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Avro 558

General Aviation and Light Aircraft

The Avro 558 was a British single-engined ultralight biplane built by Avro at Hamble Aerodrome for the 1923 light aircraft trials for single-seaters at Lympne Aerodrome. Two were built, powered by motorcycle engines, one with a B&H twin-cylinder air-cooled engine and the second with a 500 cc Douglas engine, and the first was later modified with a 698 cc Blackburne Tomtit; both had changes to the landing gear. The aircraft did not win the competition, but the second aircraft went on to set a world record for its class of 13,850 ft over Lympne on 13 October 1923. It is not known what happened to the two aircraft, which have not been reported since 1923.

Facts
Year
1923 1
Units Built
2 1
Mass (kg)
133 1
Maximum Mass (kg)
218 1
Engine
Douglas 500cc 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Avro 558 (Wikipedia)

Of Make

Source Avro 558 (Wikipedia)
Sources
1. Avro 558 (Wikipedia)
  • Lead, kind of vehicle
    was a British single-engined ultralight biplane
  • Design and development, design year
    The Avro 558 was designed for the 1923 light aircraft trials for single-seaters at Lympne Aerodrome.
  • Design and development, number built
    Two Avro 558 biplanes were built
  • Specifications, engine name
    Powerplant: 1 × Douglas 500cc air-cooled motorcycle engine, 18 hp (13 kW)
  • Specifications, empty weight
    Empty weight: 294 lb (133 kg)
  • Specifications, gross weight
    Gross weight: 480 lb (218 kg)
  • Lead, maker
    The Avro 558 was a British single-engined ultralight biplane built by Avro at Hamble Aerodrome.
  • Lead, nationality
    was a British single-engined ultralight biplane
  • In Group: Single-Engine Piston Light Aircraft, Lead, kind of aircraft
    The Avro 558 was a British single-engined ultralight biplane built by Avro at Hamble Aerodrome.
  • Exemplifies: Aviation, Lead, aircraft
    The Avro 558 was a British single-engined ultralight biplane built by Avro at Hamble Aerodrome.
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