What was found
DURING H-CHECK, FOUND CRACK IN TOP END OF MAIN CABIN FLOOR PANEL NR 59. REPAIRED IAW SRM 53-01 FIGURE 4, SRM 53-05 FIGURE 1, SRM 51-10-3, 51-30-2, PAGE 239.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING H-CHECK, FOUND CRACK IN TOP END OF MAIN CABIN FLOOR PANEL NR 59. REPAIRED IAW SRM 53-01 FIGURE 4, SRM 53-05 FIGURE 1, SRM 51-10-3, 51-30-2, PAGE 239.