What was found
DURING M-CHECK FOUND FLOOR PANEL 26, CORROSION AT AFT BOTTOM SECTION. PANEL CORRODED BEYOND LIMITS IAW SRM 53-01, FIG 1. REPAIRED PANEL IAW SRM 53-05, FIG 1. CUTOUT DAMAGE 4.25" X 1.25" HFEC NDT SRM 06-10-01 NO CRACK FOUND.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING M-CHECK FOUND FLOOR PANEL 26, CORROSION AT AFT BOTTOM SECTION. PANEL CORRODED BEYOND LIMITS IAW SRM 53-01, FIG 1. REPAIRED PANEL IAW SRM 53-05, FIG 1. CUTOUT DAMAGE 4.25" X 1.25" HFEC NDT SRM 06-10-01 NO CRACK FOUND.