As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CONTINUE REPAIR** R/T AFT BS 1016 TO BS 1132 FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFED (TTG8Q0051PJS). ; / REMOVED AND REPLACED CLOSURE ANGLE AT RT AFT BS 1016 - 1132 FUSELAGE FIN TO BODY INTERFACE PER B737-700 SRM 51-40-02-0G-0 AND DWG 148A8300; FINAL INSPECTION; REMOVED TO REPLACED R/H CLOSURE ANGLE. ATTACH TO TTG8Q0051PJS.