P/N: gyn165
Category: Nuts
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| Condition | Price | Stock |
|---|---|---|
| New Surplus | $80.00 | 1 Available |
The gyn165 is a self-locking prevailing-torque nut designed to prevent vibration-induced loosening in aircraft bolted joints. Manufactured from steel or corrosion-resistant steel to AN/MS/NAS standards, this nut maintains clamp load without requiring lock washers or safety wire. Install to specified torque values per the aircraft maintenance manual and AC 43.13-1B guidance.
Verify compatibility with the Illustrated Parts Catalog before replacement. Suitable for airframe structural connections, engine mounts, and control system assemblies where reliable fastening is critical.
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 gyn165 is a self-locking prevailing-torque nut designed to prevent vibration-induced loosening in aircraft bolted joints. Manufactured from steel or corrosion-resistant steel to AN/MS/NAS standards, this nut maintains clamp load without requiring lock washers or safety wire.
The gyn165 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The gyn165 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.