BS L 118:1975
Current
The latest, up-to-date edition.
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)
Hardcopy , PDF
English
30-05-1975
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 and 87/74680 DC (08/2005) Reviewed and confirmed by BSI, January 2011. (12/2010)
|
DocumentType |
Standard
|
Pages |
10
|
PublisherName |
British Standards Institution
|
Status |
Current
|
BS L 117:1975 | 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) |
BS L 117:1975 | 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) |
BS 3763:1970 | The International System of units (SI) |
BS 350:2004 | Conversion factors for units |
ASTM E 215 : 2016 : REDLINE | Standard Practice for Standardizing Equipment and Electromagnetic Examination of Seamless Aluminum-Alloy Tube |
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