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Fastener standards for materials address the very metals that fasteners are composed of. With different applications requiring varying levels of corrosion resistance, resistance to deformity and high strength at different high temperatures, different manufacturing processes, dimensions, as well as considerations of matching metals to prevent galvanic corrosion. This list addresses those made from steel alloys.
This SAE Aerospace Standard (AS) provides material identification codes for aluminum alloys, copper alloys, carbon steels, alloy steels, titanium alloys, corrosion resistant materials, and heat resistant materials that are used to make AN, MS, and AS engine and propeller standard utility parts. This document also provides similar material codes for company parts (such as nuts, bolts, etc.) having design configuration similar to other company parts or the engine and propeller standard utility parts (AN, MS, and AS) that are not of the same material.
This specification describes the physical, mechanical and metallurgical requirements for carbon and alloy steel wire, rods and bars in coils intended for the manufacture of mechanical fasteners which include: bolts, nuts, rivets, screws, washers and special formed parts manufactured cold.
This specification describes the physical, mechanical and metallurgical requirements for stainless steel wire and rods in coils intended for cold and warm formed mechanical fasteners, which includes bolts, nuts, rivets, screws, washers and special formed parts.
This specification covers a high-expansion steel in the form of bars 1.063 inch (27 mm) and under in nominal diameter or distance between parallel sides.
This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides (thickness).
This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides (thickness).
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, and forging stock.
This specification covers a corrosion-resistant steel in the form of wire.
This specification covers a corrosion- and heat-resistant steel in the form of work-strengthened bars and wire 1-1/4 inches (31.8 mm) and under in nominal diameter or least distance between parallel sides.
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, and flash welded rings up to 5.00 inches (127 mm), inclusive, in nominal diameter or least distance between parallel sides (thickness) and stock for forging, flash welded rings, or heading of any size.
This specification covers a free-machining, corrosion-resistant steel in the form of cold-worked bars and wire up to 1.750 inches (44.45 mm), inclusive, in nominal diameter or least distance between parallel sides (see 8.4 ).
This specification covers a corrosion- and heat-resistant steel in the form of work-strengthened bars and wire, 1-1/4 inches (31.8 mm) and under in nominal diameter or least distance between parallel sides.
This specification covers a corrosion-resistant steel in the form of cold-worked bars and wire up to 1.750 inches (44.45 mm), inclusive, in nominal diameter or least distance between parallel sides.
This specification covers a premium aircraft-quality corrosion and heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, and forging stock.
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
This specification covers a premium aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings.
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings 1.50 inches or less in diameter or least distance between parallel sides (thickness).
This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This SAE Standard covers the mechanical and material requirements for eight property classes of steel, externally threaded metric fasteners in sizes M1.6 through M36, inclusive, and suitable for use in automotive and related applications. Products included are bolts, screws, studs, U-bolts, preassembled screw and washer assemblies (sems), and products manufacturered the same as sems except without washer. Products not covered are tapping screws, thread-rolling screws, and self- drilling screws. Mechanical and material requirements for these products are covered in other SAE documents. The term stud as referred to herein, applies to a cylindrical rod of moderate length, threaded on either one or both ends or throughout its entire length. It does not apply to headed, collared, or similar products which are more closely characterized by requirements shown herein for bolts. For specification purposes, this document treats U-bolts as studs. Thus, wherever the world studs appears, U-bolts is also implied. U-bolts covered by this document are those used primarily in the suspension and related areas of vehicles. (Designers should recognize that the U configuration may not sustant a load equivalent to two bolts or studs of the same size and grade; thus actual load-carrying capacity of U-bolts should be determined by saddle load tests.)
This specification covers a free-machining, low-alloy steel in the form of round bars 3.50 inches (88.9 mm) and under in nominal diameter produced by a die-drawing process.
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock procured in SI (metric) units. AMS 6304 is the inch/pound version of this MAM. These products have been used typically for parts, such as shafts, and fasteners, for service up to 540 degrees C, but usage is not limited to such applications.