Alpi Pioneer 300 Kite

Italian light-sport aircraft From Wikipedia, the free encyclopedia

The Alpi Pioneer 300 Kite also branded Pionner 300 FG (for fixed gear) is an Italian ultralight and light-sport aircraft designed and produced by Alpi Aviation of Pordenone. The aircraft is supplied as a kit for amateur construction or complete and ready-to-fly.[1]

National originItaly
StatusIn production (2017)
Quick facts Pioneer 300 Kite, General information ...
Pioneer 300 Kite
P300 Kite (FG) at Le Touquet Airport - (LFAT), France
General information
Typeultralight or Light-sport aircraft
National originItaly
ManufacturerAlpi Aviation
StatusIn production (2017)
History
Developed fromAlpi Pioneer 300
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Design and development

The Pioneer 300 Kite is a fixed gear version of the Alpi Pioneer 300. Designed to comply with the US light-sport aircraft rules, it features a cantilever low-wing, an enclosed cockpit with two-seats-in-side-by-side configuration under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft is made from wood and covered with composite material. Its 7.55 m (24.8 ft) span wing has an area of 10 m2 (110 sq ft) and mounts flaps. It is powered by a 100 hp (75 kW) Rotax 912ULS engine.[2]

Apart from being available fully assembled it is also available as two different kits, one a 51% kit and the other EuroKit, which includes a factory assembled airframe, but lacks the engine installation.[1]

As of May 2025, the design does not appear on the Federal Aviation Administration's list of approved special light-sport aircraft.[3]

Specifications (Pioneer 300 Kite)

Data from Tacke and manufacturer[1][4]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 6.25 m (20 ft 6 in)
  • Wingspan: 7.55 m (24 ft 9 in)
  • Wing area: 10 m2 (110 sq ft)
  • Empty weight: 315 kg (694 lb)
  • Gross weight: 560 kg (1,235 lb)
  • Fuel capacity: 80 litres (18 imp gal; 21 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
  • Propellers: 2-bladed composite

Performance

  • Maximum speed: 240 km/h (150 mph, 130 kn)
  • Cruise speed: 220 km/h (140 mph, 120 kn)
  • Stall speed: 72 km/h (45 mph, 39 kn)
  • Range: 900 km (560 mi, 490 nmi)
  • Service ceiling: 5,000 m (16,000 ft)
  • g limits: +3.8/-1.9
  • Rate of climb: 6 m/s (1,200 ft/min)
  • Wing loading: 56.0 kg/m2 (11.5 lb/sq ft)

References

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