As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE REAR SPAR OF THE RT ELEVATOR IS CRACKED ON THE LOWER I/B SIDE OF THE SECOND FROM THE I/B HINGE FITTING. THE CRACK IS APPROXIMATELY .25 LONG. THIS CRACK LENGTH IS WITHIN THE .250 STOP DRILL LIMITS OF BAC S/B 727-55-0089. THE CRACK WILL BE STOP-DRILLED UNTIL REPAIR/MODIFICATION PER DAL EO 4-70183-12AD.