What was found
CORROSION ON CENTER FUSELAGE III RH SPLICE FR 89 AND Y=+11. REMOVED AND REPLACED CENTER FUSELAGE III SPLICE BETWEEN FR 89 AND Y=+11 IAW SRM 51-40-08.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON CENTER FUSELAGE III RH SPLICE FR 89 AND Y=+11. REMOVED AND REPLACED CENTER FUSELAGE III SPLICE BETWEEN FR 89 AND Y=+11 IAW SRM 51-40-08.