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Marking of Electrical Insulating Materials

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AS5942
  • Current
Published 2019-12-27 by SAE International in United States
This specification establishes the performance requirements for the identification of wire and cable by indirect markings that have been applied to electrical insulating materials including heat shrink sleeving, wrap around labels and “tie-on” tags as well as any other types of materials used for indirect marking. This specification covers the processes used to mark these materials, including impact ink marking, thermal transfer, hot stamp, and lasers, etc. This specification does not cover the direct marking on insulated electrical wires and cables.
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CRIMPING TOOLS, TERMINAL, HAND OR POWER ACTUATED, WIRE TERMINATION, ACCESSORY HARDWARE FOR AS22520/28 AND AS22520/29 TOOLS

AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS22520/30
  • Current
Published 2019-12-27 by SAE International in United States
No Abstract Available.
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Mitigating Wire Insulation Damage During Processing and Handling

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AIR5717
  • Current
Published 2019-12-27 by SAE International in United States
Wire and cable products progress through a series of handling or operational steps from the time they leave the manufacturer, and until a finished harness or assembly is ready for installation on a vehicle. Throughout these many steps, environmental or processing conditions may be present which can generate damage detrimental to the wire or cable and/or its intended application.
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Titanium Alloy Sheet 6Al - 4V Driver Sheet

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4932D
  • Current
Published 2019-12-27 by SAE International in United States
This specification covers a titanium alloy in the form of sheet.
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WASHER, FLAT, COUNTERSUNK CORROSION AND HEAT RESISTANT STEEL (UNS S66286)

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS9768
  • Current
Published 2019-12-27 by SAE International in United States
No Abstract Available.
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BOLT, SPLINE DRIVE, EXTENDED WASHER, REDUCED SHANK, AMS5662 (UNS N07718) 1275 MPa UTS, METRIC

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • MA4147A
  • Current
Published 2019-12-27 by SAE International in United States
No Abstract Available.
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Qualified Hoses for Marine Applications

Hydraulic Hose and Hose Fittings Committee
  • Ground Vehicle Standard
  • J1942/1_201912
  • Current
Published 2019-12-27 by SAE International in United States
The following list consists of hose data provided as of December, 2019, and is for convenience in determining acceptability of nonmetallic flexible hose assemblies intended for usage under 46 CFR 56.60-25. Where the maximum allowable working pressure (MAWP) or type of fitting is not specified, use the manufacturer's recommended MAWP or type of fitting. This list has been compiled by SAE staff from information provided by the manufacturers whose product listings appear in this document. Manufacturers wishing to list their products in this document shall: a Successfully test their hose to the requirements of SAE J1942, Table 1. b Submit a letter of certification to the SAE J1942 test requirements for each specific type of hose tested (see sample table, Table 1) along with the test results. All sizes should be included in the same letter which must also include all of the information necessary to make a SAE J1942-1 listing. c The SAE will review the letter and may, at their discretion, request to see further test results. A copy of the submittal letter…
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Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7651) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4204D
  • Current
Published 2019-12-27 by SAE International in United States
This specification covers an aluminum alloy in the form of plate 0.250 to 5.500 inch (6.35 to 139.70 mm), inclusive in nominal thickness (see 8.5).
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PIN, STRAIGHT, HEADLESS, DOWEL - CORROSION AND HEAT RESISTANT STEEL (UNS S66286), STANDARD AND OVERSIZE

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS9390D
  • Current
Published 2019-12-27 by SAE International in United States
No Abstract Available.
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FITTING, TEE, SWIVEL NUT TO MALE FLARELESS ON RUN, EXTERNAL SWAGE ON SIDE

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
  • Aerospace Standard
  • AS6494
  • Current
Published 2019-12-26 by SAE International in United States
No Abstract Available.
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