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BOLTS AND SCREWS, STEEL, CORROSION AND HEAT RESISTANT Precipitation Heat Treated Before Roll Threaded 160 000 psi Minimum Tensile Strength
- Aerospace Standard
- AS4506
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers bolts and screws made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, and of 160 000 psi minimum ultimate tensile strength at room temperature, with maximum test temperature of parts at 1000 °F.
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Topic
Data Sets - Support Documents
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| TABLE 1 | Thread Height | |
| TABLE 2 | Tensile Test Load | |
| TABLE 3 | Summary of Acceptance Tests | |
| TABLE 4 | Sampling Data | |
| TABLE 5 | Classification of Defects | |
| 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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