Rationale:
AMS-QQ-A-250/4B stabilizes this specification because it is no longer state of the art and equivalent technical requirements are contained in other SAE Aerospace Material Specifications.
Related Topics:
Heat treatment
Aluminum alloys
Tensile strength
Copper
Chromium
Manganese
Nickel
Titanium
Also known as: SAE AMSQQA 250/4
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