As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1480/1510.5 AND STG 3 / 4 LH WITH DENT. UPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1461/1480 AND STGR 3/4 LH WAS REPAIRED I.A.W. SRM 53-00-01-212 REPAIR 14 FIG. 201 AND INSPECTION REQUIREMENTS SEE TABLE V ZONE A - CATEGORY B.