As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE HAS A .95 VERTICAL CRACK AT BS 727B; APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. REFER TO FAULT TTG8Q01BZXU WHERE EA 26-153-01210 WAS ADDED AS A SUBTASK. REFER TO FAULT TTG8Q01BZXU WHERE EA 26-153-01210 WAS ADDED AS A SUBTASK.