As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL FUSELAGE; STA 1016; 8' ABOVE LH VERTICAL STAB ATTACH LUG. LONGITUDINAL SUPPORT IS CRACKED IN RADIUS / REMOVED AND REPLACED LONGITUDINAL SUPPORT ABOVE LH VERTICAL ATTACH LUG STA 1016 IAW SRM 51-40-02-0G-0 AND BOEING DWG 176A3101 REV B