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BS L 117:1975

Current
Current

The latest, up-to-date edition.

Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: not tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

05-30-1975

NO CONTENTS SECTION

Describes manufacture, inspection and testing of heat resisting alloys for aerospace purposes. Gives chemical composition and mechanical properties. This covers tube of aluminium magnesium silicon copper chromium alloy.

Committee
ACE/61/-/24
DevelopmentNote
Supersedes 73/35606 DC (08/2005) Reviewed and confirmed by BSI, January 2011. (12/2010)
DocumentType
Standard
Pages
8
PublisherName
British Standards Institution
Status
Current

BS L 118:1975 Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)

BS L 118:1975 Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
BS 3763:1970 The International System of units (SI)
BS 350:2004 Conversion factors for units

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