P/N: 525-124-9003
Category: Nuts
Shipping for this part is quoted to your address. We email you the total to approve before anything is charged.
| Condition | Price | Stock |
|---|---|---|
| New Surplus | $6.50 | 147 Available |
| New | Quote | 33 Available |
The 525-124-9003 is a self-locking aircraft nut designed to maintain prevailing torque and resist vibration-induced loosening. This metal fastener conforms to aerospace standards including MS, NAS, and AN specifications. Commonly installed in panel fastening applications on business aircraft such as the Bombardier Challenger 300.
The self-locking feature prevents fastener rotation during flight operations and maintenance cycles. Installation requires standard torque practices per your aircraft's maintenance documentation and Illustrated Parts Catalog.
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 525-124-9003 is a self-locking aircraft nut designed to maintain prevailing torque and resist vibration-induced loosening. This metal fastener conforms to aerospace standards including MS, NAS, and AN specifications.
The 525-124-9003 is currently available in the following conditions: New Surplus, New. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 525-124-9003 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.