What was found
AT C-CHECK, LEFT WING FIXED LEADING EDGE INTERIOR VERTICAL WEB AT WBL 92.8 CRACKED AT ATTACH FASTENERS AT AFT END. STOP DRILL, HFEC STOP DRILL. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 15 X 3. N/R 1093.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LEFT WING FIXED LEADING EDGE INTERIOR VERTICAL WEB AT WBL 92.8 CRACKED AT ATTACH FASTENERS AT AFT END. STOP DRILL, HFEC STOP DRILL. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 15 X 3. N/R 1093.