What was found
FUSELAGE INTERNAL STRUCTURE, MAIN DECK FLOOR PANEL 242 QF IS CRACKED FROM FRAME 47 TO FRAME 51. 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 242 QF IS CRACKED FROM FRAME 47 TO FRAME 51. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".