BS L 162:1976
Withdrawn
Specification. Cold compressed hand forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)
Hardcopy , PDF
English
05-28-1976
09-27-2012
NO CONTENTS SECTION
Describes manufacture, inspection and testing of heat resisting alloys for aerospace use. G ives chemical composition and mechanical properties. This covers cold compressed hand forgings of aluminium zinc magnesium copper chromium alloy.
| Committee |
ACE/61/-/24
|
| DevelopmentNote |
Supersedes 72/36415 DC. (08/2005) Inactive for the new design. (12/2007)
|
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
British Standards Institution
|
| Status |
Withdrawn
|
| BS L 160:1976 | Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
| BS L 161:1976 | Specification. Hand and die forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
| BS 3763:1970 | The International System of units (SI) |
| BS L 161:1976 | Specification. Hand and die forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
| BS 350:2004 | Conversion factors for units |
| BS L 160:1976 | Specification. Bars and extruded sections of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22) |
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