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1968-11-01
Standard
AMS2814B
This specification covers spooling and packaging of bare welding wire to ensure cleanliness and freedom from corrosion, spool sizes and weights of spooled wire, and package weights of cut lengths.
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.
1968-11-01
Standard
AMS2510C
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.
1968-11-01
Standard
AMS2469C
This specification establishes the requirements for a hard anodic coating on aluminum and aluminum alloys.
1968-11-01
Standard
AMS2401B
This specification covers the engineering requirements for cadmium deposited on ferrous metals.
1968-11-01
Standard
AMS2503B
This specification covers the engineering requirements for finishing aircraft parts and assemblies with a black enamel.
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.
1968-11-01
Standard
AMS2400M
This specification covers the requirements for electrodeposited cadmium on metal parts.
1968-06-01
Magazine
1968-05-01
Standard
AMS2669A
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of October, 1991.
1968-05-01
Standard
AMS2421A
This specification covers the requirements for surface preparation of magnesium and magnesium alloys to provide a surface finish which can be soft soldered.
1968-05-01
Standard
AMS2420A
This specification covers the requirements for preparation of aluminum and aluminum alloys for soldering by zinc immersion pre-treatment followed by copper plating and tin or tin-zinc alloy plating.
1968-05-01
Standard
AMS2664
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.
1968-05-01
Standard
AMS2675C
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 nickel alloy filler metal.
1968-05-01
Standard
AMS2350K
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.
1968-05-01
Standard
AMS2667A
This specification covers the engineering requirements for producing brazed joints in parts fabricated from austenitic corrosion and heat resistant steels, but may also be used on carbon or low-alloy steels or copper alloys, and the properties of such joints.
1968-05-01
Standard
AMS2690
This specification defines the equipment, procedures, and requirements for joining leads by parallel gap resistance welding. For attaching leads by parallel gap resistance welding in the assembly of microelectronic circuitry to thin film substrates.
1968-02-01
Technical Paper
680383
Herbert E. Lindner
Inspection for quality control of spur and helical gears and splines involves the ability to obtain information at a proper precision level, and to use this information as related to requirements. Measurements of gears and splines provide information on the active elements as produced, that is, profile, lead, and index. These factors combined indentify a map of the surf ace of the active elements. Analysis of this map provides optimum quality control application.
1968-02-01
Technical Paper
680490
Arthur Bender
Three methods of tolerancing are described. In widest use is the method of extremes, which produces unnecessarily close limits on the components. For the same over-all limits on the assembly the probability method allows wider limits on the components, but there are some unrealistic assumptions involved. A third method is described which results in tolerances falling between the other two. A case history is discussed comparing the three methods.
1968-02-01
Technical Paper
680655
Kirk E. Birrell
Manufacturing processes of discrete parts have increased in complexity and productivity with a simultaneous tightening of dimensional tolerances. Computers, which have been at the forefront of this dramatic manufacturing evolution, are now being applied in the dimensional quality control function. These applications include simple error and tolerance calculations as well as more sophisticated data storage, adaptive control, statistical error analysis, and optimizing routines. Computers are being dedicated to discrete component process control as well as used on a time-sharing basis. This paper explores the development and application of computerized measurement techniques to acquaint the technical manager-process planner with this new and growing field.
1967-11-01
Standard
AMS2521
null, null
This specification covers optical-quality coatings applied to instrument glasses.
1967-11-01
Standard
AMS2435A
This specification covers the engineering requirements for applying tungsten carbide/cobalt coatings to metal parts by the detonation process and the properties of such coatings.
1967-11-01
Standard
AMS2350J
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.
1967-11-01
Standard
AMS2475B
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.
1967-11-01
Standard
AMS2436A
This specification covers the engineering requirements for applying aluminum oxide to metal parts by detonation deposition and the properties of such coatings.
1967-11-01
Standard
AMS2303
null, null
This specification covers steel cleanliness requirements for aircraft-quality ferro-magnetic, hardenable corrosion-resistant steels by magnetic particle inspection methods. Applicable primarily to blooms, billets, tube rounds, stock for forging or flash welded rings, slabs, bars, sheet, strip, plate, tubing, and extrusions used in fabricating parts subject to magnetic particle inspection, but may be used for qualification of a heat melt, or lot of steel.
1967-11-01
Standard
AMS2665B
This specification covers the engineering requirements for producing brazed joints in parts fabricated from steels, iron alloys, nickel alloys, cobalt alloys, and copper alloys by use of silver alloys, and the properties of such joints. This procedure has been used typically for joints requiring high strength up to 400 degrees F (204 degrees C), but usage is not limited to such applications.
1967-08-01
Magazine

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