P/N: 625-00407-0
Category: Plates, Doublers & Reinforcements
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 | 12 Available |
The 625-00407-0 is a steel lockplate that prevents fastener rotation in aircraft bolted joints under vibration. Installed beneath a nut or bolt head, the plate's tab bends against a flat surface or slot to lock the connection securely. This positive locking device aligns with FAA AC 43.13-1B guidance for aircraft structural fastening.
Torque the joint per applicable maintenance manual specifications, then bend the lockplate tab to secure. Essential for critical joints where vibration-induced loosening must be prevented.
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 625-00407-0 is a steel lockplate that prevents fastener rotation in aircraft bolted joints under vibration. Installed beneath a nut or bolt head, the plate's tab bends against a flat surface or slot to lock the connection securely.
The 625-00407-0 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 625-00407-0 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.