P/N: 868229-1
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 | 2 Available |
The 868229-1 is a self-locking nut designed to resist vibration-induced loosening in aircraft fastening applications. This prevailing torque nut maintains clamp load without rotating, making it ideal for airframe panel attachments and structural connections subject to flight vibration. Manufactured to MS/NAS locknut standards (comparable to MS21042 or MS21044 specifications), it provides reliable fastening in aerospace service.
Install per aircraft Illustrated Parts Catalog requirements and FAA AC 43.13-1B guidance. Do not use on rotating shafts or components requiring continuous rotation.
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 868229-1 is a self-locking nut designed to resist vibration-induced loosening in aircraft fastening applications. This prevailing torque nut maintains clamp load without rotating, making it ideal for airframe panel attachments and structural connections subject to flight vibration.
The 868229-1 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 868229-1 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.