Angus Aquila - Aeroplane - avia.wikisort.org

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The Angus Aquila was a 1930s British single-seat low-wing monoplane designed and built by Arthur Leighton Angus.[1] It had an open cockpit and was powered by a 40 hp (30 kW) Salmson AD.9 radial engine.[1] The Aquila was registered G-ABIK[2] and test flown in early 1931 at Hanworth Aerodrome near London but it was destroyed in a crash on 21 March 1931 killing Angus.[1][3]

Aquila
Role	Single-seat monoplane Type of aircraft
National origin	United Kingdom
Manufacturer	Arthur Leighton Angus
Designer	Arthur Leighton Angus
First flight	1931
Number built	1

Specifications

General characteristics

Crew: 1
Empty weight: 488 lb (221 kg)
Gross weight: 700 lb (318 kg)
Powerplant: 1 × Salmson AD.9 radial piston engine , 40 hp (30 kW)

Performance

Endurance: 2 hours 0 minutes

References

Notes

Jackson 1974, p. 285
Civil Aviation Authority - Aircraft Register - G-ABIK Archived 12 September 2012 at the Wayback Machine
"Airman killed at Hanworth". News. The Times. No. 45778. London. 23 March 1931. col c, p. 9.

Sources

Jackson, A.J. (1973). British Civil Aircraft since 1919 Volume 1. London: Putnam. ISBN 0-370-10006-9.

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На других языках

[de] Angus Aquila

Die Angus Aquila war ein Leichtflugzeug des britischen Konstrukteurs A. L. Angus vom Beginn der 1930er Jahre.

- [en] Angus Aquila

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