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This specification covers a magnesium alloy in the form of sand castings.

This SAE recommended practice defines and establishes tolerances and attributes of cold rolled strip steels. Differences between cold rolled strip and cold rolled sheet products are discussed so that process designers can make informed material selection decisions.

This specification covers a copper alloy (naval brass) in the form of bars and rods. These products have been used typically for automatic screw machine parts, but usage is not limited to such applications. These products have better corrosion resistance than AMS4610 but are less readily machinable.

This specification covers a titanium alloy in the form of forgings up to 4.000 inches (101.60 mm) inclusive and forging stock.

This specification covers a high-strength, corrosion-resistant alloy in the form of bar up to 1.75 inches (44.4 mm) in diameter (see 8.2 and 8.7).

This specification covers a high-strength, corrosion-resistant alloy in the form of bars up to 1.75 inches (44.4 mm) in diameter (see 8.2 and 8.7).

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and forging stock.

This procurement specification covers inserts made from A286 alloy of the type identified under the Unified Numbering System as UNS S66286, solid film lubricated with a piastic self locking device, integrated locking keys to positively secure the insert against rotation when properly installed in threaded holes.

This specification establishes requirements for a corrosion-removing compound in the form of a liquid concentrate.

This specification covers requirements for silver deposited on metal parts with a nickel strike between the basis metal and the silver deposit.

This SAE Technical Report documents efforts toward developing a Test Method for the evaluation of hose protection sleeves used in hydraulic fluid power applications. These sleeves are intended for general application and hydraulic systems on industrial equipment and commercial products. These sleeves shall be capable of providing protection to pin hole failures in hydraulic systems operating to working pressures specified by the manufacturer. Hose assembly burst containment is not in the scope of this document.

in this AIR should be considered, as opposed to long-life operation and environmental requirements of a manned aircraft, engine-driven pump. Appendix A is intended to indicate typical environments for several different types of missiles. The actual requirements for a given system should be used and specified in the detailed specification.Missile pumps are categorized by a moderate testing life and a relatively short operational service life. Generally, the pumps are operated at higher speeds, temperatures, and pressures than those used in manned aircraft systems, yet reliability must be extremely high, since there rarely is a redundant system aboard the missile. Due to the short but critical life and performance requirements, development, reliability and acceptance testing should be focussed on eliminating infant mortality failures. Missile pumps must be compatible with very severe environmental conditions during the service life.

This document is intended to supplement the SAE J1939 documents by offering the SAE J1939 information in a form that can be sorted and search for easier use.

This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.

This GA introduces the cycle interruption option of AMS2774 (when their is a furnace outage during a long heat treatment operation)

SCOPE IS UNAVAILABLE.

This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.

This specification covers a titanium alloy in the form of sheet.