As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV AT SAA, A CREASE WAS FOUND IN THE FUSELAGE SKIN AT STA 1420, S-28R. THE CREASE EXCEEDED THE ALLOWABLE SRM LIMIT. A REPAIR WAS ACCOMPLISHED PER BOEING INSTRUCTIONS. STARTING AT 12,000 CYCLES AFTER REPAIR INSTALLATION AND EVERY 12,000 CYCLES THEREAFTER, THE PERIPHERAL ROW OF FASTENERS COMMON TO THE REPAIR MUST BE LFEC INSPECTED FOR CRACKS.