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Introduction

Charles Fauvel biography

Fauvel gliders and airplanes

  Gliders / motorgliders
    AV-1 / AV-2 / AV-3
    AV-17
    AV-36 / AV-361
    AV-45 / AV-451
    AV-46
    AV-48
    AV-22
    AV-221
    AV-222
  Airplanes
    AV-7
    AV-10
    AV-14
    AV-28
    AV-29
    AV-31
    AV-42
    AV-44
    AV-60
    AV-61
    Other projects

Why a flying wing ?

Some technical materials...

In flight

Archives

Precursors and successors

References




AV-222
     
The Swedish AV-222
SE-XSL
AV-222 under construction
in Germany
Scale model (1/6th scale)
The AV-222 built in France
by Jean-Claude Néglais
(click on the pictures to enlarge them in a new window)

After having designed and flown the AV-221, Charles Fauvel developed a version for amateur construction, and named it the AV-222. Lighter and of a less complex structure, this flying wing could be disassembled into three sections (the center section had no dihedral). It had a laminar airfoil (optional, or the more conventional Fauvel airfoil), and could be equipped with a choice of a classic landing gear or a mono-gear (the last being the recommended one because it is lighter, more economical to fabricate and easier to install). The craft mounted either a Rectimo engine (40 HP), Limbach (60 HP) of Volkswagen origin, or the 2-cycle Rotax. Fuel tanks could contain up to 30 liters (with 45 as an option). Several sets of AV-222 plans were sold in France, Germany, Italy, Sweden, United Kingdom and in the United States. The first AV-222 flying wing, constructed by Hans Martinson and registered SE-XSL, flew in Sweden in May 1992, while several other construction projects are pursued in France, Germany and in the United States.

Characteristics and performance of the AV-222
Wing span 16.40 m
Length 4.95 m
Wing area 23.05 m2
Airfoil Fauvel F2
Aspect ratio 10.7
Empty weight 350 kg
Max. gross weight 650 kg
Max. speed 210 km/h
Best glide ratio 27:1
Min. sink rate 0.90 m/sec