Repair of gas turbine blade tip without recoating the repaired blade tip

A method for repairing a damaged gas turbine blade, comprising the steps of

• furnishing the damaged gas turbine blade made of a base metal and which has previously been in service;
• removing any damaged material from a damaged blade tip of the damaged gas turbine blade;
• and
• weld repairing the damaged blade tip with a repair alloy having a nominal composition, in weight percent, of from about 7.4 to about 7.8 percent chromium, from about 5.3 to about 5.6 percent tantalum, from about 2.9 to about 3.3 percent cobalt, from about 7.6 to about 8.0 percent aluminum, from about 0.12 to about 0.18 percent hafnium, from about 0.5 to about 0.6 percent silicon, from about 3.7 to about 4.0 percent tungsten, from about 1.5 to about 1.8 percent rhenium, from about 0.01 to about 0.03 percent carbon, from about 0.01 to about 0.02 percent boron, balance nickel to form a tip-repaired gas turbine blade having a repaired blade tip, wherein the repair alloy has a composition different from the base metal, and wherein the method does not include any step of coating a lateral surface of the repaired blade tip with a non-ceramic coating after the step of weld repairing.