P/N: 4511126-4
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 Surplus | 6 Available |
The 4511126-4 is an aerospace-grade I-beam structural component for Cessna Citation airframes. This primary load-bearing member resists bending forces in the aircraft's fuselage structure. Fabricated from aluminum alloy per aerospace standards, the beam integrates into subassemblies and main airframe sections.
Installation requires approved fasteners and adherence to aircraft maintenance manual specifications. Follow 14 CFR Part 43 guidelines and verify compatibility with the applicable Illustrated Parts Catalog before installation.
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 4511126-4 is an aerospace-grade I-beam structural component for Cessna Citation airframes. This primary load-bearing member resists bending forces in the aircraft's fuselage structure.
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 Surplus. 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 4511126-4.