What was found
DURING M-CHECK FOUND FLOOR PANEL 26, 2 FASTENER HOLES ARE ELONGATED. REPAIRED PANEL IAW SRM 53-05, FIG 1. CUTOUT DAMAGE 4.5"X2". 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, 2 FASTENER HOLES ARE ELONGATED. REPAIRED PANEL IAW SRM 53-05, FIG 1. CUTOUT DAMAGE 4.5"X2". HFEC NDT SRM 06-10-01, NO CRACK FOUND.