P/N: 21076-3
Category: Nuts
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 | 2 Available |
The 21076-3 is a self-locking two-lug nut plate with captive threads for aircraft structural applications. Constructed from steel with an all-metal prevailing-torque mechanism that prevents fastener loosening under vibration. Installed by riveting to skin or substructure, providing one-side thread access for panel and fairing assembly.
Conforms to MS/NASM nut plate standards used across general aviation and commercial airframes. Installation requires appropriate rivets and torque application per aircraft maintenance manual specifications.
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 21076-3 is a self-locking two-lug nut plate with captive threads for aircraft structural applications. Constructed from steel with an all-metal prevailing-torque mechanism that prevents fastener loosening under vibration.
The 21076-3 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 21076-3 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.