As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND LOWER FUSELAGE SKIN AND STRINGER CORRODED WITH RIVETS POPPED AT STA 312 TO 328, STRINGER 27L TO 26R. THE CORRODED AREA OF SKIN WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-2. STRINGER 28 WAS REMOVED AND REPLACED IAW SRM 53-30-2 AND 51-30-2.