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Alpi Pioneer 300

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Top speed
  
270 km/h

Manufacturer
  
Wingspan
  
8.1 m

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The Alpi Pioneer 300 is an Italian ultralight and light-sport aircraft, designed produced by Alpi Aviation, of Pordenone. The aircraft is supplied as a kit for amateur construction.

Contents

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Design and development

The Pioneer 300 was derived from the Asso V Champion and designed to comply with the Fédération Aéronautique Internationale microlight rules, as well as the US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, a choice of fixed or retractable tricycle landing gear and a single engine in tractor configuration. The fixed landing gear version is intended for the US light-sport aircraft category that does not permit retractable gear on landplanes.

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The aircraft is made with a wooden frame, covered with composite skin panels. Its 8.10 m (26.6 ft) span wing is tapered in planform. Standard engines available are the 100 hp (75 kW) Rotax 912ULS, 85 hp (63 kW) Jabiru 2200 and 120 hp (89 kW) Jabiru 3300.

Variants

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Pioneer 300 Standard
Base model, standard engine is the 100 hp (75 kW) Rotax 912ULS.
Pioneer 300 Hawk
Model with upgraded canopy and interior, with plywood wing skins and oleo strut suspension.
Pioneer 300 Kite
Model with fixed gear and gross weight of 560 kg (1,235 lb) for the US light-sport aircraft market.
Pioneer 300 Turbo
Model with luxury interior, carbon fibre instrument panel and Rotax 914 turbocharged engine of 115 hp (86 kW) giving a cruise speed of 265 km/h (165 mph).
Pioneer 330 Acro
Aerobatic model, with inverted-capable version of the 100 hp (75 kW) Rotax 912ULS and a strengthened airframe with flight load factors of +6/-3g.

Specifications (Pioneer 300)

Data from Bayerl & Tacke

General characteristics

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  • Crew: one
  • Capacity: one passenger
  • Wingspan: 8.10 m (26 ft 7 in)
  • Wing area: 11.0 m2 (118 sq ft)
  • Empty weight: 285 kg (628 lb)
  • Gross weight: 472.5 kg (1,042 lb)
  • Fuel capacity: 80 litres (18 imp gal; 21 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, 75 kW (100 hp)
  • Propellers: 2-bladed composite
  • Performance

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  • Maximum speed: 270 km/h (168 mph; 146 kn)
  • Cruising speed: 250 km/h (155 mph; 135 kn)
  • Stall speed: 60 km/h (37 mph; 32 kn)
  • Rate of climb: 8 m/s (1,600 ft/min)
  • Wing loading: 42.95 kg/m2 (8.80 lb/sq ft)

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    References

    Alpi Pioneer 300 Wikipedia