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SAE AMS4294A
- Aluminum Alloy Extrusions, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T5511), Press Heat Treated, Stress Relieved by Stretching, Straightened, and Artificially Aged (Cancelled: Dec 2010)
- standard by SAE International, 12/02/2010
- Publisher: SAE
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This document has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of December 2010. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED".This specification covers an aluminum alloy in the form of extruded bars and rods.These extrusions have been used typically for parts requiring moderate strength and where distortion during machining must be minimized, but usage is not limited to such applications.These extrusions have been used for applications which do not require the technical requirements and quality assurance provisions of AMS 2772 heat treatment.
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