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E-25 General Standards for Aerospace and Propulsion Systems
AS7471F - Bolts and Screws, Nickel Alloy, UNS N07001 Tensile Strength 165 ksi, Corrosion and Heat Resistant, Procurement Specification
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Document Number:
AS7471F
Project Initiation:
12-25-2010
Project Number:
E-25-12-10TGB
Revision Number:
F
Sponsor Name:
Roy Clarke
Title
Bolts and Screws, Nickel Alloy, UNS N07001 Tensile Strength 165 ksi, Corrosion and Heat Resistant, Procurement Specification
Scope
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07001. The following specification designations and their properties are covered: AS7471: 165 ksi minimum ultimate tensile strength at room temperature 75 ksi stress-rupture strength at 1350 °F AS7471-1: 165 ksi minimum ultimate tensile strength at room temperature 99 ksi minimum ultimate shear strength at room temperature Primarily for aerospace propulsion systems applications where a good combination of tensile strength, and resistance to relaxation at elevated temperatures up to approximately 1500 °F is required.
Rationale
Delete fatigue test from the para. 1 Scope, as the test is not required.
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