As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN LEFT ELEVATOR LOWER SKIN JUST I/B AND AFT OF PANEL NR 9311. THE CRACK WAS STOP DRILLED IAW SRM 55-20-3. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, 51-10-2, AND 51-30. A CALCULATED BALANCE WAS PERFORMED IAW SRM 51-80-7 AND WAS WITHIN LIMITS.