Aluminium Alloy BS L157 2014A-T6 Sheet
Technical Data Sheet
Aluminium alloy BS L157 is the aerospace specification for 2014A-T6 bare sheet and strip. L157 / 2014A is alloyed with copper (3.90-5.00%) giving it high strength levels of 430 N/mm² UTS minimum. As such L157 finds usage in many aerospace and defence high strength applications where is poor corrosion resistance is not a factor. Aircraft Materials stocks L157 in a wide range of sheet thicknesses ready for same day shipment
| Chemical Composition Limits | ||||||||||
| Weight% | Si | Fe | Cu | Mn | Cr | Mg | Ni | Zn | Ti+Zr | Ti |
| L157 | 0.50 - 0.90 | 0.50 max | 3.9 - 5.0 | 0.4 - 1.2 | 0.10 max | 0.2 - 0.8 | 0.10 max | 0.25 max | 0.20 max | 0.15 max |
Typical Mechanical Properties
| Material | Condition | Thickness (mm) | 0.2% Proof Stress (MPa) | Tensile Strength (MPa) | Elongation (%) |
| L157 | T6 | 0.4-0.8 | 370 | 430 | 6 |
| L157 | T6 | 0.8-1.6 | 380 | 440 | 7 |
| L157 | T6 | 1.6-6.0 | 390 | 440 | 7 |
Availability
Aluminium Alloy BS L157 is available in Sheet and Strip. For all stock availability of Aluminium BS L157 contact Sales.
Specifications
Similar Specification
2014A
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Disclaimer
Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.
