What was found
PANEL SPLICE BRACKET CORRODED AROUND NUT PLATE HOLES, BS 916, BETWEEN PANELS 139CL AND 139DL. REPLACED TEE FITTING IAW SRM 51-10-02-0G-0 & SRM 51-40-02-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL SPLICE BRACKET CORRODED AROUND NUT PLATE HOLES, BS 916, BETWEEN PANELS 139CL AND 139DL. REPLACED TEE FITTING IAW SRM 51-10-02-0G-0 & SRM 51-40-02-0G-0.