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CURRENT
2017-11-15
Standard
AS6324
AS6324 specifies the requirements for comparative testing of new copper and copper alloy conductors to AS29606 qualified conductors. AS29606 approved conductors are used for the construction of insulated wire defined in SAE Aerospace wire standards (i.e., AS22759, AS81044, etc.). AS6324 defines testing which meets or exceeds the minimum test requirements of AS29606 and AS22759 and its detailed specification sheets.
2017-10-13
WIP Standard
AS7510A
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system.
CURRENT
2017-10-04
Standard
AMS03_9A
This SAE Standard specifies the requirements for the electro-deposition of silver on ferrous-base, copper-base, aluminum-base, zinc-base and nickel base materials. It is primarily intended for use on electrical and electronic items which are to be plated with silver to increase the electrical conductivity of the surface.
CURRENT
2017-09-11
Standard
AS7510
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system. FAR 23.954, FAR 25.901, FAR 25.954 and FAR 25.981 certification requirements have identified the need for high current capable flexible fluid assembled couplings. The coupling assembly does not require inspection and maintenance to remain current capable for the life of the aircraft.
CURRENT
2017-07-13
Standard
AMS3681E
This specification covers an electrically-conductive adhesive supplied as two components, a silver-filled, epoxy-base adhesive and a separate curing agent which may be paste or liquid.
CURRENT
2017-02-23
Standard
AMS3266A
This specification covers two types of electrically conductive, elastomeric polythioether sealing compounds that cure at room temperature. The sealing compound is supplied as either a two-component system or as premixed and frozen.
CURRENT
2016-03-28
Standard
AMS2658D
This specification establishes hardness and electrical conductivity acceptance criteria of finished or semi-finished parts of wrought aluminum alloys.
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