P/N: 204-040-115-3
Category: Nuts
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| Condition | Price | Stock |
|---|---|---|
| New Surplus | $950.00 | 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.
The 204-040-115-3 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 204-040-115-3 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.