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Inspection Instruments

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1972

25

Abstract

It was feared that should the wheel hubs and flanges develop stress relieving cracks and the aircraft be subjected to particularly high lateral loading, part or all of a wheel flange could break.

Citation

(1972), "Inspection Instruments", Aircraft Engineering and Aerospace Technology, Vol. 44 No. 7, pp. 26-28. https://doi.org/10.1108/eb034924

Publisher

:

MCB UP Ltd

Copyright © 1972, MCB UP Limited

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