As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME 295 HAS SIGNS OF CORROSION BETWEEN STRINGERS 26L AND 25R. BLENDED AREA AT STR 26L AT FS295 MATERIAL LOSS OF .004" OF ORIGINAL THICKNESS OF .050", BLENDED AREA AT STR 25R AT FS295 MATERIAL LOSS OF .002" OF ORIGINAL THICKNESS OF .050" NO FURTHER CORROSION NOTED IAW SRM 51-42-06, 53-21-06, 51-21-11, AND 51-21-06.