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F r o m W i k i p e d i a , t h e f r e e e n c y c l o p e d i a
Avis
Role
Utility aircraft
Type of aircraft
Manufacturer
Auster
First flight
late 1947
Number built
2
Developed from
Auster Autocrat
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)
[ edit ]
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 passengers
Length: 23 ft 7 in (7.18 m )
Wingspan: 36 ft 4 in (11.07 m )
Height: 6 ft 5.5 in (1.969 m ) tail down, propeller horizontal
Wing area: 185 sq ft (17.2 m 2 )
Aspect ratio : 6.982
Airfoil : NACA 23012
Empty weight: 1,480 lb (671 kg )
Gross weight: 2,550 lb (1,157 kg )
Fuel capacity: Fuel:34 imp gal (41 US gal; 150 L ) in two wing root fuel tanks; Oil:3 imp gal (3.6 US gal; 14 L ) aft of engine.
Powerplant: 1 × de Havilland Gipsy Major 10 4-cylinder inverted air-cooled in-line piston engine, 145 hp (108 kW ) maximum at 2,550rpm; 108 hp (81 kW ) continuous at 2,300 rpm
Propellers: 2-bladed Weybridge wooden fixed pitch propeller
Performance
Maximum speed: 115 mph (185 km/h, 100 kn ) fully loaded
Cruise speed: 100 mph (160 km/h, 87 kn ) fully loaded
Stall speed: 40 mph (64 km/h, 35 kn ) fully loaded, flaps down
Range: 500 mi (800 km, 430 nmi) fully loaded in still-air
Service ceiling: 12,000 ft (3,700 m ) fully loaded
Rate of climb: 510 ft/min (2.6 m/s) fully loaded
Wing loading: 13.8 lb/sq ft (67 kg/m2 ) fully loaded
Fuel consumption mpg: 13 + 1 ⁄3 mpg‑imp (4.7 km/L)
Fuel consumption: 0.525 lb/mi (0.148 kg/km)
Power/mass : 17.5 lb/hp (10.6 kg/kW) fully loaded at 2,300 rpm; 14.9333 lb/hp (9.0836 kg/kW) at 2,200 rpm
Take-off run: 185 yd (169 m ) in 5 mph (4.3 kn; 8.0 km/h) wind
Landing run: 130 yd (120 m ) in 5 mph (4.3 kn; 8.0 km/h) wind
References
[ edit ]
^ Bridgman, Leonard, ed. (1949). Jane's all the World's Aircraft 1949-50 . London: Sampson Low, Marston & Co. pp. 20c–21c.
^ Selig, M. "The Incomplete Guide to Airfoil Usage" . m-selig.ae.illinois.edu . Retrieved 22 November 2018 .
Further reading
[ edit ]
Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation . London: Studio Editions. p. 84.
World Aircraft Information Files . London: Bright Star Publishing. pp. File 889 Sheet 85.
Simpson, R. W. (1995). Airlife's General Aviation . Shrewsbury: Airlife Publishing. p. 42.
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e
R e t r i e v e d f r o m " https://en.wikipedia.org/w/index.php?title=Auster_Avis&oldid=1226829366 "
C a t e g o r i e s :
● S i n g l e - e n g i n e d t r a c t o r a i r c r a f t
● H i g h - w i n g a i r c r a f t
● 1 9 4 0 s B r i t i s h c i v i l u t i l i t y a i r c r a f t
● 1 9 4 0 s B r i t i s h m i l i t a r y u t i l i t y a i r c r a f t
● A u s t e r a i r c r a f t
● 1 9 4 0 s a i r c r a f t s t u b s
H i d d e n c a t e g o r i e s :
● U s e d m y d a t e s f r o m M a r c h 2 0 1 8
● U s e B r i t i s h E n g l i s h f r o m M a r c h 2 0 1 8
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● S h o r t d e s c r i p t i o n i s d i f f e r e n t f r o m W i k i d a t a
● A l l s t u b a r t i c l e s
● T h i s p a g e w a s l a s t e d i t e d o n 2 J u n e 2 0 2 4 , a t 0 2 : 3 4 ( U T C ) .
● T e x t i s a v a i l a b l e u n d e r t h e C r e a t i v e C o m m o n s A t t r i b u t i o n - S h a r e A l i k e L i c e n s e 4 . 0 ;
a d d i t i o n a l t e r m s m a y a p p l y . B y u s i n g t h i s s i t e , y o u a g r e e t o t h e T e r m s o f U s e a n d P r i v a c y P o l i c y . W i k i p e d i a ® i s a r e g i s t e r e d t r a d e m a r k o f t h e W i k i m e d i a F o u n d a t i o n , I n c . , a n o n - p r o f i t o r g a n i z a t i o n .
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