As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WITH PITCH TRIM INDICATOR IN T/O POSITION, UPON ROTATION, ACFT OVER ROTATED AND IT TOOK BOTH HANDS TO CONTROL. NORMAL FLIGHT CONTROL FORCES WITH TRIM INDICATOR AT FULL NOSE DOWN. FOUND TRIM INDICATOR SHOWING INCORRECT T/O POSITION. REMOVED ELEV TRIM TAB CONTROL WHEEL AND CORRECTED TRIM TAB INDICATOR POS. INSTALLED ELEV TRIM TAB CONTROL WHEEL IAW MM 27-31-08. ELEVATOR AND ELEV TRIM TAB TRAVEL/DEFLECTION CHECKS GOOD IAW MM 27-31-00-221.