As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN HAS DENT BS 440+6' 1' ABOVE STR 18L. REPAIRED PER SRM 53-00-01-2R-36 (REPAIR 36). UPON FURTHER INVESTIGATION DENT WAS FOUND TO BE A PREVIOUS BLEND. BLEND MEASURED 1. X .9' X .007' ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS, PER SRM 53-00-01-1A-1. CUT OUT DAMAGE AND REPAIRED SKIN, PER SRM 53-00-01-2R-36 (REPAIR 36).