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Viewing 19231 to 19260 of 19915
1945-10-01
Standard
AMS7312
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings, oil scraper rings, and dual oil control rings in aircraft piston engines.
1945-10-01
Standard
AMS4827A
This specification covers bearings of a leaded bronze cast on one or both faces of a steel backing.
1945-10-01
Standard
AMS4825A
This specification covers bearings of a leaded bronze cast on one or both faces of a steel backing.
1945-10-01
Standard
AMS2505
This specification has been declared "CANCELLED "by the Aerospace Materials Division, SAE, as of December 2008. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED ".
1945-10-01
Standard
AMS5591
This specification covers a corrosion and heat resistant steel in the form of seamless tubing.
1945-10-01
Standard
AMS6281
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
1945-10-01
Standard
AMS2415
This specification covers the requirements for electrodeposited and diffused lead and indium plate.
1945-10-01
Standard
AMS3128
null, null
This specification covers a pigment material in the form of a paste comprising aluminium powder mixed in a suitable binder.
1945-10-01
Standard
AMS3165
This specification covers a petroleum-base liquid solvent.
1945-10-01
Standard
AMS6372
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.75 inch (19 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
1945-10-01
Standard
AMS5044A
This specification covers a carbon steel in the form of sheet and strip.
1945-10-01
Standard
AMS2241A
This specification covers established manufacturing tolerances applicable to corrosion and heat-resistant steel, iron alloy, titanium, and titanium alloy bars and wire. 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.
1945-10-01
Standard
AMS2241
null, null
This specification covers established manufacturing tolerances applicable to corrosion and heat-resistant steel, iron alloy, titanium, and titanium alloy bars and wire. 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.
1945-10-01
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.
1945-10-01
Standard
AMS4822A
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of January 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED ".
1945-10-01
Standard
AMS6350A
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
1945-10-01
Standard
AMS6357B
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
1945-10-01
Standard
AMS2243A
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).
1945-10-01
Standard
AMS2402B
This specification covers the requirements for electrodeposited zinc plating. Unless otherwise stated on the engineering drawing, high strength steel parts having a hardness of 45 HRC or greater shall not be electroplated.
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
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
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
AMS6412B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
1945-08-01
Magazine
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.
1945-08-01
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
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
AMS6440B
This specification covers a 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
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.
Viewing 19231 to 19260 of 19915

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