This specification covers an aluminum alloy procured in the form of sheet Alclad on both sides. These products have been used typically for formed structural parts requiring good formability in T4 temper and ability to develop improved resistance to fatigue crack growth and high toughness with moderate strength when aged to T62 temper, but usage is not limited to such applications.
SAE AMS 4405A-2012由美国机动车工程师协会 US-SAE 发布于 2012-04-05。
SAE AMS 4405A-2012 在中国标准分类中归属于: V11 航空与航天用金属铸锻材料,在国际标准分类中归属于: 49.025.20 铝。
SAE AMS 4405A-2012 由 SAE AMS 4405-2006 变更而来。
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