What was found
CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT AFT END STA 360 STR 14L SHEARBEAM OUTBOARD CHORD ANGLE. REPAIRED PER BOEING DWG NR 69-48985/51-10-02. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT AFT END STA 360 STR 14L SHEARBEAM OUTBOARD CHORD ANGLE. REPAIRED PER BOEING DWG NR 69-48985/51-10-02. (X)