P/N: 100-261-2084
Category: Plates, Doublers & Reinforcements
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 100-261-2084 is an upper load plate serving as a structural backing component in aircraft assemblies. This aluminum or steel plate distributes clamp-up and shear loads around fasteners, preventing localized skin or frame deformation where fittings, brackets, or hinges attach. Installation uses approved AN/MS/NAS fasteners with torque values specified in the aircraft maintenance manual or engineering order.
The plate follows drawing-specific standards for material and dimensions, ensuring proper load distribution in critical structural connections.
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 100-261-2084 is an upper load plate serving as a structural backing component in aircraft assemblies. This aluminum or steel plate distributes clamp-up and shear loads around fasteners, preventing localized skin or frame deformation where fittings, brackets, or hinges attach.
The 100-261-2084 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 100-261-2084 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.