Tag Archives: SAE

SAE AMS4782G

Nickel Alloy, Brazing Filler Metal 71Ni – 10Si – 19Cr 1975 DEGREES F (1080 DEGREES C) Solidus, 2075 DEGREES F (1135 DEGREES C) Liquidus

Published by: 2017-03-28 / 2017-03-28 / 5 pages
SAE AMS4782G covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder.

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SAE J2762_201703

Method for Removal of Refrigerant from Mobile Air Conditioning System to Quantify Charge Amount

Published by: 2017-03-10 / 2017-03-10 / 9 pages

This Standard provides an overview of results and requirements needed to remove refrigerant from a mobile air conditioning system for determining refrigerant emissions (leakage).

This reclaim procedure for use on fleet vehicles in a field service environment should produce an accuracy and repeatability sufficient to determine refrigerant loss within 2 g.

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SAE AS47643

Verification Methods for MIL-STD-1760E Aircraft Station Interfaces

Published by: 2017-03-30 / 2017-03-30 / 190 pages
SAE AS47643 establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760 Revision E.

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SAE ARP4162B

Balancing Machine Proving Rotors

Published by: 2017-03-17 / 2017-03-17 / 10 pages
SAE ARP4162B specifies a series of balancing machine proving rotors and related test weights as directly required for the evaluation of gas turbine rotor balancing machines.

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SAE AMS03_4A

The Pre-Treatment and Protection of Steel Items of Specified Maximum Tensile Strength Exceeding 1450 MPa (Stabilized: Mar 2017)

Published by: 2017-03-21 / 2017-03-21 / 19 pages
SAE AMS03_4A specifies the special treatments and precautions that are to be observed when protective and other surface treatments are applied to items, including springs, made from steel of specified maximum tensile strength exceeding 1450 MPa. The requirements of this Standard qualify those in process specifications and override the latter where there is conflict. The Standard also gives advice on design, manufacture, and preparation of items prior to cleaning and protection.

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SAE AMS4939C

Titanium Alloy Sheet, Strip, and Plate 3Al – 8V – 6Cr – 4Mo – 4Zr Solution Heat Treated

Published by: 2017-03-28 / 2017-03-28 / 8 pages
SAE AMS4939C covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.60 mm) nominal thickness.

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SAE AS15531A

Digital Time Division Command/Response Multiplex Data Bus (Stabilized: Mar 2017)

Published by: 2017-03-21 / 2017-03-21 / 49 pages
SAE AS15531A contains requirements for a digital time division command/response, multiplex data bus, for use in systems integration, that is functionally equivalent to MIL-STD-1553B with Notice 2. Even with the use of this document, differences may exist between multipex data buses in different system applications due to particular application requirements and the options allowed in this document. The system designer must recognize this fact and design the multiplex bus controller (BC) hardware and software to accommodate such differences. These designer selected options must exist to allow the necessary flexibility in the design of specific multiplex systems in order to provide for the control mechanism, architectural redundancy, degradation concept, and traffic patterns peculiar to the specific application requirements.

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