I'm in the process of completely refurbishing a 72 (and then a 73) Decathlon. I've got the fuselage completely stripped down to the bare frame. I've found one of the longerons and two of the cross tubes have extensive pitting. The joint in between the sections of pitting on the longeron has a reinforcing patch welded on. There is no documentation for this repair. Dale at ACA told me to do a punch test on it. I've never done a punch test on a tube and I can't find any data for doing one. Is anyone familiar with this process? I also asked Dale about pitting limits and he didn't give me any numbers. I've been an A&P since 84 but this is my first tube and fabric project. I would welcome any suggestions before I start replacing tubes.