Description

This unit has been bench tested by an FAA certified repair station and it comes with an 8130 single release dated 06/03/2026.

This specific -T2 variant is built for a 28 VDC nominal power environment and is commonly factory-configured or STC-installed on high-performance general aviation platforms, specifically the Beechcraft Baron series (such as the 95-B55 or 58).

• Automatic Trim Coordination: Continuously communicates with the primary autopilot pitch computer to execute automated aerodynamic trim updates. This relieves sustained control-wheel pressure on the pitch servo during steady state climbs, descents, and atmospheric variations. 
• Precision Electromechanical Drive: Utilizes an internal, high-efficiency electric motor and internal gear reduction profile to drive an external flight control cable pulley, delivering minute adjustments to the aircraft’s pitch trim tab system. 
• Integrated Bridle Cable Interface: Designed to secure seamlessly into the airframe’s trim control system using dedicated mounting brackets and specialized cable guards to prevent primary aircraft cable fouling or slippage during high-G or high-workload maneuvers. 
• Rigid Metal Housing Profile: Housed in a heavy-duty, corrosion-resistant metallic casing built to isolate the internal electrical winding circuits and sensors from severe engine vibration profiles and thermal shifts inside unpressurized tailcones or under-floor spaces.