AN3-5A
-
Aft Forward Fuselage Assembly – Part 3
Used rivet stems and clamps to hold center seatbelt channels into place while locating and pilot drilling seat ribs and channels to forward floor. Clecoed -14L/R angles into place. Located idler assembly and pilot drilled to lower cross member and seat belt attach assembly. Updrilled all holes in fuselage floor then removed floor for better…
-
Forward Fuselage Assembly – Part 6
Clecoed lower floor/firewall stiffener and floor stiffener into place. Deburred upper firewall and riveted to fuselage box. Deburred forward fuselage floor and clecoed into place. Will wait until very end to rivet floor into place. F11 complete! Hours Worked: 1.42
-
Fuselage Box Assembly – Part 10
Riveted upper cross tie #2 to vertical channels and upper cross tie box to vertical channels #1. Fit cross tie splice plates to upper splice plates via AN3 bolt holes and riveted plates to cross tie box. F21 complete! Hours Worked: 0.67
-
LH Main Spar Assembly – Part 6
Bolts inserted into LH spar and torqued. LH Main spar complete! Spar test fit and final drilling of alignment holes and wing attach blocks will be separated into WC02 task Hours Worked: 3.00
-
RH Main Spar Assembly – Part 9
Completion of the riveting and bolting of the RH spar. Rivets finished, blemishes primed, and all attach angles bolted and final torqued. Did not bolt spar blocks on and clecoed left in tip web. Hours Worked: 5.75
-
Wing Conversion Work – Part 2
Modification of rear spars for model B conversion Hours Worked: 2.45