P/N: 100a703025
Category: Fasteners & Hardware
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.
Aircraft hardware is manufactured to military and aviation specifications. The NUT, STOP conforms to its applicable AN (Air Force-Navy), MS (Military Standard), or NAS (National Aerospace Standard) specification. Contact us for specific specification details.
Aviation hardware is available in various materials including cadmium-plated steel, stainless steel, aluminum alloy, and titanium depending on the application. Contact us for material certification and specifications for the 100a703025.
Yes, we sell hardware in various quantities from single units to bulk lots. The NUT, STOP is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.