Browse Standards AS7468A
Historical REVISED 1997-12-01

Bolts, Cobalt-Chromium-Nickel Alloy, UNS R30035, Tensile Strength 260 ksi, Procurement Specification AS7468A

This procurement specification covers aircraft bolts made from a corrosion resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30035. The following specification designations and their properties are covered: AS7468, 260 ksi minimum ultimate tensile strength at room temperature, 135 ksi tension to 13.5 ksi tension fatigue at room temperature; AS7468-1, 260 ksi minimum ultimate tensile strength at room temperature, 145 ksi minimum ultimate shear strength at room temperature. Primarily for aerospace propulsion system applications where an excellent combination of strength, fatigue, and corrosion resistance is required at temperatures upto 700°F.
AS7468B
2012-11-19
Latest
Reaffirmed
AS7468A
1997-12-01
Historical
Revised
AS7468
1991-01-17
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Purchase more aerospace standards and aerospace material specifications and save! AeroPaks offer a customized subscription plan that lets you pay for just the documents that you need, when you need them.

Get Involved

Want to participate in updating this standard?

X