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 IN TAIL SECTION SKIN AT STA 1062 APPROXIMATELY FOUR INCHES BELOW LONGERON 15L. THE FASTENER WAS REMOVED IAW SRM 51-30-2 AND THE CRACKED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 28. A DOUBLER REPAIR WAS INSTALLED IAW 51-10-3.