P/N: ms20615-4m16
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 | 12 Available |
The MS20615-4M16 is a universal-head solid rivet manufactured from Monel nickel alloy for aircraft structural fastening. This rivet provides superior corrosion resistance and strength in airframe sheet-metal joints, particularly in high-stress areas exposed to moisture and temperature cycling. Installed by driving the rivet through aligned holes with a bucking bar and pneumatic or hand rivet tool, creating a permanent mechanical bond.
Commonly used to fasten aircraft skins to stringers, frames, and substructure components. Installation follows MS standards and FAA AC 43.13-1B guidance for proper setting and inspection.
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 MS20615-4M16 is a universal-head solid rivet manufactured from Monel nickel alloy for aircraft structural fastening. This rivet provides superior corrosion resistance and strength in airframe sheet-metal joints, particularly in high-stress areas exposed to moisture and temperature cycling.
Aircraft hardware is manufactured to military and aviation specifications. The RIVET,SOLID 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 ms20615-4m16.
Yes, we sell hardware in various quantities from single units to bulk lots. The RIVET,SOLID is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.