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2017-04-19
WIP Standard
AMS2672H
This specification covers the requirements for producing brazed joints on aluminum and alumiinum alloys by torch or furnace brazing.
2017-04-19
WIP Standard
ARP1341C
This document provides a recommended practice for determining decarburization and carburization in heat treated carbon and low-alloy steel parts other than case hardened parts. It is not applicable to raw materials.
2017-04-19
WIP Standard
ARP4992C
This SAE Aerospace Recommended Practice (ARP) describes a method for classifying the frequencies of analysis of solutions used in the processing of metals, such as electroplating, anodizing, and conversion coating and associated processes but usage is not limited to such applications.
2017-04-19
WIP Standard
AMS2487B
This specification describes the engineering requirements for producing an electrically-insulating, non-powdery anodic coating on titanium and titanium alloys and the properties of such coatings.
2017-04-18
Article
The MX-Z series of laser markers from Omron provide high quality, permanent identification with what the company claims is superior flexibility in terms of marking and connectivity with the ability to integrate easily to other systems or controls.
CURRENT
2017-04-18
Standard
AMS4285F
This specification covers an aluminum alloy in the form of centrifugal castings.
CURRENT
2017-04-18
Standard
AMS5389D
This specification covers a corrosion and heat resistant nickel alloy in the form of sand castings.
CURRENT
2017-04-18
Standard
AMS4779J
This specification 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.
2017-04-17
Article
Audi reveals details of the structural technology of its upcoming A8 as Audi and Porsche Chairmen pledge closer co-operation.
CURRENT
2017-04-17
Standard
AMS5549H
This specification covers a corrosion and moderate heat resistant steel in the form of plate.
2017-04-14
Article
Boeing 787 Dreamliner will be first commercial airplane to fly with FAA-certified, additive-manufactured titanium structural components.
CURRENT
2017-04-14
Standard
AMS2451/5B
This specification covers the requirements for brush plating of hard chromium by electrodeposition.
2017-04-14
WIP Standard
AMS6408E
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.

These products have been used typically for hotwork tooling or for parts requiring a steel capable of through-hardening to a minimum hardness of 50 HRC in section thicknesses up to 12 inches (305 mm) with relatively high levels of strength, fatigue resistance, ductility, and thermal stability for use in service from -100 to +1000 °F (-73 to 538 °C) and where such parts may require welding, but usage is not limited to such applications.

2017-04-14
WIP Standard
AMS6539A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2017-04-14
WIP Standard
AMS6547A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2017-04-14
WIP Standard
AMS6549A
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2017-04-14
WIP Standard
AMS6548A
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2017-04-14
WIP Standard
AMS6516B
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
2017-04-14
WIP Standard
AMS6527F
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
2017-04-14
WIP Standard
AMS6559A
This specification covers a premium aircraft-quality, high-alloy tool steel in the form of bars, wire, forgings, and forging stock. These products have been used typically for critical parts, such as bearings operating under heavy loads and high speeds at moderate temperatures and subject to very rigid inspection standards, but usage is not limited to such applications.
2017-04-14
WIP Standard
AMS6558A
This specification covers a premium aircraft-quality, high-alloy steel in the form of bars, wire, forgings, and forging stock. These products have been used typically for critical parts, such as bearings operating under heavy loads and high speeds at moderate temperatures and subject to very rigid inspection standards, but usage is not limited to such applications.
2017-04-14
WIP Standard
AMS6560A
This specification covers a premium aircraft-quality, high-alloy steel in the form of bars, wire, forgings, and forging stock.
2017-04-14
WIP Standard
AMS6551A
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2017-04-14
WIP Standard
AMS6557A
This specification covers a premium aircraft-quality, high-alloy tool steel in the form of bars, wire, forgings, and forging stock. These products have been used typically for critical parts, such as bearings operating under heavy loads and high speeds at moderate temperatures and subject to very rigid inspection standards, but usage is not limited to such applications.
2017-04-14
WIP Standard
AMS6556A
This specification covers a premium aircraft-quality, high-alloy steel in the form of bars, wire, forgings, and forging stock. These products have been used typically for critical parts, such as bearings operating under heavy loads and high speeds at moderate temperatures and subject to very rigid inspection standards, but usage is not limited to such applications.
CURRENT
2017-04-14
Standard
AMS2451/1B
This specification establishes the requirements for a general-purpose brush plating of nickel applied by electrodeposition.
2017-04-14
WIP Standard
AMS6411J
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts requiring high tensile strength and good ductility with relatively high impact strength, superior transverse properties, and hardness, but usage is not limited to these applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment. ARP1110 recommends practices to minimize such conditions.
2017-04-14
WIP Standard
AS1182D
The purpose of this document is to provide the aerospace industry with standards for minimum stock removal allowances for bars and mechanical tubing to provide surfaces which are free from decarburization, seams, laps, tears, cracks, pits, and other injurious surface imperfections.
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