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

1994-06-01
HISTORICAL
MAM4911A
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.
Standard

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

2003-03-12
CURRENT
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.
Standard

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

1988-04-01
HISTORICAL
MAM4911
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.
Standard

Titanium Alloy, Sheet, Strip, and Plate, 13.5v 11cr 3.0al, Solution Heat Treated

1994-04-01
HISTORICAL
AMS4917E
This specification covers a titanium alloy in the form of sheet, strip, and plate. Primarily for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated. Suitable for parts, such as pressure vessels and aircraft structures, requiring high strength-to-weight ratio and stability up to 550 degrees F (288 degrees C). This alloy may have poor crack propagation resistance in the precipitation heat treated condition. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP982 recommends practices to minimize such conditions.
Standard

Titanium Alloy Sheet, Strip, and Plate 8al 1mo 1v Duplex Annealed

2003-04-29
HISTORICAL
AMS4916G
This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring strength and fracture toughness up to 800 degrees F (427 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; ARP982 recommends practices to minimize such conditions.
Standard

Titanium Alloy, Sheet, Strip, and Plate, 8al 1mo 1v, Duplex Annealed

1994-04-01
HISTORICAL
AMS4916F
This specification covers a titanium alloy in the form of sheet, strip, and plate. Primarily for parts requiring strength and fracture toughness up to 800 degrees F (427 degrees C). Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP982 recommends practices to minimize such conditions.
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