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Bolts and Screws, Titanium Alloy 6.0Al – 4.0V Procurement Specification For
- Aerospace Standard
- AS7460A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers aircraft-quality bolts and screws made of 6.0Al-4.0V titanium alloy and of 160 ksi tensile strength at room temperature.
Rationale
Updated para 3.5 by adding “two to” three threads in agreement with NASM1312-8 test methodology. Added additional difinitions to para 2.2. General updating for SAE requirements for obsolete specifications and standards.
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | THREAD HEIGHT | |
| 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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