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![]() Matt Whiting wrote: Cessna uses a bolt installed in shear through fittings like you fingers meshed. This is called "double shear" and as long as the bolt is a snug fit in the hole the bolt can hold more load than the airplane is designed to experience. But a bolt in tension is stronger than a bolt in shear. I'd have to pull out my AISC manual to be sure, but I believe that a bolt in double shear has more capacity than in tension. If you are comparing single shear to tension, then I agree with you. Matt That's right. The 70% figure refers to single shear. I made a mistake on the Grade 8 bolt head marking. It has six radial marks, not five. Five is a Grade 7, not a common bolt. The grades go clear to Grade 16, IIRC. Dan |
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Aircraft grade bolt have many standards, more to do with
heat-treating and plating and tolerances on the thread and shank fit and finish. Aircraft hardware is a detailed study all to itself. wrote in message oups.com... | | Matt Whiting wrote: | | | Cessna uses a bolt installed in shear through fittings like | you fingers meshed. This is called "double shear" and as | long as the bolt is a snug fit in the hole the bolt can hold | more load than the airplane is designed to experience. | But a bolt in tension is stronger than a bolt in shear. | | I'd have to pull out my AISC manual to be sure, but I believe that a | bolt in double shear has more capacity than in tension. If you are | comparing single shear to tension, then I agree with you. | | Matt | | That's right. The 70% figure refers to single shear. | | I made a mistake on the Grade 8 bolt head marking. It has six | radial marks, not five. Five is a Grade 7, not a common bolt. The | grades go clear to Grade 16, IIRC. | | Dan | |
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