NUT (P/N 52-1610-048) - New Surplus

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.

What is the NUT (P/N 52-1610-048)?

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.

What conditions is the 52-1610-048 available in?

The 52-1610-048 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.

How do I get pricing for the 52-1610-048?

The 52-1610-048 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.

Do you offer expedited shipping for the 52-1610-048?

Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.