What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Aircraft was in cruise flight at FL 290 on an IFR flight from johnson county, Kansas city, MO (ojc) to rhinelander, WI (rhi). The PIC initiated a descent using the autopilot. The a/p immediately disengaged and the aircraft pitched up violently. With the help of a passenger (rated pilot) the PIC was able to maintain control of the aircraft. An emergency was declared and the aircraft diverted to Waterloo, IA (alo). The aircraft descended to 8000 feet. While determining controllability in the landing configuration, a temperature inversion occurred and the trim actuator began to work. The aircraft made an uneventful landing at alo. It was determined that the trim actuator had frozen during climb out. A service bulletin calling for the actuator to be lubed and the boot covering the actuator to be reinstalled with the drain holes facing down at the next scheduled inspection. The owner elected to comply with this bulletin immediately. During that procedure it was determined that the boots had been installed from the factory incorrectly. The drain holes were facing upward. The aircraft had been parked over night on the ramp in light rain and drizzle prior to this flight. Total airframe hours = 255.
As the FAA filed it
(-23) AIRCRAFT WAS IN CRUISE FLIGHT AT FL 290 ON AN IFR FLIGHT FROM JOHNSON COUNTY, KANSAS CITY, MO (OJC) TO RHINELANDER, WI (RHI). THE PIC INITIATED A DESCENT USING THE AUTOPILOT. THE A/P IMMEDIATELY DISENGAGED AND THE AIRCRAFT PITCHED UP VIOLENTLY. WITH THE HELP OF A PASSENGER (RATED PILOT) THE PIC WAS ABLE TO MAINTAIN CONTROL OF THE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO WATERLOO, IA (ALO). THE AIRCRAFT DESCENDED TO 8000 FEET. WHILE DETERMINING CONTROLLABILITY IN THE LANDING CONFIGURATION, A TEMPERATURE INVERSION OCCURRED AND THE TRIM ACTUATOR BEGAN TO WORK. THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT ALO. IT WAS DETERMINED THAT THE TRIM ACTUATOR HAD FROZEN DURING CLIMB OUT. A SERVICE BULLETIN CALLING FOR THE ACTUATOR TO BE LUBED AND THE BOOT COVERING THE ACTUATOR TO BE REINSTALLED WITH THE DRAIN HOLES FACING DOWN AT THE NEXT SCHEDULED INSPECTION. THE OWNER ELECTED TO COMPLY WITH THIS BULLETIN IMMEDIATELY. DURING THAT PROCEDURE IT WAS DETERMINED THAT THE BOOTS HAD BEEN INSTALLED FROM THE FACTORY INCORRECTLY. THE DRAIN HOLES WERE FACING UPWARD. THE AIRCRAFT HAD BEEN PARKED OVER NIGHT ON THE RAMP IN LIGHT RAIN AND DRIZZLE PRIOR TO THIS FLIGHT. TOTAL AIRFRAME HOURS = 255.