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1966-09-01
Standard
AMS2362
This specification establishes a procedure for designating minimum stress-rupture property requirements of castings by means of this AMS number and a series of dash numbers.
1966-09-01
Standard
AMS2400L
This specification covers the requirements for electrodeposited cadmium on metal parts.
1966-09-01
Standard
AMS2480B
This specification covers the requirements for producing a zinc phosphate coating on ferrous alloys and the properties of the coating. This process has been used typically to produce a coating that will ensure satisfactory paint adherence, but usage is not limited to such applications.
1966-09-01
Standard
AMS2413A
This specification covers the engineering requirements for electrodeposition of silver and rhodium and the properties of the deposit.
1966-09-01
Standard
AMS2360
null, null
This specification establishes a procedure for designating minimum room temperature tensile property requirements of castings by means of this AMS number and a series of dash numbers.
1966-09-01
Standard
AMS2816D
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
1966-09-01
Standard
AMS2350G
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.
1966-09-01
Standard
AMS2411
This specification covers the requirements for silver deposited on metal parts with a nickel strike between the basis metal and the silver deposit.
1966-09-01
Standard
AMS2470F
This specification establishes the requirements for anodic coatings on aluminum alloys.
1966-09-01
Standard
AMS2815F
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.
1966-09-01
Standard
AMS2474A
This specification establishes the engineering requirements for producing chemical-film coatings on aluminum and aluminum alloys and the properties of such coatings. Primarily for aluminum and aluminum alloys where increased corrosion resistance, improved paint adhesion, or a low-electrical resistance coating is required. Also useful for improving the corrosion resistance and paint adhesion properties of abraded or discontinuous anodized surfaces of aluminum and aluminum alloy parts.
1966-09-01
Standard
AMS2450C
This specification covers the procedure to be used for spraying metallic parts with aluminum and the properties of the coating.
1966-09-01
Standard
AMS2430E
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.
1966-08-01
Standard
J966_196608
This SAE Recommended Practice provides a test procedure for determining passenger car tire revolutions per mile. It is intended to supplement SAE J678.
1966-03-01
Standard
AMS2409C
This specification covers the engineering requirements for producing a thin tin coating on aluminum alloys by an immersion process.
1966-03-01
Standard
AMS2425
This specification covers the requirements for gold deposited on metal surfaces and the properties of the deposit.
1966-03-01
Standard
AMS2350F
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.
1966-03-01
Standard
AMS2419
This specification covers the engineering requirements for electrodeposition of titanium-cadmium on metal parts and the properties f the deposit. This process has been used typically to provide corrosion resistance to high strength steel for use in fracture critical applictions such as aircraft landing gear and naval arrestor hooks at temperatures below 450 degrees F (232 degrees C) by limiting the generation of hydrogen and potential hydrogen embrittlement, but usage is not limited to such applications.
1966-03-01
Standard
AMS2416D
This specification covers the engineering requirements for an electrodeposit of cadmium into an electrodeposit of nickel on carbon, low-alloy, and corrosion-resistant steels.
1966-03-01
Standard
AMS2755A
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of July 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”. Cancelled specifications are available from SAE.
1966-03-01
Standard
AMS2472A
This specification establishes the requirements for dyed anodic coatings on aluminum alloys.
1966-03-01
Standard
AMS2469B
This specification establishes the requirements for a hard anodic coating on aluminum and aluminum alloys.
1966-03-01
Standard
AMS2422A
This specification covers the engineering requirements for electrodeposition of gold and the properties of the deposit.
1966-02-01
Technical Paper
660204
George R. Biggs
The purpose of this paper is to give a brief outline of the philosophies and methods used in the quality and reliability programs of the leading manufacturer of business and personal aircraft. As noted in the article, the personnel involved are numerous and range from trainee to scientist covering every basic modern science except the most exotic ones. While the activities are not radical, they do represent practical refinements of techniques which have been proven by results. We hope they contribute to the progress of our industry.
1966-02-01
Technical Paper
660166
G. D. Mattison
The fact that different countries use different dimensioning systems spurred the New Products Engineering Group of John Deere Waterloo Tractor Works to develop a system for interchangeability of parts manufactured in their factories. This paper discusses how the group undertook their assignment.
1966-02-01
Technical Paper
660091
Dwayne Gray
Zero Defects is a program that attacks mistakes and errors at all levels. It is a management tool for the reduction of defects through prevention, not detection. In the three years since its inception, the program has saved millions of dollars in American industry, proving the employee can do his job right the first time when properly motivated. Success of the program depends on: total management support, careful planning, dynamic program administration, and intense employee indoctrination. The basis of the Zero Defects concept is the challenge to strive for error free performance, and the recognition of those who have accepted the challenge.
1966-01-10
Technical Paper
660122
B. J. Ludwig
The use of computers in the Quality Control Department of an automotive assembly plant is described. The concept of Real Time reporting is detailed; information on production problems affecting quality is relayed to appropriate areas for corrective action. All information is then processed daily to provide a 5-Day Summary Report on each quality variation. Computers are also used to assess repair time and to compare results of service complaints with similar conditions at each assembly plant.
1965-10-20
Technical Paper
650964
EARL R. SMITH
1965-09-01
Standard
AMS2401A
This specification covers the engineering requirements for cadmium deposited on ferrous metals.
1965-09-01
Standard
AMS2816C
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.

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