As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFW - FOUND AND BLENDED OUT DAMAGE ON THE INNER SURFACE OF FUSELAGE SKIN. THE BLEND OUT IS APPROXIMATELY 1 INCH BY 2 INCHES WITH APPROX .050 MATERIAL REMAINING. THE DAMAGE IS UNDERNEATH STRINGER 38L. REFINISHED AND INSTALLED A FILLER. APPROVED BY ENGINEERING PER MRB767-1016. (M)