As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK IN AFT PRESSURE BULKHEAD T-CAP AT RT LAV NEAR STRINGER 34 AND A .5 INCH CRACK IN T-CAP AT RT LAV NEAR STRINGER 14. A REPLACEMENT SECTION OF T-CAP WAS SPLICED IN AT EACH LOCATION IAW SRM 53-03, FIGURE 37 AND ECRA 5310-03392.