As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-1 CHECK INSPECTION, FOUND NR 1 PYLON INNER DOUBLER, VERTICAL STIFFENER FORWARD PYLON TO LEADING EDGE SUPPORT ANGLE IS CRACKED. REMOVED AND INSTALLED DOUBLER VERTICAL STIFFENER FORWARD PYLON IAW DC8 SRM 51-1-0. INSTALLED HARDWARE IAW DC8 SRM 51-1-20D. C-1 CHECK INSPECTION WORK CARD NUMBER 1007. NON-ROUTINE TASK CARD NUMBER 93069.