Electrical shielding termination systems

An aircraft electrical system, comprising:

• a conductor having a shielding, the shielding comprising a shielding termination;
• and
• a conductor shielding termination assembly, comprising:
• a housing tube defining an inner diameter housing channel therethrough, wherein the housing tube is made of conductive material;
• a shoulder bushing configured to insert within the inner diameter housing channel of the housing tube, the shoulder bushing defining an inner diameter bushing channel sized to receive an unshielded portion of the conductor;
• and
• a clamping assembly configured to clamp around the housing tube and/or the conductor to axially lock the housing tube and the conductor and to trap a shielding termination between the housing tube and the clamping assembly, wherein the clamping assembly forms a clamping inner diameter channel sized to receive a shielded portion of the conductor.