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 ON THE NR 3 ENGINE PYLON PER AD 97-05-08 REVEALED A CRACK IN HOLE LOCATION -D-. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND AN ADDITIONAL INSURANCE CUT TAKEN. THE REWORK WAS ACCOMPLISHED PER FED EX S/B 2000-5410A01 AND ER/A 382909-14AD.