What was found
DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DAC DWG NR 5613646 AND DC8 SRM 51-3-0.