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The Auster Avis was a four-seat light aircraft developed from the Auster Autocrat. It featured a redesigned fuselage incorporating four doors and a circular cross-section towards the tail, new undercarriage, and new wing flaps. It was planned in two versions, the Mk 1 for civil use, and the Mk 2 for military and air ambulance duties. However, only two prototypes were built, and Auster abandoned the project in favour of the Auster J-5 Autocar.

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  • Auster Avis (en)
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  • The Auster Avis was a four-seat light aircraft developed from the Auster Autocrat. It featured a redesigned fuselage incorporating four doors and a circular cross-section towards the tail, new undercarriage, and new wing flaps. It was planned in two versions, the Mk 1 for civil use, and the Mk 2 for military and air ambulance duties. However, only two prototypes were built, and Auster abandoned the project in favour of the Auster J-5 Autocar. (en)
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sameAs
span m
stall speed mph
stall speed note
  • fully loaded, flaps down (en)
wing area sqft
wing loading lb/sqft
wing loading note
  • fully loaded *Fuel consumption mpg: (en)
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dbp:primeUnits%3F_
  • imp (en)
first flight
  • late 1947 (en)
capacity
crew
fuel capacity
  • Fuel: in two wing root fuel tanks; Oil: aft of engine. (en)
height ft
height in
manufacturer
ref
  • Jane's all the World's Aircraft 1949-50, The Incomplete Guide to Airfoil Usage (en)
type
  • Utility aircraft (en)
has abstract
  • The Auster Avis was a four-seat light aircraft developed from the Auster Autocrat. It featured a redesigned fuselage incorporating four doors and a circular cross-section towards the tail, new undercarriage, and new wing flaps. It was planned in two versions, the Mk 1 for civil use, and the Mk 2 for military and air ambulance duties. However, only two prototypes were built, and Auster abandoned the project in favour of the Auster J-5 Autocar. (en)
airfoil
aspect ratio
ceiling ft
ceiling note
  • fully loaded (en)
climb rate ftmin
climb rate note
  • fully loaded (en)
cruise speed mph
cruise speed note
  • fully loaded (en)
developed from
empty weight lb
eng1 hp
eng1 name
eng1 note
  • maximum at 2,550rpm; continuous at 2,300 rpm (en)
eng1 number
eng1 type
fuel consumption lb/mi
gross weight lb
height note
  • tail down, propeller horizontal (en)
length m
max speed mph
max speed note
  • fully loaded (en)
number built
power/mass
  • fully loaded at 2,300 rpm; at 2,200 rpm *Take-off run: in wind *Landing run: in wind (en)
prop blade number
prop name
  • Weybridge wooden fixed pitch propeller (en)
range miles
range note
  • fully loaded in still-air (en)
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is Link from a Wikipage to another Wikipage of
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