As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE TAIL SECTION EXTERNAL SKIN HAS DINGS ON SURFACE AT 4 INCHES AFT OF FR 87, BETWEEN RIB 2LT AND RIB 3LT ABOUT 4 SQ INCHES. BLENDED FUSELAGE TAIL SECTION SKIN SURFACE DENTS IAW SRM 51-73-10 PG 209 PARA F DEEPEST BEFORE 0.197 AFTER 0.191, LOSS 0.006. ALL WITHIN LIMITS IAW SRM 53-19-12 FIG 102 PARA 5. REPROTECTED AREAS IAW SRM 51-21-10 PG 2 PARA 2 AND 51-75-10 PG 204 PARA 4 AND PG 225 PARA 10