- Fauvel AV.22
__NOTOC__ Infobox Aircraft
name=AV.22
caption=
type=Sailplane and motorglider
manufacturer=Homebuilt
designer=Charles Fauvel
first flight=5 April avyear|1956
introduced=
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variants with their own articles=The Fauvel AV.22 was an unorthodoxglider produced inFrance in the 1950s, 60s, and 70s. Originally intended to be produced in series, it was later marketed to homebuilders. Like otherCharles Fauvel designs, it was a tailless aircraft, and this particular design featured wings with a slight forward sweep. The original AV.22 design was unpowered, but later versions were equipped with an engine mounted in the nose for self-launching. The AV.22 was entered in a 1959 competition to select a standard glider for the French aeroclubs, but lost to theWassmer Bijave .The first powered version was the AV.221, which flew on 8 April 1965. In addition to the powerplant, the fuselage was also redesigned to accommodate a passenger side-by-side with the pilot. A simplified version of this aircraft was marketed for homebuilding as the AV.222. Options included a choice of airfoils, and either one or two mainwheels as undercarriage.
Variants
* AV.22 - initial glider version
** AV.221 - two-seat motor glider
** AV.222 - simplified AV.221 for homebuilding.pecifications (AV.222)
aerospecs
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met or eng?= metcrew=One pilot
capacity=1 passenger
length m=5.22
length ft=17
length in=2
span m=16.40
span ft=53
span in=10
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width m=
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wing area sqm=23.0
wing area sqft=248
swept area sqm=
swept area sqft=
rot area sqm=
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volume m3=
volume ft3=
aspect ratio= 12.0
empty weight kg=325
empty weight lb=716
gross weight kg=550
gross weight lb=1,212
lift kg=
lift lb=eng1 number=1
eng1 type=Volkswagen automotive engine
eng1 kw= 45
eng1 hp= 60
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range km=
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endurance h=
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ceiling m=
ceiling ft=
glide ratio= 26
climb rate ms=3.0
climb rate ftmin=590
sink rate ms= 0.9
sink rate ftmin= 177armament1=
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armament6=aircontent
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lists=References
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