What was found
TUL - VERTICAL STABILIZER RIGHT SIDE SKIN IS CRACKED .5 INCH AT STABILIZER TO FUSELAGE MATE POINT. STOP DRILLED CRACK VISUAL AND NDT VERIFIED STOP DRILL OF CRACK. INSTALLED DOUBLER PER BOEING SERVICE BULLETIN 727-55-82. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TUL - VERTICAL STABILIZER RIGHT SIDE SKIN IS CRACKED .5 INCH AT STABILIZER TO FUSELAGE MATE POINT. STOP DRILLED CRACK VISUAL AND NDT VERIFIED STOP DRILL OF CRACK. INSTALLED DOUBLER PER BOEING SERVICE BULLETIN 727-55-82. (M)