As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#1 ENGINE LH CORE COWL AFT FRAME 3/4" CRACK ACCESS 417AL. REMOVED HAT BRACKETS AND SHIMS IAW B767 SRM 51-40-02. REMOVED DAMAGED PART OF THE FRAME TOP IAW B767 SRM 54-45-01 REPAIR 13 REV 122. PERFORMED EDDY CURRENT INSPECTION OF THE LH CORE COWL AFT FRAME, NO DEFECTS NOTED. MADE REPAIR PARTS TO THE SAME CONTOUR AS THE INITIAL FRAME IAW B767 SRM 54-45-01 PAINTED AND INSTALLED REPAIR IAW B767 SRM 54-10-02 PAGE 2,3,4 REV 122.