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Viewing 241 to 270 of 35866
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.
HISTORICAL
1996-05-01
Standard
AMS4920B
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 requir 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
2007-06-27
Standard
AMS4920D
This specification covers a titanium alloy in the form of forgings and forging stock.
HISTORICAL
2011-05-25
Standard
AMS4920E
This specification covers a titanium alloy in the form of forgings and forging stock.
CURRENT
2015-02-19
Standard
AMS4920F
This specification covers a titanium alloy in the form of forgings, 6.000 inches (152.40 mm) and under in cross-sectional thickness and forging stock of any size.
HISTORICAL
1952-11-01
Standard
AMS4921
This specification covers one grade of commercially-pure titanium in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1957-07-01
Standard
AMS4921A
This specification covers one grade of commercially-pure titanium in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1966-09-30
Standard
AMS4918A
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1977-01-15
Standard
AMS4918E
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1965-09-01
Standard
AMS4918
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1995-05-01
Standard
AMS4918G
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1971-05-15
Standard
AMS4918C
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1984-10-01
Standard
AMS4918F
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
2003-01-07
Standard
AMS4918J
This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts not requiring heat treatment but requiring high mechanical properties in the annealed condition, but usage is not limit to such application. This alloy exhibits high strength-to-weight ratios up to 750 degrees F (399 degrees C). Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.
HISTORICAL
2006-05-17
Standard
AMS4918L
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1996-06-01
Standard
AMS4918H
This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts not requiring heat treatment but requiring high mechanical properties in the annealed condition, but usage is not limit to such application. This alloy exhibits high strength-to-weight ratios up to 750 degrees F (399 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.
HISTORICAL
2003-07-31
Standard
AMS4918K
This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts not requiring heat treatment but requiring high mechanical properties in the annealed condition, but usage is not limit to such application. This alloy exhibits high strength-to-weight ratios up to 750 degrees F (399 degrees C). Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.
Viewing 241 to 270 of 35866