What was found
RT SIDE FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE BS 1016 - BS 1132 HAS CHAFFING DAMAGE / REMOVED AND REPLACED CLOSURE ANGLE R/H SIDE FUSELAGE FIN TO BODY INTERFACE; AT BS 1016 - BS 1132 IAW SRM 51-40-02-0G-0 DWG 148A8300; 148A3590
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT SIDE FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE BS 1016 - BS 1132 HAS CHAFFING DAMAGE / REMOVED AND REPLACED CLOSURE ANGLE R/H SIDE FUSELAGE FIN TO BODY INTERFACE; AT BS 1016 - BS 1132 IAW SRM 51-40-02-0G-0 DWG 148A8300; 148A3590