As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUNCTIONAL FAIL OF THE STABILIZER TRIM CONTROL COLUMN CUTOUT SWITCHES AND CIRCUIT. PERFORM WIRING CONTINUITY CHECK FORM SRM TO STAB TRIM CONTROL MODULE RESULT WAS SATISFACTORY IAW WDM 27-41-11 AND 27-41-24 REV 41. PERFORMED STABILIZER TRIM ELEVATOR CONTROL ACTUATED LIMIT SWITCH ADJUSTMENT IAW AMM 27-41-07-835-001 REV 88 STEP A TO E. PERFORM OPERATIONAL TEST, RESULT WAS NORMAL IAW AMM 27-41-07-835-001 REV 88 STEP E(4).