This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring a combination of weldability, ductility, and good notch-toughness down to -423 °F (-253 °C), but usage is not limited to such applications. Certain processing procedures and service conditions may cause those products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.
SAE AMS 4909J-2012由美国机动车工程师协会 US-SAE 发布于 2012-08-16。
SAE AMS 4909J-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: 49.025.30 钛。
SAE AMS 4909J-2012 由 SAE AMS 4909H-2008 变更而来。
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