What was found
AT C-CHECK, LT WING FIXED LEADING EDGE INTERIOR, LOWER SUPPORT ANGLE AT STA 130 IS CRACKED AT ATTACH HOLES. REMOVED AND REPLACED ANGLE SUPPORT PER SRM 51-10-1, 20 X 3. N/R 1089.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LT WING FIXED LEADING EDGE INTERIOR, LOWER SUPPORT ANGLE AT STA 130 IS CRACKED AT ATTACH HOLES. REMOVED AND REPLACED ANGLE SUPPORT PER SRM 51-10-1, 20 X 3. N/R 1089.