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Viewing 164041 to 164070 of 188746
HISTORICAL
1972-11-01
Standard
AMS4051D
This specification covers an aluminum alloy in the form of sheet and plate.
HISTORICAL
1972-11-01
Standard
AMS3826
This specification covers one style of glass cloth impregnated with a polyester resin system, the resin being processed to a "B" stage condition.
HISTORICAL
1972-11-01
Standard
J496_197211
Table 3, Practical Length Increments and Ranges, indicates spring pin sizes. Information on availability of individual lengths in the various types, weights, and materials may be obtained from suppliers. The tolerance on length for coiled type spring pins shall be plus or minus 0.010 in. for sizes up to and including 5/16 in.; and plus or minus 0.015 in. for sizes larger than 5/16 in.
HISTORICAL
1972-11-01
Standard
AMS5020A
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008. 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 ".
HISTORICAL
1972-11-01
Standard
J88_197211
This SAE Standard sets forth the instrumentation and procedure to be used in measuring the exterior sound levels for self-propelled sweepers as defined in SAE J2130 and self-propelled off-road work machines in categories 1,2,4, and 5 of SAE J1116. This document does not address the operation of safety devices such as backup alarms, horns, or accessories. The sound levels obtained by using the test procedures set forth in this document are repeatable and are representative of the higher range of sound levels generated by machines under actual field operating conditions. Due to variability of field operating conditions, this data is not intended to be used for construction site boundary noise evaluations.
HISTORICAL
1972-11-01
Standard
AMS5031B
This specification covers a low-carbon steel in the form of covered welding electrodes.
HISTORICAL
1972-11-01
Standard
AMS5556C
This specification covers a corrosion and heat resistant steel in the form of seamless or welded and drawn tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when such parts are welded during fabrication, but usage is not limited to such applications. The alloy provides oxidation resistance up to 1500 degrees F (816 degrees C) but is useful at that temperature only when stresses are low.
HISTORICAL
1972-11-01
Standard
AMS5559B
This specification covers a corrosion and heat-resistant steel in the form of welded tubing.
HISTORICAL
1972-11-01
Standard
AMS3892/2
This specification covers one type of graphite fiber in the form of tow.
HISTORICAL
1972-11-01
Standard
AMS3892/3
This specification covers one type of graphite fiber in the form of tow.
HISTORICAL
1972-11-01
Standard
AMS3894
This specification and its supplementary detail specifications cover tape and sheet fabricated using carbon fibers impregnated with epoxy resin.
HISTORICAL
1972-11-01
Standard
AMS3892/1
This specification covers one type of graphite fiber in the form of tow.
HISTORICAL
1972-11-01
Standard
AMS7454F
1. SCOPE: 1.1 Type: This specification covers high quality holts and screws made of a low-alloy, heat resistant steel. 1. 2 Application: Primarily for joining parts where high strength up to 900'F (480'C) is reqnired.
HISTORICAL
1972-11-01
Standard
J551A_197211
This SAE Standard covers the measurement of broadband electromagnetic radiation over the frequency range of 30 to 1000 MHz from a vehicle or other device powered by an internal combustion engine or electric motor. Operation of all engines (main and auxiliary) of a vehicle or device is included. All equipment normally operating when the engine is running is also included except operator-controlled equipment, which is excluded. The recommended level applies only to complete vehicles or devices in their final manufactured form. Vehicle mounted rectifiers used for battery charging in electric vehicles are included in this document when operated in their charging mode.
HISTORICAL
1972-11-01
Standard
AMS5331C
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of September 1996. It is recommended, therefore, that this specification not be specified for new designs. This specification covers a low-alloy steel in the form of sand castings. Primarily for cast parts requiring heat treatment to minimum yield strengths up to 180,000 psi (1240 MPa).
HISTORICAL
1972-11-01
Standard
AMS5024E
This specification covers a free-cutting carbon steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1972-11-01
Standard
AMS7301C
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
HISTORICAL
1972-11-01
Standard
AMS7240C
This specification covers plain helical lock washers fabricated from heat treated carbon steel.
HISTORICAL
1972-11-01
Standard
AMS7273A
This specification covers a fluorosilicone (FVMQ) rubber in the form of molded rings.
HISTORICAL
1972-11-01
Standard
AMS3824
This specification covers "E" glass in the form of woven cloth. This cloth has been used typically as a reinforcing materials for structural plastic laminates and is supplied with finishes suitable for use with various resin matrices, but usage is not limited to such applications.
HISTORICAL
1972-11-01
Standard
AIR1228
This SAE Aerospace Information Report (AIR) establishes the part numbers and/or description of the critical components and operational guidelines for the standard hydraulic impulse machine for testing hydraulic hose assemblies, tubing, coils, and fittings and may be used for similar fluid system components, if desired. The standard impulse machine is established for the following purposes: As referee in the event of conflicting data from two or more nonstandard impulse machines. Such a referee machine might be built by an impartial testing activity. A design guide for future machines being built by manufacturers and users, or the upgrading of present machines. A design guide for higher pressure machines or special purpose machines being designed. It is not the intention of this document to obsolete present machines.
HISTORICAL
1972-11-01
Standard
AMS2664B
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.
HISTORICAL
1972-11-01
Standard
AMS2669B
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of October, 1991.
HISTORICAL
1972-11-01
Standard
AMS5565E
This specification covers a corrosion-resistant steel in the form of welded tubing. This tubing has been used typically for parts, such as fluid-conducting lines not subjected to high pressure, requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 degrees F (427 degrees C) during fabrication may impair corrosion resistance.
HISTORICAL
1972-11-01
Standard
AMS2350V
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.
HISTORICAL
1972-11-01
Standard
AMS4135K
This specification covers an aluminum-base alloy in the form of die forgings, hand forgings, rolled rings, and stock for forging or rolled rings.
HISTORICAL
1972-11-01
Standard
AMS5759E
This specification covers a corrosion and heat-resistant cobalt alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts requiring high strength up to 1500 °F (816 °C) and oxidation resistance up to 2000 °F (1093 °C), but usage is not limited to such applications.
HISTORICAL
1972-11-01
Standard
J306A_197211
This SAE Standard defines the limits for a classification of automotive gear lubricants in rheological terms only. Other lubricant characteristics are not considered.
HISTORICAL
1972-11-01
Standard
AMS5668E
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts, such as bolts, turbine blades, and turbine seals, requiring oxidation resistance and high strength at 1250 to 1500 degrees F (675 to 816 degrees C), but usage is not limited to such applications.

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