Systems and methods for servicing a turbomachine

A method for servicing a turbomachine, the turbomachine having a rotor and a plurality of rotor blades, the rotor having a plurality of hook elements for receiving a retention device, the method comprising:

• receiving, by a computing system, current data indicating each current hook element of the plurality of hook elements that has a dowel pin hole and a current number of stakes for each current hook element;
• receiving, by the computing system, a defined spacing rule for dowel pins in the plurality of hook elements;
• receiving, by the computing system, a maximum number of stakes per dowel pin hole;
• receiving, by the computing system, an input from an operator via a user interface indicative of rotor servicing being performed;
• determining, by the computing system in response to receiving the input from the operator indicative of rotor servicing being performed, for each current hook element, first potential combinations of other hook elements of the plurality of hook elements with the respective current hook element based on the defined spacing rule, and the current number of stakes at each of the hook elements of each of the first potential combinations;
• identifying, by the computing system, whether first solution combinations exist from the first potential combinations, the current number of stakes at each of the hook elements in each of the first solution combinations being less than the maximum number of stakes;
• and
• when the first solution combinations are identified to exist:
• determining, by the computing system, at least one desired solution of the first solution combinations having a highest number of potential future services;
• controlling, by the computing system, the user interface to highlight the at least one desired solution from remaining ones of the first solution combinations;
• and
• installing the dowel pins and the stakes into the rotor based at least in part on the at least one desired solution.