Today we worked on steps 1 and 2 29iS/U-04, first we sanded the bottom flange of the F-01201A-1 and the top of the F-01201B-1 where later we would smear the sealant, then we prepared the sealant and applied it. Later we riveted the upper firewall assembly to the fuselage , dimpled the nutplates and riveted them. At the end of the day we did the step 6 29iS/U-10, in which we riveted the nutplates to F-00078.
We worked on page 28is/U-03 about drilling the brake pedals, rudder pedal assembly and securing tthe rudder pedal assembly
