As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICALSTAB.INTERNALSIDE. STA 1016; LATTERAL EXPANTION JOINT ANGLE IS CRACKED IN RADIUS 3' O/B OF STR 2R; 8' ABOVE FUSELAGE SKIN / REMOVED AND REPLACED VERTICAL LATERAL EXPANSION JOINT ANGLE STA 1016 IAW SRM 51-40-02-0G-0 AND BOEING DWG 176A 3101 REV-.