S-TEC Autopilot Programmer/Computer Controller Unit

This part number designates a panel-mounted primary autopilot controller and computer unit manufactured by S-TEC Corporation (Genesys Aerosystems). It serves as the primary user interface and processing brain for the S-TEC System 55 / 55X series flight control systems.
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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.

Key Technical Capabilities
  • Dual-Axis Flight Guidance: Processes complex aerodynamic algorithms to manage both lateral (roll) and vertical (pitch) flight paths simultaneously, supporting tracking for headings, nav radials, and altitude holds. 
  • Advanced Approach Intercepts: Features automated logic loops designed to seamlessly intercept and track precision instrument approaches—including ILS glideslopes, localizers, and GPS/WAAS approach profiles.
  • Control Wheel Steering (CWS): Interfaces with a temporary control yoke button allowing the pilot to manually fly the aircraft to a new attitude or altitude parameter and instantly capture it upon release without disengaging the autopilot system.
  • Integrated Autotrim Drive: Continuously communicates with electric pitch trim servos to automatically relieve structural pressure on the elevator linkages, ensuring smooth transitions and preventing nose-heavy or tail-heavy states during flap or landing gear deployment.

Additional information

Part Number

01192-0-0T

Serial Number

01192-1615-16579

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