P/N: 212-46240-05-1
Category: Nuts
Flat-rate shipping. Choose Ground or a faster service at checkout.
Flat-rate shipping covers most parts. If your order turns out to need freight or special handling, we'll contact you with the updated shipping cost before it ships. You can pay the difference or cancel for a full refund. International buyers pay any duties and import taxes.
| Condition | Price | Stock |
|---|---|---|
| New | $115.00 | 5 Available |
The 212-46240-05-1 is a threaded aircraft nut designed to secure bolts and studs in airframe and system assemblies. This fastener provides reliable retention on non-rotating connections such as equipment brackets, structural mounts, and panel attachments. Manufactured to AN, MS, or NAS specifications depending on application requirements, the nut ensures consistent clamping force and prevents fastener loosening under vibration.
Installation requires torque application per aircraft maintenance manual specifications and FAA AC 43.13 guidance. Verify part number in 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 212-46240-05-1 is a threaded aircraft nut designed to secure bolts and studs in airframe and system assemblies. This fastener provides reliable retention on non-rotating connections such as equipment brackets, structural mounts, and panel attachments.
The 212-46240-05-1 is currently available in the following conditions: New. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-46240-05-1 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.