About: Auster Avis

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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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dbo: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)
dbo:manufacturer
dbo:numberBuilt
  • 2 (xsd:nonNegativeInteger)
dbo:predecessor
dbo:wikiPageID
  • 11126288 (xsd:integer)
dbo:wikiPageLength
  • 4532 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1037309001 (xsd:integer)
dbo:wikiPageWikiLink
dbp:airfoil
dbp:aspectRatio
  • 6.982000 (xsd:double)
dbp:capacity
  • 3 (xsd:integer)
dbp:ceilingFt
  • 12000 (xsd:integer)
dbp:ceilingNote
  • fully loaded (en)
dbp:climbRateFtmin
  • 510 (xsd:integer)
dbp:climbRateNote
  • fully loaded (en)
dbp:crew
  • 1 (xsd:integer)
dbp:cruiseSpeedMph
  • 100 (xsd:integer)
dbp:cruiseSpeedNote
  • fully loaded (en)
dbp:developedFrom
dbp:emptyWeightLb
  • 1480 (xsd:integer)
dbp:eng1Hp
  • 145 (xsd:integer)
dbp:eng1Name
dbp:eng1Note
  • maximum at 2,550rpm; continuous at 2,300 rpm (en)
dbp:eng1Number
  • 1 (xsd:integer)
dbp:eng1Type
  • 4 (xsd:integer)
dbp:firstFlight
  • late 1947 (en)
dbp:fuelCapacity
  • Fuel: in two wing root fuel tanks; Oil: aft of engine. (en)
dbp:fuelConsumptionLb/mi
  • 0.525000 (xsd:double)
dbp:grossWeightLb
  • 2550 (xsd:integer)
dbp:heightFt
  • 6 (xsd:integer)
dbp:heightIn
  • 5.500000 (xsd:double)
dbp:heightNote
  • tail down, propeller horizontal (en)
dbp:lengthM
  • 7.180000 (xsd:double)
dbp:manufacturer
dbp:maxSpeedMph
  • 115 (xsd:integer)
dbp:maxSpeedNote
  • fully loaded (en)
dbp:numberBuilt
  • 2 (xsd:integer)
dbp:power/mass
  • fully loaded at 2,300 rpm; at 2,200 rpm *Take-off run: in wind *Landing run: in wind (en)
dbp:primeUnits?_
  • imp (en)
dbp:propBladeNumber
  • 2 (xsd:integer)
dbp:propName
  • Weybridge wooden fixed pitch propeller (en)
dbp:rangeMiles
  • 500 (xsd:integer)
dbp:rangeNote
  • fully loaded in still-air (en)
dbp:ref
  • Jane's all the World's Aircraft 1949-50, The Incomplete Guide to Airfoil Usage (en)
dbp:spanM
  • 11.070000 (xsd:double)
dbp:stallSpeedMph
  • 40 (xsd:integer)
dbp:stallSpeedNote
  • fully loaded, flaps down (en)
dbp:type
  • Utility aircraft (en)
dbp:wikiPageUsesTemplate
dbp:wingAreaSqft
  • 185 (xsd:integer)
dbp:wingLoadingLb/sqft
  • 13.800000 (xsd:double)
dbp:wingLoadingNote
  • fully loaded *Fuel consumption mpg: (en)
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • 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)
rdfs:label
  • Auster Avis (en)
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