P/N: 146204
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 | 100 Available |
The 146204 is a self-locking nut designed to prevent fastener loosening from vibration in aircraft structures. Steel or aluminum construction with a nylon insert or deformed thread that creates prevailing torque resistance. Conforms to aerospace standards AN365 (hex types) or NASM21042 (anchor nuts) depending on application.
Commonly secures access panels, inspection covers, and structural attachments in airframe assemblies. Installation requires torque per aircraft maintenance manual specifications. Prevailing torque must be verified before reuse; replace if torque falls below minimum thresholds defined in NASM33588.
Confirm part specification compatibility with aircraft IPC documentation.
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 146204 is a self-locking nut designed to prevent fastener loosening from vibration in aircraft structures. Steel or aluminum construction with a nylon insert or deformed thread that creates prevailing torque resistance.
The 146204 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 146204 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.