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Electrical Wiring Fuel Compatibility

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AIR6820
  • Current
Published 2018-12-12 by SAE International in United States

This SAE Aerospace Information Report (AIR) is limited to the subject of compatibility of wiring as part of aircraft Electrical Wiring and Interconnect Systems (EWIS) installed in and around aircraft fuel tanks.

Guidelines for the Use and Installation of Bonded Cable Harness Supports

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • ARP6881
  • Current
Published 2018-10-15 by SAE International in United States
This ARP provides recommended use and installation procedures for bonded cable harness supports.
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CABLE ASSEMBLY, EXTERNAL POWER, AIRCRAFT 115/200 VOLT, 400 HERTZ POWER DISTRIBUTION FLIGHT LINE (FOR A/E 24A-166A)

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AS7974/2A
  • Current
Published 2018-01-18 by SAE International in United States
No Abstract Available.
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EWIS Wiring Insulation Breakdown Testing

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • ARP6216
  • Current
Published 2017-07-24 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) identifies the minimum requirements for the testing of insulated electrical wiring for on-aircraft, aeronautical and aerospace applications. The testing requirements defined herein, ensure that a wire fault can be found safely when using a high potential voltage tester (hipot). This test is intended to aid in finding a breach in the wire insulation, and not for the identification of the resistance of the insulation. The test method defined herein is limited to equipment which ia able to control and limit the DC output to 1500 VDC maximum. This type of wire dielectric tester is typically designed to trip on current leakage and not necessarily on arc detection. This test method is solely designed to identify gross/large wire insulation damage or degradation. For additional related information on this topic and related test methods, refer to the documents cited in Section 2. They are intended to aid the reader in the direction of this ARP and to provide more indepth information on wire and component insulation testing.
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CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT, SINGLE-JACKETED 270 VDC, 90 KW

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AS7974/5A
  • Current
Published 2017-07-07 by SAE International in United States
No Abstract Available.
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CABLE AND PLUG ASSEMBLY, EXTERNAL POWER 115/200 VOLTS 3 PHASE, SINGLE POINT REFUELING

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AS24208A
  • Current
Published 2017-04-11 by SAE International in United States
No Abstract Available.
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Hot Stamp Wire Marking Concerns for Aerospace Vehicle Applications

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AIR5575A
  • Current
Published 2017-01-24 by SAE International in United States
This SAE Aerospace Information Report (AIR) discusses the often overlooked relationship between hot stamp marking and the environmental conditions that contribute aircraft wiring problems and discusses current beliefs of military service experts, regulatory agencies and industry standard writing bodies about the potential hazards imposed by the hot stamping process.
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Guidelines for Wire Identification Marking Using the Hot Stamp Process

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • ARP5369B
  • Current
Published 2016-12-01 by SAE International in United States
These guidelines have been written to provide process information regarding the hot stamp method of marking wire identification directly on aerospace wires and cables.
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CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT 28 VOLT DC, OPERATING POWER

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AS90347A
  • Current
Published 2016-11-12 by SAE International in United States
No Abstract Available.
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CONDUIT ASSEMBLY, FLEXIBLE, RADIO FREQUENCY SHIELDING

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • AS25067A
  • Current
Published 2016-11-11 by SAE International in United States
No Abstract Available.
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