P/N: 212-p-1405-001
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 212-p-1405-001 is an elevator trim tab mounted at the trailing edge of the elevator surface. This control component adjusts the elevator's neutral position, reducing pitch control forces during flight. Actuated by cockpit trim inputs, it allows pilots to maintain aircraft attitude without constant control pressure.
Installation and rigging must follow the aircraft maintenance manual and FAA 14 CFR Part 43 requirements. Verify compatibility with the 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 212-p-1405-001 is an elevator trim tab mounted at the trailing edge of the elevator surface. This control component adjusts the elevator's neutral position, reducing pitch control forces during flight.
The ELEVATOR 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 ELEVATOR 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 212-p-1405-001.