Anti-rotation mounting assembly for an aircraft structure

An anti-rotation mounting assembly for an aircraft structure, the anti-rotation mounting assembly comprising:

• a base structural member including a threaded aperture and a dowel aperture, the threaded aperture extending along a mating axis, the dowel aperture disposed radially outward of the threaded aperture;
• a component including a threaded element, the threaded element engaged with the base structural member at the threaded aperture;
• an anti-rotation bracket including a first body portion, a second body portion, and a third body portion, the first body portion including a ring and a dowel, the ring disposed axially between and contacting the base structural member and the component, the ring circumscribing the threaded element, the dowel disposed within the dowel aperture, the second body portion extending between and to the first body portion and the third body portion, the third body portion disposed radially outward of the component;
• and
• a safety cable extending between and to a first cable end and a second cable end, the safety cable engaged with the component at the first cable end, the safety cable engaged with the third body portion at the second cable end.