P/N: 1185-04cn0112
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 | 2 Available |
The 1185-04cn0112 is a helical-coil thread insert for repairing damaged threads in aluminum aerospace structures. This metal insert restores thread integrity in fastener holes that have stripped or worn, allowing standard bolts and screws to maintain secure connections. Installed using matched drill, tap, and insertion tools per aircraft maintenance procedures, the insert follows NASM21209 or NAS1394/NAS1395 specifications.
Common in wing structures, fuselage panels, and engine mounts where threaded joints require reinforcement. Installation requires verification against the applicable Illustrated Parts Catalog and adherence to manufacturer insertion procedures.
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 1185-04cn0112 is a helical-coil thread insert for repairing damaged threads in aluminum aerospace structures. This metal insert restores thread integrity in fastener holes that have stripped or worn, allowing standard bolts and screws to maintain secure connections.
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 1185-04cn0112.
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.