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Standard
2013-09-10
This SAE Aerospace Standard (AS) presents all appropriate boss dimensions from .125 inch to 2.0 inch tube sizes.
Book
2013-09-05
Ian K. Jennions
The third volume in the Integrated Vehicle Health Management (IVHM) series focuses on the technology that actually supports the implementation of IVHM in real-life situations. Edited by Ian K. Jennions, Director of the IVHM Center at Cranfield University, UK, this book was written collaboratively by twenty-seven authors from industry, academia and governmental research agencies. Topics include: -Sensors, instrumentation and signal processing -Fault detection and diagnostics -Prognostics and metrics -Architecture -Data Management -Vehicle level reasoning systems -System's design -Applications and disruptive technologies Integrated Vehicle Heath Management: The Technology follows two bestsellers, also published by SAE International, which cover the fundamentals aspects of this new body of knowledge (Integrated Vehicle Health Management: Perspectives on an Emerging Field), and the business justification needed so that investments in the technology make sense (Integrated Vehicle Health Management: Business Case Theory and Practice).
WIP Standard
2013-09-05
This SAE AIR provides a description of a reference method for viscosity tests of thickened (AMS 1428) anti-icing fluids.
WIP Standard
2013-09-04
This specification covers a carbon soil and paint remover compound in the form of a liquid. Primarily for removal of carbonaceous soils and paint from aircraft turbine engine parts by immersing the parts in liquid at room temperature.
WIP Standard
2013-09-04
This specification covers a strongly alkaline scale conditioner in the form of a liquid or a water-soluble powder. This product has been used typically in conditioning heat scale formed on aircraft turbine engine high-temperature alloy part by immersion in a solution of the compound at elevated temperature, but usage is not limited to such applications. These compounds are unsuitable for cleaning aluminum parts.
WIP Standard
2013-09-04
This specification covers an alkaline permanganate oxide conditioner in the form of a water-soluble powder or a liquid for dilution with water. This product has been used typically for conditioning of oxidation products on aircraft turbine engine components fabricated from steels, nickel alloys, and cobalt alloys by immersion in a solution of the cleaner at elevated temperature, but usage is not limited to such applications.
WIP Standard
2013-09-04
This specification covers an inhibited phosphoric acid in the form of a liquid concentrate or a water soluble powder for dilution with water. Primarily for derusting of aircraft turbine engine ferrous components and removal of heat scale and other contamination from the surface of nickel alloys by immersion at room temperature. Should not be used on steel parts having hardness of 40 HRC or over.
Standard
2013-09-03
This SAE Aerospace Information Report (AIR) developed by a broad cross section of personnel from the aviation industry and government agencies is offered to provide state-of-the-art information for the use of individuals and organizations designing new or upgraded turboshaft engine test facilities.
Standard
2013-08-29
This SAE Aerospace Recommended Practice (ARP) provides guidelines for the format and content of documents defining the interface between electronic propulsion control systems and aircraft systems. The scope includes civilian aircraft powered by turbofan, turboprop, and turboshaft engines equipped with electronic engine controls.
WIP Standard
2013-08-23
This Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries, and to protect the aircraft from corrosion created by waste spill. The ULD is designed to accommodate one horse or several.
Standard
2013-08-21
This standard covers self-propelled off-road work machines as categorized in SAE J1116 and Agricultural Tractors as defined in ANSI/ASAE S390.
Standard
2013-08-12
This SAE Aerospace Information Report (AIR) provides descriptions of test methods for determining if an aircraft surface coating of any thickness has adverse effects on aircraft deicing/anti-icing fluids with respect to fluid holdover time performance and aerodynamic performance. Although not the primary mandate of the G-12 Aircraft Ground Deicing Committee, this document also provides descriptions of suggested test methods for evaluating aircraft surface coatings with respect to durability, hardness, weathering, aerodynamic drag, ice adhesion, ice accumulation, contact angle, and thermal conductivity. These additional tests can provide informational data for characterizing the coatings and may be useful to operators when evaluating the coatings.
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