What was found
CLT - DURING Q-4 INSPECTION, FOUND ANGLE CRACKED, .50 INCH. SELF-ANGLE AT STA 291, STR 13R. REMOVED AND REPLACED ANGLE PER SRM 51-10-02. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-4 INSPECTION, FOUND ANGLE CRACKED, .50 INCH. SELF-ANGLE AT STA 291, STR 13R. REMOVED AND REPLACED ANGLE PER SRM 51-10-02. (X)