As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME AT FS 333.00 HAS SEVERAL AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 25L AND STR 25R. FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-00. REMOVED, LOCATED, DRILLED, AND INSTALLED FRAME IAW SRM 51-40-11, 51-42-06 & 51-42-21.