What was found
LT WING NR 2 SLAT LOWER COVE PANEL HAS EVIDENCE OF A CRACK ON INBOARD SIDE INBOARD MAIN TRACK ATTACH POINT TO SLAT REMOVED. FABRICATED AND INSTALLED NEW COVE PANEL, IAW B757 SRM 51-40-02, 51-40-05 AND BOEING DWG 114N4076 REV C. PERFORMED SATISFACTORY OPERATIONS CHECK, IAW B757 AMM 27-81-02-4 FIG 401.