P/N: 100a703025
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 | 4 Available |
The 100a703025 is a prevailing-torque stop nut designed to resist loosening from vibration and thermal cycling in aircraft assemblies. This self-locking fastener maintains clamp load on control linkage attachments and other critical connections. Manufactured to AN364/AN365 or MS21042 specifications, the stop nut features an internal locking mechanism that provides reliable prevailing torque without adhesive compounds.
Installation requires verification of thread size and class, followed by torque application per aircraft maintenance manual specifications. Suitable for general aviation and commercial aircraft structural and control system applications.
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 100a703025 is a prevailing-torque stop nut designed to resist loosening from vibration and thermal cycling in aircraft assemblies. This self-locking fastener maintains clamp load on control linkage attachments and other critical connections.
The 100a703025 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 100a703025 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.