As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER, AND PRE-COOLER EXHAUST CUT OUT ADJACENT TO THE AFT CORNER AT N.S.248, ON THE RIGHT SIDE OF THE STRUT STRUCTURAL ASSEMBLIES FOR NR 3 AND NR 4 PYLONS. INTERIM REPAIR FOR THE NR 3 AND NR 4 STRUT. STRUCTURE ACCOMPLISHED AS PER BOEING MESSAGE 1-178658174 AND FAA FORM 81-00-9.