As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
OVERSIZED HOLES FOUND DURING ACCOMPLISHMENT OF SB A310-53-2072 ON WING CENTER SECTION UPPER SURFACE STIFFENER 9 AND 10. REPAIR CONSISTS OF INSTALLING OF BOTH HOLES EN 6115-V5X IN TRANSITION FIT IAW EA 6-5315-103426 AND RAS 048117/009/2006 ISSUE "A".