P/N: 80-004-3-16
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 |
|---|---|
| New Surplus | 11 Available |
The 80-004-3-16 is a threaded insert designed to reinforce and repair internal threads in aluminum aircraft structures. This insert creates strong, reliable attachment points in soft parent materials where standard threads would fail under vibration and repeated loading. Installation involves drilling the parent hole to specification, tapping the internal thread form per NAS1394 or MS51830 standards, then inserting the component using the appropriate insertion tool.
Commonly used in fuselage panels, wing structures, and engine mounts where fastener serviceability is critical. Follows AS8879 internal thread specifications for aerospace applications.
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 80-004-3-16 is a threaded insert designed to reinforce and repair internal threads in aluminum aircraft structures. This insert creates strong, reliable attachment points in soft parent materials where standard threads would fail under vibration and repeated loading.
Aircraft hardware is manufactured to military and aviation specifications. The INSERT 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 80-004-3-16.
Yes, we sell hardware in various quantities from single units to bulk lots. The INSERT is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.