What was found
CRACKS ON CHANNEL OF FLOOR PANEL NR 222 X. CHANNEL WAS REPAIRED IAW SRM 53-20-50, FIG 201. HFEC INSPECTION WAS PERFORMED, NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-001.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS ON CHANNEL OF FLOOR PANEL NR 222 X. CHANNEL WAS REPAIRED IAW SRM 53-20-50, FIG 201. HFEC INSPECTION WAS PERFORMED, NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-001.