Turbine component and a process of fabricating a turbine component

A process of fabricating a component, the component being a fuel tip nozzle, combustion cap assembly or transition component, comprising:

• excavating a base metal of the component to form a fill region, the fill region surrounding a combustion zone and extending in a plurality of directions along a surface of the component to surround one or more diffusers;
• and
• filling the fill region with a filler metal;
• wherein the filler metal has a filler metal elongation that is at least 25% greater than a base metal elongation of the base metal;
• wherein the filler has a composition, by weight, of about 0.005% C, 0.150% Mn, about 0.005% P, about 0.002% S, about 0.03% Si, about 15.50% Cr, about 16.0% Mo, about 3.50% W, about 0.15% V, about 0.10% Co, about 6.00% Fe, incidental impurities, and a balance of Ni.