What was found
CLT - Q-1 - BS 360 STR 14, STRINGER CLIP ANGLE HAS A .50 INCH CRACK. REPLACED ANGLE PER REPAIR 51-10-02 AND 01. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - Q-1 - BS 360 STR 14, STRINGER CLIP ANGLE HAS A .50 INCH CRACK. REPLACED ANGLE PER REPAIR 51-10-02 AND 01. (X)