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Viewing 36781 to 36810 of 43606
1969-11-01
Standard
AMS6432
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1969-11-01
Standard
AMS4228
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of April 1996. Alloy: A201.0-T6 UNS Number: A12010
1969-11-01
Standard
AMS4128
This specification covers an aluminum alloy in the form of bars and rods 0.500 inch (12.50 mm) and over in nominal diameter or least difference between parallel sides.
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.
1969-11-01
Standard
AMS5632C
This specification covers two types of corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
1969-11-01
Standard
AMS5671B
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging and flash welded rings. These products have been used typically for parts requiring high strength at temperatures in the range 800 1100 degrees F (427 to 593 degrees C), particularly those which are formed or welded, but usage is not limited to such applications.
1969-11-01
Standard
AMS4926C
This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock for flash welded rings.
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.
1969-11-01
Standard
AMS5338A
This specification covers a low-alloy steel in the form of investment castings. These castings have been used typically for small structural parts of intricate design requiring heat treatment to minimum tensile strengths up to 175 ksi (1207 MPa), but usage is not limited to such applications.
1969-11-01
Standard
AIR1077
This report is intended for use by those people involved in the design and application of high temperature hydraulic systems and components. It is, in essence, a first attempt at the standardization of seal ring, groove, and gland design for hydraulic piston heads. Specifically, the report covers some design, application, and test aspects of metallic seal rings for reciprocating hydraulic service at -65 F to +630 F fluid or ambient temperature and up to 4000 psi for cylinder diameters ranging from 1/2 inch to 6 inches. An attempt has been made to consider all features of seal ring design including configuration, materials, hardness, dimensions, surface finishes, surface treatment, leak treatment, leak testing, and general quality. In addition to this, allowable cylinder breathing and general quality requirements of mating hardware are discussed. Also, at the end of this report, there is a brief paragraph on other types of seal rings.
1969-11-01
Standard
AMS4930A
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
1969-11-01
Standard
AMS5824
This specification covers a corrosion-resistant steel in the form of welding wire.
1969-11-01
Standard
AMS5580E
This specification covers a corrosion and heat-resistant nickel alloy in the form of seamless tubing.
1969-11-01
Standard
AMS4070G
This specification covers an aluminum alloy in the form of drawn, round seamless tubing. This tubing has been used typically for parts, such as brackets, conduits, and low-pressure fluid lines, requiring good weldability, moderate strength, and good resistance to corrosion, but usage is not limited to such applications.
1969-11-01
Standard
AMS5355B
This specification covers a corrosion resistant steel in the form of investment castings. These castings have been used typically for parts requiring good corrosion resistance and strength up to 600 °F (316 °C), but usage is not limited to such applications (See 8.3). Certain processing procedures and service conditions may cause these castings to become subject to stress-corrosion cracking; ARP1110 recommends practices to minimize such conditions. Where stress-corrosion is considered to be a factor, precipitation heat treatment should be performed at a temperature not lower than 1000 °F (538 °C).
1969-11-01
Standard
AMS5336A
This specification covers a low-alloy steel in the form of investment castings. These castings have been used typically for small structural parts of intricate design requiring heat treatment to minimum tensile strengths up to 150 ksi (1034 MPa), but usage is not limited to such applications.
1969-11-01
Standard
AMS4906A
This specification has been Cancelled by the Aerospace Materials Division, SAE, as of August 1994.
1969-11-01
Standard
AMS4096
This specification covers an aluminum alloy in the form of sheet and plate clad on two sides.
1969-11-01
Standard
AMS4229
This specification covers an aluminum alloy in the form of sand, permanent mold, and composite mold castings.
1969-11-01
Standard
AMS4965A
This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock for forging and flash welded rings.
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.
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.
1969-11-01
Standard
AMS7498D
This specification covers flash welded rings made of titanium and selected titanium alloys.
1969-11-01
Standard
AMS5731D
This specification covers a corrosion and heat resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts, such as flanges, cases, and fasteners, requiring moderate strength up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1500 degrees F (816 degrees C), particularly those which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.