P/N: 212-46240-1
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 |
|---|---|
| New | 1 Available |
The 212-46240-1 is a metallic trim rod that transmits motion from the trim actuator to control-surface linkage. This component adjusts tab or stabilizer position to reduce pilot control forces during flight. Constructed per OEM specifications, the rod connects the trim system actuator to the control surface, allowing synchronized movement.
Installation requires verification of length, orientation, and hardware per the aircraft maintenance manual. Used in trim tab linkage systems across general and corporate aviation platforms.
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 212-46240-1 is a metallic trim rod that transmits motion from the trim actuator to control-surface linkage. This component adjusts tab or stabilizer position to reduce pilot control forces during flight.
The TRIM ROD 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. 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 ROD. 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 212-46240-1.