As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 6.5 INCH CRACK IN STA 178 BULKHEAD SKIN PANEL ALONG HORIZONTAL STIFFENER AT WL 218, ON LT SIDE. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2.