As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACK ON BOTTOM OF LONGERON BY VERTICAL FRAME OF NR 2 ENGINE APRON. FOUND CRACK TO BE ON PREVIOUS REPAIR ANGLE. REMOVED REPAIR ANGLE INSPECTED AND HFEC AREA NO DEFECTS FOUND. FABRICATED, INSTALLED NEW REPAIR ANGLE IAW SRM 54-50-02.