What was found
FUSELAGE INTERNAL STRUCTURE, MAIN DECK FLOOR PANEL 241 PG IS CRACKED FROM FRAME 53 TO FRAME 54. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE INTERNAL STRUCTURE, MAIN DECK FLOOR PANEL 241 PG IS CRACKED FROM FRAME 53 TO FRAME 54. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".