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Viewing 211 to 240 of 45396
HISTORICAL
2001-05-01
Standard
AMS4930E
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring good weldability and ductility, combined with good notch-toughness down to -320 degrees F (-196 degrees C), but usage is not limited to such applications.
HISTORICAL
2006-09-22
Standard
AMS4930F
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
2002-12-13
Standard
AMS4931B
This specification covers a titanium alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring a combination of high tensile strength up to 750 degrees F (399 degrees C) and high fracture toughness, but usage is not limited to such applications.
HISTORICAL
2007-11-16
Standard
AMS4931C
This specification covers a titanium alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1993-04-01
Standard
AMS4931A
This specification covers a titanium alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring a combination of high tensile strength up to 750 degrees F (399 degrees C) and high fracture toughness, but usage is not limited to such applications.
HISTORICAL
1992-04-01
Standard
AMS4931
This specification covers a titanium alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1966-03-15
Standard
AMS4930
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1985-04-01
Standard
AMS4930C
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1994-04-01
Standard
AMS4930D
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1969-11-01
Standard
AMS4930A
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
2017-09-22
WIP Standard
AMS4914G
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inches in thickness. These products have been used typically in applications requiring high strength-to-weight ratio and stability up to 550 °F (288 °C), but usage is not limited to such applications. Parts are typically formed in the solution heat treated condition and subsequently precipitation heat treated to final condition.
HISTORICAL
1976-01-15
Standard
AMS4930B
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
CURRENT
2014-04-08
Standard
AMS4914F
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inches (3.18 mm) in thickness.
HISTORICAL
2009-09-28
Standard
AMS4914E
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inches in thickness.
HISTORICAL
2009-05-28
Standard
AMS4914D
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inches in thickness.
HISTORICAL
1976-01-15
Standard
AMS4915C
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1968-11-01
Standard
AMS4915B
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1966-09-30
Standard
AMS4915A
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1966-03-15
Standard
AMS4915
This specification covers a titanium alloy in the form of sheet, strip, and plate.
CURRENT
1981-01-01
Standard
AMS4913B
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of December, 1991.
HISTORICAL
1991-10-01
Standard
AMS4913A
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of December, 1991.
HISTORICAL
1961-01-15
Standard
AMS4913
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of December, 1991.
HISTORICAL
2003-07-23
Standard
AMS4914C
This specification covers a titanium alloy in the form of sheet and strip. These products have been used typically for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 degrees F (288 degrees C) in the precipitation heat treated condition, but usage is not limited to such applications.
HISTORICAL
2002-01-16
Standard
AMS4914B
This specification covers a titanium alloy in the form of sheet and strip. These products have been used typically for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 degrees F (288 degrees C) in the precipitation heat treated condition, but usage is not limited to such applications.
HISTORICAL
1992-07-01
Standard
AMS4914A
This specification covers a titanium alloy in the form of sheet and strip.
HISTORICAL
1984-04-01
Standard
AMS4914
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inches in thickness. These products have been used typically in applications requiring high strength-to-weight ratio and stability up to 550 °F (288 °C), but usage is not limited to such applications. Parts are typically formed in the solution heat treated condition and subsequently precipitation heat treated to final condition.
HISTORICAL
2002-08-20
Standard
AMS4920C
This specification covers a titanium alloy in the form of forgings and forging stock. These forgings have been used typically for parts that do not require heat treatment but require high mechanical properties in the annealed condition and for which processing above the beta transus is permissible, but usage is not limited to such applications. This alloy exhibits high strength-to-weight ratios up to 750 degrees F (399 degrees C).
HISTORICAL
1984-07-01
Standard
AMS4920
This specification covers a titanium alloy in the form of forgings and forging stock.
HISTORICAL
1990-04-01
Standard
AMS4920A
This specification covers a titanium alloy in the form of forgings and forging stock.
Viewing 211 to 240 of 45396

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