As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE INNER SKIN IS CORRODED IN FRONT OF FRAME AT FS 661+62 BETWEEN STGR 26L AND 26R. REPAIRED FUSELAGE INNER SKIN CORROSION IN FRONT OF FRAME AT F.S. 661+62 AND BETWEEN STGR 26L TO STGR 26R IAW EMDEAVOR AIR EA CRJ953-1554, REV IR, DATED 9/29/2023.