P/N: 96-526013-625
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 |
|---|---|
| New Surplus | 1 Available |
The 96-526013-625 is an elevator trim tab actuator assembly from the Hawker Beechcraft/Textron 96-526013 family. This actuator converts control inputs into linear motion to position the elevator tab for precise pitch trim control. Installed between the control linkage and elevator tab, it enables smooth tab positioning throughout the flight envelope.
Installation and rigging must follow aircraft maintenance manual procedures, with Illustrated Parts Catalog compatibility verification required before installation.
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 96-526013-625 is an elevator trim tab actuator assembly from the Hawker Beechcraft/Textron 96-526013 family. This actuator converts control inputs into linear motion to position the elevator tab for precise pitch trim control.
The ACTUATOR ASSEMBLY - ELEVATOR TAB C 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: New Surplus. 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 ASSEMBLY - ELEVATOR TAB C. 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 96-526013-625.