P/N: 6324130-801
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 |
| As Removed | 1 Available |
The 6324130-801 is a trim tab mounted at the trailing edge of elevator or rudder surfaces. This control surface reduces pilot input forces by biasing the primary control, maintaining pitch or yaw trim during flight. The tab deflects opposite to the main surface, allowing hands-off flight stability without constant control pressure.
Installation requires rigging per the aircraft maintenance manual to ensure proper balance and prevent flutter. Verify part number against 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 6324130-801 is a trim tab mounted at the trailing edge of elevator or rudder surfaces. This control surface reduces pilot input forces by biasing the primary control, maintaining pitch or yaw trim during flight.
The TRIM TAB 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, 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 TRIM TAB. 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 6324130-801.