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
05-30-1975
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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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