This procurement specification covers aircraft quality studs made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286 and of 130 000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200°F.
SAE AS7481-1991由美国机动车工程师协会 US-SAE 发布于 1991-01-07。
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