As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF LEFT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 157 BETWEEN STRINGER S 4 AND 5. THE CRACKED SECTION OF SKIN WAS REMOVED IAW SRM 55-30-3. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-3 AND SRM 51-30-2.