As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A LARGE AMOUNT OF FORWARD ELEVATOR TRIM WAS REQUIRED AFTER TAKEOFF. ALSO DURING DESCENT THE TRIM WAS ALL THE WAY FORWARD AGAINST THE STOP. INSPECTED SYSTEM. FOUND HARDWARE FOR ELEV TRIM CONTROL WHEEL BACKED 3/4 OF THE WAY OUT, ALLOWING ELEV TRIM INDICATOR DRIVE TO JUMP OF OUT GROOVE IN CONTROL WHEEL. PROPERLY INSTALLED TRIM IND DRIVE AND CONTROL WHEEL ASSY AS REQUIRED. OPS CHECK GOOD. IAW MM 27-32-01.