This is a side entry to my larger wing spar conversion thread. If you're converting your Citabria's wood spar wings to aluminum using Milman's STC then you'll follow their directions and move things right along. Milman also makes a leading edge STC that can only be installed if you also have their spars. The leading edges wrap around the back of the top of the front spar, around the nose ribs and then down and around the back of the bottom of the front spar.
The problem is, it's a little bit of a dance to get both STC's installed and the information provided by Milman leaves room for some creativity and interpretation.
In my case, I took the lack of reference to the Milman leading edges STC in the spars STC instructions to mean that the two could be installed one after the other. Once I was close to finishing the first wing I went looking for the instructions for the leading edges STC and it became clear I'd have to back track on the first wing to get the leading edges sections into place. The directions for the leading edges refer to some of the coordination required but I thought I'd try to map it all out for any of you, or for any of our future members, that will be going down the same road at some point.
I'll post here as I get the details worked out but it seems that you have to build your wing through installing the fuel tank, trammeling the three outboard bays, and having all of the minor trimmings in place(strut attach brackets, trailing edge, aileron cove, wingtip, etc.). The inboard bay doesn't have to be trammeled yet because you'll be taking out the fuel tank and inboard drag wires to install the leading edges.
So, get the wings mostly done and check the installation of the fuel tank and other bits near the wing root.
Then remove the inboard drag wires, the fuel tank, the two wing attach fittings, and the root rib so you slide the fuel tank support out also. With the fuel tank and tank support out of the way, reinstall the wing attach fittings, the root rib, and the inboard drag wires.
I made a brace to act as a compression strut between the two wing attach fittings so I can trammel the inboard bay before reinstalling the wing.
With the brace installed, I'll trammel the whole wing one more time and then get it set up on my work table so it's perfectly flat. At that point it will be ready for installation of the leading edges. The inboard leading edge section will be installed first so, with it in place I'll be able to reassemble the inboard area of the wing before installing the outboard leading edge sections.
Does that make sense? I'm going to keep going and post as this works itself out. I'll also revise this post as I get the details worked out. That's where I'm at though.
The problem is, it's a little bit of a dance to get both STC's installed and the information provided by Milman leaves room for some creativity and interpretation.
In my case, I took the lack of reference to the Milman leading edges STC in the spars STC instructions to mean that the two could be installed one after the other. Once I was close to finishing the first wing I went looking for the instructions for the leading edges STC and it became clear I'd have to back track on the first wing to get the leading edges sections into place. The directions for the leading edges refer to some of the coordination required but I thought I'd try to map it all out for any of you, or for any of our future members, that will be going down the same road at some point.
I'll post here as I get the details worked out but it seems that you have to build your wing through installing the fuel tank, trammeling the three outboard bays, and having all of the minor trimmings in place(strut attach brackets, trailing edge, aileron cove, wingtip, etc.). The inboard bay doesn't have to be trammeled yet because you'll be taking out the fuel tank and inboard drag wires to install the leading edges.
So, get the wings mostly done and check the installation of the fuel tank and other bits near the wing root.
Then remove the inboard drag wires, the fuel tank, the two wing attach fittings, and the root rib so you slide the fuel tank support out also. With the fuel tank and tank support out of the way, reinstall the wing attach fittings, the root rib, and the inboard drag wires.
I made a brace to act as a compression strut between the two wing attach fittings so I can trammel the inboard bay before reinstalling the wing.
With the brace installed, I'll trammel the whole wing one more time and then get it set up on my work table so it's perfectly flat. At that point it will be ready for installation of the leading edges. The inboard leading edge section will be installed first so, with it in place I'll be able to reassemble the inboard area of the wing before installing the outboard leading edge sections.
Does that make sense? I'm going to keep going and post as this works itself out. I'll also revise this post as I get the details worked out. That's where I'm at though.
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