What was found
CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 360 STRINGER 11L CHANNEL. INSTALLED NEW FABRICATED ANGLE PER REPAIR DOCUMENT 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-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 360 STRINGER 11L CHANNEL. INSTALLED NEW FABRICATED ANGLE PER REPAIR DOCUMENT SRM 51-10-02. (X)