
| Mechanical Properties | ||||||||
| Forming | Machining | Welding | Brazing/Soldering | Protective Anodising | Aesthetic Anodising | Temper | Restrict Min N/mm | Stress Min N/mm |
| Good | Good | Good | Good | Good | Good | T4 T5 T6 |
90 160 190 |
150 200 230 |
| Chemical Composition EN AW-6063(A) | |
| Si | 0.30-0.6 |
| Fe | 0.15-0.35 |
| Cu | 0.10 |
| Mn | 0.15 |
| Mg | 0.6-0.9 |
| Cr | 0.05 |
| Zn | 0.15 |
| Ti | 0.10 |
| Others (each) | 0.05 |
| Others (total) | 0.15 |
| Aluminium | Remainder |
(The chemical composition of aluminium and aluminium alloys is supplied in percentage by mass. Limits are expressed as a maximum unless shown as a range or a minimum)
Aluminum alloy 6063A is a variation of 6063 but with greater strength. The advantage of aluminium alloy 6063A is that is still has good surface finish qualities.
Aluminium alloy 6063A is used in the same applications as 6063 but can also be found in the following; Road & Rail transport.
* Properties given are typical and should only be used for comparisons of alloys. Actual values will depend on section specification.
** Aerospace materials are covered by the ‘L’ series of British standards.
Note: Whilst every effort is made to ensure the accuracy of data provided, Capalex does not guarantee or accept liability for its accuracy.