As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION OF THE FWD ENGINE MOUNT SUPPORT FITTING HOLES PER AD 97-05-08 REVEALED A CRACK IN THE BORE OF HOLES A & B. THE HOLES WERE OVERSIZED TO REMOVE THE CRACK INDICATIONS AND AN INSURANCE CUT ADDED. LARGER DIAMETER BOLTS WERE THEN INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 380942-14AD AND FED EX S/B 2000-5410A01.