As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT CANTED KEEL AREA, TIE ANGLE FROM THE LOWER FUSELAGE SKIN TO THE WING IS CRACKED AT A BOLT HOLE FS 608 APPROX. REMOVED CRACKED TIE ANGLE AND INSTALLED NEW TIE ANGLE TWA SN 17-5259 AND INSTALLED FASTENERS PER SRM 51-30-1 AND SRM 51-30-5 AND SEALED. OP-16 05/05/00 MCI.