A method for repairing a turbomachine component (C), the method comprising the steps of: setting up a laser cladding machine including a laser source a powder feeder and an air source , the laser cladding machine being configured in such a way that a laser beam , a powder jet and an air jet , respectively generated by the laser source , the powder feeder and the air source , converge on an area to be repaired within a narrow recess of said turbomachine component; defining a path including areas to be repaired by laser cladding within said narrow recess, said path being extended between a first end point and a second end point; moving forward one of the laser cladding machine and the turbomachine component (C) relatively to the other of the laser cladding machine and the turbomachine component (C), in order that said path is covered from the first to the second end point by the laser beam and the powder jet for repairing said areas to be repaired; moving backward one of the laser cladding machine and the turbomachine component (C) relatively to the other of the laser cladding machine and the turbomachine component (C), in order that said path is covered from the second to the first end point by the air jet for blowing away the powder in excess from said recess with heated air; wherein the turbomachine component is a stator case having stator blades and damaged areas in the narrow recess between adjacent stator blades are repaired; and wherein one of the laser cladding machine and the turbomachine component (C) is moved relatively to the other by moving a robotic arm along a circular path (P), the robotic arm comprising the laser source and the powder feeder . setting up a laser cladding machine including a laser source a powder feeder and an air source , the laser cladding machine being configured in such a way that a laser beam , a powder jet and an air jet , respectively generated by the laser source , the powder feeder and the air source , converge on an area to be repaired within a narrow recess of said turbomachine component; defining a path including areas to be repaired by laser cladding within said narrow recess, said path being extended between a first end point and a second end point; moving forward one of the laser cladding machine and the turbomachine component (C) relatively to the other of the laser cladding machine and the turbomachine component (C), in order that said path is covered from the first to the second end point by the laser beam and the powder jet for repairing said areas to be repaired; moving backward one of the laser cladding machine and the turbomachine component (C) relatively to the other of the laser cladding machine and the turbomachine component (C), in order that said path is covered from the second to the first end point by the air jet for blowing away the powder in excess from said recess with heated air; wherein the turbomachine component is a stator case having stator blades and damaged areas in the narrow recess between adjacent stator blades are repaired; and wherein one of the laser cladding machine and the turbomachine component (C) is moved relatively to the other by moving a robotic arm along a circular path (P), the robotic arm comprising the laser source and the powder feeder . <EOS>