As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE VERTICAL T/E ACCESS PANEL ATTACHMENT STRUCTURE HAS CORROSION AT 4 EA LOCATION LT SIDE REF N00745. EXFOLIATED CORROSION BEYOND LIMITS ON STRIP AND CONNECTING PROFILE IAW SRM 55-30-00. REMOVED AND REPLACED STRIP AND PROFILE IAW SRM 51-72-10. AREAS ON PROFILE EDGE AND PROFILE L-SECTION WITHIN LIMITS OF SRM 55-30-00.