800XP.^[1]

Operational history

A VL-3 set a world two-seat ultralight class record of 274.78 km/h (170.74 mph) in 2005.^[1]

Variants

VL-3 FG

Fixed landing gear model^[1]

VL-3 RG

Retractable landing gear model^[1]

Specifications (VL-3 Sprint)

Aveko VL-3 Sprint

Data from Bayerl and JMB Aircraft^[1][3]

General characteristics

• Crew: one
• Capacity: one passenger
• Length: 6.24 m (20 ft 6 in)
• Wingspan: 8.44 m (27 ft 8 in)
• Height: 2.05 m (6 ft 9 in)
• Wing area: 9.77 m² (105.2 sq ft)
• Empty weight: 285 kg (628 lb)
• Gross weight: 472.5 kg (1,042 lb)
• Fuel capacity: 90 to 120 litres (20 to 26 imp gal; 24 to 32 US gal)
• Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)

Performance

• Maximum speed: 292 km/h (181 mph; 158 kn)
• Cruising speed: 250 km/h (155 mph; 135 kn)
• Stall speed: 53 km/h (33 mph; 29 kn)
• Never exceed speed: 305 km/h (190 mph; 165 kn)
• Rate of climb: 6 m/s (1,200 ft/min)

References

External links

• Official website