Jump to content

Chatelain AC.5

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by TSRL (talk | contribs) at 09:59, 20 January 2020 (Specifications). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

AC.5 Bijou
Role recreational aircraft
Manufacturer homebuilt
Designer Armand Chatelain
First flight 10 September 1956
Primary user private pilot owners

The Chatelain AC-5 is a 1950s French two-seat homebuilt aircraft designed by Armand Chatelain.

Development

The AC-5 was a high-wing monoplane with a wing of all-wood construction and a fuselage made of steel tubes.

Specifications

Data from [1]

General characteristics

  • Crew: 2
  • Length: 5.20 m (17 ft 1 in)
  • Wing area: 14.00 m2 (150.7 sq ft)
  • Empty weight: 335 kg (739 lb)
  • Gross weight: 570 kg (1,257 lb)
  • Powerplant: 1 × Minié 4.DC.32 air-cooled horizontally-opposed piston engine, 56 kW (75 hp)
  • Propellers: 2-bladed SIPA propeller

Performance

  • Maximum speed: 165 km/h (103 mph, 89 kn)
  • Range: 500 km (310 mi, 270 nmi)
  • Service ceiling: 4,000 m (13,000 ft)

References

  1. ^ "Chatelain AC-5". Aviafrance.com. Retrieved 6 March 2019.