P/N: J-2223-114
Category: Bolts
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 8 Available |
The J-2223-114 is an aircraft structural bolt designed for clamping and alignment of airframe components under tension or shear loads. Manufactured from alloy or corrosion-resistant steel per aerospace standards (AN, MS, or NAS), this fastener provides reliable load transfer in primary and secondary structural assemblies. Installation requires torque application per the aircraft maintenance manual and AC 43.13 guidance to ensure proper preload and component security.
Hardware traceability to approved aerospace standards must be maintained before returning the aircraft to service.
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 J-2223-114 is an aircraft structural bolt designed for clamping and alignment of airframe components under tension or shear loads. Manufactured from alloy or corrosion-resistant steel per aerospace standards (AN, MS, or NAS), this fastener provides reliable load transfer in primary and secondary structural assemblies.
The J-2223-114 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The J-2223-114 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.