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Viewing 1411 to 1440 of 1454
HISTORICAL
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 ".
HISTORICAL
1945-10-01
Standard
AMS2415
This specification covers the requirements for electrodeposited and diffused lead and indium plate.
HISTORICAL
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.
HISTORICAL
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.
HISTORICAL
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.
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
AMS2223
This specification covers established inch/pound manufacturing tolerances applicable to copper and copper alloy seamless tubing 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 a specified range.
HISTORICAL
1945-06-01
Standard
AMS2615
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.
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
AMS2400D
This specification covers the requirements for electrodeposited cadmium on metal parts.
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
1944-11-01
Standard
AMS2601B
This specification provides requirements and procedures for gas-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2602A
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2605A
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2607A
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2606B
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2810
This specification provides requirements for the identification and packaging of sheet, strip, extrusions, and molded parts made of natural rubber, synthetic rubber, reclaimed rubber, and combinations of the above with other materials such as asbestos, cork, and fabrics. AMS2817 covers preferred requirements for identification and packaging of preformed packings.
HISTORICAL
1944-11-01
Standard
AMS2510A
This specification covers the engineering requirements for finishng aircraft parts and assemblies with an engine gray enamel.
HISTORICAL
1944-11-01
Standard
AMS2402A
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.
HISTORICAL
1944-08-01
Standard
AMS2450A
This specification covers the procedure to be used for spraying metallic parts with aluminum and the properties of the coating.
HISTORICAL
1944-08-01
Standard
AMS2640A
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
HISTORICAL
1944-06-01
Standard
AMS2400C
This specification covers the requirements for electrodeposited cadmium on metal parts.
HISTORICAL
1942-12-01
Standard
AMS2400B
This specification covers the requirements for electrodeposited cadmium on metal parts.
HISTORICAL
1942-12-01
Standard
AMS2402
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.
HISTORICAL
1942-03-01
Standard
AMS2470A
This specification establishes the requirements for anodic coatings on aluminum alloys.
HISTORICAL
1942-01-01
Standard
AMS2450
This specification covers the procedure to be used for spraying metallic parts with aluminum and the properties of the coating.
HISTORICAL
1942-01-01
Standard
AMS2601A
This specification provides requirements and procedures for gas-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS2602
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS2605
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS2607
This specification provides requirements and procedures for air-pressure leak testing of parts.
Viewing 1411 to 1440 of 1454