This specification covers an aluminum alloy in the form of rolled or cold finished bars, rods, and wire, and of flash welded rings. These products have been used typically for parts requiring high strength where limited formability is acceptable. Certain design and processing procedures may cause these products to be susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.
SAE AMS 4122L-2012由美国机动车工程师协会 US-SAE 发布于 2012-05-31。
SAE AMS 4122L-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 4122L-2012 由 SAE AMS 4122K-2007 变更而来。
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