As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A C-CHECK, NR 2 SLAT ACT ATTACH OUTBOARD BRACKET INSIDE PLATE HAS NEW CRACK. REMOVED CRACKED STIFFENER AND FABBED NEW FROM BAC 1503-100145, PO 3111123 DIM 9.2 X 3.5 INCHES IAW S/B 727-57-0130 REV 3 FIG 1. PART TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 S/B 727-57-0130 REV 3 FIG 1.