As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE ACCOMPLISHING THE ENGINE PYLON AND WING MODIFICATIONS REQUIRED BY AD 2000-20-09, 2 ATTACH HOLES FOR THE INBOARD SIDE LOAD FITTING WERE DAMAGED. THE HOLES WERE OVERSIZED TO CLEAN AND ROUND CONDITION AND INSPECTED FOR CRACKS. OVERSIZE BOLTS WERE INSTALLED IN THE HOLES PER ER/A 384569-14AD.