P/N: 365a31-2146-20
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 | 34 Available |
The 365a31-2146-20 is a steel lock nut designed to secure threaded fastener joints and maintain prevailing torque under aircraft vibration. This aerospace-grade component follows MS21042 standards and resists loosening in critical airframe applications including bracket attachments, panel fasteners, and structural connections. Installation requires torque per aircraft maintenance manual specifications, with prevailing torque verification before reuse.
Suitable for general aviation and commercial aircraft hardware.
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 365a31-2146-20 is a steel lock nut designed to secure threaded fastener joints and maintain prevailing torque under aircraft vibration. This aerospace-grade component follows MS21042 standards and resists loosening in critical airframe applications including bracket attachments, panel fasteners, and structural connections.
Aircraft hardware is manufactured to military and aviation specifications. The LOCK,NUT 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 365a31-2146-20.
Yes, we sell hardware in various quantities from single units to bulk lots. The LOCK,NUT is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.