What was found
FUSELAGE HAS A .72 VERTICAL CRACK AT BS 727E APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. C\W 26-153-01211.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE HAS A .72 VERTICAL CRACK AT BS 727E APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. C\W 26-153-01211.