What happened
During the takeoff roll, at an indicated airspeed of approximately 70 to 75 knots, the pilot experienced a sudden change in pitch where the nose of the aircraft dipped and then rose off the ground. In an attempt to stabilize the aircraft, the pilot pushed the control yoke forward to level the airplane. The aircraft subsequently contacted the runway and skidded to a stop. The impact resulted in the landing gear collapse.
The investigation
An examination of the aircraft revealed that critical hardware was missing from the stabilator trim rod. Specifically, the forward attachment hardware and the aft attachment nut were not installed. Investigation into the maintenance history showed that approximately 60 flight hours and 11 months prior to the accident, a repair station had removed, repaired, and reinstalled the stabilator trim tab. Physical inspection of the stabilator trim tab attachment point confirmed it was visible and not obscured by any cowlings or coverings.