Canadian Vickers Velos

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Canadian Vickers Velos
Canadian Vickers Velos ExCC.jpg
Role Survey floatplane
National origin Canada
Manufacturer Canadian Vickers
First flight 1928
Introduction 1928
Retired 1928
Status destroyed
Primary user Royal Canadian Air Force
Number built 1

The Canadian Vickers Velos was a 1927 Canadian twin-engined float-equipped sesquiplane designed and built by Canadian Vickers Limited. Designed for survey work, it proved difficult to fly and only one was built.

Operator[edit]

 Canada

Specification[edit]

Data from [1]

General characteristics

  • Length: 44 ft 0 in (13.41 m)
  • Wingspan: 68 ft 0 in (20.73 m)
  • Max takeoff weight: 7,918 lb (3,592 kg)
  • Powerplant: 2 × Pratt & Whitney Wasp radial piston engine

Performance

  • Maximum speed: 85 mph (137 km/h; 74 kn)

See also[edit]

Related lists

References[edit]

Notes
  1. ^ Orbis 1985, p. 1040
Bibliography
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.