What was found
AT C CHECK, LW TOP SKIN PANEL HAS FIBERGLASS REPAIR NOT FINISHED BETWEEN WING AND FUSELAGE. REMOVED LW TOP SKIN PANEL LOCATED BETWEEN WING AND FUSELAGE PER SRM 51-30-2. INSTALLED BONDED REPAIR AT LW TOP PANEL PER SRM 51-40-6 FIG 1 MAT USED 2024 T3 .020 , 2024T3 .025 AND ADHESIVE FILM AF163-2K SIZE 20X27.5. INSTALLED LW TOP SKIN PANEL PER SRM 51-30-2, N/R 1186.