As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFW FUSELAGE SKIN APPROXIMATELY 10 INCHES FORWARD OF FORWARD CARGO DOOR AT STRINGER 32 RT HAD A GOUGE BLENDED BEYOND SRM LIMITS. AREA OF DISCREPANCY IS 2 INCHES BY 1 INCH WITH A DEPTH OF .050 INCH. MATERIAL REMAINING IS .156 INCH. HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS WITH NO FINDINGS. REPAIRED PER SRM 53-00-01-1A WITH EXCEPTIONS PER MRB 767 3276.