As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION MX FOUND MULTIPLE DENTS TO THE FUSELAGE SKIN BETWEEN FS 169.00 & FS 193.00 ABOVE STRINGER 23R. THE DENTS MEASURE AS FOLLOWS. A. .200” X .100” X .002” DEEP. B. .500” X .300” X .010” DEEP. C. .250” X .100” X .002” DEEP. D. .300” X .200” X .005” DEEP. E. .150” X .100” X .001” DEEP. REPAIRED IAW 253-03196.