A nacelle drag-link assembly for a thrust reverser of a propulsion system, the nacelle drag-link assembly comprising: a drag-link fitting comprising a base region and a coupling socket extending from the base region, the coupling socket having a first coupling aperture and a second coupling aperture; a drag link comprising an inner structure end, an outer structure end, and a link body formed between the inner structure end and the outer structure end, wherein an inner width of the coupling socket is greater than an outer width of the inner structure end of the drag link, and the outer structure end comprises a pivot area to link with a blocker door of the thrust reverser; a coupling assembly installed through an aperture of the inner structure end and between the first coupling aperture and the second coupling aperture of the coupling socket; and a vibration damping assembly installed in contact with the drag-link fitting and one or more of: the drag link and the coupling assembly; characterized in that the nacelle drag-link assembly further comprises: a first flanged bushing installed within the first coupling aperture; a second flanged bushing installed within the second coupling aperture; a third flanged bushing installed within the aperture of the inner structure end; and a fourth flanged bushing installed within the aperture of the inner structure end, wherein the coupling assembly passes through the first, second, third, and fourth flanged bushings (202, 204, 206, 208). a drag-link fitting comprising a base region and a coupling socket extending from the base region, the coupling socket having a first coupling aperture and a second coupling aperture; a drag link comprising an inner structure end, an outer structure end, and a link body formed between the inner structure end and the outer structure end, wherein an inner width of the coupling socket is greater than an outer width of the inner structure end of the drag link, and the outer structure end comprises a pivot area to link with a blocker door of the thrust reverser; a coupling assembly installed through an aperture of the inner structure end and between the first coupling aperture and the second coupling aperture of the coupling socket; and a vibration damping assembly installed in contact with the drag-link fitting and one or more of: the drag link and the coupling assembly; characterized in that the nacelle drag-link assembly further comprises: a first flanged bushing installed within the first coupling aperture; a second flanged bushing installed within the second coupling aperture; a third flanged bushing installed within the aperture of the inner structure end; and a fourth flanged bushing installed within the aperture of the inner structure end, wherein the coupling assembly passes through the first, second, third, and fourth flanged bushings (202, 204, 206, 208). a first flanged bushing installed within the first coupling aperture; a second flanged bushing installed within the second coupling aperture; a third flanged bushing installed within the aperture of the inner structure end; and a fourth flanged bushing installed within the aperture of the inner structure end, wherein the coupling assembly passes through the first, second, third, and fourth flanged bushings (202, 204, 206, 208).