Grahame-White Type 10 Charabanc

Back to the Virtual Aircraft Museum
  Virtual Aircraft Museum / United Kingdom / Grahame-White  

Grahame-White Type 10 Charabanc

There is no text information for this aircraft at the moment.

Comments
arachni_name, e-mail, 02.01.2021 13:53

1

reply

Brian Johnston, e-mail, 27.05.2012 18:55

An article about this aircraft, including a 3-view can be found in the 'Flight Global Archive' in the issue of October 1913.

reply

Terrence I. Murphy, e-mail, 10.02.2012 15:34

The Grahame-White Type X Charabanc or Aerobus was an 1910s British passenger-carrying biplane designed and built by the Grahame-White Aviation Company based at Hendon Aerodrome, North London.
The Charabanc was built by the Grahame-White company to meet the demand for passenger-carrying flights, which could not be satisfied by the existing two-seat designs. Designed by J.D. North, it was an unequal-span pusher biplane with ailerons on both upper and lower wings and a biplane tail unit with three rudders mounted on booms. An elongated nacelle mounted on the lower wing housed the pilot in the front and four-passengers in two rows of two seats behind. The wing spars, tail booms and outer interplane struts were of hollow section spruce, and the nacelle and inner struts were of ash.
It first flew in 1913 powered by a 120 hp (89 kW) Austro-Daimler engine, and in this form was flown by Louis Noel with seven passengers aboard to set a new British record on 22 September 1913: a week later he succeeded in carrying nine passengers, staying aloft for nearly twenty minutes. but to meet the entry requirements for the 1913 Michelin Cup, which required an all-British aircraft, this was replaced by a British-built 100 hp Green engine. The Charabanc went on to win the cup, covering a distance of 300 miles on 9 November 1913 piloted by R.H. Carr.
The first parachute descent from an aircraft in Great Britain was made by W. Newell from the aircraft at Hendon on 9 May 1914.
General characteristics
• Crew: 1
• Capacity: 4 passengers
• Length: 37 ft 6 in (11.43 m)
• Wingspan: 62 ft 6 in (19.05 m)
• Wing area: 790 ft2 (73.39 m2)
• Empty weight: 2000 lb (907 kg)
• Gross weight: 3100 lb (1406 kg)
• Powerplant: 1 × Green E.6 6-cylinder inline piston, 100 hp (75 kW)
Performance
• Maximum speed: 51 mph (82 km /h)

reply

Do you have any comments?

Name    E-mail


All rhe World's Rotorcraft AVIATION TOP 100 - www.avitop.com Avitop.com