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Viewing 9751 to 9780 of 10047
HISTORICAL
1945-07-01
Standard
AMS6535B
Primarily for use where welding and moderate tensile properties are required. May be used where minimum tensile strength up to 180,000 psi (1240 MPa) is required for wall thicknesses up to 0.125 in. (3 mm) and proportionately lower strength is required in heavier thicknesses. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of 19 April 1988. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1945-07-01
Standard
AMS6550B
Primarily for general use is light wall-thickness sections where minimum tensile strength up to 160,000 psi (1105 MPa) is required and parts may be welded during fabrication. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of April 19, 1988. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1945-07-01
Standard
AMS6327B
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
HISTORICAL
1945-07-01
Standard
AMS6325B
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
HISTORICAL
1945-07-01
Standard
AMS5045
This specification covers a carbon steel in the form of sheet and strip.
HISTORICAL
1945-07-01
Standard
AMS2232
This specification covers established inch/pound manufacturing tolerances applicable to carbon steel sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term 'excl' is used to apply only to the higher figure of the specified range. Tolerances for products sizes not listed herein shall be as agreed upon by purchaser and vendor.
HISTORICAL
1945-07-01
Standard
AMS6317B
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
HISTORICAL
1945-07-01
Standard
AMS5610C
This specification covers two types of free-machining, corrosion and moderate heat resistant steel in the form of bars, wire, forgings, and forging stock.
HISTORICAL
1945-07-01
Standard
AMS2252
This specification covers established inch/pound manufacturing tolerances applicable to low-alloy steel sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term 'excl' is used to apply only to the higher figure of the specified range.
HISTORICAL
1945-07-01
Standard
AMS5042C
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
HISTORICAL
1945-07-01
Standard
AMS3410A
This specification covers a silver-brazing flux in the form of a paste which contains not more than 35% water by weight.
HISTORICAL
1945-06-01
Standard
AMS2615
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.
HISTORICAL
1945-05-01
Standard
AMS6254D
HISTORICAL
1945-05-01
Standard
AMS6324
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts, 0.750 inch (19.05 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 50 HRC when properly hardened and tempered and also parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
HISTORICAL
1945-05-01
Standard
AMS5686
This specification covers a corrosion-resistant steel in the form of wire. This wire has been used typically for fabricating into rivets, but usage is not limited to that application.
HISTORICAL
1945-05-01
Standard
AMS5022B
This specification covers a carbon steel in the form of bars, forgings, mechanical tubing, and stock for forging or heading.
HISTORICAL
1945-05-01
Standard
AMS6250D
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-05-01
Standard
AMS6260B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-05-01
Standard
AMS6263B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-05-01
Standard
AMS6264B
This specification covers an aircraft quality, low alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-05-01
Standard
AMS6272C
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-05-01
Standard
AMS6270C
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-05-01
Standard
AMS5565A
This specification covers a corrosion-resistant steel in the form of welded tubing. This tubing has been used typically for parts, such as fluid-conducting lines not subjected to high pressure, requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 degrees F (427 degrees C) during fabrication may impair corrosion resistance.
HISTORICAL
1945-05-01
Standard
AMS5560A
This specification covers a corrosion-resistant steel in the form of seamless tubing. This tubing has been used typically for parts, such as fluid-conducting lines, not subjected to high pressure and requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 °F (427 °C) during fabrication may impair corrosion resistance.
HISTORICAL
1945-05-01
Standard
AMS2251
This specification covers established inch/pound manufacturing tolerances applicable to low-alloy steel bars ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "exclusive " is used to apply only to the higher figure of the specified range.
HISTORICAL
1945-05-01
Standard
AMS2475A
This specification establishes the requirements for chromate conversion coatings on magnesium alloys. This process has been used typically to improve corrosion resistance and adherence of organic finishes but usage is not limited to such applications. The dichromate treatment may not be suitable for alloys with high manganese content. The chrome pickle treatment has been used as touch-up for previously dichromate-treated surfaces and for improving corrosion protection temporarily, but usages are not limited to such applications.
HISTORICAL
1945-05-01
Standard
AMS2243
This specification covers manufacturing tolerances applicable to seamless and welded tubing of corrosion and heat-resistant steel ordered to inch dimensions. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. Tubing may be specified by two dimensions only (OD and wall thickness, ID and wall thickness, or OD and ID).
HISTORICAL
1945-05-01
Standard
AMS6274C
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-05-01
Standard
AMS5640B
This specification covers three types of a free-machining, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
HISTORICAL
1945-05-01
Standard
AMS5570D
This specification covers a corrosion and heat resistant steel in the form of seamless tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when such parts are welded during fabrication, and also for parts requiring oxidation resistance up to 1500 degrees F (816 degrees C) but useful at that temperature only when stresses are low; usage is not limited to such applications.