P/N: 52-1610-048
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 | 40 Available |
Part 52-1610-048 is a threaded fastener nut conforming to AN or MS standards for aircraft structural and systems applications. This nut provides secure clamping load and retention when paired with bolts or screws on airframe brackets and assemblies. Typically manufactured from steel or aluminum alloy, it resists vibration loosening in high-stress flight environments.
Installation requires torque verification per the aircraft maintenance manual and confirmation against the Illustrated Parts Catalog before assembly. Used across general aviation and commercial aircraft for reliable fastener retention.
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.
Part 52-1610-048 is a threaded fastener nut conforming to AN or MS standards for aircraft structural and systems applications. This nut provides secure clamping load and retention when paired with bolts or screws on airframe brackets and assemblies.
Aircraft hardware is manufactured to military and aviation specifications. The NUT 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 52-1610-048.
Yes, we sell hardware in various quantities from single units to bulk lots. The NUT is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.