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Central Centaur Iia




  type Biplane airliner
  manufacturer Central Aircraft Company Limited
  designer A A Fletcher
  first Flight 1919
  primary User Central Aircraft Company Limited
  number Built 2


The Central Centaur IIA was a British civil six-passenger joyriding biplane produced by Central Aircraft Company Limited of London .


HISTORY


Following the success of the earlier Centaur IV for joyriding, A.A. Fletcher designed a larger twin-engined aircraft. Designated the Centaur IIB the first aircraft, registered G-EAHR, first flew during July 1919 1. The fuselage had an open cockpit for the two crew and six passengers. A second example, registered G-EAPC, was built. It had the same designation Centaur IIB but had an enclosed cabin for seven passengers. The second aircraft first flew in May 1920 .

The second aircraft was tested by the Air Ministry in the 1920 Commercial Aeroplane Competition . It was described at the time as old-fashioned and low-powered, another problem was that loaded with all the fuel required for the three and half hour test flight meant it was unable to carry passengers or pilots. The aircraft did not win the competition. The prototype was destroyed in an accident at Northolt Aerodrome in July 1919 , shortly after the competition. The second aircraft crashed in October 1920 at Hayes, Middlesex, with a loss of six lives . No further examples were built.


AIRCRAFT



SPECIFICATIONS (CENTAUR IIA)

  plane Or Copter plane
  jet Or Prop prop
  ref British Civil Aircraft since 1919 Volume 1
  crew 2 (6 passengers)
  length Main 29 ft 3 in
  length Alt 1196 m
  span Main 63 ft 8 in
  span Alt 1941 m
  empty Weight Main 4996 lb
  empty Weight Alt 2271 kg
  max Takeoff Weight Main 7,250 lb
  max Takeoff Weight Alt 3289 kg
  engine (prop) Beardmore
  type Of Prop inline piston
  number Of Props 2
  power Main 160 hp
  power Alt 119 kw
  max Speed Main 90 mph
  max Speed Alt 145 km/h




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