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Bolts, Cobalt-Chromium-Nickel Alloy UNS R30035, Tensile Strength 260 ksi, Procurement Specification
- Aerospace Standard
Published November 19, 2012 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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.
AS7468B has been reaffirmed to comply with the SAE five-year review policy.
|Aerospace Standard||Bolts and Screws, Steel, UNS S66286 Tensile Strength 160 ksi, Procurement Specification|
|Aerospace Standard||Bolts and Screws, Steel, Corrosion-Resistant, UNS S17400 Tensile Strength 140 ksi Procurement Specification|
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|
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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