Samiksha Jaiswal (Editor)

Angus Aquila

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First flight
  
1931

Manufacturer
  
Arthur Leighton Angus

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

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 min
  • References

    Angus Aquila Wikipedia


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