As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON REMOVAL LEFT LOWER FUSELAGE BS 280 BULKHEAD WEB FOUND STIFFNER ANGLE AT LBL 26 CRACKED. REMOVED DISCREPANT STIFFNER ANGLE AT LBL 26, FS 280 AND INSTALLED NEW SERVICEABLE STIFFNER ANGLE IAW SRM 51-42-06-001-001 & 51-42-06-001-001-A01. MAJOR REPAIR.