What was found
LEFT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFING DAMAGE AFT OF BS 1016. REPAIRED CLOUSURE ANGLE AT BS 1016 PER SRM 5380712R6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFING DAMAGE AFT OF BS 1016. REPAIRED CLOUSURE ANGLE AT BS 1016 PER SRM 5380712R6.