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BS EN 2088:2005
Aerospace series. Aluminium alloy AL-P2014A. T4 or T42. Clad sheet and strip. 0,4 mm = a = 6 mm
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Summary
Strips;Proof stress;Elongation;Sheet materials;Tensile strength;Dimensions;Chemical composition;Mechanical properties of materials;Thickness;Aluminium;Air transport engineering;Aircraft components;Bending;Aluminium alloys;Heat treatment
Technical characteristics
| Publisher | British Standards Institution (BSI) |
| Publication Date | 12/31/2016 |
| Page Count | 10 |
| Themes | Heat treatment |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
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31/12/2016
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