As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION OF THE NR 1 ENGINE FWD MOUNT SUPPORT FITTING ATTACH HOLES PER AD 97-05-08 REVEALED A CRACK INDICATION IN THE HOLE G-LOCATION. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK INDICATION AND AN INSURANCE CUT APPLIED. AN OVERSIZE FASTENER WAS THEN INSTALLED. THE WORK WAS ACCOMPLISHED PER FED-EX S/B 727-5410A01 AND ER/A 384663- 14AD.