P/N: 25-8w67-6a
Category: Structural Components
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 25-8w67-6a is a leading-edge panel for aircraft wing or control surface restoration. This structural component preserves aerodynamic contour while protecting underlying airfoil structure during flight. Fabricated in metal or composite materials per OEM specifications, the panel installs using aircraft-grade fasteners and sealants.
Used during wing maintenance, damage repair, or leading-edge replacement in MRO operations. Installation follows the Aircraft Maintenance Manual and Structural Repair Manual for your specific airframe. Verify part compatibility against the Illustrated Parts Catalog before ordering.
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 25-8w67-6a is a leading-edge panel for aircraft wing or control surface restoration. This structural component preserves aerodynamic contour while protecting underlying airfoil structure during flight.
The LEADING EDGE 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 LEADING EDGE. 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 25-8w67-6a.