As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV, SEVERAL DENTS AND TWO EXISTING SKIN REPAIRS WERE FOUND BETWEEN STA 1621 AND STA 1661, S19R TO S23R. THE DENTS AND EXISTING REPAIR DOUBLERS WERE REMOVED AND A SINGLE REPAIR WAS INSTALLED AND APPROVED BY BOEING VIA FAA FORM 8100-9 FOR STATIC STRENGTH. A DTA IS DUE WITHIN 12 MONTHS.