P/N: 50-524138
Category: Controls & Cables
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 50-524138 is an elevator tab control linkage that transmits pitch-trim inputs from the cockpit to the elevator trim tab. This mechanical component connects the trim wheel or servo actuator to the tab control surface, enabling pitch-trim adjustment during flight. Installed within the pitch-trim control run between the flight deck and empennage, it requires rigging per the aircraft maintenance manual to ensure proper free-play and control authority.
Verify compatibility with your aircraft's Illustrated Parts Catalog 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 50-524138 is an elevator tab control linkage that transmits pitch-trim inputs from the cockpit to the elevator trim tab. This mechanical component connects the trim wheel or servo actuator to the tab control surface, enabling pitch-trim adjustment during flight.
The ELEV TAB CONTROL 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 ELEV TAB CONTROL. 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 50-524138.