What was found
DURING H-CHECK, FOUND CRACK IN MAIN CABIN FLOOR PANEL NR 28, 2 EA HAT CHANNELS ON END OF PANEL. REPAIRED IAW SRM 53-22-01-801-663A, & 51-90-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING H-CHECK, FOUND CRACK IN MAIN CABIN FLOOR PANEL NR 28, 2 EA HAT CHANNELS ON END OF PANEL. REPAIRED IAW SRM 53-22-01-801-663A, & 51-90-0.