P/N: 2111314-3
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 |
|---|---|
| New Surplus | 1 Available |
The 2111314-3 is a structural stiffener designed to reinforce aircraft fuselage skin panels against local buckling. This component increases panel rigidity in primary and secondary airframe structures by resisting compressive loads and skin deformation. Typically fabricated from aluminum and installed using riveted attachments per aircraft maintenance manual specifications.
Installation follows FAA AC 43.13-1B acceptable sheet-metal practices, with stiffener orientation and fastener spacing determined by structural repair manual data. Used in fuselage bays where skin buckling prevention is critical to airframe integrity.
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 2111314-3 is a structural stiffener designed to reinforce aircraft fuselage skin panels against local buckling. This component increases panel rigidity in primary and secondary airframe structures by resisting compressive loads and skin deformation.
The 2111314-3 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 2111314-3 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.