P/N: J-2223-114
Category: Fasteners & Hardware
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.
Aircraft hardware is manufactured to military and aviation specifications. The BOLT conforms to its applicable AN (Air Force-Navy), MS (Military Standard), or NAS (National Aerospace Standard) specification. Contact us for specific specification details.
Aviation hardware is available in various materials including cadmium-plated steel, stainless steel, aluminum alloy, and titanium depending on the application. Contact us for material certification and specifications for the J-2223-114.
Yes, we sell hardware in various quantities from single units to bulk lots. The BOLT is available in: As Removed. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.