As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH WING I/B FLAP INTERNAL STRUCTURE WAS FOUND 1EA FASTENER HOLE ENLARGED AT RIB25A RS PLUS 5" FABRICATED WEB AND INSTALLED WITH FASTENERS AT LH I/B FLAP RIB25A RS PLUS 5" I.A.W AIRBUS DRAWING NO:A57960114 REV E SHEET 1 & A300-600 SRM 51-40-21-001, PARA7 PAGE 24-50 AND PARA13, PAGE 149 - 156. THE REPAIR CLASSIFIED AS CAT A MAJOR PER GMM 6-2-100.