A method for repairing a turbomachine component (C), the method comprising the steps of: - setting up a laser cladding machine; - preparing at least a portion of a turbomachine component to be repaired by removing a damaged volume of said component; - rotating one of said laser cladding machine and turbomachine component with respect to the other of said laser cladding machine and turbomachine component; - rebuilding said damaged volume by laser cladding in order to obtain a rebuilt volume in said component; - applying a heat treatment to at least said rebuilt volume of said turbomachine component; - finishing a surface of said rebuilt volume; - non-destructively testing said rebuilt volume; characterized in that the step of setting up the laser cladding machine includes the sub-steps of: - identifying a set of inter-correlated laser cladding process parameters and tuning the parameters depending on the type and geometry of the component to the repaired; - identifying a sample; - welding a first layer on said sample by said laser cladding machine after imposing said set of laser cladding process parameters; - comparing a plurality of geometric data of the first layer with a respective plurality of reference data ranges; - if the plurality of geometric data are outside the respective plurality of reference data ranges, modifying the set of inter-correlated laser cladding process parameters and repeating the third and fourth sub-steps of the setting up step ; - if said plurality of geometric data are within said plurality of reference data ranges, welding a plurality of further layers on said sample by said laser cladding machine; and - testing said plurality of further layers by micrographic inspection for defining the parameters to operate said rebuilding phase. - setting up a laser cladding machine; - preparing at least a portion of a turbomachine component to be repaired by removing a damaged volume of said component; - rotating one of said laser cladding machine and turbomachine component with respect to the other of said laser cladding machine and turbomachine component; - rebuilding said damaged volume by laser cladding in order to obtain a rebuilt volume in said component; - applying a heat treatment to at least said rebuilt volume of said turbomachine component; - finishing a surface of said rebuilt volume; - non-destructively testing said rebuilt volume; - identifying a set of inter-correlated laser cladding process parameters and tuning the parameters depending on the type and geometry of the component to the repaired; - identifying a sample; - welding a first layer on said sample by said laser cladding machine after imposing said set of laser cladding process parameters; - comparing a plurality of geometric data of the first layer with a respective plurality of reference data ranges; - if the plurality of geometric data are outside the respective plurality of reference data ranges, modifying the set of inter-correlated laser cladding process parameters and repeating the third and fourth sub-steps of the setting up step ; - if said plurality of geometric data are within said plurality of reference data ranges, welding a plurality of further layers on said sample by said laser cladding machine; and - testing said plurality of further layers by micrographic inspection for defining the parameters to operate said rebuilding phase. <EOS>