P/N: 5310-728-6367
Category: Nuts
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 | 550 Available |
The 5310-728-6367 is a self-locking nut that prevents fastener loosening through prevailing-torque retention. This all-metal or nylon-insert design maintains bolt tension in aircraft structures subject to vibration and thermal cycling. Commonly specified under NASM21042 or MS21044 aerospace standards depending on temperature requirements.
Used for airframe panel fastening, control surface attachments, and structural assemblies where blind installation is required. Installation torque and replacement procedures should follow the aircraft Illustrated Parts Catalog and Structural Repair Manual specifications.
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 5310-728-6367 is a self-locking nut that prevents fastener loosening through prevailing-torque retention. This all-metal or nylon-insert design maintains bolt tension in aircraft structures subject to vibration and thermal cycling.
The 5310-728-6367 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 5310-728-6367 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.