P/N: 25-8wg1-118a
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 | 4 Available |
The 25-8wg1-118a is an aileron assembly with integrated trim tab for wing roll control. This component reduces pilot control forces and maintains lateral trim by aerodynamically biasing the aileron's neutral position. Mounted on the wing trailing edge, the aileron converts control inputs into banking maneuvers while the trim tab minimizes sustained control pressure during level flight.
Installation and rigging must follow the aircraft maintenance manual specifications. Verify compatibility with your aircraft's Illustrated Parts Catalog before installation to ensure proper fit and control authority.
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 25-8wg1-118a is an aileron assembly with integrated trim tab for wing roll control. This component reduces pilot control forces and maintains lateral trim by aerodynamically biasing the aileron's neutral position.
The AILERON W 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 AILERON W 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 25-8wg1-118a.