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Viewing 9841 to 9870 of 10147
HISTORICAL
1945-08-01
Standard
AMS6320B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1945-08-01
Standard
AMS2412
This specification covers the requirements for silver deposited on metal parts with a copper strike between the basis metal and the silver deposit. This process has been used typically to provide a bearing surface and to prevent galling or seizing of metal surfaces of parts made of materials where a high baking temperature may be detrimental to the properties of the basis material.
HISTORICAL
1945-08-01
Standard
AMS6328
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-08-01
Standard
AMS6415B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-08-01
Standard
AMS6440B
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1945-07-01
Standard
AMS6365A
This specification covers an aircraft-quality, low-alloy steel in the form of seamless tubing. This tubing has been used typically for thin wall-thickness sections where minimum tensile strength up to 160 ksi (1103 MPa) is required and where parts may be welded during fabrication, but usage is not limited to such applications.
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
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
AMS6327B
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
HISTORICAL
1945-07-01
Standard
AMS6475
This specification covers a nitriding grade of aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for nitrided parts requiring highest surface hardness, high core hardness, resistance to heat, and less distortion than parts made from steel requiring quenching to case harden, but usage is not limited to such applications.
HISTORICAL
1945-07-01
Standard
AMS5620
This specification covers two types of corrosion and heat resistant steel in the form of bars, wire, forgings, and forging stock.
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
1945-07-01
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
AMS6360B
This specification covers an aircraft-quality, low-alloy steel in the form of seamless tubing. This tubing has been typically used in thin wall-thickness sections where minimum tensile strength up to 160,000 psi (1103 MPa) is required and where parts may be welded during fabrication, but usage is not limited to such applications.
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
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
1945-06-01
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
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.