
| Mechanical Properties | ||||||||
| Forming | Machining | Welding | Brazing/Soldering | Protective Anodising | Aesthetic Anodising | Temper | Restrict Min N/mm | Stress Min N/mm |
| Good | Good | Not Suitable | Not Suitable | Fair | Not Suitable | T3 T3510/ T3511 |
260 260 - |
393 393 - |
| Chemical Composition EN AW-2024 | |
| Si | 0.5 |
| Fe | 0.5 |
| Cu | 3.8-4.9 |
| Mn | 0.3-0.9 |
| Mg | 1.2-1.8 |
| Cr | 0.10 |
| Zn | 0.25 |
| Ti | 0.15 |
| Others (each) | 0.5 |
| 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)
Aluminium alloy 2024 has a very high strength, slightly higher than 2014. High fatigue strength is used to an advantage on structures and parts where good strength to weight ratio are required.
Alloy 2024 commonly used for aerospace components – machined or fabricated items. Also used for engineering.
* 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.