Victa Aircruiser

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Addbot (talk | contribs) at 23:39, 20 March 2013 (Bot: Migrating 2 interwiki links, now provided by Wikidata on d:q2483835). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.


Victa Aircruiser
Role Four-seat light touring monoplane
National origin Australia
Manufacturer Victa
Designer Henry Millicer
First flight 18 July 1966
Number built 1
Developed from Victa Airtourer
Variants AESL CT/4 Airtrainer

The Victa Aircruiser was an 1960s Australian four-seat touring monoplane designed by Henry Millicer and built by Victa.[1]

Development

Following the success of the earlier Airtourer, Millicer designed a four-seat version which he called the Aircruiser.[1] The prototype registered VH-MVR first flew on 18 July 1966.[1] Like the airtourer it was a low-wing monoplane with a fixed nosewheel landing gear and powered by a 210 hp (157 kW) Continental IO-360-H piston engine.[1] Rather than the sliding roof of the Airtourer the four-seat Aircruiser had a fixed cabin roof.[1]

Following the sale of the design rights of the Airtourer to Aero Engine Services Limited (AESL) of New Zealand the rights to the Aircruiser were also sold to AESL in 1969.[1] AESL re-designed the aircraft as the AESL CT/4 Airtrainer, a fully aerobatic military trainer.[1]

Specifications

General characteristics

See also

Related development

References

Notes

  1. ^ a b c d e f g Simpson 1991, p. 332

Bibliography

  • Simpson, R.W. (1991). Airlife's General Aviation. England: Airlife Publishing. ISBN 1-85310-194-X. {{cite book}}: Cite has empty unknown parameter: |coauthors= (help)