The spruce, plywood, and epoxy for the fuselage and canard have been ordered. I was hoping to pick it all up at Oshkosh next week, but they have to have 2 weeks to cut the material. Now I am faced with scarf joints in the fuselage longerons and spar caps. It's not ideal but it is acceptable practice according to FAR43.13 as long as a 1:12 joint is used.
On a brighter note, I am following a lead that might get me all of the foam for the airplane for free. The downside is that I may have to splice together some blocks. I'm not sure if that is a good idea or not; I know that other canard builders fabricate their wings from multiple blocks.
I spent a little time drawing out the foam for the canard too.
Total hours: 9.3
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