P/N: 25TR221AG
Category: Flight Control Surfaces
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| Serviceable | 1 Available |
The 25TR221AG is a lower rudder tab that provides yaw trim and stability control on aircraft flight control systems. This trailing-edge component deflects to reduce pilot pedal input during asymmetric thrust conditions. Mounted on the rudder's lower section using a continuous hinge, it requires installation and rigging per the aircraft's IPC and AMM to ensure neutral position and proper travel limits.
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 25TR221AG is a lower rudder tab that provides yaw trim and stability control on aircraft flight control systems. This trailing-edge component deflects to reduce pilot pedal input during asymmetric thrust conditions.
The LOWER TAB - RUDDER 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: Serviceable. 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 LOWER TAB - RUDDER. 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 25TR221AG.