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BS EN 4283:2005
Aerospace series. Aluminium alloy AL-P2219-T87. Plate. 6 mm < a = 40 mm
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Summary
Hardness;Aluminium alloys;Rolling;Chemical composition;Elongation;Air transport engineering;Tensile strength;Sheet materials;Electrical conductivity;Aluminium;Corrosion resistance;Stress corrosion;Aircraft components;Thickness;Heat treatment;Proof stress
Technical characteristics
| Publisher | British Standards Institution (BSI) |
| Publication Date | 12/07/2005 |
| Page Count | 10 |
| Themes | Proof stress |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
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07/12/2005
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