What was found
A 1.5 INCH CRACK WAS FOUND CENTER FUSELAGE 3 PASSENGER CABIN FLOOR STRUCTURE FR86 LBL24. PANEL SUPPORT WAS REPLACED IAW SRM 51-41-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1.5 INCH CRACK WAS FOUND CENTER FUSELAGE 3 PASSENGER CABIN FLOOR STRUCTURE FR86 LBL24. PANEL SUPPORT WAS REPLACED IAW SRM 51-41-01.