SAE International Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed MAM4911B

Description
This specification covers a titanium alloy in the form of sheet, strip, and plate procured in metric units. AMS 4911 is the inch/pound version of this MAM. These products have been used typically for parts requiring strength up to 400 degrees C, but usage is not limited to such applications. 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.
Description
This specification covers a titanium alloy in the form of sheet, strip, and plate procured in metric units. AMS 4911 is the inch/pound version of this MAM. These products have been used typically for parts requiring strength up to 400 degrees C, but usage is not limited to such applications. 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.

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Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed - MAM4911B - SAE International
Warrendale, PA, United States
Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed
MAM4911B
Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed MAM4911B
This specification covers a titanium alloy in the form of sheet, strip, and plate procured in metric units. AMS 4911 is the inch/pound version of this MAM. These products have been used typically for parts requiring strength up to 400 degrees C, but usage is not limited to such applications. 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.

This specification covers a titanium alloy in the form of sheet, strip, and plate procured in metric units. AMS 4911 is the inch/pound version of this MAM. These products have been used typically for parts requiring strength up to 400 degrees C, but usage is not limited to such applications. 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.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number MAM4911B
Product Name Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed
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