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HISTORICAL
1969-11-01
Standard
AMS2815J
This specification covers procedures for marking bare wire for welding to provide positive identificaiton of cut lengths, regardless of length, and of spools, and to ensure that the wire is clean and free from foreign materials and corrosion.
HISTORICAL
1969-11-01
Standard
AMS2664A
This specification covers the engineering requirements for producing brazed joints in parts made of steels, iron alloys, nickel alloys, and cobalt alloys by use of silver alloy filler metals, and the properties of such joints.
HISTORICAL
1969-11-01
Standard
AMS2816G
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
HISTORICAL
1969-11-01
Standard
AMS2350N
To establish the issue of specifications, standards, and recommended practices published by standardizing agencies other than divisions and committees of the Aerospace Council of SAE approved for use in determining conformance to requirements of Aerospace Material Specifications (AMS) and other specifications in which this specification is referenced.
HISTORICAL
1969-11-01
Standard
AMS2695
This specification covers electrical connections made with single, solid, round copper or copper alloy wire wrapped around copper alloy terminals without the use of solder.
HISTORICAL
1969-11-01
Standard
AMS2371
null, null
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought corrosion and heat-resistant steel and alloy products and of forging stock.
HISTORICAL
1969-11-01
Standard
AMS2406E
This specification covers the requirements for electrodeposited hard chromium plate.
HISTORICAL
1969-11-01
Standard
AMS2411A
This specification covers the requirements for silver deposited on metal parts with a nickel strike between the basis metal and the silver deposit.
HISTORICAL
1969-05-01
Standard
AMS2646B
Detection of discontinuities such as cracks, laps, porosity, cold shuts, lack of bond, and similar defects. Because inspection can be performed in normal light, this method can be used when fluorescent penetrant inspection is impracticable.
HISTORICAL
1969-05-01
Standard
AMS2815H
This specification covers procedures for marking bare wire for welding to provide positive identificaiton of cut lengths, regardless of length, and of spools, and to ensure that the wire is clean and free from foreign materials and corrosion.
HISTORICAL
1969-05-01
Standard
AMS2640H
HISTORICAL
1969-05-01
Standard
AMS2816F
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
HISTORICAL
1969-05-01
Standard
AMS2350M
To establish the issue of specifications, standards, and recommended practices published by standardizing agencies other than divisions and committees of the Aerospace Council of SAE approved for use in determining conformance to requirements of Aerospace Material Specifications (AMS) and other specifications in which this specification is referenced.
HISTORICAL
1969-05-01
Standard
AMS2475C
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
1969-05-01
Standard
AMS2375
null, null
AMS 2375D results from a Five Year Review and update of this specification.
HISTORICAL
1969-05-01
Standard
AMS2370
null, null
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought carbon and low-alloy steel products and of forging stock.
HISTORICAL
1969-05-01
Standard
AMS2410E
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
1969-05-01
Standard
AMS2412E
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
1969-05-01
Standard
AMS2430F
This specification covers the engineering requirements for automatic peening of surfaces of parts by impingement of metallic shot, glass beads, or ceramic shot. To induce residual compressive stress in surface layers of parts, thereby increasing fatigue strength and resistance to stress-corrosion cracking but usage is not limited to such applications.
1969-02-01
Technical Paper
690228
J. G. Schofer
Computers for data processing and process control are being used for foundry management. Data processing applications are listed with brief explanations. The process control application is melting control of a 108 in. water wall cupola being continuously tapped into a 100 ton electric induction holding furnace. The process control computer project objectives, computer system, and instrumentation are described.
1969-02-01
Technical Paper
690577
H. R. Neifert, F. J. Wren
This paper discusses how periodic revision of tapered roller bearing ratings and reappraisal of the rating formula used by The Timken Roller Bearing Co. are accomplished by a continuing testing program on standard product bearings. An extensive sampling plan, designed to include bearing product up to 6 in. O.D. from both domestic and overseas manufacturing plants, is fully described. A review of recent fatigue tests on over 5000 bearings illustrates the experimental basis for the rating increases announced in 1967. Limited bearing fatigue tests conducted under conditions of lubricant, temperature, and speed different from those used for establishing bearing ratings indicate the need for determining rating adjustment factors to compensate for the influence of the application environment.
1969-02-01
Technical Paper
690227
Roger Wellington
Engine development entails about equal measures of performance testing and durability, or life testing. The differing requirements of these two types of testing have resulted in separate data acquisition systems. For performance work the system design reflects the needs for flexibility, accuracy, considerable calculation of data, and for the printing and plotting of results. For a durability facility, where the output is test hours instead of data, the data system design stresses test monitoring and control. This system has not yet gone on line, although a hand wired system has been in service for ten years.
HISTORICAL
1969-02-01
Standard
J380_196902
Specific gravity is a nondestructive test used as a quality control check of the consistency of formulation and processing of brake lining. The specific gravity and the range of specific gravity are peculiar to each formulation and, therefore, the acceptable values or range must be established for each formulation by the manufacturer. Specific gravity alone shows nothing about a materials in use performance. The specific gravity of sintered metal powder friction materials, particularly those which have steel backing members, is usually determined somewhat differently. Reference ASTM B 376. Purpose To establish a uniform procedure for determining the specific gravity of brake friction material.
HISTORICAL
1968-11-01
Standard
AMS2505B
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
1968-11-01
Standard
AMS2815G
This specification covers procedures for marking bare wire for welding to provide positive identificaiton of cut lengths, regardless of length, and of spools, and to ensure that the wire is clean and free from foreign materials and corrosion.
HISTORICAL
1968-11-01
Standard
AMS2673A
This specification covers the engineering requirements for producing brazed joints of aluminum and aluminum alloys by immersion in molten flux bath.
HISTORICAL
1968-11-01
Standard
AMS2816E
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
HISTORICAL
1968-11-01
Standard
AMS2510C
HISTORICAL
1968-11-01
Standard
AMS2350L
To establish the issue of specifications, standards, and recommended practices published by standardizing agencies other than divisions and committees of the Aerospace Council of SAE approved for use in determining conformance to requirements of Aerospace Material Specifications (AMS) and other specifications in which this specification is referenced.
HISTORICAL
1968-11-01
Standard
AMS2416E
This specification covers the engineering requirements for an electrodeposit of cadmium into an electrodeposit of nickel on carbon, low-alloy, and corrosion-resistant steels.

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