What was found
CRACK ON FLOOR PANEL 221S. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50, FIG 202, SHEET 1. STOP DRILLED AND NO CRACKS WERE FOUND IAW SRM 53-20-50, FIG. 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FLOOR PANEL 221S. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50, FIG 202, SHEET 1. STOP DRILLED AND NO CRACKS WERE FOUND IAW SRM 53-20-50, FIG. 202.