What was found
CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT HORIZONTAL STAB CENTER SECTION THRUST BEAM ATTACH ANGLE. REPLACED ANGLE PER REPAIR DOCUMENT 51-10-02. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT HORIZONTAL STAB CENTER SECTION THRUST BEAM ATTACH ANGLE. REPLACED ANGLE PER REPAIR DOCUMENT 51-10-02. (M)