As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURAL INSPECTION AT THE LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN STRINGERS 40 & 43L & RT, BETWEEN FRAMES 47 AND 52. FOUND THE SKIN, INTERNAL DOUBLER AND STRINGERS WITH CORROSION. REPAIRED IAW INSTRUCTIONS UNDER REF. 80359037 AND EOD 32S-53-0192-R00.