What was found
L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS DEEP CHAFFING / REMOVED DAMAGE ANGLE AND INSTALLED NEW ANGLE AT L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE PER REF B737-700 SRM 51-40-02-0G-0 AND DWG 148A8300
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS DEEP CHAFFING / REMOVED DAMAGE ANGLE AND INSTALLED NEW ANGLE AT L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE PER REF B737-700 SRM 51-40-02-0G-0 AND DWG 148A8300