As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE ACCOMPLISHING INSPECTIONS OF THE FASTENER HOLES ON THENR 1 ENGINE PYLON FWD ENGINE MOUNT FITTING PER AD 97-05-08, A CRACK INDICATION WAS NOTED AT HOLE B. THE FASTENER HOLE WAS OVERSIZED TO REMOVE THE CRACK INDICATION WITH AN ADDITIONAL 1/32 INCH INSURANCE CUT. AN OVERSIZE BOLT WAS THEN INSTALLED. THE REPAIR WAS ACCOMPLISHED PER FED-EX S/B 2000-5410A01 AND ER/A 380610-14AD.