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The design of a bolt structure also involves careful consideration of its mechanical properties, such as tensile strength, shear strength, and fatigue resistance. Tensile strength refers to the maximum load a bolt can withstand while being pulled in tension, whereas shear strength is associated with the load bearing capacity when the bolt experiences forces perpendicular to its axis. Fatigue resistance is particularly important in structures subjected to repeated loading cycles, as it ensures that the bolt can withstand the wear and tear of regular operation without failure.


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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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