Superseded , Under review Standard
Historical

BS EN 2087:2005

Aerospace series. Aluminium alloy AL-P2014A. T6 or T62. Clad sheet and strip 0,4 mm = a = 6 mm

Summary

Aircraft components;Air transport engineering;Elongation;Aluminium alloys;Dimensions;Mechanical properties of materials;Bending;Sheet materials;Tensile strength;Thickness;Aluminium;Chemical composition;Strips;Proof stress;Heat treatment

Technical characteristics

Publisher British Standards Institution (BSI)
Publication Date 12/31/2016
Cancellation Date 05/15/2025
Page Count 10
Themes Heat treatment
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