P/N: 26-1004-9316-7
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 | 1 Available |
The 26-1004-9316-7 is a hex self-locking nut designed to resist vibration loosening in aircraft structural assemblies. This prevailing-torque nut maintains clamp load during flight operations and ground handling through internal locking mechanisms that create friction when installed. Manufactured to MS or NAS aerospace fastener standards for certified aircraft use.
Install with calibrated torque wrench per the aircraft maintenance manual, verifying thread size and specification in the Illustrated Parts Catalog. Commonly used on airframe attachments, control surface hinges, and engine mount connections where vibration-resistant joints are critical to flight safety.
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 26-1004-9316-7 is a hex self-locking nut designed to resist vibration loosening in aircraft structural assemblies. This prevailing-torque nut maintains clamp load during flight operations and ground handling through internal locking mechanisms that create friction when installed.
The 26-1004-9316-7 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 26-1004-9316-7 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.