P/N: 184572
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 |
|---|---|
| Serviceable | 1 Available |
The 184572 is a self-locking stop nut designed to prevent vibration loosening in aircraft structural assemblies. This prevailing-torque fastener uses an internal nylon insert or deformed thread to create resistance, maintaining secure connections under flight loads and vibration. Commonly manufactured to AN363, AN365, or MS21042 specifications in steel construction.
Install with at least one thread visible above the nut, torqued to aircraft-specified values. Used to secure equipment brackets, control linkages, and structural components throughout the airframe. Follow FAA AC 43.13-1B guidance regarding reuse limits and inspection procedures for self-locking nuts.
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 184572 is a self-locking stop nut designed to prevent vibration loosening in aircraft structural assemblies. This prevailing-torque fastener uses an internal nylon insert or deformed thread to create resistance, maintaining secure connections under flight loads and vibration.
The 184572 is currently available in the following conditions: Serviceable. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 184572 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.