
| 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-2014 | |
| Si | 0.15-1.2 |
| Fe | 0.7 |
| Cu | 3.9-5.0 |
| Mn | 0.40-1.2 |
| Mg | 0.20-0.8 |
| Cr | 0.10 |
| Zn | 0.25 |
| Ti | 0.15 |
| 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)
Aluminium alloy 2014 has very high strength, and very good machining characteristics.
Alloy 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.