P/N: 169-524085-7
Category: Actuators
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 169-524085-7 is an elevator tab actuator assembly that drives the elevator trim tab in aircraft pitch control systems. This component converts control input into linear motion to adjust the trim tab position, enabling pitch trim adjustments during flight. Commonly found in Beechcraft and similar general aviation aircraft, the actuator integrates with the elevator trim tab control linkage.
Installation and rigging must follow the Aircraft Maintenance Manual and applicable Illustrated Parts Catalog specifications.
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.
The 169-524085-7 is an elevator tab actuator assembly that drives the elevator trim tab in aircraft pitch control systems. This component converts control input into linear motion to adjust the trim tab position, enabling pitch trim adjustments during flight.
The 169-524085-7 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 169-524085-7 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.