What was found
RIGHT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFING DAMAGE FORWARD OF BS 1016. REMOVED AND REPLACED RH CLOSURE SKATE ANDGLE PER SRM 5140020G0 AND DWG 147A0030; DWG 147A0070; DWG 147A3200 NO SRM ALLOWABLE DAMAGE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFING DAMAGE FORWARD OF BS 1016. REMOVED AND REPLACED RH CLOSURE SKATE ANDGLE PER SRM 5140020G0 AND DWG 147A0030; DWG 147A0070; DWG 147A3200 NO SRM ALLOWABLE DAMAGE.