P/N: 404-528
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 | 1 Available |
The 404-528 is a self-locking nut designed to resist vibration-induced loosening in aircraft hardware assemblies. This steel nut provides prevailing torque that maintains fastener security without requiring lock washers or safety wire. Commonly used to secure brackets, clamps, and structural attachments on airframe components where fastener retention is critical.
Installation follows standard torque procedures per aircraft maintenance manuals and FAA AC 43.13 guidance. Avoid use in rotating-joint applications where prevailing torque could cause excessive friction.
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 404-528 is a self-locking nut designed to resist vibration-induced loosening in aircraft hardware assemblies. This steel nut provides prevailing torque that maintains fastener security without requiring lock washers or safety wire.
The 404-528 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 404-528 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.