Abstract: An aircraft interior bushing assembly is disclosed comprising interoperating bushings, each bushing comprising a recessing portion, a radially inner surface operably configured to contact a surface defining a void in a panel, a perimeter portion wherein the perimeter portion is substantially larger than the recessing portion, a support arm receiver, and a support arm coupled to each bushing. Each support arm comprises a first end coupled to the bushing, and a second end comprising a conduit receiver. In one form, the bushing assembly is operably configured to support a conduit at a distance from the radially inner surface of the interoperating bushings to substantially prohibit contact between the conduit and the bushing assembly once the conduit is installed and fixed to the conduit receiver.

Abstract: An aircraft interior bushing assembly is herein disclosed comprising a pair of interoperating bushings, each bushing comprising a recessing portion, a radially inner surface operably configured to contact a surface defining a void in a panel, a perimeter portion wherein the radial dimension of the perimeter portion is substantially larger than the recessing portion, a support arm receiver, and a support arm removably coupled to each bushing. Each support arm comprises a first end coupled to the bushing, a second end comprising a conduit receiver, a clamp receiver, and at least one connector portion provided on the first end of the support arm operatively configured to removably engage the support arm receiver. In one form, the bushing assembly is operably configured to support a conduit at a distance from the radially inner surface of the interoperating bushings to substantially prohibit contact between the conduit and the bushing assembly once the conduit is installed and fixed to the conduit receiver.