As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CANTED BULKHEAD AT FS 588.10 & STRINGER 8L .65 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-041. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.