As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME AT FS 605 IS CORRODED BETWEEN STR 26L AND STR 26R. FOUND CORROSION LIMITED TO AREA OF STA 27 TO 26L. DAMAGE FOUND TO BE WITHIN LIMITS REPAIRABLE LIMITS IAW SRM 53-00-15 REPAIR NR 2, STEPS 1 THRU 4. PERFORMED FRAME REPAIR IAW SRM 53-00-15 STEPS 5A (1) THRU 5A (6).