As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO STIFFENERS AND AFT SIDE OF WEB ON RT WING AT STA 180.36 SUSTAINED DAMAGE FROM TOOLING. THE STIFFENERS WERE REMOVED AND THE DAMAGED AREA WAS BLENDED IAW SRM 51-30-2 AND 57-10-1. STIFFENERS AND REPAIR PLATES WERE FABRICATED AND INSTALLED IAW SRM 57-10-2 ANS 57-10-6.