As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MDCC CROSSBEAM CRACKED AT FRAME 58, Y1700. IAW SRM 53-10-15 FIGURE 211 REWORK THE STIFFENER & CUT OUT THE CRACK. PERFORM HFEC INSPECTION TO THE CUT OUT & REWORKED AREA IAW NTM 51-10-08 & NO CRACK FOUND. MANUFACTURED THE REPAIR ANGLE & DRILL THE FASTENER HOLES IAW SRM 53-10-15 FIGURE 211. INSTALL THE REPAIR ANGLE IAW SRM 53-10-15 FIGURE 211. THIS REPAIR CATEGORY IS A, MAJOR REPAIR IAW GMM 6-2-100.