What was found
DURING ROUTINE INSP, NR 5 SLAT FOUND CRACKED BEYOND PREVIOUS STOP DRILL IN O/B ANGLE AT THE ACTUATOR ROD END. STOP DRILLED CRACK, FAB, INSTALLED PER IAW SRM 57-50-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSP, NR 5 SLAT FOUND CRACKED BEYOND PREVIOUS STOP DRILL IN O/B ANGLE AT THE ACTUATOR ROD END. STOP DRILLED CRACK, FAB, INSTALLED PER IAW SRM 57-50-3.