What was found
DURING ROUTINE C CHECK INSPECTION, RT WING, T/E LWR PANEL EXTERNAL , INTERNAL SKIN DELAMINATED, XW 0.000 - XW 90.000. REMOVED AND REPLACED PANEL ON RT WING T/E, XW 0.000 XW 90.000 IAW DC-8 SRM 51-3-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 14. TORQUED IAW DC-8 SRM 51-3-1.