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The 'full-threaded' part of the name implies that the entire length of the rod is threaded, from end to end. This design offers several advantages over partially threaded rods. It allows for maximum engagement with nuts or tapped holes, providing superior holding power and load distribution. Additionally, full threading provides more flexibility in adjusting the length of the assembly, as the rod can be cut to size without losing any thread engagement area.

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Aircraft structural fasteners come in various forms, including bolts, nuts, rivets, screws, and pins. Each type of fastener is designed to perform a specific function, whether it's providing a secure connection between two parts or allowing for easy disassembly and reassembly of components for maintenance and repairs. These fasteners are typically made from durable materials such as stainless steel, titanium, or aluminum, which are chosen for their strength, corrosion resistance, and lightweight properties.

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