Criteria

Text:
Topic:
Content:
Display:

Results

Viewing 9931 to 9960 of 10243
1945-10-01
Standard
AMS2242
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of corrosion and heat resistant steels, iron alloys, titanium, and titanium alloys ordered to inch 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.
1945-08-01
Standard
AMS2650
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of 1-1-84. It is recommended that this specification not be specified for new designs. This cover sheet should be attached to the initial issue of the sUbject specification. Noncurrent refers to those procedures which have previously been widely used and which may be required on some existing designs in the future. The Aerospace Materials Division does not recommend these as standard procedures for future use in new designs. Each of these "Noncurrent" specifications is available from SAE upon request. This specification has been CANCELLED by the Aerospace Materials Division, SAE, as of August, 1989. By this action, subject specification number and its title will be deleted from the active specification index of Aerospace Material Specifications.
1945-08-01
Standard
AMS6412B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
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.
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.
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.
1945-08-01
Standard
AMS6440B
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
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.
1945-08-01
Standard
AMS6322B
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.
1945-08-01
Standard
AMS2410
This specification covers the engineering requirements for electrodeposition of silver on other metals, usually with a nickel strike between the basis metal and the silver.
1945-08-01
Standard
AMS6470B
This specification covers an aircraft quality nitriding grade low alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
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.
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.
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.
1945-07-01
Standard
AMS6325B
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
1945-07-01
Standard
AMS5045
This specification covers a carbon steel in the form of sheet and strip.
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.
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.
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.
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.
1945-07-01
Standard
AMS6317B
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
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.
1945-07-01
Standard
AMS6327B
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
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.
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.
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.
1945-06-01
Standard
AMS2615
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.
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.