P/N: c1-240-125
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 |
|---|---|
| Serviceable | 1 Available |
The c1-240-125 is a primary flight control aileron mounted on the wing trailing edge. This control surface banks the aircraft by generating differential lift through opposing deflection on each wing. Operating about the longitudinal axis, the aileron responds to pilot input via control cables or hydraulic actuators.
Typically constructed from aluminum alloy with internal ribbing for structural strength, it requires rigging and securing per the aircraft maintenance manual. Verify compatibility using the Illustrated Parts Catalog before installation on your specific airframe.
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 c1-240-125 is a primary flight control aileron mounted on the wing trailing edge. This control surface banks the aircraft by generating differential lift through opposing deflection on each wing.
The AILERON 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: Serviceable. 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. 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 c1-240-125.