As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE FWD MOUNT FITTING AFT UPPER I/B AND O/B HOLES HAVE A 2.5 SQ INCH AREA OF CORROSION EACH AT RECESS DIAMETERS AND AROUND UPPER SURFACE WORKED LEVEL 1 CORROSION ON NR 1 ENGINE FWD MOUNT HOLES AND REMOVED CORROSION AND REPAIRED IAW FED-EX EA NR 6-5450-118038, RELEASE DATE 4 JANUARY 2008.