Aluminium Alloy BS L164 2014A-T4 Clad Sheet
Technical Data Sheet
Aluminium alloy BS L164 is the aerospace specification for 2014A-T4 Alclad sheet and strip. L164 / 2014A is alloyed with copper (3.90-5.00%) giving it high strength, which it retains after its heat treatment. As such L164 finds usage in many aerospace and defence high strength applications. Aircraft Materials stocks L164 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 |
| Alloy L164 | 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
| Grade | Condition | Thickness (mm) | 0.2% Proof Stress (MPa) | Tensile Strength (MPa) | Elongation (%) |
| Alloy L164 | T4 | 0.4 - 1.6 | 240 | 385 min | 14 |
| Alloy L164 | T4 | 1.6 - 6.0 | 245 | 390 min | 14 |
Availability
Aluminium Alloy L164 is available in Sheet and Strip T4. For all stock availability of Aluminium L164 contact Sales.
Specifications
Similar Specification
2014A
Clad 1050A
BS L166
Customer Reviews - What Customers Say About Us!
| CLICK HERE TO VIEW OUR BROCHURE |
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.
