As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1.5 INCH CRACK IN LEFT CIRCUMFERENTIAL FRAME REINFORCEMENT PLATE AT STA 804, STRINGER 14L. A 1.5 INCH CRACK WAS ALSO FOUND IN RIGHT CIRCUMFERENTIAL FRAME REINFORCEMENT PLATE AT STA 804, STRINGER 14R. FRAME REINFORCEMENT ANGLE REPAIRS WERE ACCOMPLISHED IAW SRM 51-40-3, FIGURE 1.