As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE INTERIOR RT SIDE. AFTER REMOVAL OF THE OUTER SPLICE STRAP FOUND THE INNER SPLICE STRAP AT BS 1825 FROM STR 1 TO STR 6 HAS CORROSION. R & R SPLICE STRAP WITH STRAP FABRICATED IAW DWG 148N3138 SHT 1, REV C AND INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR IS MAJOR.