AMS 4918

SAE International: This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm), inclusive.

AMS 4901

SAE International: This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate up through 1.000 inch (25.40 mm), inclusive.

AMS 4902

SAE International: This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate up through 1.000 inch (25.40 mm). This material typically has been used for parts requiring aqueous corrosion resistance, moderate strength up to 400 °F (204 °C) and oxidation resistance up to 600 °F (316 °C), but usage is not limited to such applications.

AMS 4900

SAE International: This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate

AMS 4919

SAE International: This specification covers a titanium alloy in the form of sheet, strip, and plate 0.025 to 3.000 inches (0.64 to 76.20 mm), inclusive, in nominal thickness.

 

 

 

Disclaimer: The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. Changes may be made to the information contained herein.

 

 

 

AMS 4911

SAE International: 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.

 

 

Disclaimer: The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. Changes may be made to the information contained herein.

MIL/AMS-T-9047

Military Specification / SAE International: Titanium and Titanium Alloy Bars (rolled or forged) and reforged stock, aircraft quality (15 DEC 1978) [S/S BY SAE-AMS-T-9047]. This specification covers aircraft quality, commercially pure titanium and alpha, alpha-beta and beta titanium alloy rolled or forged bar and reforging stock products.

 

 

Disclaimer: The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. Changes may be made to the information contained herein.

MIL/AMS-T-9046

Military Specification / SAE International: This specification covers aircraft quality titanium and titanium alloy metal sheet, strip and plate products.

In September 1999, MIL-T-9046J was cancelled, and superseded by SAE AMS-T-9046. AMS-T-9046 was a word-for-word translation of MIL-T-9046J Amendment 2, with minor editorial and format changes. Unfortunately, AMS-T-9046 still covered nearly 20 grades of titanium and multiple conditions, rendering it somewhat complicated for users. In May 2006, AMS-T-9046 was cancelled as well, referring future procurement for each alloy and condition to a separate AMS specification.

If your contract requires use of the superseding specification, refer to the table below pointing to the Superseding Specifications for several material designations within AMS-T-9046.

 

 

Disclaimer: The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. Changes may be made to the information contained herein.

Reference: https://performancetitanium.com/understanding-milams-t-9046-supersession/

AMS 6931

SAE International: This specification covers a titanium alloy in the form of bars, forgings, and stock for forging.

 

 

 

Disclaimer: The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. Changes may be made to the information contained herein.

AMS 4928

SAE International: This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes up through 6.000 inches (152.40 mm) inclusive in diameter or least distance between parallel sides and stock of any size for forging or flash welded rings.

 

 

 

Disclaimer: The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. Changes may be made to the information contained herein.