As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFING DAMAGE FORWARD OF BS 1016. REMOVED AND REPLACED LH CLOSURE SKATE ANGLE BS 1006 BS 1016 PER SRM 5140020G0; DWG 147A0030; DWG 147A0070 AND DWG 147A3200; NO SRM ALLOWABLE DAMAGE.