What was found
DURING C2 CHECK, A 5 INCH CRACK IN FLOOR PANEL 152UG BETWEEN FRAMES 53.6 TO 54 & BETWEEN -Y953 & -Y1456. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 5I , FIG. 211 & AMM 53-00-00-020-52A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C2 CHECK, A 5 INCH CRACK IN FLOOR PANEL 152UG BETWEEN FRAMES 53.6 TO 54 & BETWEEN -Y953 & -Y1456. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 5I , FIG. 211 & AMM 53-00-00-020-52A.