KEA Chelidon

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Chelidon
KEA Chelidon.jpg
Role training and Reconnaissance
Manufacturer EAF (KEA)
Designer Team supervised by Charles H. Lowe-Wylde
First flight February 11, 1927
Retired 1938
Produced 1927
Number built 1 (original order for 18 aircraft)


The Chelidon (Χελιδών, meaning 'Swallow' in Greek, also spelled in English as Helithon) was the first airplane developed by the Greek EAF (KEA) aircraft factory with management provided by Blackburn Aircraft Limited at the time. According to one source, it was designed by Charles H Lowe-Wylde, although in the contemporary Jane's edition it is mentioned that "it was designed largely by Greeks" (under the supervision of Mr. Wylde), according to Greek Navy specifications. Its development was completed in a virtually record time of 8 weeks, and first flight was made on February 11, 1927. It was a two-seater military biplane designed for advanced training and other roles including reconnaissance. It could also be transformed into a hydroplane. It used a Salmson 120 hp engine (future variants were to use Armstrong Siddeley Lynx engine) and had a maximum speed of 150 km/h. An order was originally placed (December 1926) by the Greek Navy for 18 aircraft but no further production followed, as, after the three month test flight period, it was considered inferior to alternative proposed models. The example built was used for technical personnel training at KEA and was most probably scrapped in 1938.


General characteristics

  • Crew: 2 (pilot and student/observer)
  • Length: 18 ft 11.9in (5.79m)
  • Wingspan: 16ft 11.5in (8.17m)
  • Height: ()
  • Powerplant: 1 × 120 hp or 130 hp SALMSON, ()

Performance


References[edit]

  • Jane's "All the World's Aircraft" (1928 edition)
  • Greek ERGA magazine, December 15, 1926 issue (info about Greek Navy order)
  • "Cross country" Hothersall & Travers 1990 ISBN 0-9515461-0-4 H. G. Travers (Helithon's test pilot) log book info and notes.