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Bolts and Screws, Steel, UNS S66286 Tensile Strength 130 ksi, Procurement Specification
- Aerospace Standard
Published August 26, 2020 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable, iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
Paragraph added to show definition for a rateable lap. Paragraphs also modified to bring into line with existing standards.
Data Sets - Support Documents
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|Table 1||Test loads|
|Table 2||UNJ ext thread depth at 2H/3 and allowable thread lap depth|
|Table 3||Summary of acceptance tests|
|Table 4||Sampling data|
|Table 5||Classification of visual and dimensional characteristics|
|Table 6||Sampling data|
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
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