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SAE AMS4911

Revision N, March 1, 2014

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Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed



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Product Details:

  • Revision: Revision N, March 1, 2014
  • Published Date: March 2014
  • 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 sheet, strip, and plate up through 4.000 inches (101.60 mm) inclusive in thickness.

Application

These products have been used typically for parts requiring strength up to 750 °F (399 °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