P/N: 204-040-115-3
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 | 1 Available |
The 204-040-115-3 is a self-locking nut designed to resist vibration-induced loosening in aircraft fastening applications. Steel or aluminum construction provides prevailing torque through internal locking mechanisms that grip mating bolts without additional fasteners. Commonly installed on airframe brackets and structural assemblies where AN or MS bolts require secure, permanent connections.
Installation follows aircraft maintenance manual torque specifications and reuse limits to ensure proper locking function. Verify part compatibility with your aircraft's Illustrated Parts Catalog before installation.
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 204-040-115-3 is a self-locking nut designed to resist vibration-induced loosening in aircraft fastening applications. Steel or aluminum construction provides prevailing torque through internal locking mechanisms that grip mating bolts without additional fasteners.
Aircraft hardware is manufactured to military and aviation specifications. The NUT SELF LOCKING 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 204-040-115-3.
Yes, we sell hardware in various quantities from single units to bulk lots. The NUT SELF LOCKING is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.