What was found
LH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1016.00 THRU STA 1006.00 / REMOVED AND REPLACED L/H FUSELAGE FIN BODY INTERFACE CLOSURE ANGLE STA 1006 TO STA 1016 PER REF DWG 147A0030 AND B737-700 SRM 51-40-02-0G-0
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1016.00 THRU STA 1006.00 / REMOVED AND REPLACED L/H FUSELAGE FIN BODY INTERFACE CLOSURE ANGLE STA 1006 TO STA 1016 PER REF DWG 147A0030 AND B737-700 SRM 51-40-02-0G-0