Pottier P.100

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P.100, P.110, P.105 and P.130
Aerosport 2011 p2.JPG
Pottier P.130 at the Aerosport show (2011)
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[edit]

  • 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)[edit]

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 ft2)
  • 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)
  • Range: 650 km (400 miles)
  • Rate of climb: 6.2 m/s (1,220 ft/min)

Notes[edit]

  1. ^ Taylor 1989, p.751
  2. ^ a b c d e f Jane's All the World's Aircraft 1987–88, p.588

References[edit]

  • 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.