As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME BS 1510 CRACKED AT TAIL CONE GUIDE LUG 2 OCLOCK POSITION. HFEC INSPECTED IAW NDT SPM 06-10-01.001. TWO CRACKS FOUND. TOP CRACK .6" LONG BOTTOM CRACK .9" LONG . 5/16 FROM GUIDE HOLE MADE 1 INCH HOLE ACCOMPLISHED HFEC INSPECTION PER NDT SPM 06-10-01.001 OF CUT-OUT, NO CRACKS NOTED. FABRICATION AND REPAIR INSTALL PER PRI INSTRUCTIONS OF ER/A 520646-14 REV. O.