As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CROSSBEAM FOUND TO BE CORRODED AT RT AND LT SIDE PANEL NUTPLATE LOCATIONS. INSTALLED 5 EA RIVETS CROSSBEAM IAW SRM 51-42-06-001-001-A01. RESTORED A023 FINISH IAW SRM 51-21-16-001-001-A01. APPLIED CIC AT REPAIRED AREA IAW SRM 51-21-11-001-001-A01.