As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1030.00 THRU STA 1132.02. / REMOVED AND REPLACED L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE STA 1030.00 THRU STA 1132.02 PER REF B737-700 SRM 51-40-02-0G-0 AND DWG #148A8300