As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STABILIZER LEADING EDGE SKIN AT ZFS=136.803 UPPER PANEL RIGHT SIDE AFT CORNER ATTACH TANG WAS FOUND CRACKED APPROXIMATELY 0.281 INCH. THE CRACK WAS TRIMMED OUT APPROXIMATELY 1 INCH BY 1 INCH AND REPAIRED WITH AN EXTERNAL DOUBLER.