As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A/C REQUIRED 5 UNITS OF RUDDER TRIM IN CLIMB, 3 UNITS IN CRUISE. T/S IN PROGRESS. ACCOMPLISHED FIM 27-21-00 FIG 109 TO STEP 36 NO FAULTS FOUND. CHECKED RUDDER RATIO CHANGER SYS PER 27-21-00-5 RUDDER TRIM CONTROL SYS AND YA YAW DAMPNER 27-21-00-5 NO FAULTS FOUND.