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Aluminium Alloy BS L165 2014A-T6 Clad Sheet

Technical Data Sheet

Aluminium alloy BS L165 is the aerospace specification for 2014A-T6 Alclad sheet and strip. In order to combat 2014A's poor corrosion resistance, L165 is clad with pure aluminium. L165 / 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 L165 in a wide range of sheet thicknesses ready for same day shipment.

Chemical Composition Limits
Weight%SiFeCuMnCrMgNiZnTi+ZrTi
L1650.50 - 0.900.50 max3.9 - 5.00.4 - 1.20.10 max0.2 - 0.80.10 max0.25 max0.20 max0.15 max

Typical Mechanical Properties

GradeConditionThickness (mm)0.2% Proof Stress Min (N/mm2)Tensile Strength Min (N/mm2)Elongation on on 50 mm Min (%)
L165T60.4 - 0.83454157
L165T60.8 - 1.63454208
L165T61.6 - 6.03554209

Availability

Aluminium Alloy L165 is available in Sheet and Strip T6. For all stock availability of Aluminium L165 contact Sales.

Specifications

Similar Specification

2014A

Clad 1050A

BS L167

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