What was found
DURING HFEC OPEN-HOLE INSPECION ON THE LT WING LEADING EDGE INBOARD SLAT NR 7 OUTER SKIN, FASTENER HOLES FOUND CRACK INDICATIONS. REPAIRED IAW SRM 57-43-01-2R, FIGURE 202, SHEET 1, REPAIR 8, AND EA G-5750-T0333917 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.