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Assessing Cleanliness of Hydraulic Fluid Power Components and Systems

CTTC C1, Hydraulic Systems
  • Ground Vehicle Standard
  • J1227_201908
  • Current
Published 2019-08-29 by SAE International in United States

To describe laboratory methods for determining and reporting the contaminant level of the wetted portion of hydraulic fluid power components, parts, subsystems and systems, and of fill fluids. For each type of item, it provides a method of obtaining the liquid sample and the contamination level thereof. It also includes procedures for establishing a sampling plan and guidelines for establishing levels of acceptance, but does not set those levels.

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Superfinishing of HVOF Applied Tungsten Carbide Coatings

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2452
  • Current
Published 2019-07-15 by SAE International in United States
This specification covers requirements for the superfinishing of High Velocity Oxygen/Fuel (HVOF) applied tungsten carbide thermal spray coatings.
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Fluids for Aerospace Hydraulic Systems

  • Professional Development
  • C1966
Published 2019-07-11
This four-hour short course provides an introduction to fluids for aerospace hydraulic systems. Topics covered include an introduction to basics fluid properties, rheology, tribology, and fluid product development. In addition, the history and performance of different classes of fluids are discussed in detail, and specific failure modes such as erosion and sludge formation will be described. Along with an introduction to fluid degradation, information on used oil analysis test methods and interpretation will be provided.By attending this seminar, you will be able to: Describe the general properties and components of a fluidInterpret a fluid specification or reportIdentify key performance advantages and disadvantages for different fluid typesExplain fluid degradation processes1 Day .4 CEUs
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Wire, Electrical, Crosslinked Polyalkene, Crosslinked Alkane-Imide Polymer, or Polyarlyene Insulated, Copper or Copper Alloy

AE-8D Wire and Cable Committee
  • Aerospace Standard
  • AS81044B
  • Current
Published 2019-07-08 by SAE International in United States
AS81044 covers single conductor electric wires made as specified in the applicable detail specification with tin-coated, silver-coated, or nickel-coated copper or copper alloy conductors insulated with crosslinked polyalkene, crosslinked alkane-imide polymer, or polyarylene. The crosslinked polyalkene, crosslinked alkane-imide polymer, or polyarylene may be used alone or in combination with other insulation materials as specified in the detail specification.
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MOUNTING HARDWARE, CUSHION CLAMP, METAL FOR CABLE HARNESS TYING AND SUPPORT, TYPE V, CLASS 1

AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS23190/4D
  • Current
Published 2019-07-03 by SAE International in United States
No Abstract Available.
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New and Newly Retreaded Tire Appearance

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP6307A
  • Current
Published 2019-07-02 by SAE International in United States
This document is for establishing and addressing anomalies on appearance of new and newly retreaded tires prior to installation on aircraft. It is intended to use cosmetics as well as functionality to make a determination of acceptability. However, if cosmetic appearance is not a requirement, use the inspection criteria from ARP6225. This ARP does not supersede (E)TSO-C62 minimum requirements, including marking requirements.
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Ethylene-Propylene-Diene (EPDM) Rubber General Purpose 45 - 55

AMS CE Elastomers Committee
  • Aerospace Material Specification
  • AMS3260D
  • Current
Published 2019-06-17 by SAE International in United States
This specification covers an ethylene propylene (EPDM) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
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Ethylene Propylene Rubber Phosphate Ester Resistant 65 - 75

AMS CE Elastomers Committee
  • Aerospace Material Specification
  • AMS3253B
  • Current
Published 2019-06-17 by SAE International in United States
This specification covers an ethylene propylene elastomer in the form of molded sheet and shapes, color coded purple per ARP1527.
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Gland Design: Nominal 3/8 Inch Cross Section for Compression-Type Seals

A-5B Gears, Struts and Couplings Committee
  • Aerospace Standard
  • AS4832A
  • Current
Published 2019-06-17 by SAE International in United States
This SAE Aerospace Standard (AS) offers gland details for a 0.364 inch (9.246 mm) cross-section gland (nominal 3/8 inch) with proposed gland lengths for compression-type seals with two backup rings over a range of 7 to 21 inches (178 to 533 mm) in diameter. The dash number system used is similar to AS568A. A 600 series has been chosen as a logical extension of AS568A, and the 625 number has been selected for the initial number, since 300 and 400 series in MIL-G-5514 and AS4716 begin with 325 and 425 sizes. Seal configurations and design are not a part of this document. This gland is for use with compression-type seals including, but not limited to, O-rings, T-rings, D-rings, cap seals, etc.
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Heat Resistant Aluminized Paint

AMS G8 Aerospace Organic Coatings Committee
  • Aerospace Material Specification
  • AMS3604A
  • Current
Published 2019-06-11 by SAE International in United States
This specification establishes requirements for a heat resistant aluminized organic coating with sufficient corrosion and erosion resistance for the finished substrate.
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