As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GEN ITEM: 63-54-1-2805// INNER SKIN CRACK AT AFT UPPER CORNER ON NO1 PYLON AT ACCESS PANEL 436BR CUTOUT (M) 2328. STOPPED DRILL CRACK FABRICATED AND INSTALLED REPAIR DOUBLER INST ALLED RUB STRIP IAW B767 SRM 54-53-01-2R-7 REPAIR 7. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET NO 34 PAGES 1-3 FOR DET AILS. REF NON-ROUTINE 167037-0400-0183 FOR DETAILS