What was found
C-CHECK, RT WING LOWER TO FUSELAGE FS 640 & XW 0 CRACKED ANGLE. DOT 64157. REMOVED CRACKED ANGLE FROM RT WING LWR TO FUSELAGE STA 640 & XWO PER SRM 51-1-21 PAR 1. FABRICATED NEW ANGLE SAME MATERIAL & THICKNESS 2024-T3 0.050 (14 X 1.15 X 1) IAW DC-8 SRM 53-8-3 FIG 1. CLEANED ANGLE AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA, NEW ANGLE IAW DC-8 SRM 51-1-8 PG 13, 16. INSTALLED NEW ANGLE PER SRM 51-1-21 PAR 1 FIG 32.