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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.