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

 

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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.