As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND TWO .25 INCH CRACKS AT FASTENER HOLES IN RIGHT SIDE VERTICAL STABILIZER EXTERNAL SKIN JUST BELOW PANEL 9516. THE PANEL WAS REMOVED FOR ACCESS. THE CRACKED SKIN WAS CUT OUT IAW SRM 54-30-3. REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3, FIGURE 6 AND SRM 51-30-2. THE PANEL WAS REINSTALLED.