What was found
AT C-CHECK, STA 328 FLOORBEAM UPPER CHORD TO FLOOR PANEL BLEEDING CORROSION FROM APPROX RBL 12 TO LBL 12. CUT OUT DAMAGED AREA, INSTALLED ANGLES, REPAIR PER BOEING SRM 53-1-8. ANGLE 15 BY 1 BY 1.25, 13 BY 1 BY 1 AND FILLER 1.75 BY 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, STA 328 FLOORBEAM UPPER CHORD TO FLOOR PANEL BLEEDING CORROSION FROM APPROX RBL 12 TO LBL 12. CUT OUT DAMAGED AREA, INSTALLED ANGLES, REPAIR PER BOEING SRM 53-1-8. ANGLE 15 BY 1 BY 1.25, 13 BY 1 BY 1 AND FILLER 1.75 BY 1.