As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT 80 KNOTS, CREW EXPERIENCED AILERON CONTROL ANOMOLIES. EXCESSIVE FORCE HAD TO BE USED TO CTR RT TURN POSITION. AFTER ABORT SITTING, STATIC CONTROLS FELL NORMAL. FOUND RT TAB ATTACH BRACKET BROKEN AND HANGING FROM TAB. INSPECTED ACFT IAW 05-50-61 AND FOUND RT TRIM TAB CONTROL ROD BRACKET BROKEN. R & R RT AILERON TRIM TAB, HARDWARE AND RIGGED IAW -8, MM 27-13-00 AND SRM MM 57-60-71.