This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers an aluminum alloy in the form of sheet and plate supplied in the -T861 temper. These products have been used typically for structural parts requiring a combination of high strength and good corrosion resistant and whose fabrication does not involve welding; but usage is not limited to such applications.
SAE AMS 4271A-2013由美国机动车工程师协会 US-SAE 发布于 2013-07-25。
SAE AMS 4271A-2013 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: 77.120.10 铝和铝合金。
SAE AMS 4271A-2013 溶液热处理和冷加工以及人工老化铝合金片材和板材4.4Cu 1.5Mg 0.60Mn (2024-T861) 由 SAE AMS 4271-2011 变更而来。
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