Angus Aquila
Aquila | |
---|---|
Role | Single-seat monoplane |
National origin | United Kingdom |
Manufacturer | Arthur Leighton Angus |
Designer | Arthur Leighton Angus |
First flight | 1931 |
Number built | 1 |
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]
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
- ^ a b c 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.
Categories:
- 1930s British civil utility aircraft
- Low-wing aircraft
- Aircraft first flown in 1931
- Aviation accidents and incidents in England
- 1930s aircraft stubs