NUTPLATE: ST (P/N 506-541) - New Surplus
P/N: 506-541
Category: Nuts
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
Available Inventory
| Condition | Stock |
|---|---|
| New Surplus | 4 Available |
Product Description
The 506-541 is a steel nutplate (anchor nut) that provides threaded attachment points in aircraft airframe structures. This fastener is installed using solid rivets where backside access is limited, such as on access panels and structural components. The nutplate conforms to NAS/MS standards like NASM21047, ensuring compatibility with standard aerospace bolts and screws.
Installation requires following torque practices per FAA AC 43.13-1B and verifying thread size against aircraft maintenance documentation. Commonly used on Piper aircraft and similar general aviation platforms.
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.
Frequently Asked Questions
What is the NUTPLATE: ST (P/N 506-541)?
The 506-541 is a steel nutplate (anchor nut) that provides threaded attachment points in aircraft airframe structures. This fastener is installed using solid rivets where backside access is limited, such as on access panels and structural components.
What conditions is the 506-541 available in?
The 506-541 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
How do I get pricing for the 506-541?
The 506-541 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.
Do you offer expedited shipping for the 506-541?
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.