As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, THE SIDE COWL PANEL VERTICAL STIFFENER HAD WORN THROUGH AT REPAIR AND METAL HAD NOT BEEN ROUTED OUT TO PREVENT FURTHER CRACKING. ACCOMP EDDY CURRENT INSPECTION PER NDT 51-00-03 AND FOUND CRACK CONTAINED. REPAIRED PER SRM 54-01, FIG 1. REPLACED DOUBLER.