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Bolts, Cobalt-Chromium-Nickel Alloy UNS R30035, Tensile Strength 260 ksi, Procurement Specification
- Aerospace Standard
- AS7468B
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers bolts made from a corrosion resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30035.
Rationale
AS7468B has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
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Topic
Data Sets - Support Documents
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| TABLE 1 | UNJ External 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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