What was found
CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT BS 360, STR 11L ANGLE. REPAIRED AND REPLACED STRINGER ANGLE PER REPAIR DOCUMENT SRM 51-40-02. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT BS 360, STR 11L ANGLE. REPAIRED AND REPLACED STRINGER ANGLE PER REPAIR DOCUMENT SRM 51-40-02. (X)