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Bolts and Screws, Steel, UNS S66286 Tensile Strength 130 ksi, Procurement Specification
- Aerospace Standard
- AS7477H
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
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 |
Issuing Committee
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.
Reference
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