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Bolts and Screws, Steel, UNS S66286 Tensile Strength 160 ksi, Procurement Specification
- Aerospace Standard
- AS4506C
- 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
AS6416 added to references, many paragraphs updated or deleted, specs updated, photo of bolt head deleted, figures redrawn, and notes updated.
Recommended Content
Topic
Data Sets - Support Documents
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| Table 1 | External thread depth at 2H/3 and allowable thread lap depth | |
| Table 2 | Test loads | |
| Table 3 | Values for “k” | |
| Table 4 | Summary of acceptance tests | |
| Table 5 | Sampling data nondestructive test - visual and dimensional characteristics for Classes Major A, Major B, Minor A, and Minor B | |
| Table 6 | Sampling data destructive tests - mechanical and metallic characteristics | |
| Table 7 | Classification of visual and dimensional characteristics |
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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