What was found
C-CHECK, ABOUT XTS 6.000 BELOW LT WING IS A CRACK SEE MARK DOT 38262. REMOVED CRACKED ANGLE FROM WING ABOUT STA XRS 6.000 IAW DC-8 SRM 51-1-21 PAR 1 FIG 32. FABRICATED NEW ANGLE SAME MATERIAL & THICKNESS 2024-T3 0.050 (20 X 11) IAW DC-8 SRM 57-3-1 FIG 25. CLEANED ANGLE AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA & ANGLE PER SRM 51-1-8 PG 13, 16. INSTALLED NEW ANGLE PER SRM 51-1-21 PAR 1 FIG 32.