As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ACFT WAS FOUND TO HAVE A GOUGE ON FUSELAGE SKIN UNDER THE NR 2 ENGINE. MAINTENANCE CUTOUT THE DAMAGE AREA UNDER NR 2 ENGINE FROM FRAMES 68 TO 70 STRINGER 14R. FABRICATED A FILLER AND DOUBLER AND INSTALLED IAW ETD 2014-145-062583. ACFT RELEASED AFTER PRESSURIZATION CHECKS.