What was found
(LOG 2826403) LH FUSELAGE TO VERTICAL STAB CLOSURE ANGLE IS CHAFED. REMOVED AND REPLACED LH FUSELAGE TO VERTICAL STAB CLOSURE ANGLE IAW 737-800 SRM 51-40-02-OG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 2826403) LH FUSELAGE TO VERTICAL STAB CLOSURE ANGLE IS CHAFED. REMOVED AND REPLACED LH FUSELAGE TO VERTICAL STAB CLOSURE ANGLE IAW 737-800 SRM 51-40-02-OG.