What was found
DURING ROUTINE INSPECTION, NR 4 LEAD EDGE SLAT FOUND CRACKED AT I/B ACTUATOR ATTACH RIB. STOP DRILL, FAB AND INSTALLED PER IAW SRM 51-40-3 & SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, NR 4 LEAD EDGE SLAT FOUND CRACKED AT I/B ACTUATOR ATTACH RIB. STOP DRILL, FAB AND INSTALLED PER IAW SRM 51-40-3 & SRM 51-30-2.