Aircraft Systems

Abstract

Descriptions of the Super VC1O's Hydraulic, Electrical, Flying Controls, Fuel, Air Conditioning and Pressurization, Flight Systems, Radio, Electronics and Anti‐icing Systems. THE June 1962 issue of AIRCRAFT ENGINEERING contained a comprehensive engineering description of the Standard VC10 and one of the articles contained in that issue dealt with systems, testing and equipment. However, the systems were dealt with comparatively briefly and it is therefore the object of this article to describe the principal systems in greater detail. The systems of the Standard and Super VC10 aircraft are essentially similar and the following description is based on British Aircraft Corporation's descriptive engineering notes.

Citation

(1965), "Aircraft Systems", Aircraft Engineering and Aerospace Technology, Vol. 37 No. 4, pp. 128-133. https://doi.org/10.1108/eb034007