P/N: 010a-24018-11
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 010a-24018-11 is a rudder trim tab that fine-tunes yaw control on the vertical tail surface. This movable trailing-edge component biases the rudder to correct persistent yaw tendencies and reduce pedal forces during coordinated flight. The trim tab deflects independently to maintain hands-off lateral stability without requiring continuous pilot input.
Typically aluminum construction with riveted or bolted attachment to the rudder structure. Installation and rigging must follow aircraft maintenance manual procedures and FAA AC 43.13-1B guidance for control-surface alignment.
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 010a-24018-11 is a rudder trim tab that fine-tunes yaw control on the vertical tail surface. This movable trailing-edge component biases the rudder to correct persistent yaw tendencies and reduce pedal forces during coordinated flight.
The RUDDER 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: 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 RUDDER 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 010a-24018-11.