Abstract: The present invention relates to a hybrid cure mechanism developed to polymerize highly filled/loaded, optically opaque, acrylate polymeric material compositions by radiant energy. The hybrid cure mechanism, when incorporated into a resinous composition, can be utilized to repair surface coatings on high performance aircraft where an extended composition pot life or application life and rapid cure capability combined with an acceptable shelf life stability are required. More specifically, the present invention relates to an electrically conductive resinous paint or gap filler for a suitably prepared composite or metallic surface. The composition also has applications on a production line of high performance aircraft.