FLIGHT CONTROL WHEEL AUTO PILOT AND TRIM (P/N 5618105-12) - As Removed
P/N: 5618105-12
Category: Autopilot Systems
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
Available Inventory
| Condition | Stock |
|---|---|
| As Removed | 2 Available |
Product Description
The 5618105-12 is a flight control wheel assembly integrating autopilot disconnect and electric pitch-trim switches. This yoke-mounted component provides aileron control inputs while enabling immediate manual override of autopilot and trim systems through momentary switch activation. Pilots use the integrated switches to disengage automation and adjust aircraft pitch during normal flight operations and emergency situations.
The assembly mounts to the cockpit control column and interfaces with autopilot and trim control circuits. Installation requires verification against your aircraft's Illustrated Parts Catalog and adherence to maintenance manual procedures.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
Frequently Asked Questions
What is the FLIGHT CONTROL WHEEL AUTO PILOT AND TRIM (P/N 5618105-12)?
The 5618105-12 is a flight control wheel assembly integrating autopilot disconnect and electric pitch-trim switches. This yoke-mounted component provides aileron control inputs while enabling immediate manual override of autopilot and trim systems through momentary switch activation.
Is the 5618105-12 compatible with my aircraft's avionics suite?
Avionics compatibility depends on your aircraft model and existing installation. The FLIGHT CONTROL WHEEL AUTO PILOT AND TRIM is available in: As Removed. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.
Does the 5618105-12 come with an 8130-3 airworthiness tag?
Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.
Do you offer bench testing for the 5618105-12?
We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.
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