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SAE AMS4970

Revision K, September 1, 2016

Complete Document

Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated



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Product Details:

  • Revision: Revision K, September 1, 2016
  • Published Date: September 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 up to 4.000 inches (101.60 mm) inclusive and forging stock.

Application

This alloy has been used typically for parts requiring strength up to 900 °F (482 °C), but usage is not limited to such applications.

Certain processing procedures and service conditions may cause these products to become subject to stresscorrosion cracking; ARP982 recommends practices to minimize such conditions.

AIA/NAS Aerospace Standards