Following general construction order on plans, assembled -02 seat belt assembly and riveted. Fist assembly to fuselage and temporarily clecoed F10-02 angle to assembly to ensure straightness. Pilot drilled and clecoed assembly to side panels and floor. Determined SNB-F10-25 gusset spacers were the incorrect thickness so modified SNX spacers to work. Located spacers and gussets, pilot drilled, and clecoed. Riveted F10-19 seat pan channel clips to forward seat pan channel. Located and pilot drilled aft seat pan ribs to seat pan forward channel then clecoed ribs, forward channel, and seat pan channels together. Located (temporary) assembly to fuselage and clecoed to seat belt attach angle, aft spar web, and fuselage floor.
Hours Worked: 3.77
Leave a Reply