As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION OF FUSELAGE SKIN AT LOWER FRAME 10 UNDER FORWARD END OF PANEL 130A. THE DOMED HOTPLATES ARE RETAINING WATER. THIS PANEL IS REMOVED ONLY AT 2C INSPECTION. SUBMITTER RECOMMENDED REMOVAL AT EACH C-INSPECTION TO INSPECT FOR CORROSION. AC TT: 6,845.8 HOURS. (X)