I had a question that is likely somewhere in the forum but as yet I have not found it by searching. Now that the rain has started I can finally spend some quality time on the project! I was working on the aileron idler bellcrank and after removing the powder coating and squaring the tabs to each other I can get the washers and bellcrank installed into the fuselage. The question concerns torqueing the bolt, if torqued to the 20 – 25 in lbs specified for this bolt nut combination the tabs compress binding the assembly. Obviously I’m missing something. I have enjoyed the hundreds of post I've read so far and learned much in the process. Thanks for your input.