P/N: c6wa1122-28
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 c6wa1122-28 is an aluminum alloy reinforcement plate for aileron trim tab assemblies. This structural component maintains alignment and distributes loads within the aileron tab structure while providing hardware attachment points. Installed in the tab assembly per Aircraft Maintenance Manual specifications, the plate uses AN/MS/NAS fasteners as designated.
Manufactured by Bombardier de Havilland (CAGE 71867), this part supports aileron control surface integrity in general and commercial aviation applications.
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 c6wa1122-28 is an aluminum alloy reinforcement plate for aileron trim tab assemblies. This structural component maintains alignment and distributes loads within the aileron tab structure while providing hardware attachment points.
The PLATE-AILERON-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 PLATE-AILERON-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 c6wa1122-28.