P/N: 65b11518-17
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 |
The 65b11518-17 is a structural beam designed to carry bending and shear loads in aircraft airframe assemblies. Manufactured from aerospace aluminum or steel, this load-carrying member supports fuselage and wing substructures. The beam installs to mating ribs and frames using OEM-approved hardware and specified torque values.
Installation requires reference to the aircraft's Structural Repair Manual (SRM), Aircraft Maintenance Manual (AMM), and Illustrated Parts Catalog (IPC) for correct positioning and fastener requirements. Critical for maintaining structural integrity in wing assemblies.
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 65b11518-17 is a structural beam designed to carry bending and shear loads in aircraft airframe assemblies. Manufactured from aerospace aluminum or steel, this load-carrying member supports fuselage and wing substructures.
The BEAM 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 BEAM. 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 65b11518-17.