As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 280 BETWEEN 11 LBL/RBL AT COCKPIT. (CPIL) TCI 53-10-219
CORROSION LEVEL 2. FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 280 BETWEEN 11 LBL/RBL AT COCKPIT WAS REPLACED PER PER CRJ/900 SRM 51-42-06-001-001-A01 PAR. 6. C. AND CRJ900 SRM 51-42-20-001-001 -A01 PAR. 6. D.