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Air Ministry Official Notices

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 December 1936

Abstract

Failures having occurred on Monospar S.T.25 engine mounting members, at a point approximately 2½ in. from the engine attachment of the upper tubular member between the welded gusset plates, it has been decided that a modification to the engine mounting is essential.

Citation

(1936), "Air Ministry Official Notices", Aircraft Engineering and Aerospace Technology, Vol. 8 No. 12, pp. 343-343. https://doi.org/10.1108/eb030132

Publisher

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MCB UP Ltd

Copyright © 1936, MCB UP Limited