P/N: 5042002-1
Category: General Aircraft Parts
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 | 2 Available |
The 5042002-1 is a triangulated truss member serving as a load-bearing structural component in aircraft fuselage assemblies. Fabricated from aerospace-grade aluminum alloy, this truss distributes concentrated loads between frames and ribs through its diagonal web members, reducing stress concentration in the airframe. Installed within fuselage substructures to support equipment mounts, avionics racks, and panel interfaces.
Assembly uses approved aerospace fasteners with torque specifications per the aircraft maintenance manual. Verify part compatibility with the 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 5042002-1 is a triangulated truss member serving as a load-bearing structural component in aircraft fuselage assemblies. Fabricated from aerospace-grade aluminum alloy, this truss distributes concentrated loads between frames and ribs through its diagonal web members, reducing stress concentration in the airframe.
The 5042002-1 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 5042002-1 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.