As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C, BS 470 AT STR 7L RIVET PULLED RIVET TAIL. REMOVED IAW SRM 51-30-2. EVIDENCE OF CORROSION BETWEEN SKIN AND INTERNAL DOUBLER. FUSELAGE SKIN REPAIRED BETWEEN BS 440 AND BS 507 STR 2L TO 7L IAW SMRO EO NR 2000-002-05. UPS ENGINEERING FILE NR 5330-2220.