P/N: 5305-00-001-4822
Category: Screws
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 | 30 Available |
The 5305-00-001-4822 is a self-locking socket head cap screw with a pre-applied locking element for aircraft fastening applications. This screw resists vibration loosening through its integrated patch, pellet, or strip locking mechanism, qualifying to MIL-DTL-18240 specifications. Commonly installed on access panels and structural assemblies where repeated removal and reinstallation occur.
Installation requires torque application per the aircraft maintenance manual and thread size verification in the Illustrated Parts Catalog. The self-locking feature eliminates the need for separate lock washers or thread-locking compounds in critical vibration-prone locations.
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 5305-00-001-4822 is a self-locking socket head cap screw with a pre-applied locking element for aircraft fastening applications. This screw resists vibration loosening through its integrated patch, pellet, or strip locking mechanism, qualifying to MIL-DTL-18240 specifications.
The 5305-00-001-4822 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 5305-00-001-4822 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.