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HISTORICAL
2010-02-24
Standard
AMS4901R
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate.
HISTORICAL
1955-08-15
Standard
AMS4902
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate. This material typically has been used for parts requiring aqueous corrosion resistance, moderate strength up to 400 °F (204 °C) and oxidation resistance up to 600 °F (316 °C), but usage is not limited to such applications.
HISTORICAL
2011-06-23
Standard
AMS4901S
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate.
CURRENT
2015-03-24
Standard
AMS4901T
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate up through 1.000 inch (25.40 mm), inclusive.
CURRENT
1969-11-01
Standard
AMS4906A
This specification has been Cancelled by the Aerospace Materials Division, SAE, as of August 1994.
HISTORICAL
2014-03-11
Standard
AMS4905E
This specification covers one type of titanium alloy plate in the beta-annealed condition of plate up through 4.000 inches (101.60 mm) inclusive in thickness (See 8.5).
CURRENT
2017-11-03
Standard
AMS4905F
This specification covers one type of titanium alloy plate in the beta-annealed condition up through 4.000 inches (101.60 mm) inclusive in thickness (see 8.6).
HISTORICAL
1994-03-01
Standard
AMS4905B
This specification covers one type of titanium alloy plate in the beta-annealed condition. This plate has been used typically for parts in damage-tolerant, stress-corrosion-resistant applications requiring strength up to 750 degrees F (399 degrees C), but usage is not limited to such applications.
HISTORICAL
2008-02-04
Standard
AMS4905D
This specification covers one type of titanium alloy plate in the beta-annealed condition.
HISTORICAL
1981-04-01
Standard
AMS4905
This specification covers one type of titanium alloy plate in the beta-annealed condition.
HISTORICAL
1988-01-01
Standard
AMS4905A
This specification covers one type of titanium alloy plate in the beta-annealed condition.This plate has been used typically for parts in damage-tolerant, stress-corrosion-resistant applications requiring strength up to 750 degrees F (399 degrees C), but usage is not limited to such applications.
CURRENT
2015-03-24
Standard
AMS4904C
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 2.000 inches (50.80 mm), inclusive.
HISTORICAL
2004-01-12
Standard
AMS4905C
This specification covers one type of titanium alloy plate in the beta-annealed condition.
HISTORICAL
2007-07-05
Standard
AMS4904A
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
2011-06-07
Standard
AMS4904B
This specification covers a titanium alloy in the form of sheet, strip, and plate.
CURRENT
2015-03-24
Standard
AMS4903C
This specification covers a titanium alloy in the form of sheet strip, and plate up through 2.000 inches (50.80 mm), inclusive.
HISTORICAL
2003-04-17
Standard
AMS4904
This specification covers a titanium alloy in the form of sheet, strip, and plate. This material has been typically 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. 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
2011-06-07
Standard
AMS4903B
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
2007-06-13
Standard
AMS4903A
This specification covers a titanium alloy in the form of sheet, strip, and plate.
2017-04-26
WIP Standard
AMS4907L
This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring a combination of weldability, ductility, and good notch-toughness down to –423 °F (–253 °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.
HISTORICAL
1968-11-01
Standard
AMS4908B
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1975-06-15
Standard
AMS4908C
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1957-07-01
Standard
AMS4908A
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1952-11-01
Standard
AMS4908
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs.
CURRENT
2013-09-26
Standard
AMS4907K
This specification covers a titanium alloy in the form of sheet, strip, and plate on product 0.008 to 3.000 inches (0.20 to 76.20 mm), inclusive in thickness.
HISTORICAL
2009-12-17
Standard
AMS4907J
This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring a combination of weldability, ductility, and good notch-toughness down to -423 °F (-253 °C), but usage is not limited to such applications.
HISTORICAL
2005-12-07
Standard
AMS4907H
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
2001-11-19
Standard
AMS4907G
This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring a combination of weldability, ductility, and good notch-toughness down to -423 degrees F (-253 degrees C), but usage is not limited to such applications.
HISTORICAL
1994-05-01
Standard
AMS4907F
This specification covers a titanium alloy in the form of sheet, strip, and plate.
Viewing 31 to 60 of 45396