What was found
DURING C-CHECK INSPECTION, FOUND FLOOR BEAM TO FUSELAGE FRAME ATTACH FITTING AT RIGHT FS 235 WITH LEVEL 2 CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND FLOOR BEAM TO FUSELAGE FRAME ATTACH FITTING AT RIGHT FS 235 WITH LEVEL 2 CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.