What was found
CRACKED CLIP IN LEFT WING TO FUSELAGE INTERNAL STRUCTURE, STA 640.000 BETWEEN S-23L AND S-24L. REMOVED CRACKED CLIP IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICATED NEW CLIP IAW SRM 53-2-0 FIG 1F. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-3-0 PG 1, SRM 51-1-21.