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SAE AMS4976

Revision K, July 2017

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Titanium Alloy, Forgings 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo - 08Si Solution and Precipitation Heat Treated



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Product Details:

  • Revision: Revision K, July 2017
  • Published Date: July 2017
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 7
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form

This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal diameter or least distance between parallel sides and 9 in2 (58 cm2) and under in cross-sectional area and forging stock of any size (see 8.5).

Application

These products have been used typically for parts requiring high strength and toughness and good creep resistance up to 1000 °F (538 °C), but usage is not limited to such applications.

Certain processing procedures and service conditions may cause these forgings to become subject to stress-corrosion cracking; ARP982 recommends practices to minimize such conditions.

AIA/NAS Aerospace Standards