As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 48 MONTH INSPECTION FOUND CRACK IN BOTTOM AFT SECTION OF RUDDER TRIM TAB. REPAIRED RUDDER TRIM TAB CRACK PER AQRD ERO-106811 REVISION IR TITLED N661QS RUDDER TRIM TAB REPAIR DATED AUG 25 2022, FAA APPROVED ON FORM FORM 8110-3 DATED AUG 25-2022. CHECKED BALANCE OF RUDDER AFTER REPAIR AND PAINT AND FOUND TO BE WITHIN LIMITS IAW CESSNA 560XL SRM 51-60-00, 51-60-03.