- Avro Avis
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The Avro 562 Avis was a two-seat light biplane designed and built by the A.V.Roe and Company Limited at Hamble for the 1924 Lympne Light Aeroplane Trials.
The Avis was a single-bay unstaggered biplane with full span ailerons on upper and lower wings. It had a fixed landing gear with a tail skid and could be powered by powered by a nose-mounted 32hp
Bristol Cherub II engine or a 35hpBlackburne Thrush radial piston engine. Jackson 1990, p.222.] It had tandem open cockpits. First flown with the Thrush engine prior to the meeting, it was refitted with the Cherub, and first flown with this engine byBert Hinkler at Lympne on 30 September 1924. On the next day it won the Grosvenor trophy at a speed of 65.87 mph. Jackson 1990, pp.222-223.]For the 1926 trials it was re-engined with a 38hp Blackburne Thrush, being eliminated after a forced landing. In 1927, it was re-engined again with a
Bristol Cherub I and passed into private ownership until it was scrapped in 1931. Jackson 1990, p.224.]pecifications
aerospecs
ref= [ [http://www.britishaircraft.co.uk/aircraftpage.php?ID=263 British Aircraft] ]
met or eng?= engcrew=1 (pilot)
capacity=1 (passenger)
length m=9.17
length ft=30
length in=1
span m=7.32
span ft=24
span in=0
swept m=
swept ft=
swept in=
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rot dia m=
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dia m=
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width m=
width ft=
width in=
height m=2.74
height ft=9
height in=0
wing area sqm=22.9
wing area sqft=246
swept area sqm=
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rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=268
empty weight lb=590
gross weight kg=92.5
gross weight lb=995
lift kg=
lift lb=eng1 number=1
eng1 type=Blackburne Thrush three-cylinder air-cooled radial engine
eng1 kw= 26
eng1 hp= 35
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eng2 lbf-ab=max speed kmh=120
max speed mph=75
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lists=References
*cite book |last= Jackson|first= A.J.|authorlink= |coauthors= |title= British Civil Aircraft since 1919 Volume 1|year= 1974|publisher= Putnam|location= London|isbn=0 370 10006 9
*External links
* [http://www.britishaircraft.co.uk/aircraftpage.php?ID=263 British Aircraft Directory - Avro Avis]
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