This SAE Aerospace Standard (AS) establishes the requirements for AS3504 and AS3505 thin wall self-locking inserts made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718.
Rationale:
This revision corrects an error in the paragraph title for the ‘as-received’ self-locking torque test, Section 4 (Quality Assurance Provisions) has been substantially revised (including removal of AQLs, Table 6 completely revised, and Table 8 deleted), revise 1st cycle requirements for max locking torque for reuse testing, references have been updated including thread specification to AS8879 and others.
Related Topics:
Manufacturing processes
Heat resistant alloys
Heat resistant materials
Materials identification
Assembling
Nickel alloys
Heat treatment
Identification numbers
Production
Also known as: SAE AS 3506
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