P/N: 169-524085-7
Category: Flight Controls
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 ACTUATOR ASSEM-TAB ELEVATOR may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the ACTUATOR ASSEM-TAB ELEVATOR. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 169-524085-7.