As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND VERTICAL STABILIZER REAR SPAR LOWER ACCESS PANEL CRACKED IN SEVERAL PLACES. THE CRACKS WERE APPROXIMATELY .5 INCH LONG. THE CRACKS WERE STOP DRILLED IAW SRM 53-01, FIGURE 2. DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-3.