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Studs, Corrosion and Heat Resistant Steel, UNS S66286 Tensile Strength 130 ksi 1800 °F Solution Heat Treated, Aged Before Roll Threading Procurement Specification
- Aerospace Standard
- AS7482B
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers studs made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286. The following specification designations and their properties are covered:
Rationale
Mechanical test references updated, thread specification changed to AS8879 and general updating to conform to current requirements.
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Unnamed Dataset 4 | ||
| TABLE 1 | UNJ EXT THREAD DEPTH AT 2H/3 AND ALLOWABLE THREAD LAP DEPTH | |
| TABLE 2 | TEST LOADS | |
| 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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