P/N: 525-123-9004
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 | 4 Available |
The 525-123-9004 is a steel self-locking nut designed to secure airframe and system components against vibration loosening. This prevailing-torque nut resists rotation under operational vibration, maintaining fastener integrity in bracket and panel assemblies. Conforms to NSN 5310-01-313-2368 and references AN, MS, or NAS standards depending on application.
Install and torque per your aircraft maintenance manual and FAA AC 43.13-1B guidance for hardware specifications and prevailing-torque nut procedures.
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 525-123-9004 is a steel self-locking nut designed to secure airframe and system components against vibration loosening. This prevailing-torque nut resists rotation under operational vibration, maintaining fastener integrity in bracket and panel assemblies.
The 525-123-9004 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 525-123-9004 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.