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SAE AMS4908

Revision G, January 1, 2003

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Titanium Alloy, Sheet and Strip 8Mn Annealed, 110 ksi (758 MPa) Yield Strength



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Product Details:

  • Revision: Revision G, January 1, 2003
  • Published Date: January 2003
  • Status: Not Active, See comments below
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 8
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form: This specification covers a titanium alloy in the form of sheet and strip.

Application: Primarily for parts requiring good formability and strength up to 600°F (315°C). Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP 982 recommends practices to minimize such conditions.

AIA/NAS Aerospace Standards