P.100, P.110, P.105
Role Utility aircraft
National origin France
Manufacturer Homebuilt
Designer Jean Pottier
First flight 16 October 1980

The Pottier P.100 and its derivatives were a family of single-engine aircraft developed in France in the 1970s and 80s.[1] They were high-wing cantilever monoplanes of conventional design with enclosed cabins and fixed tricycle undercarriage.[2] The P.100 had two seats, arranged side-by-side, while the P.110 had its fuselage stretched by 50 cm (20 in) to include a third seat and a greater wingspan.[2] The P.105 was a hybrid of the two designs, featuring the shorter, two-seat fuselage of the P.100 and the longer-span wings of the P.110.[2]

Variants

  • P.100TS - two-seat version[2]
  • P.110TS - three-seat version[2]
  • P.105TS - version with fuselage of P.100 and wings of P.110[2]

Specifications (P.100)

Data from Jane's All the World's Aircraft 1987–88 p. 588

General characteristics

  • Crew: One pilot
  • Capacity: 1 passenger
  • Length: 6.50 m (21 ft 4 in)
  • Wingspan: 6.85 m (22 ft 5 in)
  • Wing area: 9.3 m2 (100 sq ft)
  • Empty weight: 435 kg (959 lb)
  • Gross weight: 680 kg (1,500 lb)
  • Powerplant: 1 × Continental O-200 , 75 kW (100 hp)

Performance

  • Maximum speed: 250 km/h (160 mph, 140 kn)
  • Range: 650 km (400 mi, 350 nmi)
  • Rate of climb: 6.2 m/s (1,220 ft/min)

Notes

  1. ↑ Taylor 1989, p.751
  2. 1 2 3 4 5 6 Jane's All the World's Aircraft 1987–88, p.588

References

Wikimedia Commons has media related to Pottier P.130.
  • Jane's All the World's Aircraft 1987–88. London: Jane's Publishing.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.


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