P/N: 25cf2385
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 |
|---|---|
| New | 1 Available |
Part 25cf2385 is an extruded aluminum angle for structural reinforcement in aircraft assemblies. This angle transfers loads and provides stiffening at skin-to-frame joints, commonly installed as a bracket or stiffener in fuselage and wing structures. Conforming to aerospace specifications including AMS-QQ-A-200 series standards, the component integrates with existing airframe geometry using standard fasteners.
Installation follows aircraft structural repair manual requirements and FAA AC 43.13 guidance for proper alignment, fastener selection, and torque specifications.
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.
Part 25cf2385 is an extruded aluminum angle for structural reinforcement in aircraft assemblies. This angle transfers loads and provides stiffening at skin-to-frame joints, commonly installed as a bracket or stiffener in fuselage and wing structures.
The ANGLE 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: New. 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 ANGLE. 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 25cf2385.