S-tec 55x Installation Manual Now

Provides automatic pitch trim adjustments to relieve aerodynamic forces on the pitch servo.

Programmer/Computer, Turn Coordinator, and Annunciator.

The S-TEC 55X cannot simply be spliced into any aircraft. Genesys Aerosystems (the parent company of S-TEC) maintains a massive library of Supplemental Type Certificates (STCs) for hundreds of aircraft makes and models. Checking the Approved Model List (AML)

The specific locations where brackets must be riveted or bolted. The required cable tension for the bridle cables. Mechanical Integrity Inspections S-tec 55x Installation Manual

Bridle cables must exit the servo capstan parallel to the main control cables to prevent chafing and premature wear.

2 to 4 Amps during active maneuvering; up to 7 Amps peak with automatic trim active. Mechanical Installation Steps

Ensure you have the specific master drawing list (MDL) and installation kit tailored to the aircraft's registration and serial number. Genesys Aerosystems (the parent company of S-TEC) maintains

The 55X is typically mounted in the aircraft's radio stack and integrates with various flight instruments to control both roll and pitch axes. NTSB (.gov) Programmer/Computer

Before drilling holes or running wires, you must verify that your specific aircraft is approved for the S-TEC 55X installation.

The S-TEC System 55X installation manual is generally restricted to authorized dealers, though the Pilot’s Operating Handbook and specific maintenance excerpts are available online. Alternative resources, including the Flight Line Service Manual and various wiring diagrams, can be accessed through aviation technical databases. For the official product overview, visit Genesys Aerosystems . Flight Line Service Manual For Rate Based Autopilots Mechanical Integrity Inspections Bridle cables must exit the

Ensure the mounting location provides the pilot with an unobstructed view of the display and easy physical reach.

Press the Autopilot Disconnect switch on the pilot's control yoke. The autopilot must instantly disengage, emitting the standard audio alert tone, and the controls must immediately return to completely free manual operation. Return to Service Documentation

Before loosening a single screw on the aircraft, you must verify compliance and gather the necessary legal and technical documentation. Supplemental Type Certificate (STC) Verification