Auster Avis
Template:Short description Template:DMCA Template:DMCA Template:Infobox aircraft 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.
Specifications (Avis)
Data from Jane's all the World's Aircraft 1949-50,[1] The Incomplete Guide to Airfoil Usage[2]
General characteristics
- Crew: 1
- Capacity: 3 passengersTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Aspect ratio: 6.982
- Airfoil: NACA 23012 Template:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Fuel capacity: Fuel:Template:Cvt in two wing root fuel tanks; Oil:Template:Cvt aft of engine.Template:Aircraft specs/convertTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convert
- Propellers: 2-bladed Weybridge wooden fixed pitch propellerTemplate:Aircraft specs/length
PerformanceTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Power/mass: Template:Cvt fully loaded at 2,300 rpm; Template:Cvt at 2,200 rpm
- Take-off run: Template:Cvt in Template:Cvt wind
- Landing run: Template:Cvt in Template:Cvt wind
References
Page Template:Reflist/styles.css has no content.
- ^ Page Module:Citation/CS1/styles.css has no content.Bridgman, Leonard, ed. (1949). Jane's all the World's Aircraft 1949-50. London: Sampson Low, Marston & Co. pp. 20c–21c.
- ^ Page Module:Citation/CS1/styles.css has no content.Selig, M. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 22 November 2018.
Further reading
- Page Module:Citation/CS1/styles.css has no content.Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 84.
- Page Module:Citation/CS1/styles.css has no content.World Aircraft Information Files. London: Bright Star Publishing. pp. File 889 Sheet 85.
- Page Module:Citation/CS1/styles.css has no content.Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. p. 42.
Lua error in package.lua at line 80: module 'Module:Navbox/configuration' not found.
