As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 12 YEAR CORROSION INSPECTION OF CENTER WING FUEL TANK, REMOVABLE PANEL STIFFENER WAS FOUND CRACKED AT THE END OF THE STIFFENER. DASSAULT ENGINEERING WAS CONTACTED AND PROVIDED CHANGE APPROVAL SHEET R245. STIFFENER WAS TRIMMED AND RE-INSPECTED TO ENSURE COMPLETER CRACK REMOVAL. (M)