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Viewing 45091 to 45120 of 45239
HISTORICAL
1966-03-15
Standard
AMS4916
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1976-01-15
Standard
AMS4916C
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1968-11-01
Standard
AMS4916B
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1994-04-01
Standard
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.
HISTORICAL
2003-04-29
Standard
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.
HISTORICAL
1977-01-15
Standard
AMS4916D
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1984-04-01
Standard
AMS4916E
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
2010-04-19
Standard
AMS4916K
This specification covers a titanium alloy in the form of sheet, strip, and plate.
CURRENT
2017-11-21
Standard
AMS4916L
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm) inclusive in thickness (see 8.6).
HISTORICAL
2003-10-22
Standard
AMS4916H
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
2006-05-17
Standard
AMS4916J
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1967-11-01
Standard
AMS6302B
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1975-06-15
Standard
AMS6302C
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1953-06-15
Standard
AMS6302
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1964-01-31
Standard
AMS6302A
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1994-06-01
Standard
AMS6302F
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts, such as shafts and fasteners, in service up to 1000 degrees F (540 degrees C), but usage is not limited to such applications.
HISTORICAL
2004-02-10
Standard
AMS6302G
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1982-04-01
Standard
AMS6302D
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1988-04-01
Standard
AMS6302E
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1984-10-01
Standard
AMS6501
This specification covers a maraging steel in the form of welding wire.
CURRENT
2017-11-21
Standard
AMS6302K
This specification covers an aircraft quality, low alloy, heat resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
2012-09-28
Standard
AMS6302J
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
2007-09-13
Standard
AMS6302H
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
2007-05-15
Standard
AMS6501D
This specification covers a maraging steel in the form of welding wire.
HISTORICAL
2002-03-13
Standard
AMS6501C
This specification covers a maraging steel in the form of welding wire.
HISTORICAL
1996-06-01
Standard
AMS6501B
This specification covers a maraging steel in the form of welding wire.
HISTORICAL
1995-05-01
Standard
AMS6501A
This specification covers a maraging steel in the form of welding wire.
HISTORICAL
1996-11-01
Standard
ARP1210C
This SAE Aerospace Recommended Practice (ARP) describes a class of digital computer programs for use by organizations other than the engine supplier for reduction of engine test data relating to the interface of the engine in the airframe or test facility. This ARP also is intended as a guide for the preparation of such computer programs.
HISTORICAL
1990-11-01
Standard
ARP1210B
This Aerospace Recommended Practice (ARP) describes a class of digital computer programs for use by organizations other than the engine supplier for reduction of engine test data relating to the interface of the engine in the airframe or test facility. This ARP also is intended as a guide for the preparation of such computer programs.
HISTORICAL
1974-04-01
Standard
ARP1210A
This SAE Aerospace Recommended Practice (ARP) describes a class of digital computer programs for use by organizations other than the engine supplier for reduction of engine test data relating to the interface of the engine in the airframe or test facility. This ARP also is intended as a guide for the preparation of such computer programs.
Viewing 45091 to 45120 of 45239