Piel CP-20 Pinocchio

Last updated
CP-20 Pinocchio
RoleSingle seat sports aircraft
National origin France
Designer Claude Piel
First flight1 July 1951
Statusactive
Number built2

The Piel CP-20 Pinocchio is a single engine French sport monoplane first flown in 1951. Only two were built but one was still flying over sixty years later.

Contents

Design and development

Despite sharing the name Pinocchio, the CP-20 was a completely different design from Claude Piel's first aircraft, the CP-10 Pinocchio. The CP-20 is a conventional low wing cantilever monoplane whereas the CP-10 was a Pou-du-Ciel style tandem wing design; [1] it did inherit the CP-10's rudder, wheels and firewall. The centre section of the Pinocchio's wing is rectangular in plan and the outer panels are semi-elliptical. It has broad-chord ailerons but no flaps. [2]

The fuselage is almost flat sided and bottomed but with raised, rounded decking behind the single seat cockpit and canopy. [3] The empennage is conventional, with tapered horizontal surfaces mounted near the top of the fuselage and a curved fin carrying a broad, balanced rudder. The rudder extends down to the keel, so the elevators are cut away to allow its movement. The Pinocchio has a wide track tail wheel/skid undercarriage with main wheels on vertical, cantilever legs from the wings. [2]

Only two Pinocchios were built. The first had a 34 kW (45 hp) converted Volkswagen 1.1 litres (67 cu in) litre engine. The second, built by Pierre Bordini, was originally designated the CP-210 and was powered by a 34 kW (45 hp) Salmson 9 AD engine. In July 1961 it became the CP-211, with the same Salmson engine but with a one-piece sliding canopy and more raked screen, faired landing legs and a tailwheel rather than a skid, greater fuel capacity, and a cropped vertical tail. Its time as the CP-211 was brief, for at the end of 1961 it became the CP-212, fitted with a 48 kW (65 hp) Continental A-65 air-cooled flat-four engine. [1] [2] [4]

Operational history

In 1951 the CP-20 won the 4th RSA Cup, flown at Montargis. [2] During the 1960s the CP-212 had several owners but its certificate expired in 1970. [4] In the 1990s it was restored and eventually re-registered in October 2001 as the CP-215. [4] It remained on the French civil register in 2014. [5]

Variants

Data from Massé (2004) [2]

CP-20
First airframe, as below.
CP-210
Second airframe with 34 kW (45 hp) Salmson 9 ADb radial engine [6]
CP-211
Second airframe, as CP-210 but with one piece, sliding canopy and cropped vertical tail.
CP-212
Second airframe, as CP-211 but with 48 kW (65 hp) Continental A65 engine.
CP-215
Second airframe restored. [2]

Specifications (CP-20)

Data from Massé (2004) pp. 21-28 [2]

General characteristics

Performance

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References

  1. 1 2 3 Gaillard, Pierre (1990). Les Avions Francais de 1944 à 1964. Paris: Éditions EPA. pp. 75, 122. ISBN   2-85120-350-9.
  2. 1 2 3 4 5 6 7 Massé, Xavier. Avions Piel: du CP 10 de 1944 au CP 1950 de 1983 (2004 ed.). Nouvelles Editions Latines. pp. 21–8.
  3. ↑ A view of the fuselage during a reconstruction project
  4. 1 2 3 Chillon, Jacques. Fox Papa-Registre des avions Français amateur (2009 ed.). Brive: Ver Luisant. p. 86. ISBN   978-2-3555-1-066-3.
  5. ↑ Partington, Dave (2014). European registers handbook 2014. Air Britain (Historians) Ltd. ISBN   978-0-85130-465-6.
  6. ↑ Cutaway view of CP-210 (from Piel website)
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