As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AN H CHECK, WHILE PERFORMING LH ENGINE DRAG FITTINGS CLAMP-UP AND DIAGONAL BRACE INSPECTIONS HOLE #9, COMMON TO THE LH WING UPPER SKIN, WAS FOUND OUT OF STANDARD HOLE DIAMETER TOLERANCES; DEFECT WAS REMOVED AFTER REAMING / TO 1ST OVERSIZE. C/W ERA 587544-14AD.