As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION OF A PREVIOUSLY ACCOMPLISHED REPAIR, AN ADDITIONAL CRACK WAS FOUND EMANATING FROM A PREVIOUS CUTOUT AT THE FWD UPPER CORNER OF THE ACCESS HOLE ON THE NR 2 ENGINE STRUT SKIN, AT THE OUTBD SIDE OF NAC STA 107.7. REPAIRED PER ERA 365391-14.