As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FTW - FUSELAGE SKIN HAS 6 DENTS IN NORM MORE THAN 10 INCHES STATION 351, 360 BETWEEN LONGERON 4 AND 5 RIGHT. REWORKED DENT TO ORIGINAL CONTOUR IAW MD80 SRM 53-04 FIG 38 CHECKED AREA FOR CRACK IAW NDT MANUAL 08-00-00. NO CRACK FOUND IAW NDT MANUAL 08-00-00. FABRICATE DOUBLER IAW MD80 SRM 53-04. INSTALLED NEW DOUBLER REPAIR IAW MD80 SRM 53-04 FIG 38. (M)