I can tell what is done for airplane engines when it comes to turbines, methodology should not be much of a different (I guess). Assessing such cracks means taking the responsibility of any accidents, deaths if not done without enough knowledge. Determination of limits for defects (cracks, dents, nicks, etc...) requires an extensive testing champaign in addition to usage of extensive analysis tools, and they are all defined in engine documents, technical orders, etc...
For your case, I would recommend to do nothing by yourself. Best way is to contact the owner of design. Even if you can provide data for dimensions, working conditions, it is impossible just to say it can withstand the loading, vibrations, etc... without having as much information as the design owner.
Regards