As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND VERTICAL STIFFENERS AT LEFT AND RIGHT SIDE OF NR 3 PYLON HAD ELONGATED HOLES AND WERE GALLED AT PAN SUPPORT RIB. THE STIFFENERS WERE REMOVED IAW SRM 51-10-1. NEW STIFFENERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-00, 51-21-01, AND 51-10-1.