
| 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 | T4 T6 T6511 |
230 370 370 |
370 415 435 |
| Chemical Composition EN AW-2014A | |
| Si | 0.15-0.90 |
| Fe | 0.50 |
| Cu | 3.9-5.0 |
| Mn | 0.40-1.2 |
| Mg | 0.20-0.8 |
| Cr | 0.10 |
| Zn | 0.25 |
| Ti | - |
(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 2014 A is very similar in characteristics to 2014. See chemical composition for difference.
Alloy 2014A as 2014 is commonly used for aerospace components and fittings due to its high strength. Other applications include; military vehicles, bridges, weapons manufacture and structural applications.
* 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.