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.

• Altitude Hold Stabilization: Continuously measures absolute static pressure deviations to detect micro-changes in aircraft altitude. It converts these pneumatic pressure variations into electronic feedback loops to allow the autopilot pitch computer to execute steady altitude hold functions. 
• Pitot-Static System Integration: Designed to inline “T-fitting” splice directly into the aircraft’s primary static pressure tubing array, plumbing it parallel to the primary altimeter and altitude reporting encoder. 
• Dynamic Pitch Correction: Translates instantaneous barometric altitude changes into vertical command errors, prompting the automated flight guidance loop to trim the elevator pitch servo appropriately during turbulence or environmental updrafts/downdrafts.
• Solid-State Reliability: Engineered without mechanical moving diaphragms or standard internal glass components, minimizing electrical drift and protecting the sensor calibration against severe engine vibrations and airframe shock loads.