As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WITH AUTO PILOT OFF, EXCESS PRESSURE REQUIRED TO PULL BACK YOKE FOR ROTATION ON TAKEOFF AND SAME FOR FLARING UPON LANDING ACFT. REPLACED NR1 SSCU IAW AMM TASK 27-61-05-000-801-A01 AND 27-61-05-400-801-A01. OPS CHECK GOOD. FUNCTIONAL TEST OF THE PITCH FEEL SYS ACCOMPLISHED IAW AMM TASK 27-31-00-720-805-A01 AND FUNCTIONAL TEST OF HORIZ STABALIZER TRIM SYS ACCOMPLISHED IAW AMM TASK 27-40-00-720-801-A02, OPS CHECK GOOD. FREEDOM OF MOVEMENT ACCOMPLISHED, FULL TRAVEL ACHIEVED, VERIFIED PROPER DIRECTION, NO DEFECTS NOTED. RETURNED TO SERVICE.