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Aluminium Alloy BS L167 2014A-T6 Clad Sheet

Technical Data Sheet

Aluminium alloy BS L167 is the aerospace specification for 2014A-T6 Alclad sheet and strip. In order to combat 2014A's poor corrosion resistance, L167 is clad with pure aluminium. L167 is the same alloy as L165, and will always meet the chemistry and mechanical requirements for both, but is produced to tighter rolling tolerances. L167 / 2014A is alloyed with copper (3.90-5.00%) giving it high strength, which it retains after its heat treatment. As such L165 finds usage in many aerospace and defence high strength applications. Aircraft Materials stocks L167 in a wide range of sheet thicknesses ready for same day shipment. Many stock items can be dual-certified to both L167 and L165.

Chemical Composition Limits
Weight%	Si	Fe	Cu	Mn	Cr	Mg	Ni	Zn	Ti+Zr	Ti
L167	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 Min (N/mm2)	Tensile Strength Min (N/mm2)	Elongation on 50mm Min (%)
L167	T6	0.4 - 0.8	350	415	7
L167	T6	0.8 - 1.6	350	420	8
L167	T6	1.6 - 6.0	370	420	9

Availability
Aluminium Alloy L167 is available in Sheet and Strip T6. For all stock availability of Aluminium L167 contact Sales.

Specifications
Similar Specification
2014A
Clad 1050A Close Tolerance Rolled
BS L165

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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.