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Bolts and Screws, Titanium Alloy 6.0Al - 4.0V Procurement Specification For
- Aerospace Standard
Published April 26, 2017 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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.
Hydrogen test requirement added to lot acceptance Table 3, Figures 1 to 7 redrawn.
|Aerospace Standard||Bolts and Screws, Roll Threaded Procurement Specification For|
|Aerospace Standard||Bolts and Screws, Nickel Alloy UNS N07718, Classification: 185 ksi/1200 °F Procurement Specification|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|Table 1||Thread height|
|Table 2||Test loads|
|Table 3||SUMMARY of acceptance tests|
|Table 4||Sampling data Nondestructive tests Visual and dimensional characteristics for Classes Major A, Major B, Minor A, and Minor B|
|Table 5||Classification of visual and dimensional characteristics|
|Table 6||Sampling data Destructive tests Mechanical and metallurgical characteristics|
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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