As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H FUSELAGE @ STA 1016 - STA 1046 FIN TO BODY INTERFACE FWD CLOSURE ANGLE HAS CORROSION. / REMOVED DAMAGE ANGLE AND INSTALLED NEW INTERFACE FWD CLOSURE ANGLE AT L/H FUSELAGE STA 1016 - STA 1046; PER REF B737-700 SRM 51-40-02-0G-0 AND DWG 147A0030