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SAE AMS4963

Revision D, August 1, 2016

Complete Document

Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable, Modified Strength



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Product Details:

  • Revision: Revision D, August 1, 2016
  • Published Date: August 2016
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 8
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings up through 3.999 inches (101.57 mm), inclusive and stock for forging, flash welded rings, or heading.

Application

These products have been used typically for parts to be rough machined prior to solution and precipitation heat treatment and for parts requiring high strength-to-weight ratios at or near room temperature, but usage is not limited to such applications.

Certain processing procedures and service conditions may cause these products to become subject to stresscorrosion cracking; ARP 982 recommends practices to minimize such conditions.

AIA/NAS Aerospace Standards