The bottom skin of the forward fuselage was deburred, top and bottom. The left and right lower longerons of the forward fuslage were deburred, inside and out. The parts of the spar tunnel were disassembled, deburred, inside and out and reassembled. The two main parts of the spar tunnnel were rivetted with the two clips. This was then installled in the correct location in the forward fuselage. Ready for riveting. Why am I hesitant about riveting here?Pics to follow lwhen I find the cameral
