Pro.Mecc Sparviero
| Sparviero | |
|---|---|
.JPG)
| |
| Pro Mecc Sparviero 100 at the Aerosport air show in 2013 | |
| Role | Ultralight aircraft |
| National origin | Italy |
| Manufacturer | Pro.Mecc |
| Status | In production (2012) |
| Variants | Pro.Mecc Freccia Anemo |
The Pro.Mecc Sparviero (Template:Lang-en) is an Italian ultralight aircraft, designed and produced by Pro.Mecc of Corigliano d'Otranto. The Sparviero is supplied as a kit for amateur construction or a complete ready-to-fly-aircraft.[1][2]
Design and development
The Sparviero was designed to conform to 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, fixed tricycle landing gear and a single engine in tractor configuration.[1][2]
The Sparviero is made predominantly from carbon fibre, with the wing skins fabricated from fibreglass. Its 9.23 m (30.3 ft) span wing has an area of 12 m2 (130 sq ft) and flaps. The standard engine fitted is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant, with the 80 hp (60 kW) Rotax 912UL optional. In 2011 a fast-build kit was introduced that provides a completed and painted fuselage and wings, requiring the builder only to carry out the engine and electrical installations.[1][2]
The Sparviero was later developed into the Pro.Mecc Freccia Anemo, with additional streamlining and a new elliptical planform wing.[1][2]
Operational history
Reviewer Marino Boric described the design in a 2015 review as, "not only stylish, but aggressively low-priced for mainly built of carbonfiber...."[2]
Variants
- Sparviero
- Initial model[1][2]
- Sparviero 100
- Improved model introduced in December 2009 with a lighter empty weight, higher cruise speed, lower-mounted seats and lower canopy.[1][2]
Specifications (Sparviero 100)
Data from Bayerl[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 9.23 m (30 ft 3 in)
- Wing area: 12 m2 (130 sq ft)
- Empty weight: 285 kg (628 lb)
- Gross weight: 472.5 kg (1,042 lb)
- Fuel capacity: 90 litres (20 imp gal; 24 US gal)
- Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
Performance
- Maximum speed: 240 km/h (150 mph, 130 kn)
- Cruise speed: 225 km/h (140 mph, 121 kn)
- Stall speed: 54 km/h (34 mph, 29 kn)
- Rate of climb: 6 m/s (1,200 ft/min)
- Wing loading: 39.4 kg/m2 (8.1 lb/sq ft)
References
- ^ a b c d e f g Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 71. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ a b c d e f g Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 74. Flying Pages Europe SARL, 2015. ISSN 1368-485X
External links
