As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CAPTAIN REPORTED THAT IT WAS NECESSARY TO ADJUST THE RUDDER TRIM COMPENSATOR 7 UNITS TO THE RIGHT IN FLIGHT. AT PLATFORM, MAINTENANCE PERSONNEL REPLACED THE RUDDER HYDRAULIC POWER PACKAGE AND THE YAW DAMPER ACTUATOR IAW MM 27-20-04 AND 22-13-01 RESPECTIVELY, TESTED CORRECT. DURING OVERNIGHT CHECK, THE RUDDER TRIM LOAD FEEL SPRING WAS REPLACED IAW MM 27-20-07 AND ADJUSTMENT TEST WAS PERFORMED IAW MM 27-20-00, ALL CORRECT.