As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FUSELAGE TO SPAR 3 ROD END ASSEMBLY HAD CORRODED ON THE LOWER ROD END. MAINTENANCE REMOVED AND REPLACED THE LEFT ROD ASSEMBLY IAW GST-3655A-01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLETION OF INSPECTION.