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SAE AMS4988
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SAE AMS4988 Revision C, March 1, 2014
Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated
Description / Abstract:
Form
This specification covers a titanium alloy in the form of sheet, strip, and plate in thicknesses up through 4.000 inches (101.60 mm), inclusive (See 8.7).
Application
This material has been used typically for parts to be formed or machined in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 °F (288 °C) in the precipitation heat treated condition, 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.
This specification covers a titanium alloy in the form of sheet, strip, and plate in thicknesses up through 4.000 inches (101.60 mm), inclusive (See 8.7).
Application
This material has been used typically for parts to be formed or machined in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 °F (288 °C) in the precipitation heat treated condition, 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.
SAE AMS4988 Revision C, March 1, 2014
Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated