BS 2L 95:1971
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Specification for plate of aluminium-zinc-magnesium-copper-chromium alloy (solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15)
Hardcopy , PDF
15-11-1992
English
31-08-1971
1 Inspection and testing procedure
2 Quality of material
3 Chemical composition
4 Condition
5 Heat treatment
6 Mechanical properties
Specifies plate made from aluminium and alloying constituents, with or without approved scrap, at the discretion of the manufacturer, including that which has been forged as an intermediate operation, which is finished by hot or cold rolling, but excludes forged plate.
Committee |
ACE/61/-/24
|
DevelopmentNote |
Supersedes 69/27775 DC and 91/73185 DC. Superseded by BS EN 2126, but remains current. (07/2005) Inactive for the new design. (12/2007)
|
DocumentType |
Standard
|
Pages |
8
|
PublisherName |
British Standards Institution
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
DEFSTAN 79-17/2(1998) : 1998 | COMPOUND, CLEANING, FOAMING, FOR AIRCRAFT SURFACES |
DEFSTAN 79-15/2(1998) : 1998 | COMPOUND, CLEANING GEL FOR AIRCRAFT SURFACES |
SAE AMS79_017 | Compound, Cleaning, Foaming, for Aircraft Surfaces |
SAE AMS79_015 | Compound, Cleaning Gel for Aircraft Surfaces |
BS 2L96(1971) : LATEST | PLATE OF ALUMINIUM ZINC MAGNESIUM COPPER CHROMIUM ALLOY (SOLUTION TREATED AND PRECIPITATION TREATED: NOT CONTROLLED STRETCHED) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15) |
BS 2L 88:1971 | Specification for aluminium-alloy-coated sheet and strip of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15) |
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