P/N: 2-2220-3
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 2-2220-3 is a left-hand trim tab assembly that mounts to the trailing edge of primary flight control surfaces. This secondary control surface counteracts aerodynamic loads to stabilize pitch, roll, or yaw without requiring constant pilot input. The tab hinges to its parent surface and deflects automatically or via control linkage to trim the aircraft.
Installation follows the aircraft maintenance manual with rigging, deflection limits, and balance verification per FAA AC 43.13-1B. Commonly found on general aviation and corporate aircraft control surfaces.
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 2-2220-3 is a left-hand trim tab assembly that mounts to the trailing edge of primary flight control surfaces. This secondary control surface counteracts aerodynamic loads to stabilize pitch, roll, or yaw without requiring constant pilot input.
The LH 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 LH 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 2-2220-3.