Did some more final fuselage work by temporarily reinstalling forward fuselage floor then riveting rear spar angles to fuselage sides and forward seatbelt channel to inside seat ribs. Transferred pilot holes from angles on top of spar tunnel to fuselage sides, updrilled and deburred, then riveted angles and forward wing mount angles to fuselage sides. Final riveted forward seat pan channels to vertical spar angles and top of forward tunnel zee to rear spar web assembly. Located seat support angles on side walls then updrilled side holes. Temporarily clecoed seat pan in place to transfer holes from seat pan to angles. Removed seat pan and angles to deburr parts then riveted angles to fuselage sides.
Hours Worked: 3.20
Leave a Reply