As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTIONS OF THE FORWARD ENGINE MOUNT SUPPORT FITTING ON THE NR 3 ENGINE PYLON PER AD 97-05-08, A CRACK INDICATION WAS NOTED IN HOLE C AS REFERENCED IN BAC S/B 727-54A0010. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK WITH AN ADDITIONAL INSURANCE CUT. ACCOMPLISHED PER FED-EX S/B 2000-5410A01 AND ER/A 382703-14AD.