As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMAGE WAS FOUND DURING THE ACCOMPLISHMENT OF SB 170-57-0038 ON THE LT SPAR III, FASTENER HOLE. THE PERMANENT REPAIR WAS ACCOMPLISHED BY SPOTFACING OUT THE CRACK DAMAGE THROUGH SPAR III, FABRICATING AND INSTALLING A REPAIR BUSHING IAW EO E17X-57MA-004.5.