Jump to content

Chatelain AC.9

From Wikipedia, the free encyclopedia

This is the current revision of this page, as edited by Plastikspork (talk | contribs) at 16:05, 13 December 2020 (Specifications: Fix). The present address (URL) is a permanent link to this version.

(diff) ← Previous revision | Latest revision (diff) | Newer revision → (diff)
AC.9
Role recreational aircraft
Manufacturer homebuilt
Designer Armand Chatelain
First flight 1966
Primary user Private pilot owners

The Chatelain AC.9 is a 1960s French two-seat homebuilt aircraft designed by Armand Chatelain.

Specifications

[edit]

Data from [1]

General characteristics

  • Crew: 3
  • Length: 6.55 m (21 ft 6 in)
  • Wingspan: 9.00 m (29 ft 6 in)
  • Empty weight: 420 kg (926 lb)
  • Gross weight: 850 kg (1,874 lb)
  • Powerplant: 1 × Continental O-280 4-cylinder air-cooled horizontally-opposed piston engine, 110 kW (150 hp)
  • Propellers: 2-bladed SIPA propeller

Performance

References

[edit]
  1. ^ "Chatelain AC-9". Aviafrance.com. 30 March 2003. Retrieved 6 Mar 2019.